A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A

A - Static variable in enum org.orekit.orbits.OrbitType

Name for semi major axis.

a - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

final semi major axis.

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final semi major axis.

a0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

original recovered semi major axis.

a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered semi major axis.

A2B - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Constant for A → B diraction.

A3OVK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

A3OVK2.

AberrationModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with (the inverse of) stellar aberration.

AberrationModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier

Empty constructor.

AberrationModifier(DataContext) - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier

Constructor.

AbsoluteDate - Class in org.orekit.time

This class represents a specific instant in time.

AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate

Create an instance with a default value (AbsoluteDate.J2000_EPOCH).

AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location (parsed from a string) in a time scale.

AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(Instant, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an instant in a time scale.

AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an elapsed duration since to another instant.

AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.

AbsolutePVCoordinates - Class in org.orekit.utils

Position - Velocity - Acceleration linked to a date and a frame.

AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Build from position, velocity, acceleration.

AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Build from position and velocity.

AbsolutePVCoordinates(Frame, AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Build from frame, date and PVA coordinates.

AbsolutePVCoordinates(Frame, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Build from frame and TimeStampedPVCoordinates.

AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Multiplicative constructor

AbsolutePVCoordinates(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Subtractive constructor

AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Linear constructor

AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Linear constructor

AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Linear constructor

AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.AbsolutePVCoordinates

Builds a AbsolutePVCoordinates triplet from a FieldVector3D<Derivative>.

AbsolutePVCoordinatesHermiteInterpolator - Class in org.orekit.utils

Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.

AbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

AbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

AbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).

AbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Constructor.

ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for absorption coefficient.

AbstractAlfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Abstract class for Alfriend1999 normal and maximised methods as they share lots of similarities.

AbstractAlfriend1999(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999

Default constructor.

AbstractAlmanac - Class in org.orekit.propagation.analytical.gnss.data

Base class for GNSS almanacs.

AbstractAlmanac(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Constructor.

AbstractAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers

Base class for phase ambiguity modifier.

AbstractAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier

Constructor.

AbstractAnalyticalGradientConverter - Class in org.orekit.propagation.analytical

Converter for analytical orbit propagator.

AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator, double, int) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter

Constructor.

AbstractAnalyticalMatricesHarvester - Class in org.orekit.propagation.analytical

Base class harvester between two-dimensional Jacobian matrices and analytical orbit propagator.

AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator, String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Simple constructor.

AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical

Common handling of Propagator methods for analytical propagators.

AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Build a new instance.

AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares

Bridge between measurements and least squares problems.

AbstractBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Constructor.

AbstractBuilder<T extends AbstractBuilder<T>> - Class in org.orekit.files.ccsds.ndm

Abstract builder for all CCSDS Message files parsers/writers.

AbstractBuilder(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.AbstractBuilder

Complete constructor.

AbstractConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion

This abstract class simply serve as a container for a constant thrust maneuver.

AbstractConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Generic constructor.

AbstractConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Constructor with default control cost type.

AbstractConstituentParser<H extends Header,T extends NdmConstituent<H,?>,P extends AbstractConstituentParser<H,T,?>> - Class in org.orekit.files.ccsds.utils.parsing

Parser for CCSDS messages.

AbstractConstituentParser(String, String, IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Complete constructor.

AbstractCovarianceMatrixProvider - Class in org.orekit.estimation.sequential

Abstract provider handling a predefined initial covariance matrix.

AbstractCovarianceMatrixProvider(RealMatrix) - Constructor for class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider

Simple constructor.

AbstractCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss

Base class for cycle-slip detectors.

AbstractDetector<T extends AbstractDetector<T>> - Class in org.orekit.propagation.events

Common parts shared by several orbital events finders.

AbstractDetector(double, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.AbstractDetector

Build a new instance.

AbstractDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.AbstractDetector

Build a new instance.

AbstractDragForceModel - Class in org.orekit.forces.drag

Base class for drag force models.

AbstractDragForceModel(Atmosphere) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel

Constructor.

AbstractDualFrequencyCombination - Class in org.orekit.estimation.measurements.gnss

Base class for dual frequency combination of measurements.

AbstractDualFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Constructor.

AbstractEncodedMessage - Class in org.orekit.gnss.metric.parser

Encoded messages as a sequence of bytes.

AbstractEncodedMessage() - Constructor for class org.orekit.gnss.metric.parser.AbstractEncodedMessage

Empty constructor.

AbstractEncounterLOF - Class in org.orekit.frames.encounter

Abstract class for encounter frame between two objects.

AbstractEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF

Constructor with PVCoordinates.

AbstractEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF

Constructor with FieldPVCoordinates.

AbstractEopLoader - Class in org.orekit.frames

Base class for EOP loaders.

AbstractEopLoader(String, DataProvidersManager, Supplier<TimeScale>) - Constructor for class org.orekit.frames.AbstractEopLoader

Simple constructor.

AbstractEphemerisMessage - Class in org.orekit.propagation.analytical.gnss.data

Base class for ephemeris-based navigation messages.

AbstractEphemerisMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Constructor.

AbstractFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Abstract class for FieldODEIntegratorBuilder.

AbstractFieldIntegratorBuilder() - Constructor for class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder

Empty constructor.

AbstractFieldOfView - Class in org.orekit.geometry.fov

Abstract class representing a spacecraft sensor Field Of View.

AbstractFieldOfView(double) - Constructor for class org.orekit.geometry.fov.AbstractFieldOfView

Build a new instance.

AbstractFieldOrbitInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.orbits

Abstract class for orbit interpolator.

AbstractFieldOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractFieldOrbitInterpolator

Constructor.

AbstractFieldTimeInterpolator<T extends FieldTimeStamped<KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.time

Abstract class for time interpolator.

AbstractFieldTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator

Constructor.

AbstractFieldTimeInterpolator.InterpolationData - Class in org.orekit.time

Nested class used to store interpolation data.

AbstractFixedStepFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Abstract class for integrator builder using fixed step size.

AbstractFrames - Class in org.orekit.frames

This class is an implementation of Frames that creates frames when they are first used and uses synchronization to ensure that each frame is only created once.

AbstractFrames(TimeScales, Supplier<Frame>) - Constructor for class org.orekit.frames.AbstractFrames

Simple constructor.

AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces

Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.

AbstractGaussianContribution(String, double, ForceModel, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Build a new instance.

AbstractGaussianContribution.FieldFourierCjSjCoefficients<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

Compute the C_i^j and the S_i^j coefficients with field elements.

AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class handles the short periodic coefficients described in Danielson 2.5.3-26.

AbstractGaussianContribution.FieldIntegrableFunction<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

Internal class for numerical quadrature.

AbstractGaussianContribution.FieldSlot<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

Coefficients valid for one time slot.

AbstractGaussianContribution.FieldUijVijCoefficients<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

The U_i^j and V_i^j coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.

AbstractGaussianContribution.FourierCjSjCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces

Compute the C_i^j and the S_i^j coefficients.

AbstractGaussianContribution.GaussianShortPeriodicCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces

This class handles the short periodic coefficients described in Danielson 2.5.3-26.

AbstractGaussianContribution.GaussQuadrature - Class in org.orekit.propagation.semianalytical.dsst.forces

Class used to integrate a function of the orbital elements using the Gaussian quadrature rule to get the acceleration.

AbstractGaussianContribution.IntegrableFunction - Class in org.orekit.propagation.semianalytical.dsst.forces

Internal class for numerical quadrature.

AbstractGaussianContribution.Slot - Class in org.orekit.propagation.semianalytical.dsst.forces

Coefficients valid for one time slot.

AbstractGaussianContribution.UijVijCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces

The U_i^j and V_i^j coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.

AbstractGaussianContributionContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in AbstractGaussianContribution.

AbstractGenerator - Class in org.orekit.files.ccsds.utils.generation

Base class for both Key-Value Notation and eXtended Markup Language generators for CCSDS messages.

AbstractGenerator(Appendable, String, double, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Simple constructor.

AbstractGradientConverter - Class in org.orekit.propagation.integration

Converter for states and parameters arrays.

AbstractGradientConverter(int) - Constructor for class org.orekit.propagation.integration.AbstractGradientConverter

Simple constructor.

AbstractIntegratedPropagator - Class in org.orekit.propagation.integration

Common handling of Propagator methods for both numerical and semi-analytical propagators.

AbstractIntegratedPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator

Build a new instance.

AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration

Differential equations for the main state (orbit, attitude and mass).

AbstractKalmanEstimator - Class in org.orekit.estimation.sequential

Base class for Kalman estimators.

AbstractKalmanEstimator(List<? extends PropagatorBuilder>) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanEstimator

Constructor.

AbstractLambdaMethod - Class in org.orekit.estimation.measurements.gnss

Base class for decorrelation/reduction engine for LAMBDA type methods.

AbstractLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Constructor.

AbstractLimitedVariableStepFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Abstract class for integrator using a limited number of variable steps.

AbstractListCrawler<T> - Class in org.orekit.data

Provider for data files defined in a list.

AbstractListCrawler(T...) - Constructor for class org.orekit.data.AbstractListCrawler

Build a data classpath crawler.

AbstractManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger

Base class for triggers.

AbstractManeuverTriggers() - Constructor for class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Simple constructor.

AbstractMatricesHarvester - Class in org.orekit.propagation

Base harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.

AbstractMatricesHarvester(String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.AbstractMatricesHarvester

Simple constructor.

AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements

Abstract class handling measurements boilerplate.

AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Simple constructor for mono-dimensional measurements.

AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement

Simple constructor, for multi-dimensional measurements.

AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Base class for measurements builders.

AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Simple constructor.

AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Simple constructor.

AbstractMessageParser<T> - Class in org.orekit.files.ccsds.utils.parsing

Parser for CCSDS messages.

AbstractMessageParser(String, String, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Simple constructor.

AbstractMessageWriter<H extends Header,S extends Segment<?,?>,F extends NdmConstituent<H,S>> - Class in org.orekit.files.ccsds.utils.generation

Base class for Navigation Data Message (NDM) files.

AbstractMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

AbstractMultipleShooting - Class in org.orekit.utils

Multiple shooting method using only constraints on state vectors of patch points (and possibly on epoch and integration time).

AbstractMultipleShooting(List<SpacecraftState>, List<NumericalPropagator>, double, int, boolean, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting

Simple Constructor.

AbstractNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Base class for GNSS navigation messages.

AbstractNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Constructor.

AbstractOrbitInterpolator - Class in org.orekit.orbits

Abstract class for orbit interpolator.

AbstractOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractOrbitInterpolator

Constructor.

AbstractPropagator - Class in org.orekit.propagation

Common handling of Propagator methods for analytical propagators.

AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator

Build a new instance.

AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion

Base class for propagator builders.

AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Build a new instance.

AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Build a new instance.

AbstractPropagatorConverter - Class in org.orekit.propagation.conversion

Common handling of PropagatorConverter methods for propagators conversions.

AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter

Build a new instance.

AbstractRadiationForceModel - Class in org.orekit.forces.radiation

Base class for radiation force models.

AbstractRadiationForceModel(ExtendedPVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.radiation.AbstractRadiationForceModel

Default constructor.

AbstractRelativisticClockModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical measurements with relativistic clock correction.

AbstractRelativisticClockModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier

Simple constructor.

AbstractRelativisticJ2ClockModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical measurements with relativistic J2 clock correction.

AbstractRelativisticJ2ClockModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier

Constructor for the Relativistic J2 Clock modifier.

AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Base implementation of Scheduler managing dates selection.

AbstractScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.AbstractScheduler

Simple constructor.

AbstractSelfFeedingLoader - Class in org.orekit.data

Abstract class that combines a DataProvidersManager with a supported names regular expression for DataProvidersManager.feed(String, DataLoader).

AbstractSelfFeedingLoader(String, DataProvidersManager) - Constructor for class org.orekit.data.AbstractSelfFeedingLoader

Create an abstract data loader that can feed itself.

AbstractShapiroBaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with Shapiro time delay.

AbstractShapiroBaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier

Simple constructor.

AbstractShortTermEncounter1DNumerical2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

This abstract class serves as a foundation to create 1D numerical 2D probability of collision computing method.

AbstractShortTermEncounter1DNumerical2DPOCMethod(String, UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Customizable constructor.

AbstractShortTermEncounter2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

This abstract class serves as a foundation to create 2D probability of collision computing method assuming a short term encounter model.

AbstractShortTermEncounter2DPOCMethod(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Constructor.

AbstractSingleFrequencyCombination - Class in org.orekit.estimation.measurements.gnss

Base class for single frequency combination of measurements.

AbstractSingleFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination

Constructor.

AbstractSolarActivityData<L extends AbstractSolarActivityDataLoader.LineParameters,D extends AbstractSolarActivityDataLoader<L>> - Class in org.orekit.models.earth.atmosphere.data

Abstract class for solar activity data.

AbstractSolarActivityData(String, D, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

AbstractSolarActivityData(DataSource, D, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Simple constructor.

AbstractSolarActivityData.LocalSolarActivity - Class in org.orekit.models.earth.atmosphere.data

Container for weather parameters around current date.

AbstractSolarActivityData.SolarActivityGenerator - Class in org.orekit.models.earth.atmosphere.data

Generator used in the weather data cache.

AbstractSolarActivityDataLoader<L extends AbstractSolarActivityDataLoader.LineParameters> - Class in org.orekit.models.earth.atmosphere.data

Abstract class for solar activity data loader.

AbstractSolarActivityDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Constructor.

AbstractSolarActivityDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data

Container class for Solar activity indexes.

AbstractStateCovarianceInterpolator - Class in org.orekit.propagation

Abstract class for orbit and state covariance interpolator.

AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator

Constructor.

AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator

Constructor.

AbstractTimeInterpolator<T extends TimeStamped> - Class in org.orekit.time

Abstract class for time interpolator.

AbstractTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractTimeInterpolator

Constructor.

AbstractTimeInterpolator.InterpolationData - Class in org.orekit.time

Nested class used to store interpolation data.

AbstractTimeScales - Class in org.orekit.time

Abstract base class for TimeScales that implements some common functionality.

AbstractTimeScales() - Constructor for class org.orekit.time.AbstractTimeScales

Simple constructor.

AbstractVariableStepFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Abstract class for integrator builder using variable step size.

AbstractWindUp<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss

Base class for wind-up effect computation.

AbstractWindUp(Dipole, Dipole) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractWindUp

Simple constructor.

AbstractWriter - Class in org.orekit.files.ccsds.section

Top level class for writing CCSDS message sections.

AbstractWriter(String, String) - Constructor for class org.orekit.files.ccsds.section.AbstractWriter

Simple constructor.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration.

acceleration(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Compute acceleration.

acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Compute acceleration.

AccelerationModel - Interface in org.orekit.forces.empirical

Acceleration model used by empirical force.

accept(IntegerLeastSquareSolution[]) - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance

Check if one of the candidate solutions can be accepted.

accept(IntegerLeastSquareSolution[]) - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance

Check if one of the candidate solutions can be accepted.

accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer

Parse a CCSDS Message.

accept(MessageParser<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.LexicalAnalyzer

Parse a CCSDS Message.

accept(boolean) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.BooleanConsumer

Consume a boolean.

accept(BodyFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterConsumer

Consume a body center.

accept(List<BodyFacade>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterListConsumer

Consume a body center.

accept(char) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CharConsumer

Consume a character.

accept(AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DateConsumer

Consume a date.

accept(double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleArrayConsumer

Consume an array of doubles.

accept(double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleConsumer

Consume a double.

accept(int, int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoublyIndexedDoubleConsumer

Consume a doubly indexed double.

accept(T) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumConsumer

Consume an enum.

accept(List<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumListConsumer

Consume an enum.

accept(FrameFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.FrameConsumer

Consume a frame.

accept(int, double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleArrayConsumer

Consume an indexed double array.

accept(int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleConsumer

Consume an indexed double.

accept(int, int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedIntConsumer

Consume an integer.

accept(int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedStringConsumer

Consume an indexed string.

accept(int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntConsumer

Consume an integer.

accept(int[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntegerArrayConsumer

Consume an array of integers.

accept(char, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.LabeledDoubleConsumer

Consume an indexed double.

accept(Maneuvrable) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.ManeuvrableConsumer

Consume a Maneuvrable.

accept(RotationOrder) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.RotationOrderConsumer

Consume a data.

accept(String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringConsumer

Consume a string.

accept(List<String>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringListConsumer

Consume a list of strings.

accept(TimeSystem) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.TimeSystemConsumer

Consume a time system.

accept(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.UnitListConsumer

Consume a list of units.

accept(Vector3D) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.VectorConsumer

Consume a vector.

accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer

Parse a CCSDS Message.

acceptComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer

Check if container is still accepting comments.

acceptStep(OrekitStepInterpolator, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Accept a step, triggering events and step handlers.

acceptStep(FieldAbstractAnalyticalPropagator<T>.FieldBasicStepInterpolator, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Accept a step, triggering events and step handlers.

AccuracyProvider - Interface in org.orekit.gnss.metric.messages.common

This interface represents an accuracy providerused to validate RTCM ephemeris messages.

AccurateFormatter - Class in org.orekit.utils

Formatter used to produce strings from data with high accuracy.

Acm - Class in org.orekit.files.ccsds.ndm.adm.acm

This class gathers the informations present in the Attitude Comprehensive Message (ACM).

Acm(AdmHeader, List<Segment<AcmMetadata, AcmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.Acm

Simple constructor.

AcmData - Class in org.orekit.files.ccsds.ndm.adm.acm

Data container for Attitude Comprehensive Messages.

AcmData(List<AttitudeStateHistory>, AttitudePhysicalProperties, List<AttitudeCovarianceHistory>, List<AttitudeManeuver>, AttitudeDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Simple constructor.

AcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keywords for ACM data sub-structure.

AcmElements - Enum in org.orekit.files.ccsds.ndm.adm.acm

Data elements types used in CCSDS Attitude Comprehensive Messages.

AcmMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm

Meta-data for Attitude Comprehensive Message.

AcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Create a new meta-data.

AcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for ACM container entries.

AcmParser - Class in org.orekit.files.ccsds.ndm.adm.acm

A parser for the CCSDS ACM (Attitude Comprehensive Message).

AcmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Complete constructor.

AcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.acm

ACM ephemeris blocks for a single satellite.

AcmSatelliteEphemeris(String, List<AttitudeStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris

Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

AcmWriter - Class in org.orekit.files.ccsds.ndm.adm.acm

Writer for CCSDS Attitude Comprehensive Message.

AcmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter

Complete constructor.

AdamsBashforthFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for AdamsBashforthFieldIntegrator.

AdamsBashforthFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder

Build a new instance.

AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsBashforthIntegrator.

AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a new instance.

AdamsMoultonFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for AdamsMoultonFieldIntegrator.

AdamsMoultonFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder

Build a new instance.

AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsMoultonIntegrator.

AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a new instance.

AdaptableInterval - Interface in org.orekit.propagation.events

This interface represents an event checking interval that depends on state.

AdapterDetector - Class in org.orekit.propagation.events

Base class for adapting an existing detector.

AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector

Build an adaptor wrapping an existing detector.

AdapterPropagator - Class in org.orekit.propagation.analytical

Orbit propagator that adapts an underlying propagator, adding differential effects.

AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator

Build a propagator from an underlying reference propagator.

AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical

Interface for orbit differential effects.

add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Add a handler for variable size step.

add(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Add a handler for fixed size step.

add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Add a handler for variable size step.

add(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Add a handler for fixed size step.

add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Add the argument matrix with the current matrix.

add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList

Add a driver.

addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Add a AccelerationModel entry valid after a limit date.

addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Add an AccelerationModel entry valid before a limit date.

addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).

addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.

addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.

addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState

Add an additional state.

addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState

Add an additional state.

addAdditionalStateDerivative(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState

Add an additional state derivative.

addAdditionalStateDerivative(String, double...) - Method in class org.orekit.propagation.SpacecraftState

Add an additional state derivative.

addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAnglesData(CRD.AnglesMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of angles data.

addAntennaTypeValidAfter(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Add a antenna type entry valid after a limit date.
Using addAntennaTypeValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).

addAntennaTypeValidBefore(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Add a antenna type entry valid before a limit date.
Using addAntennaTypeValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).

addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.clock.RinexClock

Add an applied differencial code bias corrections.

addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Add applied differential code bias corrections.

addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.clock.RinexClock

Add an applied phase center variations.

addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Add antenna center variation corrections.

addBDGIMMessage(IonosphereBDGIMMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add an ionosphere BDGIM message.

addBeidouCivilianNavigationMessage(BeidouCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a Beidou navigation message to the list.

addBeidouLegacyNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a Beidou navigation message to the list.

addCalibrationData(CRD.Calibration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of calibration data.

addCalibrationDetailData(CRD.CalibrationDetail) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of calibration detail data.

addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add a loader for celestial bodies.

addCelestialBodyLoader(String, CelestialBodyLoader) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Add a loader for celestial bodies.

addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addClockData(String, RinexClock.ClockDataLine) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a clock data line to a specified receiver/satellite.

addClockDataType(RinexClock.ClockDataType) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a clock data types.

addCodeBias(CodeBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Add a code bias value for the current satellite.

addComment(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set comment for relative metadata.

addComment(String) - Method in class org.orekit.files.ccsds.ndm.NdmParser

Add comment.

addComment(String) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Add comment.

addComment(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a comment line.

addComment(RinexComment) - Method in class org.orekit.files.rinex.RinexFile

Add a comment.

addComment(String) - Method in class org.orekit.files.sp3.SP3Header

Add a comment.

addConfigurationRecord(CRDConfiguration.BaseConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Add a configuration record, such as SystemConfiguation, LaserConfiguration, DetectorConfiguration, etc.

addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting

Add a constraint on one component of one patch point.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Add the contribution of the wave to Stokes coefficients.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver

Compute the contribution of the force model to the perturbing acceleration.

addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.Maneuver

Compute the contribution of the force model to the perturbing acceleration.

addCoordinate(SP3Coordinate, double) - Method in class org.orekit.files.sp3.SP3Ephemeris

Adds a new P/V coordinate.

addCoordinate(SP3Coordinate) - Method in class org.orekit.files.sp3.SP3Segment

Adds a new P/V coordinate.

addCovarianceMatrix(CartesianCovariance) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Add a covariance matrix.

addData(TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData

Add a data point.

addData(TimeStampedPVCoordinates, boolean) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Add a data point.

addDataBlock(CRD.CRDDataBlock) - Method in class org.orekit.files.ilrs.CRD

Add a data block to the current list of data blocks.

addDcb(SatelliteSystem, Dcb) - Method in class org.orekit.files.sinex.DcbStation

Add the DCB data corresponding to a satellite system.

addDcbLine(String, String, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.files.sinex.Dcb

Add the content of a DCB line to the DCBSatellite object.

addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for all predefined celestial bodies.

addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for celestial bodies.

addDefaultCelestialBodyLoader(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Add the default loaders for all predefined celestial bodies.

addDefaultCelestialBodyLoader(String, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Add the default loaders for celestial bodies.

addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders EOP history (IAU 1980 precession/nutation).

addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop

Add the default loaders EOP history (IAU 1980 precession/nutation).

addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames

Add the default loaders EOP history (IAU 1980 precession/nutation).

addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).

addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop

Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).

addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames

Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).

addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default READERS for ocean tides.

addDefaultOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Add the default readers for ocean tides.

addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default readers for gravity fields.

addDefaultPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Add the default readers for gravity fields.

addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager

Add the default providers configuration.

addDefaultUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales

Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).

addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory

Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).

addDragSensitiveValidAfter(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Add a DragSensitive entry valid after a limit date.
Using addDragSensitiveValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).

addDragSensitiveValidBefore(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Add a DragSensitive entry valid before a limit date.
Using addDragSensitiveValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).

addEarthOrientationParameter(EarthOrientationParameterMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add an Earth orientation parameter.

addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Add a differential effect.

addEntry(String, String) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined

Add a key/value entry.

addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Static method in class org.orekit.frames.FramesFactory

Add a loader for Earth Orientation Parameters history.

addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Method in class org.orekit.frames.LazyLoadedEop

Add a loader for Earth Orientation Parameters history.

addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Method in class org.orekit.frames.LazyLoadedFrames

Add a loader for Earth Orientation Parameters history.

addEphemerisName(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Adds an ephemeris name to the list.

addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector

Add an event date.

addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Add an event date.

addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Add an event detector.

addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Add an event detector.

addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator

Add an event detector.

addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add an event detector.

addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Add an event detector.

addEventDetector(T) - Method in interface org.orekit.propagation.Propagator

Add an event detector.

addFilter(DataFilter) - Method in class org.orekit.data.FiltersManager

Add a data filter.

addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Add a force model.

addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Add a force model to the global perturbation model.

addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Add a force model to the global perturbation model.

addGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a Galileo navigation message to the list.

addGlonassChannel(GlonassSatelliteChannel) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Add GLONASS satellite/channel association.

addGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a Glonass navigation message to the list.

addGPSLegacyNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a GPS legacy navigation message to the list.

addGPSLegacyNavigationMessage(GPSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a GPS civilian navigation message to the list.

addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient

Add a point to the interpolation grid.

addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Add a point to the interpolation grid.

addHandler(EventHandler) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Add one handler to the managed handlers list.

addHandlers(EventHandler...) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Add several handlers to the managed handlers list.

addInput(T) - Method in class org.orekit.data.AbstractListCrawler

Add an input to the supported list.

addIRNSSNavigationMessage(IRNSSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a IRNSS navigation message to the list.

AdditionalCovarianceMetadata - Class in org.orekit.files.ccsds.ndm.cdm

Container for the additional covariance metadata (optional).

AdditionalCovarianceMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Simple constructor.

AdditionalCovarianceMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for covariance metadatail y a entries.

AdditionalDerivativesProvider - Interface in org.orekit.propagation.integration

Provider for additional derivatives.

AdditionalParameters - Class in org.orekit.files.ccsds.ndm.cdm

Container for additional parameters data block.

AdditionalParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Simple constructor.

AdditionalParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM additional parameters entries.

AdditionalParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for additional parameters data block for CCSDS Conjunction Data Messages.

AdditionalStateProvider - Interface in org.orekit.propagation

This interface represents providers for additional state data beyond SpacecraftState.

addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CircularOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.Orbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of the Kepler evolution.

addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the Kepler evolution.

addKlobucharMessage(IonosphereKlobucharMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add an ionosphere Klobuchar message.

addManeuver(Maneuver) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Add a maneuver.

addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of the flow rate (dm/dt).

addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the flow rate (dm/dt).

addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Add a measurement.

addMeteoData(CRD.MeteorologicalMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of meteorological data.

addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Add a modifier.

addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Add a modifier.

addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Add a modifier.

addModifier(EstimationModifier<MultiplexedMeasurement>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Add a modifier.

addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Add a modifier.

addNequickGMessage(IonosphereNequickGMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add an ionosphere Nequick-G message.

addNewSegment(List<SpacecraftState>, String, int, AngularDerivativesFilter) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Injects pre-computed satellite states into this attitude ephemeris file object, returning the generated OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNewSegment(List<SpacecraftState>, CelestialBody, int, TimeScale) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations

Add the contribution of an acceleration expressed in some inertial frame.

addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of a non-Keplerian acceleration.

addObservation(Observation) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock

Adds an observation data line.

addObservation(ObservationType, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock

Adds an observation data line.

addObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservation

Add an observations data set.

addObserver(int, String, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Add an observer for an encoded messages.

addObserver(int, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor

Add an observer for encoded messages.

addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver

Add an observer for this driver.

addOccultingBody(ExtendedPVCoordinatesProvider, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Add a new occulting body.

addOccultingBody(OneAxisEllipsoid) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Add a new occulting body.

addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for ocean tides.

addOceanTidesReader(OceanTidesReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Add a reader for ocean tides.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Add an offset from the instance.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Add an offset from the instance.

addOptionalSubInterpolatorIfDefined(FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>, List<FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Add all lowest level sub interpolators to the sub interpolator list.

addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped>, List<TimeInterpolator<? extends TimeStamped>>) - Method in class org.orekit.time.AbstractTimeInterpolator

Add all lowest level sub interpolators to the sub interpolator list.

addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Add a parameter driver.

addParticipant(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Adds a participant to the list.

addPhaseBias(PhaseBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Add a phase bias value for the current satellite.

addPhaseShiftCorrection(PhaseShiftCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Add phase shift correction used to generate phases consistent w/r to cycle shifts.

addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Add a fitting point.

addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for gravity fields.

addPotentialCoefficientsReader(PotentialCoefficientsReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Add a reader for gravity fields.

addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Add a propagation configuration.

addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder

Add a propagation configuration.

addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Add a propagation configuration.

addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Add a propagation configuration.

addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator

Add a propagator.

addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Add a data provider to the supported list.

addPVProviderAfter(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Add a PVCoordinatesProvider to the collection.

addPVProviderBefore(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Add a PVCoordinatesProvider to the collection.

addQZSSCivilianNavigationMessage(QZSSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a QZSS navigation message to the list.

addQZSSLegacyNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a QZSS navigation message to the list.

addRangeData(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of range data.

addRangeSupplementData(CRD.RangeSupplement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of range supplement data.

addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Adds a receive delay to the list.

addReceiver(RinexClock.Receiver) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a new receiver to the list of stored receivers.

addReferenceClockList(List<RinexClock.ReferenceClock>, AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a list of reference clocks wich will be used after a specified date.

addResetter(ManeuverTriggersResetter) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Add a resetter.

addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Add a resetter.

addResetter(ManeuverTriggersResetter) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Add a resetter.

addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Add a resetter.

addSatellite(String) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile

Adds a new satellite to this object.

addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile

Adds a new satellite to this object.

addSatellite(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Add a new satellite with a given identifier to the list of stored satellites.

addSatellite(String) - Method in class org.orekit.files.sp3.SP3

Add a new satellite with a given identifier to the list of stored satellites.

addSatelliteCoordinate(String, CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF

Add a new P/V coordinates to the satellite.

addSatelliteCoordinates(String, List<CPF.CPFCoordinate>) - Method in class org.orekit.files.ilrs.CPF

Adds a set of P/V coordinates to the satellite.

addSatelliteVelocityToCPFCoordinate(String, Vector3D) - Method in class org.orekit.files.ilrs.CPF

Add the velocity to the last CPF coordinate entry.

addSatId(String) - Method in class org.orekit.files.sp3.SP3Header

Add a satellite identifier.

addSBASNavigationMessage(SBASNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a SBAS navigation message to the list.

addScaleFactorCorrection(SatelliteSystem, ScaleFactorCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Add scale factor correction.

addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator

Add a sequences generator for a specific measurement type.

addSensor(AttitudeDeterminationSensor) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Add a sensor used.

addSessionStatisticsData(CRD.SessionStatistics) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Add an entry to the list of session statistics data.

addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Add a new solution.

addSpanAtDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Create a new span in values and names time span map given a start date.

addSpans(AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.ParameterDriver

Cut values and names time span map given orbit determination start and end and driver periodicity.

addStationEccentricitiesValidAfter(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Add a station eccentricity vector entry valid after a limit date.
Using addStationEccentricitiesValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).

addStationEccentricitiesValidBefore(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Add a station eccentricity vector entry valid before a limit date.
Using addStationEccentricitiesValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).

addSubscriber(GeneratedMeasurementSubscriber) - Method in class org.orekit.estimation.measurements.generation.Generator

Add a subscriber.

addSupportedParameters(List<ParameterDriver>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Add supported parameters.

addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence

Add a switching condition between two attitude providers.

addSystemObservationType(SatelliteSystem, ObservationType) - Method in class org.orekit.files.rinex.clock.RinexClock

Add an observation type for a specified satellite system.

addSystemTimeOffset(SystemTimeOffsetMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Add a system time offset.

addTimeSystemCorrections(TimeSystemCorrection) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Add a time system correction to the list.

addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Adds a transmit delay to the list.

addTroposphericModelValidAfter(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).

addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).

addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Method in class org.orekit.time.LazyLoadedTimeScales

Add a loader for UTC-TAI offsets history files.

addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory

Add a loader for UTC-TAI offsets history files.

addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Add an entry valid after a limit date.

addValidAfter(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap

Add an entry valid after a limit date.

addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Add an entry valid before a limit date.

addValidBefore(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap

Add an entry valid before a limit date.

addValidBetween(T, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Add an entry valid between two limit dates.

addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Add parsed coefficients.

addWaypoint(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.utils.WaypointPVBuilder

Add a waypoint.

addWeightedPoint(AbsoluteDate, double, double) - Method in class org.orekit.utils.SecularAndHarmonic

Add a weighted fitting point.

AdmCommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm

Keys for APM and AEM entries.

AdmCommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.adm

Writer for Common metadata for CCSDS Attitude Parameter/Ephemeris Messages.

AdmCommonMetadataWriter(AdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter

Simple constructor.

AdMethodType - Enum in org.orekit.files.ccsds.definitions

Type of attitude determination method used in CCSDS Attitude Comprehensive Messages.

AdmHeader - Class in org.orekit.files.ccsds.ndm.adm

Header of a CCSDS Attitude Data Message.

AdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmHeader

Constructor.

AdmMetadata - Class in org.orekit.files.ccsds.ndm.adm

This class gathers the meta-data present in the Attitude Data Message (ADM).

AdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Simple constructor.

AdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm

Keys for ADM container entries.

AdmParser<T extends NdmConstituent<AdmHeader,?>,P extends AbstractConstituentParser<AdmHeader,T,?>> - Class in org.orekit.files.ccsds.ndm.adm

Base class for Attitude Data Message parsers.

AdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmParser

Complete constructor.

Aem - Class in org.orekit.files.ccsds.ndm.adm.aem

This class stores all the information of the Attitude Ephemeris Message (AEM) File parsed by AEMParser.

Aem(AdmHeader, List<AemSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.Aem

Simple constructor.

AemData - Class in org.orekit.files.ccsds.ndm.adm.aem

The Attitude Ephemerides data blocks class contain list of attitude data points.

AemData() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemData

Constructor.

AemMetadata - Class in org.orekit.files.ccsds.ndm.adm.aem

This class gathers the meta-data present in the Attitude Data Message (ADM).

AemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Simple constructor.

AemMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.aem

Keys for AEM container entries.

AemParser - Class in org.orekit.files.ccsds.ndm.adm.aem

A parser for the CCSDS AEM (Attitude Ephemeris Message).

AemParser(IERSConventions, boolean, DataContext, AbsoluteDate, int, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Complete constructor.

AemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.aem

AEM ephemeris blocks for a single satellite.

AemSatelliteEphemeris(String, List<AemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

AemSegment - Class in org.orekit.files.ccsds.ndm.adm.aem

This class stores the metadata and data for one attitude segment.

AemSegment(AemMetadata, AemData) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Simple constructor.

AemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem

A writer for Attitude Ephemeris Messsage (AEM) files.

AemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemWriter

Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Method called just after integration.

AggregateBoundedAttitudeProvider - Class in org.orekit.attitudes

A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.

AggregateBoundedAttitudeProvider(Collection<? extends BoundedAttitudeProvider>) - Constructor for class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Constructor.

AggregateBoundedPropagator - Class in org.orekit.propagation.analytical

A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.

AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator

Create a propagator by concatenating several BoundedPropagators.

AggregateBoundedPropagator(NavigableMap<AbsoluteDate, ? extends BoundedPropagator>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator

Create a propagator from several constituent propagators.

AggregatedPVCoordinatesProvider - Class in org.orekit.utils

Aggreate multiple PVCoordinatesProvider instances together This can be used to describe an aircraft or surface vehicle.

AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider

Class constructor.

AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider

Class constructor.

AggregatedPVCoordinatesProvider.Builder - Class in org.orekit.utils

Builder class for AggregatedPVCoordinatesProvider.

AggregatedPVCoordinatesProvider.InvalidPVProvider - Class in org.orekit.utils

Implementation of PVCoordinatesProvider that throws an illegal state exception.

AGILeapSecondFilesLoader - Class in org.orekit.time

Loader for UTC-TAI extracted from LeapSecond file from AGI.

AGILeapSecondFilesLoader(String) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader

Build a loader for LeapSecond.dat file from AGI.

AGILeapSecondFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader

Build a loader for LeapSecond.dat file from AGI.

AGILeapSecondFilesLoader.Parser - Class in org.orekit.time

Internal class performing the parsing.

Alfano2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision using the method described in :"S.

Alfano2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005

Empty constructor.

Alfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision using the method described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.

Alfriend1999() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999

Empty constructor.

Alfriend1999Max - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision assuming the worst case described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.

Alfriend1999Max() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max

Empty constructor.

alias(String) - Method in class org.orekit.utils.units.Unit

Create an alias for a unit.

AlignmentDetector - Class in org.orekit.propagation.events

Finder for satellite/body alignment events in orbital plane.

AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Protected constructor with full parameters.

alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming

Find the along tile direction for tessellation at specified point.

alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming

Find the along tile direction for tessellation at specified point.

alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming

Find the along tile direction for tessellation at specified point.

alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming

Find the along tile direction for tessellation at specified point.

AlongTrackAiming - Class in org.orekit.models.earth.tessellation

Class used to orient tiles along an orbit track.

AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming

Simple constructor.

AltCovarianceType - Enum in org.orekit.files.ccsds.ndm.cdm

Flag indicating the type of alternate covariance information provided.

AltitudeDetector - Class in org.orekit.propagation.events

Finder for satellite altitude crossing events.

AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(AdaptableInterval, double, int, EventHandler, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Protected constructor with full parameters.

AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Name for ambiguity driver.

AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Name for ambiguity driver.

AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase

Name for ambiguity driver.

AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss

Interface defining ambiguity acceptance tests.

AmbiguitySolver - Class in org.orekit.estimation.measurements.gnss

Class for solving integer ambiguity problems.

AmbiguitySolver(List<ParameterDriver>, IntegerLeastSquareSolver, AmbiguityAcceptance) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Simple constructor.

AMPERE - Static variable in class org.orekit.utils.units.Unit

Ampere unit.

andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

andCombine(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

andCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector

Create a new event detector that is the logical AND of the given event detectors.

angles(SpacecraftState) - Method in class org.orekit.utils.OccultationEngine

Compute the occultation angles as seen from a spacecraft.

angles(FieldSpacecraftState<T>) - Method in class org.orekit.utils.OccultationEngine

Compute the occultation angles as seen from a spacecraft.

AnglesMeasurement(AbsoluteDate, double, double, int, int, boolean, double, double) - Constructor for class org.orekit.files.ilrs.CRD.AnglesMeasurement

Constructor.

AngleType - Enum in org.orekit.files.ccsds.ndm.tdm

Antenna geometry represented in the angle date.

AngularAzEl - Class in org.orekit.estimation.measurements

Class modeling an Azimuth-Elevation measurement from a ground station.

AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularAzEl

Simple constructor.

AngularAzElBuilder - Class in org.orekit.estimation.measurements.generation

Builder for AngularAzEl measurements.

AngularAzElBuilder(CorrelatedRandomVectorGenerator, GroundStation, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularAzElBuilder

Simple constructor.

AngularCoordinates - Class in org.orekit.utils

Simple container for rotation/rotation rate/rotation acceleration triplets.

AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates

Simple constructor.

AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate pair.

AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate/rotation acceleration triplet.

AngularCoordinates(Rotation) - Constructor for class org.orekit.utils.AngularCoordinates

Builds angular coordinates with the given rotation, zero angular velocity, and zero angular acceleration.

AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another one.

AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

AngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a AngularCoordinates from a FieldRotation<Derivative>.

AngularDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.

AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with ionospheric delay.

AngularIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

Constructor.

AngularRaDec - Class in org.orekit.estimation.measurements

Class modeling a Right Ascension - Declination measurement from a ground point (station, telescope).

AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularRaDec

Simple constructor.

AngularRaDecBuilder - Class in org.orekit.estimation.measurements.generation

Builder for AngularRaDec measurements.

AngularRaDecBuilder(CorrelatedRandomVectorGenerator, GroundStation, Frame, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularRaDecBuilder

Simple constructor.

AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with ionospheric radio refractive index.

AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

Constructor.

AngularSeparationDetector - Class in org.orekit.propagation.events

Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.

AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector

Build a new angular separation detector.

AngularSeparationDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector

Protected constructor with full parameters.

AngularSeparationFromSatelliteDetector - Class in org.orekit.propagation.events

Detects when two moving objects come close to each other, as seen from spacecraft.

AngularSeparationFromSatelliteDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Build a new angular detachment detector.

AngularSeparationFromSatelliteDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Protected constructor with full parameters.

AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical angular measurement with tropospheric delay.

AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

Constructor.

AngularVelocity - Class in org.orekit.files.ccsds.ndm.adm.apm

Container for Attitude Parameter Message data lines.

AngularVelocity() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Simple constructor.

AngularVelocityKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for APM angular velocity entries.

Antenna - Class in org.orekit.gnss.antenna

GNSS antenna model.

Antenna(String, String, Map<Frequency, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna

Simple constructor.

AntexLoader - Class in org.orekit.gnss.antenna

Factory for GNSS antennas (both receiver and satellite).

AntexLoader(String) - Constructor for class org.orekit.gnss.antenna.AntexLoader

Simple constructor.

AntexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader

Construct a loader by specifying a DataProvidersManager.

AntexLoader(DataSource, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader

Construct a loader by specifying the source of ANTEX auxiliary data files.

anticipateNext(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Anticipate what next processing state should be.

Apm - Class in org.orekit.files.ccsds.ndm.adm.apm

This class stores all the information of the Attitude Parameter Message (APM) File parsed by APMParser.

Apm(AdmHeader, List<Segment<AdmMetadata, ApmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Apm

Simple constructor.

ApmData - Class in org.orekit.files.ccsds.ndm.adm.apm

Container for Attitude Parameter Message data.

ApmData(CommentsContainer, AbsoluteDate, ApmQuaternion, Euler, AngularVelocity, SpinStabilized, Inertia) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Simple constructor.

ApmParser - Class in org.orekit.files.ccsds.ndm.adm.apm

A parser for the CCSDS APM (Attitude Parameter Message).

ApmParser(IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Complete constructor.

ApmQuaternion - Class in org.orekit.files.ccsds.ndm.adm.apm

Container for Attitude Parameter Message quaternion logical block.

ApmQuaternion() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Simple constructor.

ApmQuaternionKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for APM quaternion entries.

ApmWriter - Class in org.orekit.files.ccsds.ndm.adm.apm

Writer for CCSDS Orbit Parameter Message.

ApmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter

Complete constructor.

AppliedDCBS - Class in org.orekit.files.rinex

Corrections of Differential Code Biases (DCBs) applied.

AppliedDCBS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedDCBS

Simple constructor.

AppliedPCVS - Class in org.orekit.files.rinex

Corrections of antenna phase center variations (PCVs) applied.

AppliedPCVS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedPCVS

Simple constructor.

appliesTo(String) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration

Check if this entry applies to a file name.

apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on an orbit.

apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on a spacecraft state.

apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect

Apply the effect to a spacecraft state.

apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Compute the effect of the maneuver on an orbit.

apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Apply the effect to a spacecraft state.

applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.HaloOrbit

Apply the differential correction to compute more accurate initial PV.

applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LibrationOrbit

Apply the differential correction to compute more accurate initial PV.

applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LyapunovOrbit

Apply the differential correction to compute more accurate initial PV.

applyDifferentialCorrection() - Method in class org.orekit.orbits.LibrationOrbit

Apply differential correction.

applyDynamicOutlierFilter(EstimatedMeasurement<T>, RealMatrix) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Set and apply a dynamic outlier filter on a measurement.

applyRelevantFilters(DataSource) - Method in class org.orekit.data.FiltersManager

Apply all the relevant data filters, taking care of layers.

applyResetters(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Apply resetters.

applyResetters(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Apply resetters.

applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Apply the rotation to a pv coordinates.

approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Approximate an already fitted model to polynomial only terms.

ApsideDetector - Class in org.orekit.propagation.events

Finder for apside crossing events.

ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ApsideDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.ApsideDetector

Protected constructor with full parameters.

ARBITRARY_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

An arbitrary finite date.

ARC_MINUTE - Static variable in class org.orekit.utils.units.Unit

Arc minute unit.

ARC_SECOND - Static variable in class org.orekit.utils.units.Unit

Arc second unit.

ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants

Conversion factor from arc seconds to radians: 2*PI/(360*60*60).

ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter

Arcseconds to radians converter.

areAdditionalDataAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the flag indicating if additional parameters are in the message.

areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Check if fees are required.

areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Check if fees are required.

asCelestialBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the associated celestial body frame.

asFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the associated frame tree node.

asOrbitRelativeFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the associated orbit relative frame.

asSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the associated spacecraft body frame.

ASTRONOMICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at astronomical dawn/dusk (18° below horizon).

AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential

Parser for tides astronomical amplitude H_f.

AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Simple constructor.

Atmosphere - Interface in org.orekit.models.earth.atmosphere

Interface for atmospheric models.

AtmosphericRefractionModel - Interface in org.orekit.models

Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.

ATT_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Attitude line element for XML messages.

attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

Attitude - Class in org.orekit.attitudes

This class handles attitude definition at a given date.

Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

AttitudeBuilder - Interface in org.orekit.attitudes

This interface represents a builder for attitude.

AttitudeCovariance - Class in org.orekit.files.ccsds.ndm.adm.acm

Covariance entry.

AttitudeCovariance(AttitudeCovarianceType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance

Simple constructor.

AttitudeCovarianceHistory - Class in org.orekit.files.ccsds.ndm.adm.acm

Covariance history.

AttitudeCovarianceHistory(AttitudeCovarianceHistoryMetadata, List<AttitudeCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory

Simple constructor.

AttitudeCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm

Metadata for covariance history.

AttitudeCovarianceHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Empty constructor.

AttitudeCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for covariance history container entries.

AttitudeCovarianceType - Enum in org.orekit.files.ccsds.ndm.adm.acm

Attitude covariance set type used in CCSDS Attitude Comprehensive Messages.

AttitudeDetermination - Class in org.orekit.files.ccsds.ndm.adm.acm

Attitude determination data.

AttitudeDetermination() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Simple constructor.

AttitudeDeterminationKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for attitude determination data entries.

AttitudeDeterminationSensor - Class in org.orekit.files.ccsds.ndm.adm.acm

Attitude determination sensor data.

AttitudeDeterminationSensor() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Simple constructor.

AttitudeDeterminationSensorKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for attitude determination data sensor entries.

AttitudeElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm

Attitude element set type used in CCSDS Attitude Comprehensive Messages.

AttitudeEndpoints - Class in org.orekit.files.ccsds.ndm.adm

Endpoints for attitude definition.

AttitudeEndpoints() - Constructor for class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Empty constructor.

AttitudeEntryKey - Enum in org.orekit.files.ccsds.ndm.adm.aem

Keys for attitude entries in XML messages.

AttitudeEphemerisFile<C extends TimeStampedAngularCoordinates,S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general

An interface for accessing the data stored in an attitude ephemeris file.

AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates> - Interface in org.orekit.files.general

A segment of an attitude ephemeris for a satellite.

AttitudeEphemerisFile.SatelliteAttitudeEphemeris<C extends TimeStampedAngularCoordinates,S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general

Contains the information about a single satellite from an AttitudeEphemerisFile.

AttitudeEphemerisFileParser<T extends AttitudeEphemerisFile<?,?>> - Interface in org.orekit.files.general

Parse an ephemeris file.

AttitudeEphemerisFileWriter - Interface in org.orekit.files.general

An interface for writing out ephemeris files to disk.

AttitudeInterpolator - Class in org.orekit.attitudes

Class for attitude interpolation.

AttitudeInterpolator(Frame, TimeInterpolator<TimeStampedAngularCoordinates>) - Constructor for class org.orekit.attitudes.AttitudeInterpolator

Constructor.

AttitudeManeuver - Class in org.orekit.files.ccsds.ndm.adm.acm

Maneuver entry.

AttitudeManeuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Build an uninitialized maneuver.

AttitudeManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for attitude maneuver entries.

AttitudePhysicalProperties - Class in org.orekit.files.ccsds.ndm.adm.acm

Spacecraft physical properties.

AttitudePhysicalProperties(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Simple constructor.

AttitudePhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for physical properties data entries.

AttitudeProvider - Interface in org.orekit.attitudes

This interface represents an attitude provider model set.

attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Sets the attitude provider.

attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Sets the attitude provider.

attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Sets the attitude provider.

attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Sets the attitude provider.

AttitudeProviderModifier - Interface in org.orekit.attitudes

This interface represents an attitude provider that modifies/wraps another underlying provider.

AttitudesSequence - Class in org.orekit.attitudes

This classes manages a sequence of different attitude providers that are activated in turn according to switching events.

AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence

Constructor for an initially empty sequence.

AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes

Interface for attitude switch notifications.

AttitudeState - Class in org.orekit.files.ccsds.ndm.adm.acm

Attitude state entry.

AttitudeState(AttitudeElementsType, RateElementsType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Simple constructor.

AttitudeStateHistory - Class in org.orekit.files.ccsds.ndm.adm.acm

Attitude state history.

AttitudeStateHistory(AttitudeStateHistoryMetadata, List<AttitudeState>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Simple constructor.

AttitudeStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm

Metadata for attitude state history.

AttitudeStateHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Simple constructor.

AttitudeStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm

Keys for attitude state history container entries.

AttitudeType - Enum in org.orekit.files.ccsds.ndm.adm

Enumerate for ADM attitude type.

AttitudeWriter - Class in org.orekit.files.ccsds.ndm.adm.aem

An AttitudeEphemerisFileWriter generating AEM files.

AttitudeWriter(AemWriter, AdmHeader, AemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter

Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Name of the single parameter of this model: the attraction coefficient.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.DeSitterRelativity

Suffix for parameter name for attraction coefficient enabling Jacobian processing.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Suffix for parameter name for attraction coefficient enabling Jacobian processing.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Suffix for parameter name for attraction coefficient enabling Jacobian processing.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction

Suffix for parameter name for attraction coefficient enabling Jacobian processing.

Authentication - Enum in org.orekit.gnss.metric.ntrip

Enumerate for authentication method in DataStreamRecord.

AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities

Container class for common parameters used by all DSST forces.

AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Simple constructor.

azimuthBetweenPoints(GeodeticPoint, GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid

Compute the azimuth angle from local north between the two points.

azimuthBetweenPoints(FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Compute the azimuth angle from local north between the two points.

B

B2A - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Constant for A ← B direction.

B_STAR - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Parameter name for B* coefficient.

B_STAR - Static variable in class org.orekit.propagation.analytical.tle.TLE

Parameter name for B* coefficient.

BAR - Static variable in class org.orekit.utils.units.Unit

Bar unit.

BaseConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

Empty constructor.

BaseRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Base class modifying theoretical range measurement with ionospheric delay.

BaseRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier

Constructor.

BaseRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Base class modifying theoretical range-rate measurement with ionospheric delay.

BaseRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier

Constructor.

BaseRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Baselass modifying theoretical range-rate measurements with tropospheric delay.

BaseRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier

Constructor.

BaseRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Base class modifying theoretical range measurements with tropospheric delay.

BaseRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier

Constructor.

BasicConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion

Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.

BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Generic constructor.

BasicConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Simple constructor.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Propagate an orbit without any fancy features.

basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Propagate an orbit without any fancy features.

basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Propagate an orbit without any fancy features.

BatchLSEstimator - Class in org.orekit.estimation.leastsquares

Least squares estimator for orbit determination.

BatchLSEstimator(LeastSquaresOptimizer, PropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator

Simple constructor.

BatchLSModel - Class in org.orekit.estimation.leastsquares

Bridge between measurements and least squares problems.

BatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.BatchLSModel

Simple constructor.

BatchLSObserver - Interface in org.orekit.estimation.leastsquares

Observer for batch least squares estimator iterations.

BDTScale - Class in org.orekit.time

Beidou system time scale.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just before integration.

beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Method called just before integration.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Method called just before integration.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just before integration.

beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Method called just before integration.

BEIDOU_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the earth's rotation rate in rad/s for Beidou user.

BEIDOU_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.

BEIDOU_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for BeiDou weeks: 2006-01-01.

BEIDOU_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Earth's universal gravitational parameter for Beidou user in m³/s².

BEIDOU_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Number of weeks in the Beidou cycle.

BeidouAlmanac - Class in org.orekit.propagation.analytical.gnss.data

Class for BeiDou almanac.

BeidouAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac

Build a new almanac.

BeidouCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a Beidou civilian navigation message.

BeidouCivilianNavigationMessage(Frequency) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Constructor.

BeidouGeo - Class in org.orekit.gnss.attitude

Attitude providers for Beidou geostationary orbit navigation satellites.

BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouGeo

Simple constructor.

BeidouIGSO - Class in org.orekit.gnss.attitude

Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.

BeidouIGSO(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO

Simple constructor.

BeidouLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a BeiDou navigation message.

BeidouLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Constructor.

BeidouMeo - Class in org.orekit.gnss.attitude

Attitude providers for Beidou Medium Earth Orbit navigation satellites.

BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo

Simple constructor.

BeidouSatelliteType - Enum in org.orekit.propagation.analytical.gnss.data

Enumerate for Beidou satellite type.

BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.

beta0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

sqrt (1 - e2).

beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sqrt (1 - e2).

beta02 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

1 - e2.

beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

1 - e2.

Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Class modeling a measurement bias.

Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias

Simple constructor.

BIG_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Truncation tolerance for big, eccentric orbits.

BistaticRange - Class in org.orekit.estimation.measurements

Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.

BistaticRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRange

Simple constructor.

BistaticRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for BistaticRange measurements.

BistaticRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeBuilder

Simple constructor.

BistaticRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical bistatic range measurement with ionospheric delay.

BistaticRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier

Constructor.

BistaticRangeRate - Class in org.orekit.estimation.measurements

Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.

BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRangeRate

Simple constructor.

BistaticRangeRateBuilder - Class in org.orekit.estimation.measurements.generation

Builder for BistaticRangeRate measurements.

BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder

Simple constructor.

BistaticRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical bistatic range-rate measurement with ionospheric delay.

BistaticRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier

Constructor.

BistaticRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical bistatic range-rate measurements with tropospheric delay.

BistaticRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier

Constructor.

BistaticRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical bistatic range measurement with tropospheric delay.

BistaticRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier

Constructor.

blendArithmeticallyWith(FieldPVCoordinates<T>, T) - Method in class org.orekit.utils.FieldPVCoordinates

blendArithmeticallyWith(PVCoordinates, double) - Method in class org.orekit.utils.PVCoordinates

BlockWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter

Empty constructor.

BodiesElements - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements

Simple constructor.

BodyCenterPointing - Class in org.orekit.attitudes

This class handles body center pointing attitude provider.

BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing

Creates new instance.

BodyFacade - Class in org.orekit.files.ccsds.definitions

Facade in front of several center bodies in CCSDS messages.

BodyFacade(String, CelestialBody) - Constructor for class org.orekit.files.ccsds.definitions.BodyFacade

Simple constructor.

BodyShape - Interface in org.orekit.bodies

Interface representing the rigid surface shape of a natural body.

BooleanDetector - Class in org.orekit.propagation.events

This class provides AND and OR operations for event detectors.

BooleanDetector(List<EventDetector>, BooleanDetector.Operator, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.BooleanDetector

Private constructor with all the parameters.

booleanValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField

Get the value of the field as a boolean.

BoundedAttitudeProvider - Interface in org.orekit.attitudes

This interface is intended for attitude ephemerides valid only during a time range.

BoundedPropagator - Interface in org.orekit.propagation

This interface is intended for ephemerides valid only during a time range.

BoxAndSolarArraySpacecraft - Class in org.orekit.forces

Class representing the features of a classical satellite with a convex body shape.

BoxAndSolarArraySpacecraft(List<Panel>) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model.

BoxAndSolarArraySpacecraft(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lighting of solar array.

BrouwerLyddanePropagator - Class in org.orekit.propagation.analytical

This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).

BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit and potential provider.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Private helper constructor.

BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit and potential.

BrouwerLyddanePropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, mass and potential provider.

BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, mass and potential.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider and potential provider.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider and potential.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit and potential provider.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Private helper constructor.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

BrouwerLyddanePropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Brouwer-Lyddane propagator.

BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Build a new instance.

BrouwerLyddanePropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, OrbitType, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Build a new instance.

BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Build a new instance.

build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in interface org.orekit.attitudes.AttitudeBuilder

Build a filtered attitude.

build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in interface org.orekit.attitudes.AttitudeBuilder

Build a filtered attitude.

build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.attitudes.FixedFrameBuilder

Build a filtered attitude.

build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.attitudes.FixedFrameBuilder

Build a filtered attitude.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.FDOABuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PVBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TDOABuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder

Generate a single measurement.

build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder

Generate a single measurement.

build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Construct a KalmanEstimator from the data in this builder.

build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder

Construct a KalmanEstimator from the data in this builder.

build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Construct a SemiAnalyticalUnscentedKalmanEstimator from the data in this builder.

build() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Construct a UnscentedKalmanEstimator from the data in this builder.

build() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Build the file from parsed entries.

build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Build a filtered attitude.

build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Build a filtered attitude.

build(boolean, boolean, RotationOrder, boolean, AbsoluteDate, double...) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Get the angular coordinates corresponding to the attitude data.

build() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.NdmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Build the file from parsed entries.

build() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Build the file from parsed entries.

build() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Build the file from parsed entries.

build() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Finalizes the build.

build() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Finalizes the build.

build() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Finalizes the build.

build() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Finalizes the build.

build() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Build the aggregated PVCoordinatesProvider.

build() - Method in class org.orekit.utils.WaypointPVBuilder

Build a PVCoordinatesProvider from the waypoints added to this builder.

buildAcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Attitude Comprehensive Messages.

buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Attitude Comprehensive Messages.

buildAemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Attitude Ephemeris Messages.

buildAemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Attitude Ephemeris Messages.

buildApmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Attitude Parameters Messages.

buildApmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Attitude Parameters Messages.

buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType

Build an attitude provider suitable for this satellite type.

buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) - Static method in class org.orekit.propagation.integration.AbstractGradientConverter

Process a state into a Gradient version without force model parameter.

buildBox(double, double, double, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Build the panels of a simple parallelepipedic box.

buildCdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Conjunction Data Messages.

buildCdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Conjunction Data Messages.

Builder() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Create a builder using the AggregatedPVCoordinatesProvider.InvalidPVProvider as the initial provider.

Builder(PVCoordinatesProvider) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Create a builder using the provided initial provider.

buildFlatArray(Flattener, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients array in flat form.

buildFromCustomAttitude(AttitudeProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Build a ThrustDirectionAndAttitudeProvider where the attitude is provided by an external.

buildFromDirectionInFrame(Frame, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Build a ThrustDirectionAndAttitudeProvider by a variable direction in a custom frame.

buildFromDirectionInLOF(LOF, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Build a ThrustDirectionAndAttitudeProvider by a variable direction in a Local Orbital Frame.

buildFromFixedDirectionInSatelliteFrame(Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Build a ThrustDirectionAndAttitudeProvider from a fixed direction in the satellite frame.

buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 2.

buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 4.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(FieldOrbit<T>, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder

Build a first order integrator.

buildIntegrator(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder

Build a first order integrator.

buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a first order integrator.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Build a new batch least squares model.

buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a new batch least squares model.

buildNdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Navigation Data Messages.

buildNdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Navigation Data Messages.

buildOcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Orbit Comprehensive Messages.

buildOcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Orbit Comprehensive Messages.

buildOemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Orbit Ephemeris Messages.

buildOemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Orbit Ephemeris Messages.

buildOmmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Orbit Mean elements Messages.

buildOmmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Orbit Mean elements Messages.

buildOpmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Orbit Parameters Messages.

buildOpmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Orbit Parameters Messages.

buildPanels(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Build the panels of a simple parallelepiped box plus one solar array panel.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Build a propagator.

buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a propagator.

buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients row.

buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Build a simple zone (connected zone without holes).

buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Build a simple zone (connected zone without holes).

buildTdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build a parser for Tracking Data Messages.

buildTdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build a writer for Tracking Data Messages.

buildTermsList(String) - Static method in class org.orekit.utils.units.Parser

Build the list of terms corresponding to a units specification.

buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder

Create a list of parse tokens.

buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder

Create a list of parse tokens.

buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder

Create a list of parse tokens.

buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder

Create a list of parse tokens.

buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.XmlTokenBuilder

Create a list of parse tokens.

buildUncachedITRF(UT1Scale) - Method in class org.orekit.frames.AbstractFrames

buildUncachedITRF(UT1Scale) - Method in interface org.orekit.frames.Frames

Build an uncached International Terrestrial Reference Frame with specific EOP history.

buildUncachedITRF(EOPHistory, UTCScale) - Static method in class org.orekit.frames.FramesFactory

Build an uncached International Terrestrial Reference Frame with specific EOP history.

buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 2.

buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 4.

BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).

BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU1980 compatibles).

BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU2000 compatibles).

BurstSelector - Class in org.orekit.time

Selector generating high rate bursts of dates separated by some rest period.

BurstSelector(int, double, double, TimeScale) - Constructor for class org.orekit.time.BurstSelector

Simple constructor.

ByteArrayEncodedMessage - Class in org.orekit.gnss.metric.parser

Encoded message as a byte array.

ByteArrayEncodedMessage(byte[]) - Constructor for class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage

Simple constructor.

C

c1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

C1 from SPTRCK #3.

c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C1 from SPTRCK #3.

C1L - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C1L.

C1SS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C1SS.

c2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

C2 from SPTRCK #3.

c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C2 from SPTRCK #3.

c4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

C4 from SPTRCK #3.

c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C4 from SPTRCK #3.

C_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_2FASX4.

C_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_3FASX6.

C_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_FASX2.

C_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_G22.

C_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_G32.

C_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_G44.

C_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_G52.

C_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

C_G54.

CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential

Caching wrapper for NormalizedSphericalHarmonicsProvider.

CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Simple constructor.

cachesTidalCorrection() - Method in class org.orekit.frames.EOPHistory

Check if the instance caches tidal corrections.

calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.

calculatePointAlongArc(double) - Method in class org.orekit.bodies.LoxodromeArc

Calculate a point at a specific percentage along the arc.

Calibration(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.Calibration

Constructor.

CalibrationDetail(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.CalibrationDetail

Constructor.

CalibrationTargetConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Empty constructor.

canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if coefficients can be added.

CANONICAL_I_J - Static variable in class org.orekit.estimation.measurements.gnss.Dipole

Canonical dipole, with primary vector set to Vector3D.PLUS_I and secondary vector set to Vector3D.PLUS_J.

canReceiveNMEA() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Check if caster can receive NMEA messages.

CarrierPhase - Enum in org.orekit.gnss.metric.ntrip

Enumerate for carrier phase in DataStreamRecord.

cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder

Construct a waypoint builder interpolating points using a linear cartesian interpolation.

CartesianCovariance - Class in org.orekit.files.ccsds.ndm.odm

Container for OPM/OMM/OCM Cartesian covariance matrix.

CartesianCovariance(Supplier<FrameFacade>) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Create an empty data set.

CartesianCovarianceKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for OPM/OMM/OCM Cartesian covariance entries.

CartesianCovarianceWriter - Class in org.orekit.files.ccsds.ndm.odm

Writer for covariance matrix data.

CartesianCovarianceWriter(String, String, CartesianCovariance) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter

Create a writer.

CartesianDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.

CartesianOrbit - Class in org.orekit.orbits

This class holds Cartesian orbital parameters.

CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from any kind of orbital parameters.

CasterRecord - Class in org.orekit.gnss.metric.ntrip

Caster record in source table.

CasterRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.CasterRecord

Build a caster record by parsing a source table line.

CCSDS_ACM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter

Version number implemented.

CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter

Version number implemented.

CCSDS_APM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter

Version number implemented.

CCSDS_CDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter

Version number implemented.

CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).

CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.

CCSDS_OCM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Version number implemented.

CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter

Version number implemented.

CCSDS_OMM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter

Version number implemented.

CCSDS_OPM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter

Version number implemented.

CCSDS_TDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter

Version number implemented.

Cdm - Class in org.orekit.files.ccsds.ndm.cdm

This class stores all the information of the Conjunction Data Message (CDM) File parsed by CdmParser.

Cdm(CdmHeader, List<CdmSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.Cdm

Simple constructor.

CdmData - Class in org.orekit.files.ccsds.ndm.cdm

Container for Conjunction Data Message data.

CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData

Constructor with RTN covariance.

CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData

Constructor with RTN covariance.

CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, XYZCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData

Constructor with RTN and XYZ covariance.

CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, SigmaEigenvectorsCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData

Constructor with RTN and sigma/eigenvector covariance.

CdmHeader - Class in org.orekit.files.ccsds.ndm.cdm

Header of a CCSDS Conjunction Data Message.

CdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeader

Constructor.

CdmHeaderKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keywords allowed in CdmHeader.

CdmHeaderProcessingState - Class in org.orekit.files.ccsds.ndm.cdm

ProcessingState for CDM header.

CdmHeaderProcessingState(CdmParser) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState

Simple constructor.

CdmMessageWriter - Class in org.orekit.files.ccsds.ndm.cdm

Cdm message writer.

CdmMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

CdmMetadata - Class in org.orekit.files.ccsds.ndm.cdm

This class gathers the meta-data present in the Conjunction Data Message (CDM).

CdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Simple constructor.

CdmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Simple constructor.

CdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM container entries.

CdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for Metadata for CCSDS Conjunction Data Messages.

CdmMetadataWriter(CdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter

Simple constructor.

CdmParser - Class in org.orekit.files.ccsds.ndm.cdm

Base class for Conjunction Data Message parsers.

CdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmParser

Complete constructor.

CdmRelativeMetadata - Class in org.orekit.files.ccsds.ndm.cdm

This class gathers the relative meta-data present in the Conjunction Data Message (CDM).

CdmRelativeMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Simple constructor.

CdmRelativeMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM container entries.

CdmSegment - Class in org.orekit.files.ccsds.ndm.cdm

This class stores the metadata and data for one object.

CdmSegment(CdmMetadata, CdmData) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmSegment

Simple constructor.

CdmWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for CCSDS Conjunction Data Message.

CdmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmWriter

Complete constructor.

CelestialBodies - Interface in org.orekit.bodies

Commonly used celestial bodies.

CelestialBody - Interface in org.orekit.bodies

Interface for celestial bodies like Sun, Moon or solar system planets.

CelestialBodyFactory - Class in org.orekit.bodies

Factory class for bodies of the solar system.

CelestialBodyFrame - Enum in org.orekit.files.ccsds.definitions

Frames used in CCSDS Orbit Data Messages.

CelestialBodyLoader - Interface in org.orekit.bodies

Interface for loading celestial bodies.

CelestialBodyPointed - Class in org.orekit.attitudes

This class handles a celestial body pointed attitude provider.

CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed

Creates new instance.

CenterName - Enum in org.orekit.files.ccsds.definitions

Orbit central bodies for which a Celestial body can be created.

CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction

Name of the single parameter of this model: the central attraction coefficient.

CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Name of the single parameter of this model: the central attraction coefficient.

Chan1997 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision using the method described in :
"Chan, K.

Chan1997() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997

Empty constructor.

changeCovarianceFrame(FieldOrbit<T>, LOF) - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance in a given local orbital frame.

changeCovarianceFrame(FieldOrbit<T>, Frame) - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance in the output frame.

changeCovarianceFrame(Orbit, LOF) - Method in class org.orekit.propagation.StateCovariance

Get the covariance in a given local orbital frame.

changeCovarianceFrame(Orbit, Frame) - Method in class org.orekit.propagation.StateCovariance

Get the covariance in the output frame.

changeCovarianceType(FieldOrbit<T>, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance matrix in another orbit type.

changeCovarianceType(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovariance

Get the covariance matrix in another orbit type.

checkAllowed(double, Object, String, double, double) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Complain if a key is not allowed.

checkDatesConsistency(AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.TimeStampedPair

Check date consistency.

checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Check dimension.

checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory

Check Earth orientation parameters continuity.

checkException() - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Check if any of the streaming thread has thrown an exception.

checkExternalFrame(Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Check external frame is properly initialized.

checkFrameAndOrbitTypeConsistency(Frame, OrbitType) - Static method in class org.orekit.propagation.StateCovariance

Check constructor's inputs consistency.

checkInputConsistency(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Static method in class org.orekit.propagation.analytical.Ephemeris

Check input consistency between states, covariances and their associated interpolators.

checkInterpolatorCompatibilityWithSampleSize(FieldTimeInterpolator<? extends FieldTimeStamped<T>, T>, int) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator

Method checking if given interpolator is compatible with given sample size.

checkInterpolatorCompatibilityWithSampleSize(TimeInterpolator<? extends TimeStamped>, int) - Static method in class org.orekit.time.AbstractTimeInterpolator

Method checking if given interpolator is compatible with given sample size.

checkMandatoryEntriesExceptExternalFrame(double, Enum<?>, Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Check is mandatory entries except external frame have been initialized.

checkNotNaN(double, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Complain if a field is NaN.

checkNotNegative(int, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Complain if a field is negative.

checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Complain if a field is null.

checkNotNull(Object, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Complain if a field is null.

checkOrbitsConsistency(Collection<Orbit>) - Static method in class org.orekit.orbits.AbstractOrbitInterpolator

Check orbits consistency by comparing their gravitational parameters µ.

checkParity(int, int) - Static method in class org.orekit.gnss.rflink.gps.SubFrame

Check parity.

checkSampleAndInterpolatorConsistency(List<SpacecraftState>, boolean, boolean) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator

Check that an interpolator exist for given sample state definition.

checkScreenVolumeConditions() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Check screen volume conditions.

checkStatesAndCovariancesConsistency(List<SpacecraftState>, List<StateCovariance>) - Static method in class org.orekit.propagation.analytical.Ephemeris

Check that given states and covariances are consistent.

checkStatesDefinitionsConsistency(List<SpacecraftState>) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator

Check that all state are either orbit defined or based on absolute position-velocity-acceleration.

checkStep(double) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder

Check that given step size is not equal to 0.

checkTimeSystems() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem

Check that, according to the CCSDS standard, every OEMBlock has the same time system.

checkUnit(Unit) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Check if parsed unit is compatible with field type.

ChronologicalComparator - Class in org.orekit.time

Comparator for TimeStamped instance.

ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator

Simple constructor.

CircularFieldOfView - Class in org.orekit.geometry.fov

Class representing a spacecraft sensor Field Of View with circular shape.

CircularFieldOfView(Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.CircularFieldOfView

Build a new instance.

CircularOrbit - Class in org.orekit.orbits

This class handles circular orbital parameters.

CircularOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from Cartesian parameters.

CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from Cartesian parameters.

CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from any kind of orbital parameters.

CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at civil dawn/dusk (6° below horizon).

CivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a GPS/QZNSS civilian navigation message.

CivilianNavigationMessage(boolean, double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Constructor.

CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the S_j(k, h) and the C_j(k, h) series and their partial derivatives with respect to k and h.

CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

C_j(k, h) and S_j(k, h) constructor.

CK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

CK2.

CK4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

CK4.

ClassicalRungeKuttaFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for ClassicalRungeKuttaFieldIntegrator.

ClassicalRungeKuttaFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder

Constructor.

ClassicalRungeKuttaFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder

Constructor using a "fielded" step.

ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ClassicalRungeKuttaIntegrator.

ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a new instance.

ClasspathCrawler - Class in org.orekit.data

Provider for data files stored as resources in the classpath.

ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

clear() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue

Clear all stored events.

clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

Clear all stored events.

clear() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Remove all handlers managed by this multiplexer.

clear() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Remove all handlers managed by this multiplexer.

clear() - Method in class org.orekit.utils.DoubleArrayDictionary

Remove all entries.

clear() - Method in class org.orekit.utils.FieldArrayDictionary

Remove all entries.

clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear the specified celestial body from the internal cache.

clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear all loaded celestial bodies.

clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Clear the specified celestial body from the internal cache.

clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Clear all loaded celestial bodies.

clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for one celestial body.

clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for all celestial bodies.

clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Clear loaders for one celestial body.

clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Clear loaders for all celestial bodies.

clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory

Clear loaders for Earth Orientation Parameters history.

clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedEop

Clear loaders for Earth Orientation Parameters history.

clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedFrames

Clear loaders for Earth Orientation Parameters history.

clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Remove all events detectors.

clearEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Remove all events detectors.

clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator

Remove all events detectors.

clearFilters() - Method in class org.orekit.data.FiltersManager

Remove all data filters.

clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient

Clear the recorded values from the interpolation grid.

clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Clear the recorded values from the interpolation grid.

clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager

Clear the set of data file names that have been loaded.

clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger

Clear the logged events.

clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger

Clear the logged events.

clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear ocean tides readers.

clearOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Clear ocean tides readers.

clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear gravity field readers.

clearPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Clear gravity field readers.

clearProviders() - Method in class org.orekit.data.DataProvidersManager

Remove all data providers.

clearStepHandlers() - Method in interface org.orekit.propagation.FieldPropagator

Remove all step handlers.

clearStepHandlers() - Method in interface org.orekit.propagation.Propagator

Remove all step handlers.

clearUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales

Clear loaders for UTC-TAI offsets history files.

clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory

Clear loaders for UTC-TAI offsets history files.

CLOCK_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Clock accuracy unit.

CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Name of the additional state for satellite clock corrections.

CLOCK_DRIFT_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite

Prefix for clock drift parameter driver, the propagator index will be appended to it.

CLOCK_OFFSET_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite

Prefix for clock offset parameter driver, the propagator index will be appended to it.

CLOCK_RATE_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Clock rate accuracy unit.

CLOCK_RATE_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Clock rate unit.

CLOCK_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Clock unit.

ClockCorrection - Class in org.orekit.gnss.metric.messages.common

Container for SSR clock correction data.

ClockCorrection(double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.ClockCorrection

Constructor.

ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss

Provider for clock corrections as additional states.

ClockCorrectionsProvider(GNSSClockElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Simple constructor.

ClockDataLine(RinexClock.ClockDataType, String, DateComponents, TimeComponents, int, double, double, double, double, double, double) - Constructor for class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Constructor.

close() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter

close() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter

close() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter

close() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Close the generator.

close() - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Close the generator.

close() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Identifier for cMm coefficients.

CNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Identifier for message type.

CNV1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Identifier for Beidou-3 B1C message type.

CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Identifier for Beidou-3 B2A message type.

CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Identifier for message type.

CNV3 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Identifier for Beidou-3 B2B message type.

co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

C / (2 * A * B) .

co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

C / (2 * A * B) .

CodeBias - Class in org.orekit.gnss.metric.messages.common

Container for code bias data.

CodeBias(int, double) - Constructor for class org.orekit.gnss.metric.messages.common.CodeBias

Constructor.

coef - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

coef for SGP C3 computation.

coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C3 computation.

coef1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

coef for SGP C5 computation.

coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C5 computation.

CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities

This class is designed to provide coefficient from the DSST theory.

CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities

Key formed by two integer values.

COLUMN_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Default column dimension for position-velocity state covariance.

CombinationType - Enum in org.orekit.estimation.measurements.gnss

Enumerate for combination of measurements types.

combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Combines observation data using a dual frequency combination of measurements.

combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Combines observation data using a combination of measurements.

combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination

Combines observation data using a combination of measurements.

combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination

Combines observation data using a single frequency combination of measurements.

combine(ObservationDataSet) - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination

Combines observation data using a combination of measurements.

combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination

Combines observation data using a combination of measurements.

combinedDerivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Compute the derivatives related to the additional state (and optionally main state increments).

combinedDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider

Compute the derivatives related to the additional state (and optionally main state increments).

CombinedDerivatives - Class in org.orekit.propagation.integration

Container for additional derivatives.

CombinedDerivatives(double[], double[]) - Constructor for class org.orekit.propagation.integration.CombinedDerivatives

Simple constructor.

combinedDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider

Compute the derivatives related to the additional state (and optionally main state increments).

combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations

Compute the derivatives related to the additional state (and optionally main state increments).

combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Compute the derivatives related to the additional state (and optionally main state increments).

CombinedObservationData - Class in org.orekit.estimation.measurements.gnss

Combined observation data.

CombinedObservationData(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData

Constructor.

CombinedObservationDataSet - Class in org.orekit.estimation.measurements.gnss

Combined observation data set.

CombinedObservationDataSet(SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Simple constructor.

COMMA_SEP - Static variable in exception org.orekit.errors.UnsupportedParameterException

Comma separator for printing list of supported parameter drivers.

CommentsContainer - Class in org.orekit.files.ccsds.section

Container for comments in various CCSDS messages.

CommentsContainer() - Constructor for class org.orekit.files.ccsds.section.CommentsContainer

Create a new meta-data.

CommonGnssData - Class in org.orekit.propagation.analytical.gnss.data

Container for common GNSS data contained in almanac and navigation messages.

CommonGnssData(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Constructor.

CommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for common ODM container entries.

CommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.odm

Writer for Common metadata for CCSDS Orbit Parameter/Ephemeris/Mean Messages.

CommonMetadataWriter(OdmCommonMetadata, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter

Simple constructor.

CommonPhysicalProperties - Class in org.orekit.files.ccsds.ndm

Container for common physical properties for both OrbitPhysicalProperties and AdditionalParameters.

CommonPhysicalProperties() - Constructor for class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Simple constructor.

ComparableMeasurement - Interface in org.orekit.estimation.measurements

Base interface for comparing measurements regardless of their type.

compare(IntegerLeastSquareSolution, IntegerLeastSquareSolution) - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator

The comparison is based on the squared distance to the float solution.

compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator

Compare two time-stamped instances.

compare(FieldTimeStamped<KK>, FieldTimeStamped<KK>) - Method in class org.orekit.time.FieldChronologicalComparator

Compare two time-stamped instances.

compareTo(ComparableMeasurement) - Method in interface org.orekit.estimation.measurements.ComparableMeasurement

compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters

compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compare the instance with another date.

compareTo(DateComponents) - Method in class org.orekit.time.DateComponents

compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Compare the instance with another date.

compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents

compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries

Join several nutation series, for fast simultaneous evaluation.

complain(String, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Complain about a missing value.

completed() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Check if maneuver has been completed.

components(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter

Generate calendar components.

compose(FieldAbsoluteDate<T>, FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Build a transform by combining two existing ones.

compose(AbsoluteDate, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform

Build a transform by combining two existing ones.

CompositeDataContext - Class in org.orekit.data

A simple implementation of DataContext that composes the constituent factories into a data context.

CompositeDataContext(TimeScales, Frames, CelestialBodies, GravityFields, GeoMagneticFields) - Constructor for class org.orekit.data.CompositeDataContext

Simple constructor.

compositeRotation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Compute a composite rotation.

compositeRotation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform

Compute a composite rotation.

compositeTranslation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Compute a composite translation.

compositeTranslation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform

Compute a composite translation.

compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer

Compute the DOP at a given date for a set of GNSS spacecrafts.

compute(LibrationOrbitType) - Method in class org.orekit.orbits.CR3BPDifferentialCorrection

Return the real starting PVCoordinates on the Libration orbit type after differential correction from a first guess.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(Cdm, double, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using an Orekit Conjunction Data Message.

compute(Cdm, T, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using an Orekit Conjunction Data Message.

compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(ShortTermEncounter2DDefinition, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using a given collision definition.

compute(FieldShortTermEncounter2DDefinition<T>, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using given collision definition.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.

compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.

compute(Cdm, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Cdm, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(ShortTermEncounter2DDefinition, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005

Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.

compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005

Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.

compute(Cdm, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Cdm, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Cdm, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Cdm, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Cdm, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using a Conjunction Data Message (CDM).

compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(Orbit, StateCovariance, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using parameters necessary for creating a collision definition instance.

compute(ShortTermEncounter2DDefinition) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(ShortTermEncounter2DDefinition, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(FieldShortTermEncounter2DDefinition<T>) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using given collision definition.

compute(double, double, double, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute(T, T, T, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Compute the probability of collision using arguments specific to the rotated encounter frame.

compute() - Method in class org.orekit.utils.AbstractMultipleShooting

Return the list of corrected patch points.

compute() - Method in interface org.orekit.utils.MultipleShooting

Return the list of corrected patch points.

computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Compute the additional constraints.

computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting

Compute the additional constraints.

computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter

Compute the additional constraints.

computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Compute a part of the Jacobian matrix from additional constraints.

computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting

Compute a part of the Jacobian matrix from additional constraints.

computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter

Compute a part of the Jacobian matrix from additional constraints.

computeC2Z(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel

Get the value of the Zeis constant.

computeC2Z(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel

Get the value of the Zeis constant.

computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the combined covariance expressed in the encounter frame.

computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the combined covariance expressed in the encounter frame.

computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.

computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.

computeCommonParametersWithDerivatives(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Compute common estimation parameters.

computeCommonParametersWithout(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Compute common estimation parameters.

computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.

computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.

computeDeltaPV(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector

Compute the relative PV between primary and secondary objects.

computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations

Compute differential equations for main state.

computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations

Compute differential equations for main state.

computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting

Compute a part of the Jacobian matrix with derivatives from epoch.

computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute recursively G_s and H_s polynomials from equation 3.1-(5).

computeGsHs(T, T, T, T, int, Field<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute recursively G_s and H_s polynomials from equation 3.1-(5).

computeHaloFirstGuess(double, LibrationOrbitFamily, double, double) - Method in class org.orekit.orbits.RichardsonExpansion

Calculate first Guess.

computeHeightCorrection(double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils

This method computes the height correction for the hydrostatic component of the mapping function.

computeHeightCorrection(T, T, Field<T>) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils

This method computes the height correction for the hydrostatic component of the mapping function.

computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear

Compute the values for the first four coefficients and their derivatives by means of series.

computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear

Compute the initial values (see Collins, 4-255, 4-256 and 4.259)

computeInitValues(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear

Compute the roots for the Hansen coefficients and their derivatives.

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the values for the first four coefficients and their derivatives by means of series.

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the initial values (see Collins, 4-255, 4-256 and 4.259)

computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Compute the roots for the Hansen coefficients and their derivatives.

computeInnovationVector(EstimatedMeasurement<?>) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Compute the unnormalized innovation vector from the given predicted measurement.

computeInnovationVector(EstimatedMeasurement<?>, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Compute the normalized innovation vector from the given predicted measurement.

computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Compute the interpolated covariance expressed in the interpolated orbit frame.

computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceBlender

Compute the interpolated covariance expressed in the interpolated orbit frame.

computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Compute the interpolated covariance expressed in the interpolated orbit frame.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the limit visibility point for a satellite in a given direction.

computeLyapunov() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection

Return the real starting PVCoordinates on the Lyapunov orbit after differential correction from a first guess.

computeLyapunovFirstGuess(double, double, double) - Method in class org.orekit.orbits.RichardsonExpansion

Calculate first Guess.

computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel

Compute the J2-squared second-order terms in equinoctial elements.

computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel

Compute the J2-squared second-order terms in equinoctial elements.

computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel

Compute the J2-squared second-order terms in equinoctial elements.

computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel

Compute the J2-squared second-order terms in equinoctial elements.

computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Conversion from osculating to mean orbit.

computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from osculating to mean orbit.

computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from osculating to mean orbit.

computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Conversion from osculating to mean orbit.

computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Conversion from osculating to mean orbit.

computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the miss distance at time of closest approach.

computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the miss distance at time of closest approach.

computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from mean to osculating orbit.

computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Conversion from mean to osculating orbit.

computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the other collision object position projected onto the collision plane.

computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the other collision object position projected onto the collision plane.

computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the other collision object position in the rotated collision plane.

computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the other collision object position in the rotated collision plane.

computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the other collision object position in the rotated collision plane.

computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the other collision object position in the rotated collision plane.

computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the other collision position and velocity relative to the reference collision object.

computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the other collision position and velocity relative to the reference collision object.

computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the combined covariance matrix diagonalized and projected onto the collision plane.

computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the combined covariance matrix diagonalized and projected onto the collision plane.

computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the projected combined covariance matrix onto the collision plane.

computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the projected combined covariance matrix onto the collision plane.

computeProjectionMatrix() - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane.

computeProjectionMatrix(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane defined by this same encounter local orbital frame.

computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the Q_n,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).

computeQns(T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the Q_n,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).

computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the projection matrix from the reference collision object inertial frame to the collision plane.

computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the projection matrix from the reference collision object inertial frame to the collision plane.

computeSquaredMahalanobisDistance(T, T, T, T) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance.

computeSquaredMahalanobisDistance(FieldVector2D<T>, FieldMatrix<T>) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance.

computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeSquaredMahalanobisDistance(double, double, double, double) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance.

computeSquaredMahalanobisDistance(Vector2D, RealMatrix) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance.

computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).

computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider

computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustDirectionProvider

Compute the thrust direction corresponding to an orbital state.

computeValue(double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max

Compute the value of the probability of collision.

computeValue(T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max

Compute the value of the probability of collision.

computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the V_n,s coefficients from 2.8.2-(1)(2).

computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

This method allows the computation of the zenith hydrostatic and zenith wet delay.

ConfigurableLowThrustManeuver - Class in org.orekit.forces.maneuvers

This class implements a configurable low thrust maneuver.

ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, ManeuverTriggers, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Constructor.

configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Configure the propagator to compute derivatives.

configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel

Configure the propagator to compute derivatives.

configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel

Configure the propagator to compute derivatives.

configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Configure ocean load deformation coefficients.

configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Configure ocean load deformation coefficients.

configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Configure the current estimated orbits.

configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel

Configure the current estimated orbits.

configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel

Configure the current estimated orbits.

constantAfter() - Method in class org.orekit.utils.WaypointPVBuilder

Indicate the resulting PVCoordinatesProvider provide a constant location of the last waypoint after to the last time.

ConstantAzimuthAiming - Class in org.orekit.models.earth.tessellation

Class used to orient tiles with respect to a geographic azimuth.

ConstantAzimuthAiming(OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.tessellation.ConstantAzimuthAiming

Simple constructor.

constantBefore() - Method in class org.orekit.utils.WaypointPVBuilder

Indicate the resulting PVCoordinatesProvider provide a constant location of the first waypoint prior to the first time.

ConstantProcessNoise - Class in org.orekit.estimation.sequential

Provider for constant process noise matrices.

ConstantProcessNoise(RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise

Simple constructor.

ConstantProcessNoise(RealMatrix, RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise

Simple constructor.

ConstantPVCoordinatesProvider - Class in org.orekit.utils

Provider based on a single point.

ConstantPVCoordinatesProvider(Vector3D, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider

Create the PVCoordinatesProvider from a fixed point in a frame.

ConstantPVCoordinatesProvider(GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider

Create a the provider from a fixed lat/lon/alt on a central body.

ConstantPVCoordinatesProvider(PVCoordinates, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider

Create the PVCoordinatesProvider from a fixed point in a frame.

Constants - Interface in org.orekit.utils

Set of useful physical constants.

ConstantThrustDirectionProvider - Class in org.orekit.forces.maneuvers.propulsion

Simple implementation of VariableThrustDirectionVector, providing a constant direction.

ConstantThrustDirectionProvider(Vector3D) - Constructor for class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider

Constructor.

ConstantThrustManeuver - Class in org.orekit.forces.maneuvers

This class implements a simple maneuver with constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, AttitudeProvider, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

containsSatellite(String) - Method in class org.orekit.files.sp3.SP3

Tests whether a satellite with the given id is contained in this orbit file.

ContextBinding - Class in org.orekit.files.ccsds.utils

Context for parsing/writing Navigation Data Message.

ContextBinding(Supplier<IERSConventions>, BooleanSupplier, Supplier<DataContext>, Supplier<ParsedUnitsBehavior>, Supplier<AbsoluteDate>, Supplier<TimeSystem>, DoubleSupplier, DoubleSupplier) - Constructor for class org.orekit.files.ccsds.utils.ContextBinding

Create a new context.

ContinueOnEvent - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent

Empty constructor.

ContinuousScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Scheduler generating measurements sequences continuously.

ContinuousScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler

Simple constructor.

Control3DVectorCostType - Enum in org.orekit.forces.maneuvers

Enumerate on types of cost for 3D control vector (thrust as a force or acceleration, including an impulse) at a given time.

convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter

Convert a row.

convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Convert an osculating orbit into a mean orbit, in DSST sense.

convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(double) - Method in class org.orekit.utils.units.UnitsConverter

Convert a value.

convert2DigitsYear(int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Convert a 2 digits year to a complete year.

convertIntervalDetector(Field<S>, ParameterDrivenDateIntervalDetector) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Convert a primitive firing intervals detector into a field firing intervals detector.

convertIntervalDetector(Field<S>, T) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Convert a primitive firing intervals detector into a field firing intervals detector.

convertStartDetector(Field<S>, A) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Convert a primitive firing start detector into a field firing start detector.

convertStopDetector(Field<S>, O) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Convert a primitive firing stop detector into a field firing stop detector.

convertToFieldOrbit(Field<T>, Orbit) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the "Fielded" instance type.

convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the instance type.

convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the instance type.

copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Copy the instance, making sure mandatory fields have been initialized.

copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Copy the instance, making sure mandatory fields have been initialized.

copy() - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder

Create a new instance identical to this one.

copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Create a copy of a DSSTPropagatorBuilder object.

copy() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Create a new instance identical to this one.

copy() - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Create a new instance identical to this one.

copy() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Create a new instance identical to this one.

copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Create a copy of a NumericalPropagatorBuilder object.

copy() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Create a new instance identical to this one.

copy() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Create a new instance identical to this one.

copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Copy an ObservationData object.

copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Copy an ObservationData object.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouGeo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouMeo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GenericGNSS

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIA

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF

Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIR

Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.

correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIR

Compute GNSS attitude with midnight/noon yaw turn correction.

CorrectionApplied - Enum in org.orekit.files.ccsds.ndm.tdm

Indicator for corrections application.

cosi0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

cosinus original inclination.

cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cosinus original inclination.

COULOMB - Static variable in class org.orekit.utils.units.Unit

Coulomb unit.

countAtDate(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale

Compute clock count corresponding to some date.

COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Covariance line element for XML messages.

COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Covariance line element for XML messages.

CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential

Provider for process noise matrices.

CovarianceMethod - Enum in org.orekit.files.ccsds.ndm.cdm

Maneuvrable possibilities used in CCSDS Conjunction Data Messages.

CPF - Class in org.orekit.files.ilrs

This class stores all the information of the Consolidated laser ranging Prediction File (CPF) parsed by CPFParser.

CPF() - Constructor for class org.orekit.files.ilrs.CPF

Constructor.

CPF.CPFCoordinate - Class in org.orekit.files.ilrs

A single record of position and possibility velocity in an SP3 file.

CPF.CPFEphemeris - Class in org.orekit.files.ilrs

An ephemeris entry for a single satellite contains in a CPF file.

CPFCoordinate(AbsoluteDate, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate

Constructor with null velocity vector.

CPFCoordinate(AbsoluteDate, Vector3D, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate

Constructor.

CPFEphemeris(String) - Constructor for class org.orekit.files.ilrs.CPF.CPFEphemeris

Constructor.

CPFHeader - Class in org.orekit.files.ilrs

Container for Consolidated laser ranging Prediction File (CPF) header.

CPFHeader() - Constructor for class org.orekit.files.ilrs.CPFHeader

Empty constructor.

CPFParser - Class in org.orekit.files.ilrs

A parser for the CPF orbit file format.

CPFParser() - Constructor for class org.orekit.files.ilrs.CPFParser

Default constructor.

CPFParser(double, int, IERSConventions, TimeScale, Frames) - Constructor for class org.orekit.files.ilrs.CPFParser

Constructor.

CPFWriter - Class in org.orekit.files.ilrs

An CPF Writer class that can take in a general EphemerisFile object and export it as a valid CPF file.

CPFWriter(CPFHeader, TimeScale) - Constructor for class org.orekit.files.ilrs.CPFWriter

Constructor.

CPFWriter(CPFHeader, TimeScale, boolean) - Constructor for class org.orekit.files.ilrs.CPFWriter

Constructor.

CR3BPConstants - Class in org.orekit.propagation.numerical.cr3bp

Set of useful physical CR3BP constants using JPL data.

CR3BPDifferentialCorrection - Class in org.orekit.orbits

Class implementing the differential correction method for Halo or Lyapunov Orbits.

CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection

Simple Constructor.

CR3BPFactory - Class in org.orekit.bodies

Factory class creating predefined CR3BP system using CR3BPSystem class.

CR3BPForceModel - Class in org.orekit.propagation.numerical.cr3bp

Class calculating the acceleration induced by CR3BP model.

CR3BPForceModel(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Simple constructor.

CR3BPMultipleShooter - Class in org.orekit.propagation.numerical.cr3bp

Multiple shooting method applicable for orbits, either propagation in CR3BP, or in an ephemeris model.

CR3BPMultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<STMEquations>, double, int) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Simple Constructor.

CR3BPRotatingFrame - Class in org.orekit.frames

Class creating the rotating frame centered on the barycenter of the CR3BP System.

CR3BPRotatingFrame(double, CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.CR3BPRotatingFrame

Simple constructor.

CR3BPSystem - Class in org.orekit.bodies

Class creating, from two different celestial bodies, the corresponding system with respect to the Circular Restricted Three Body problem hypotheses.

CR3BPSystem(CelestialBody, CelestialBody, double) - Constructor for class org.orekit.bodies.CR3BPSystem

Simple constructor.

CR3BPSystem(CelestialBody, CelestialBody, double, double) - Constructor for class org.orekit.bodies.CR3BPSystem

Simple constructor.

CRD - Class in org.orekit.files.ilrs

This class stores all the information of the Consolidated laser ranging Data Format (CRD) parsed by CRDParser.

CRD() - Constructor for class org.orekit.files.ilrs.CRD

Constructor.

CRD.AnglesMeasurement - Class in org.orekit.files.ilrs

Pointing angles record.

CRD.Calibration - Class in org.orekit.files.ilrs

Calibration Record.

CRD.CalibrationDetail - Class in org.orekit.files.ilrs

Calibration Detail Record.

CRD.CRDDataBlock - Class in org.orekit.files.ilrs

Data block containing a set of data contain in the CRD file.

CRD.FrRangeMeasurement - Class in org.orekit.files.ilrs

Range record -- Full rate, Sampled Engineering/Quicklook.

CRD.Meteo - Class in org.orekit.files.ilrs

Meteorological data.

CRD.MeteorologicalMeasurement - Class in org.orekit.files.ilrs

This data record contains a minimal set of meteorological data.

CRD.NptRangeMeasurement - Class in org.orekit.files.ilrs

Range record -- Normal Point.

CRD.RangeMeasurement - Class in org.orekit.files.ilrs

Range record.

CRD.RangeSupplement - Class in org.orekit.files.ilrs

Range Supplement Record.

CRD.SessionStatistics - Class in org.orekit.files.ilrs

Session (Pass) Statistics Record.

CRDConfiguration - Class in org.orekit.files.ilrs

Container for Consolidated laser ranging Data Format (CDR) configuration records.

CRDConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration

Constructor.

CRDConfiguration.BaseConfiguration - Class in org.orekit.files.ilrs

Base class for configuration record.

CRDConfiguration.CalibrationTargetConfiguration - Class in org.orekit.files.ilrs

Container for calibration target configuration record.

CRDConfiguration.DetectorConfiguration - Class in org.orekit.files.ilrs

Container for detector configuration record.

CRDConfiguration.LaserConfiguration - Class in org.orekit.files.ilrs

Container for laser configuration record.

CRDConfiguration.MeteorologicalConfiguration - Class in org.orekit.files.ilrs

Container for meteorological configuration record.

CRDConfiguration.SoftwareConfiguration - Class in org.orekit.files.ilrs

Container for software configuration record.

CRDConfiguration.SystemConfiguration - Class in org.orekit.files.ilrs

Container for system configuration record.

CRDConfiguration.TimingSystemConfiguration - Class in org.orekit.files.ilrs

Container for timing system configuration record.

CRDConfiguration.TransponderConfiguration - Class in org.orekit.files.ilrs

Container for transponder configuration record.

CRDDataBlock() - Constructor for class org.orekit.files.ilrs.CRD.CRDDataBlock

Constructor.

CRDHeader - Class in org.orekit.files.ilrs

Container for Consolidated laser ranging Data Format (CDR) header.

CRDHeader() - Constructor for class org.orekit.files.ilrs.CRDHeader

Empty constructor.

CRDHeader.DataType - Enum in org.orekit.files.ilrs

Data type for CRD data.

CRDHeader.RangeType - Enum in org.orekit.files.ilrs

Range type for SLR data.

CRDParser - Class in org.orekit.files.ilrs

A parser for the CRD data file format.

CRDParser() - Constructor for class org.orekit.files.ilrs.CRDParser

Default constructor.

CRDParser(TimeScale) - Constructor for class org.orekit.files.ilrs.CRDParser

Constructor.

create(CenterName) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade

Create a body facade from an input center name.

create(CenterName, DataContext) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade

Create a body facade from an input center name.

create(CenterName, CelestialBodies) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade

Create a body facade from an input center name.

create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Build an instance.

create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Build an instance.

create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.WriterBuilder

Build an instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer

Creates a DOP computer for one location.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AlignmentDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AltitudeDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ApsideDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.BooleanDetector

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.DateDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EclipseDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ElevationDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventShifter

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventSlopeFilter

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ExtremumApproachDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FieldOfViewDetector

Build a new instance.

create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FunctionalDetector

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GroundAtNightDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.MagneticFieldDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.NegateDetector

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.NodeDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Build a new instance.

create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.PositionAngleDetector

Build a new instance.

create(AbsoluteDate, GeodeticPoint, AbsoluteDate, GeodeticPoint, OneAxisEllipsoid) - Method in interface org.orekit.utils.WaypointPVBuilder.InterpolationFactory

Create a PVCoordinatesProvider which interpolates between the provided waypoints.

createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createBesselianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales

createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createBesselianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createBesselianEpoch(double) - Method in interface org.orekit.time.TimeScales

Build an instance corresponding to a Besselian Epoch (BE).

createDataFields(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Get the attitude data fields corresponding to the attitude type.

createDefaultDut1FitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for long term prediction.

createDefaultDut1FitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for short term prediction.

createDefaultNutationFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.

createDefaultNutationFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.

createDefaultPoleFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.

createDefaultPoleFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter

Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.

createFilter(ObservationData, ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Creates an Hatch filter given initial data.

createFilter(ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Creates an Hatch filter given initial data.

createFinal(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder

Create the final provider.

createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates

Convert a modified Rodrigues vector and derivatives to angular coordinates.

createFromModifiedRodrigues(T[][]) - Static method in class org.orekit.utils.FieldAngularCoordinates

Convert a modified Rodrigues vector and derivatives to angular coordinates.

createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents

Build a date from week components.

createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a GPS date.

createGPSDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a GPS date.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.Ephemeris

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Create the harvester suitable for propagator.

createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create the harvester suitable for propagator.

createInitial(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder

Create the initial provider.

createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Build an initial orbit using the current selected parameters.

createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Julian Day date.

createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Julian Day date.

createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createJulianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales

createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createJulianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createJulianEpoch(double) - Method in interface org.orekit.time.TimeScales

Build an instance corresponding to a Julian Epoch (JE).

createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator

createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Create a mapper between raw double components and spacecraft state.

createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Modified Julian Day date.

createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance corresponding to a Modified Julian Day date.

createPropagators(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Create the propagators and parameters corresponding to an evaluation point.

createSlot(FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients

Get the slot valid for some date.

createSlot(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients

Get the slot valid for some date.

createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Create an ITRF frame by transforming another ITRF frame.

createTransformedITRF(Frame, String, TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Create an ITRF frame by transforming another ITRF frame.

createVertex(Vector3D, Vector3D, double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType

Create a vertex.

crossProduct(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldPVCoordinates

Compute the cross-product of two instances.

crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates

Compute the cross-product of two instances.

CssiSpaceWeatherData - Class in org.orekit.models.earth.atmosphere.data

This class provides three-hourly and daily solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.

CssiSpaceWeatherData(String) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Simple constructor.

CssiSpaceWeatherData(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Constructor that allows specifying the source of the CSSI space weather file.

CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Constructor that allows specifying the source of the CSSI space weather file.

CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Constructor that allows specifying the source of the CSSI space weather file and customizable thread safe cache configuration.

CssiSpaceWeatherData(DataSource) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Simple constructor which use the default data context.

CssiSpaceWeatherData(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Simple constructor.

CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Simple constructor.

CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Simple constructor with customizable thread safe cache configuration.

CssiSpaceWeatherDataLoader - Class in org.orekit.models.earth.atmosphere.data

This class reads solar activity data from CSSI Space Weather files for the class CssiSpaceWeatherData.

CssiSpaceWeatherDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader

Constructor.

CssiSpaceWeatherDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data

Container class for Solar activity indexes.

CSV_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the csv files (IAU1980 and IAU2000 compatibles).

currentInterval(SpacecraftState) - Method in interface org.orekit.propagation.events.AdaptableInterval

Get the current value of maximal time interval between events handler checks.

currentInterval(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldAdaptableInterval

Get the current value of maximal time interval between events handler checks.

cycleSlipDataSet(String, AbsoluteDate, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Set the data: collect data at the current Date, at the current frequency, for a given satellite, add it within the attributes data and stuff.

CycleSlipDetectorResults - Class in org.orekit.estimation.measurements.gnss

This class is used to contains all the data computed within cycle-slip detector.

CycleSlipDetectors - Interface in org.orekit.estimation.measurements.gnss

Interface for phase measurement cycle-slip detection.

D

D1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Identifier for message type.

D2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Identifier for message type.

Data - Interface in org.orekit.files.ccsds.section

This marker interface represents segment data.

DataContext - Interface in org.orekit.data

Provides auxiliary data for portions of the application.

dataContext(DataContext) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Sets the data context used by the propagator.

DataField - Interface in org.orekit.gnss.metric.parser

Interface for data fields used to parsed encoded messages.

DataFilter - Interface in org.orekit.data

Interface for filtering data (typically uncompressing it) in data providers before passing it to data loaders.

DataFormat - Enum in org.orekit.gnss.metric.ntrip

Enumerate for data format in DataStreamRecord.

DataLoader - Interface in org.orekit.data

Interface for loading data files from data providers.

DataProvider - Interface in org.orekit.data

Interface for providing data files to file loaders.

DataProvidersManager - Class in org.orekit.data

This class manages supported data providers.

DataProvidersManager() - Constructor for class org.orekit.data.DataProvidersManager

Build an instance with default configuration.

DataQuality - Enum in org.orekit.files.ccsds.ndm.tdm

Quality of the data.

DataSource - Class in org.orekit.data

Container associating a name with a stream or reader that can be opened lazily.

DataSource(String, DataSource.StreamOpener) - Constructor for class org.orekit.data.DataSource

Complete constructor.

DataSource(String, DataSource.ReaderOpener) - Constructor for class org.orekit.data.DataSource

Complete constructor.

DataSource(String) - Constructor for class org.orekit.data.DataSource

Build an instance from file name only.

DataSource(File) - Constructor for class org.orekit.data.DataSource

Build an instance from a file on the local file system.

DataSource(URI) - Constructor for class org.orekit.data.DataSource

Build an instance from URI only.

DataSource.Opener - Interface in org.orekit.data

Interface for lazy-opening data streams one time.

DataSource.ReaderOpener - Interface in org.orekit.data

Interface for lazy-opening a characters stream one time.

DataSource.StreamOpener - Interface in org.orekit.data

Interface for lazy-opening a binary stream one time.

DataStreamRecord - Class in org.orekit.gnss.metric.ntrip

Data stream record in source table.

DataStreamRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.DataStreamRecord

Build a data stream record by parsing a source table line.

DATATION_ACCURACY - Static variable in interface org.orekit.propagation.events.EventDetectorsProvider

Accuracy of switching events dates (s).

DataType - Enum in org.orekit.gnss.metric.parser

Enum containing all low level data types that can be parsed to build a message.

DataUsed - Enum in org.orekit.files.sp3

Enumerate for data used.

DATE_AFTER - Static variable in class org.orekit.forces.drag.TimeSpanDragForce

Prefix for dates after in the parameter drivers' name.

DATE_AFTER - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Prefix for dates after in the parameter drivers' name.

DATE_AFTER - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Prefix for dates after in the tropospheric parameter drivers' name.

DATE_BEFORE - Static variable in class org.orekit.forces.drag.TimeSpanDragForce

Prefix for dates before in the parameter drivers' name.

DATE_BEFORE - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Prefix for dates before in the parameter drivers' name.

DATE_BEFORE - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Prefix for dates before in the tropospheric parameter drivers' name.

dateAtCount(double) - Method in class org.orekit.time.SatelliteClockScale

Compute date corresponding to some clock count.

DateBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger

Maneuver triggers based on a start and end date.

DateBasedManeuverTriggers(AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Simple constructor.

DateBasedManeuverTriggers(String, AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Simple constructor.

DateComponents - Class in org.orekit.time

Class representing a date broken up as year, month and day components.

DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from a year and day number.

DateComponents(int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a DateComponents.J2000_EPOCH.

DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a reference epoch.

DateDetector - Class in org.orekit.propagation.events

Finder for date events.

DateDetector(TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector

Build a new instance.

DateDetector(AdaptableInterval, double, int, EventHandler, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector

Protected constructor with full parameters.

DateDriver - Class in org.orekit.utils

Parameter driver allowing to drive a date.

DateDriver(AbsoluteDate, String, boolean) - Constructor for class org.orekit.utils.DateDriver

Simple constructor.

DatesSelector - Interface in org.orekit.time

Interface for selecting dates within an interval.

DateTimeComponents - Class in org.orekit.time

Holder for date and time components.

DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents

Build a new instance from its components.

DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from a seconds offset with respect to another one.

dateToCalendarString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a date to calendar string value with high precision.

dateToCalendarString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a date to calendar string value with high precision.

dateToString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a date to string value with high precision.

dateToString(int, int, int, int, int, double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a date to string value with high precision.

dateToString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a date to string value with high precision.

dateToString(int, int, int, int, int, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a date to string value with high precision.

DAY - Static variable in class org.orekit.utils.units.Unit

Day unit.

DAYS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter

Days to seconds converter.

Dcb - Class in org.orekit.files.sinex

Class to store DCB Solution data parsed in the SinexLoader.

Dcb() - Constructor for class org.orekit.files.sinex.Dcb

Simple constructor.

DcbDescription - Class in org.orekit.files.sinex

Class to store the DCB description parameters.

DcbDescription() - Constructor for class org.orekit.files.sinex.DcbDescription

Simple constructor.

DcbSatellite - Class in org.orekit.files.sinex

Class based on DCB, used to store the data parsed in SinexLoader for Differential Code Biases computed for satellites.

DcbSatellite(String) - Constructor for class org.orekit.files.sinex.DcbSatellite

Constructor for the DCBSatellite class.

DcbStation - Class in org.orekit.files.sinex

Class based on DCB, used to store the data parsed in SinexLoader for Differential Code Biases computed for stations.

DcbStation(String) - Constructor for class org.orekit.files.sinex.DcbStation

Simple constructor.

decode(EncodedMessage) - Method in enum org.orekit.gnss.metric.parser.DataType

Decode a piece of data extracted from an encoded message.

decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Configure the matrix decomposer.

decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder

Configure the matrix decomposer.

decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Configure the matrix decomposer.

decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Configure the matrix decomposer.

decorate(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Decorate an observed measurement.

decorateUnscented(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Decorate an observed measurement for an Unscented Kalman Filter.

deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes periodic terms from current coordinates and epoch.

deepPeriodicEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4

Computes periodic terms from current coordinates and epoch.

DeepSDP4 - Class in org.orekit.propagation.analytical.tle

This class contains the methods that compute deep space perturbation terms.

DeepSDP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4

Constructor for a unique initial TLE.

DeepSDP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4

Constructor for a unique initial TLE.

deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes secular terms from current coordinates and epoch.

deepSecularEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4

Computes secular terms from current coordinates and epoch.

DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for default type of ephemeris (SGP4/SDP4).

DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for default type of ephemeris (SGP4/SDP4).

DEFAULT_ANTEX_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.antenna.AntexLoader

Default supported files name pattern for antex files.

DEFAULT_BLQ_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Default supported files name pattern for Onsala Space Observatory files in BLQ format.

DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache

Default number of independent cached time slots.

DEFAULT_CLOCK_RATE_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils

Bad or absent clock rate values are to be set to 999999.999999.

DEFAULT_CLOCK_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils

Bad or absent clock values are to be set to 999999.999999.

DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default correction factor value.

DEFAULT_CRD_SUPPORTED_NAMES - Static variable in class org.orekit.files.ilrs.CRDParser

Default supported files name pattern for CRD files.

DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.FieldTimeStampedPair

Default date equality threshold of 1 ns.

DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.TimeStampedPair

Default date equality threshold of 1 ns.

DEFAULT_DC_TYPE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Default duty cycle type.

DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for JPL DE files.

DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator

Default extrapolation time threshold: 1ms.

DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractTimeInterpolator

Default extrapolation time threshold: 1ms.

DEFAULT_FILE_NAME - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter

Default file name for error messages.

DEFAULT_ID - Static variable in class org.orekit.files.ilrs.CPF

Default satellite ID, used if header is null when initializing the ephemeris.

DEFAULT_INDENT - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Default number of space for each indentation level.

DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for IMCCE INPOP files.

DEFAULT_INTERPOLATION_DEGREE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Default interpolation degree.

DEFAULT_INTERPOLATION_DEGREE - Static variable in class org.orekit.frames.EOPHistory

Default interpolation degree.

DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Default interpolation method.

DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Default interpolation sample size if it is not specified.

DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator

Default number of interpolation points.

DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractTimeInterpolator

Default number of interpolation points.

DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Default interpolation sample size if it is not specified.

DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Defines the default interpolation sample size if it is not specified on a segment.

DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel

Default lowest acceptable elevation angle [rad].

DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator

Default mass.

DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator

Default mass.

DEFAULT_MASS - Static variable in class org.orekit.propagation.SpacecraftState

Default mass.

DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.DateDetector

Default value for max check.

DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.FieldDateDetector

Default value for max check.

DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector

Default maximum number of iterations in the event time search.

DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default cmaximum number of iterations in the event time search.

DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Default value for maximum number of iterations.

DEFAULT_MAX_RECONNECT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient

Default maximum number of reconnect a attempts without readin any data.

DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector

Default maximum checking interval (s).

DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default maximum checking interval (s).

DEFAULT_MIN_GAP - Static variable in class org.orekit.propagation.events.DateDetector

Default value for minimum gap between added dates.

DEFAULT_MIN_GAP - Static variable in class org.orekit.propagation.events.FieldDateDetector

Default value for minimum gap between added dates.

DEFAULT_NAME - Static variable in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Default name for trigger.

DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Default value for HeaderKey.ORIGINATOR.

DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Default value for HeaderKey.ORIGINATOR.

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides

Default number of points tides field sampling.

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides

Default number of points tides field sampling.

DEFAULT_PORT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient

Default port for ntrip communication.

DEFAULT_POSITION_ANGLE - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Default position angle for covariance expressed in Cartesian elements.

DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local pressure at viewpoint (Pa).

DEFAULT_RECONNECT_DELAY - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient

Default delay before we reconnect after connection close (s).

DEFAULT_RECONNECT_DELAY_FACTOR - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient

Default factor by which reconnection delay is multiplied after each attempt.

DEFAULT_RINEX_2_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser

Default name pattern for rinex 2 observation files.

DEFAULT_RINEX_3_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser

Default name pattern for rinex 3 observation files.

DEFAULT_SCALING_THRESHOLD - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Default scaling threshold to use when sum becomes large.

DEFAULT_SCLK_OFFSET_AT_EPOCH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Default value for SCLK_OFFSET_AT_EPOCH.

DEFAULT_SCLK_SEC_PER_SI_SEC - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Default value for SCLK_SEC_PER_SI_SEC.

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides

Default step for tides field sampling (seconds).

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides

Default step for tides field sampling (seconds).

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Default regular expression for supported names that works with all officially published files.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Default regular expression for the supported name that work with all officially published files.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.AGILeapSecondFilesLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader

Default supported files name pattern.

DEFAULT_SUPPORTED_NAMES_DTC - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Default regular expression for supported names that works with test and published files for the DTCFILE file.

DEFAULT_SUPPORTED_NAMES_SOLFSMY - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Default regular expression for supported names that works with test and published files for the SOLFSMY file.

DEFAULT_TCA_DIFFERENCE_TOLERANCE - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Default time of closest approach difference tolerance.

DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local temperature at viewpoint (K).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector

Default convergence threshold (s).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.DateDetector

Default value for convergence threshold.

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector

Default convergence threshold (s).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldDateDetector

Default value for convergence threshold.

DEFAULT_TIMEOUT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient

Default timeout for connections and reads (ms).

DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA

Default yaw bias (rad).

DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF

Default yaw bias (rad).

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Galileo

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Glonass

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIR

Default yaw rates for all spacecrafts in radians per seconds.

DEFAULT_ZERO_THRESHOLD - Static variable in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Threshold below which values are considered equal to zero.

DefaultDataContext - Annotation Type in org.orekit.annotation

Indicates that the annotated method, field, or constructor uses the default data context.

DefaultDataContextPlugin - Class in org.orekit.compiler.plugin

Processes DefaultDataContext to issue warnings at compile time.

DefaultDataContextPlugin() - Constructor for class org.orekit.compiler.plugin.DefaultDataContextPlugin

Empty constructor.

DefaultEncounterLOF - Class in org.orekit.frames.encounter

Default encounter local orbital frame.

DefaultEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF

Constructor.

DefaultEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF

Field constructor.

DEG_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Degree per second unit.

DEG_PER_S_1_2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Degree per second^1/2 unit.

DEG_PER_S_3_2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Degree per second^3/2 unit.

DEGREE - Static variable in class org.orekit.utils.units.Unit

Degree unit.

DelaunayArguments - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments

Simple constructor.

DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel

Default file name for δR correction term table.

dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.ParametricAcceleration

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Check if force models depends on position only.

dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.DeSitterRelativity

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.LenseThirringRelativity

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.inertia.InertialForces

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel

Check if force models depends on position only.

dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Check if force models depends on position only.

derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate time derivative of a set of Poisson series.

derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate time derivative of a set of Poisson series.

derivative(double) - Method in class org.orekit.data.PolynomialNutation

Evaluate the time derivative of the polynomial.

derivative(T) - Method in class org.orekit.data.PolynomialNutation

Evaluate the time derivative of the polynomial.

deselectDynamicParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Deselects orbital and propagation drivers.

DeSitterRelativity - Class in org.orekit.forces.gravity

De Sitter post-Newtonian correction force due to general relativity.

DeSitterRelativity() - Constructor for class org.orekit.forces.gravity.DeSitterRelativity

Constructor.

DeSitterRelativity(CelestialBody, CelestialBody) - Constructor for class org.orekit.forces.gravity.DeSitterRelativity

Simple constructor.

detect(List<ObservationDataSet>) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Detects if a cycle-slip occurs for a given list of observation data set.

detect(List<ObservationDataSet>) - Method in interface org.orekit.estimation.measurements.gnss.CycleSlipDetectors

Detects if a cycle-slip occurs for a given list of observation data set.

DetectorConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Empty constructor.

differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation

Differentiate a scalar function using finite differences.

differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngleType, double, int) - Static method in class org.orekit.utils.Differentiation

Differentiate a vector function using finite differences.

Differentiation - Class in org.orekit.utils

Utility class for differentiating various kinds of functions.

Dipole - Class in org.orekit.estimation.measurements.gnss

Dipole configuration for satellite-to-ground and inter-satellites wind-up effects.

directionAt(double) - Method in class org.orekit.geometry.fov.CircularFieldOfView

Get boundary direction at angle.

directionAt(double) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

Get boundary direction at angle.

directionAt(double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get boundary direction at angle.

DirectoryCrawler - Class in org.orekit.data

Provider for data files stored in a directories tree on filesystem.

DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler

Build a data files crawler.

discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Find the best solutions to the Integer Least Square problem.

discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping

Compute the solution by the bootstrap method from equation (13) in P.J.G.

discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod

Find the best solutions to the Integer Least Square problem.

discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Find the best solutions to the Integer Least Square problem.

DiscreteTroposphericModel - Interface in org.orekit.models.earth.troposphere

Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading

Compute displacement of a ground reference point.

displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement

Compute displacement of a ground reference point.

displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TectonicsDisplacement

Compute displacement of a ground reference point.

displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement

Compute displacement of a ground reference point.

DivertedSingularityAiming - Class in org.orekit.models.earth.tessellation

Class used to orient tiles such that there are no singularities within the zone of interest.

DivertedSingularityAiming(SphericalPolygonsSet) - Constructor for class org.orekit.models.earth.tessellation.DivertedSingularityAiming

Simple constructor.

divide(String, Unit) - Method in class org.orekit.utils.units.Unit

Create quotient of units.

doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState

Notify the user's listener of the event.

doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState

Notify the user's listener of the event.

doModify(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier

Modify measurement.

doModify(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier

Modify measurement.

doModifyWithoutDerivatives(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier

Modify measurement.

DOP - Class in org.orekit.gnss

This class is a container for the result of a single DOP computation.

DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP

Constructor.

DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer

Minimum elevation : 0°.

DOPComputer - Class in org.orekit.gnss

This class aims at computing the dilution of precision.

DormandPrince54FieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for DormandPrince54FieldIntegrator.

DormandPrince54FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder

Build a new instance.

DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince54Integrator.

DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a new instance.

DormandPrince853FieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for DormandPrince853FieldIntegrator.

DormandPrince853FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder

Build a new instance.

DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince853Integrator.

DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a new instance.

DoubleArrayDictionary - Class in org.orekit.utils

String → double[] mapping, for small number of keys.

DoubleArrayDictionary() - Constructor for class org.orekit.utils.DoubleArrayDictionary

Constructor with default initial capacity.

DoubleArrayDictionary(int) - Constructor for class org.orekit.utils.DoubleArrayDictionary

Constructor with specified capacity.

DoubleArrayDictionary(DoubleArrayDictionary) - Constructor for class org.orekit.utils.DoubleArrayDictionary

Constructor from another dictionary.

DoubleArrayDictionary(Map<String, double[]>) - Constructor for class org.orekit.utils.DoubleArrayDictionary

Constructor from a map.

DoubleArrayDictionary.Entry - Class in org.orekit.utils

Entry in a dictionary.

DoubleDihedraFieldOfView - Class in org.orekit.geometry.fov

Class representing a spacecraft sensor Field Of View with dihedral shape (i.e.

DoubleDihedraFieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.DoubleDihedraFieldOfView

Build a Field Of View with dihedral shape (i.e.

doubleToString(double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a double to string value with high precision.

doubleToString(double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a double to string value with high precision.

doubleValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField

Get the value of the field as a double.

dP - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder

Position error (m).

DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for drag coefficient.

dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag.

dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag.

dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag.

dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag.

dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag

Compute the acceleration due to drag.

dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag

Compute the acceleration due to drag.

DragForce - Class in org.orekit.forces.drag

Atmospheric drag force model.

DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce

Simple constructor.

DragSensitive - Interface in org.orekit.forces.drag

Interface for spacecraft that are sensitive to atmospheric drag forces.

DRIFT_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation

Suffix for ground clock drift parameters name.

DSST_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Constant for DSST mean elements theory.

DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces

Atmospheric drag contribution to the DSSTPropagator.

DSSTAtmosphericDrag(DragForce, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor with custom force.

DSSTAtmosphericDrag(Atmosphere, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor assuming spherical spacecraft.

DSSTAtmosphericDrag(Atmosphere, DragSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor with custom spacecraft.

DSSTBatchLSModel - Class in org.orekit.estimation.leastsquares

Bridge between measurements and least squares problems.

DSSTBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver, PropagationType) - Constructor for class org.orekit.estimation.leastsquares.DSSTBatchLSModel

Simple constructor.

DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces

This interface represents a force modifying spacecraft motion for a DSSTPropagator.

DSSTHarvester - Class in org.orekit.propagation.semianalytical.dsst

Harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.

DSSTJ2SquaredClosedForm - Class in org.orekit.propagation.semianalytical.dsst.forces

Second order J2-squared force model.

DSSTJ2SquaredClosedForm(J2SquaredModel, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Constructor.

DSSTJ2SquaredClosedFormContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.

DSSTJ2SquaredClosedFormContext(AuxiliaryElements, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Simple constructor.

DSSTNewtonianAttraction - Class in org.orekit.propagation.semianalytical.dsst.forces

Force model for Newtonian central body attraction for the DSST propagator.

DSSTNewtonianAttraction(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Simple constructor.

DSSTNewtonianAttractionContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTNewtonianAttraction.

DSSTNewtonianAttractionContext(AuxiliaryElements, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext

Simple constructor.

DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst

This class propagates orbits using the DSST theory.

DSSTPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for DSST propagator.

DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Build a new instance.

DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Build a new instance.

DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces

Solar radiation pressure contribution to the DSSTPropagator.

DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values and spherical spacecraft.

DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values, but custom spacecraft.

DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Constructor with customizable reference values but spherical spacecraft.

DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Complete constructor.

DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces

Tesseral contribution to the central body gravitational perturbation.

DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Simple constructor with default reference values.

DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Simple constructor.

DSSTTesseralContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTTesseral.

DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces

Third body attraction perturbation to the DSSTPropagator.

DSSTThirdBody(CelestialBody, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Complete constructor.

DSSTThirdBodyDynamicContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTThirdBody.

DSSTThirdBodyDynamicContext(AuxiliaryElements, CelestialBody, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Constructor.

DSSTThirdBodyStaticContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTThirdBody.

DSSTThirdBodyStaticContext(AuxiliaryElements, double, double, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext

Constructor.

DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces

Zonal contribution to the central body gravitational perturbation.

DSSTZonal(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Constructor with default reference values.

DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Simple constructor.

DSSTZonalContext - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTZonal.

DtcDataLoader - Class in org.orekit.models.earth.atmosphere.data

This class reads solar activity data from DTCFILE files for the class JB2008SpaceEnvironmentData.

DtcDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Constructor.

DtcDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data

Container class for Solar activity indexes.

DTM2000 - Class in org.orekit.models.earth.atmosphere

This atmosphere model is the realization of the DTM-2000 model.

DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000

Simple constructor for independent computation.

DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000

Simple constructor for independent computation.

DTM2000InputParameters - Interface in org.orekit.models.earth.atmosphere

Container for solar activity data, compatible with DTM2000 Atmosphere model.

DualFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering

Hatch Filter using Carrier-Phase measurements taken at two different frequencies, to form a Divergence-Free phase combination.

DualFrequencyHatchFilter(ObservationData, ObservationData, ObservationData, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter

Constructor for the Dual Frequency Hatch Filter.

DualFrequencySmoother - Class in org.orekit.estimation.measurements.filtering

Handler to perform pseudo-range smoothing using Divergence-Free phase combinations.

DualFrequencySmoother(double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Simple constructor.

DUMMY - Static variable in class org.orekit.files.sp3.SP3Coordinate

Dummy coordinate with all fields set to 0.0.

Duration - Class in org.orekit.forces.maneuvers.jacobians

Generator for one column of a Jacobian matrix for special case of maneuver duration.

Duration(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.Duration

Simple constructor.

DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Default suffix for duration driver.

DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Default suffix for duration driver.

durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compute the physically elapsed duration between two instants.

durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the physically elapsed duration between two instants.

durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the physically elapsed duration between two instants.

durationFrom(FieldTimeStamped<T>) - Method in interface org.orekit.time.FieldTimeStamped

Compute the physically elapsed duration between two instants.

durationFrom(TimeStamped) - Method in interface org.orekit.time.TimeStamped

Compute the physically elapsed duration between two instants.

DutyCycleType - Enum in org.orekit.files.ccsds.definitions

Type of duty cycle used in CCSDS Orbit Comprehensive Messages.

DynamicOutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.

DynamicOutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Simple constructor.

E

e - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

final eccentricity.

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final eccentricity.

e0sq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

original eccentricity squared.

e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity squared.

E_X - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentricity vector first component.

E_Y - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentricity vector second component.

EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth.

EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Earth Angular Velocity, in rad/s, from TIRF model.

EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth-Moon barycenter.

EARTH_RADII - Static variable in class org.orekit.utils.units.Unit

Earth Radii used as Bstar unit in CCSDS OMM.

EARTH_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Earth radius in km.

EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth

Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.

EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Creates a new default instance.

EarthOrientationParameterMessage - Class in org.orekit.files.rinex.navigation

Container for data contained in a Earth Orientation Parameter navigation message.

EarthOrientationParameterMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Simple constructor.

EarthShape - Interface in org.orekit.models.earth

All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.

EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth

Implementation of refraction model for Earth standard atmosphere.

EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates a new default instance.

EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates an instance given a specific pressure and temperature.

ECC - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentricity.

ECC_ANOM - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentric anomaly.

ECC_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentric argument of latitude.

ECC_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for eccentric argument of longitude.

eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the mean latitude argument from the eccentric latitude argument.

eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the mean longitude argument from the eccentric longitude argument.

eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the mean latitude argument from the eccentric latitude argument.

eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the mean longitude argument from the eccentric longitude argument.

eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the true latitude argument from the eccentric latitude argument.

eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the true longitude argument from the eccentric longitude argument.

eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the true latitude argument from the eccentric latitude argument.

eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the true longitude argument from the eccentric longitude argument.

ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.

ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.

ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.

eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Sets the Earth Centered Inertial frame used for propagation.

eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Sets the Earth Centered Inertial frame used for propagation.

eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Sets the Earth Centered Inertial frame used for propagation.

eci(Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Sets the Earth Centered Inertial frame used for propagation.

EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical

This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.

EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Private helper constructor.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential.

EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential provider.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Private helper constructor.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Eckstein-Hechler propagator.

EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EclipseDetector - Class in org.orekit.propagation.events

Finder for satellite eclipse related events.

EclipseDetector(ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(OccultationEngine) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(AdaptableInterval, double, int, EventHandler, OccultationEngine, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector

Protected constructor with full parameters.

EclipticProvider - Class in org.orekit.frames

An inertial frame aligned with the ecliptic.

EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider

Create a transform provider from MOD to an ecliptically aligned frame.

EclipticProvider(IERSConventions, TimeScales) - Constructor for class org.orekit.frames.EclipticProvider

Create a transform provider from MOD to an ecliptically aligned frame.

ECOM2 - Class in org.orekit.forces.radiation

The Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).

ECOM2(int, int, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.ECOM2

Constructor.

ECOM_COEFFICIENT - Static variable in class org.orekit.forces.radiation.ECOM2

Parameter name for ECOM model coefficients enabling Jacobian processing.

eeta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

original eccentricity * eta.

eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity * eta.

EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.

EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.

EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.

EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.

EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.

EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EGM96 model: 6378136.3 m.

EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².

EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for EGM files.

EGMFormatReader - Class in org.orekit.forces.gravity.potential

This reader is adapted to the EGM Format.

EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader

Simple constructor.

EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader

Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.

EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.

EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.

EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.

EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.

EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.

EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EIGEN5C model: 6378136.46 m.

EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².

ElevationDetector - Class in org.orekit.propagation.events

Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.

ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.

ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.

ElevationDetector(AdaptableInterval, double, int, EventHandler, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Protected constructor with full parameters.

ElevationExtremumDetector - Class in org.orekit.propagation.events

Detector for elevation extremum with respect to a ground point.

ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector

Build a new detector.

ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector

Build a detector.

ElevationExtremumDetector(AdaptableInterval, double, int, EventHandler, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector

Protected constructor with full parameters.

ElevationFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering

Elevation pre-processing filter.

ElevationFilter(GroundStation, double) - Constructor for class org.orekit.estimation.measurements.filtering.ElevationFilter

Constructor.

ElevationMask - Class in org.orekit.utils

Class for modeling the ground elevation values around a given point.

ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask

Creates an instance of an Elevation mask based on the passed in parameter.

Ellipse - Class in org.orekit.bodies

Model of a 2D ellipse in 3D space.

Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse

Simple constructor.

Ellipsoid - Class in org.orekit.bodies

Modeling of a general three-axes ellipsoid.

Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid

Simple constructor.

EllipsoidTessellator - Class in org.orekit.models.earth.tessellation

Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.

EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator

Simple constructor.

EllipticalFieldOfView - Class in org.orekit.geometry.fov

Class representing a spacecraft sensor Field Of View with elliptical shape.

EllipticalFieldOfView(Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.geometry.fov.EllipticalFieldOfView

Build a new instance.

ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic mean anomaly from the elliptic eccentric anomaly.

ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic mean anomaly from the elliptic eccentric anomaly.

ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic true anomaly from the elliptic eccentric anomaly.

ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic true anomaly from the elliptic eccentric anomaly.

ellipticMeanToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic eccentric anomaly from the elliptic mean anomaly.

ellipticMeanToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic eccentric anomaly from the elliptic mean anomaly.

ellipticMeanToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic true anomaly from the elliptic mean anomaly.

ellipticMeanToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic true anomaly from the elliptic mean anomaly.

ellipticTrueToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic eccentric anomaly from the elliptic true anomaly.

ellipticTrueToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic eccentric anomaly from the elliptic true anomaly.

ellipticTrueToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the elliptic mean anomaly from the elliptic true anomaly.

ellipticTrueToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the elliptic mean anomaly from the elliptic true anomaly.

emitterToInert(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp

Compute rotation from emitter to inertial frame.

emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUp

Compute rotation from emitter to inertial frame.

emitterToInert(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp

Compute rotation from emitter to inertial frame.

emptyCache(Field<CFE>) - Static method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get an empty immutable cache, cast to the correct type.

emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache

Get an empty immutable cache, cast to the correct type.

EnablingPredicate - Interface in org.orekit.propagation.events

This interface represents an event enabling predicate function.

EncodedMessage - Interface in org.orekit.gnss.metric.parser

Interface for getting bits forming encoded messages.

EncounterLOF - Interface in org.orekit.frames.encounter

Interface for encounter local orbital frame.

EncounterLOFType - Enum in org.orekit.frames.encounter

Enum for encounter local orbital frame.

endMessage(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

End CCSDS message.

endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

End CCSDS message.

endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

End CCSDS message.

endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

End parsing.

ensureCompatible(String, List<Unit>, boolean, List<Unit>) - Static method in class org.orekit.utils.units.Unit

Ensure some units are compatible with reference units.

ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState

Check if two instances have the same set of additional states available.

ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState

Check if two instances have the same set of additional states available.

enterSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter

Enter the section.

enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Enter into a new section.

enterSection(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Enter into a new section.

enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Enter into a new section.

enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Enter into a new section.

EOPBasedTransformProvider - Interface in org.orekit.frames

Interface for Transform providers that use Earth Orientation Parameters.

EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU1980 compatibles).

EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU2000 compatibles).

EOPEntry - Class in org.orekit.frames

This class holds an Earth Orientation Parameters entry.

EOPEntry(int, double, double, double, double, double, double, double, double, double, double, ITRFVersion, AbsoluteDate) - Constructor for class org.orekit.frames.EOPEntry

Simple constructor.

EOPFittedModel - Class in org.orekit.frames

Container for fitted model for Earth Orientation Parameters.

EOPFittedModel(SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic) - Constructor for class org.orekit.frames.EOPFittedModel

Simple constructor.

EOPFitter - Class in org.orekit.frames

Earth Orientation Parameters fitter for EOP prediction.

EOPFitter(SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter) - Constructor for class org.orekit.frames.EOPFitter

Simple constructor.

EOPHistory - Class in org.orekit.frames

This class loads any kind of Earth Orientation Parameter data throughout a large time range.

EOPHistory(IERSConventions, int, Collection<? extends EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory

Simple constructor.

EOPHistory(IERSConventions, int, Collection<? extends EOPEntry>, boolean, TimeScales) - Constructor for class org.orekit.frames.EOPHistory

Simple constructor.

EopHistoryLoader - Interface in org.orekit.frames

Interface for loading Earth Orientation Parameters history.

EopHistoryLoader.Parser - Interface in org.orekit.frames

Interface for parsing EOP data files.

Ephemeris - Class in org.orekit.propagation.analytical

This class is designed to accept and handle tabulated orbital entries.

Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Legacy constructor with tabulated states and default Hermite interpolation.

Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states.

Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states.

Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states and associated covariances.

Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states and associated covariances.

EPHEMERIS_TYPE_PPT3 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Constant for EPHEMERIS_TYPE PPT3.

EPHEMERIS_TYPE_SGP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Constant for EPHEMERIS_TYPE SGP.

EPHEMERIS_TYPE_SGP4 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Constant for EPHEMERIS_TYPE SGP4.

EPHEMERIS_TYPE_SGP4_XP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Constant for EPHEMERIS_TYPE SGP4-XP.

EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Constant for EPHEMERIS_TYPE Special Perturbations.

EphemerisFile<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general

An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.

EphemerisFile.EphemerisSegment<C extends TimeStampedPVCoordinates> - Interface in org.orekit.files.general

A segment of an ephemeris for a satellite.

EphemerisFile.SatelliteEphemeris<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general

Contains the information about a single satellite from an EphemerisFile.

EphemerisFileParser<T extends EphemerisFile<?,?>> - Interface in org.orekit.files.general

Parse an ephemeris file.

EphemerisFileWriter - Interface in org.orekit.files.general

An interface for writing out ephemeris files to disk.

EphemerisGenerator - Interface in org.orekit.propagation

Generator for ephemerides.

EphemerisOcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm

An EphemerisFileWriter generating OCM files.

EphemerisOcmWriter(OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter

Constructor used to create a new OCM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

EphemerisOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem

An EphemerisFileWriter generating OEM files.

EphemerisOemWriter(OemWriter, OdmHeader, OemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter

Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

EphemerisPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Ephemeris propagator.

EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Constructor using the default attitude provider.

EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Constructor.

EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Constructor with covariances and default attitude provider.

EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder

Constructor.

EpochDerivativesEquations - Class in org.orekit.propagation.numerical

Computes derivatives of the acceleration, including ThirdBodyAttraction.

EpochDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.EpochDerivativesEquations

Simple constructor.

EPSILON_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Default value for epsilon.

equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint

equals(Object) - Method in class org.orekit.bodies.GeodeticPoint

equals(Object) - Method in class org.orekit.estimation.measurements.ObservableSatellite

equals(Object) - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

equals(Object) - Method in class org.orekit.gnss.SatInSystem

equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters

Check if the instance represents the same parameters as given line parameters.

equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Check if the instance represents the same parameters as given line parameters.

equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

Check if the instance represents the same parameters as given line parameters.

equals(Object) - Method in class org.orekit.models.earth.displacement.Tide

equals(Object) - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Check if this tle equals the provided tle.

equals(Object) - Method in class org.orekit.propagation.analytical.tle.TLE

Check if this tle equals the provided tle.

equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

equals(Object) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents the same time as another instance.

equals(Object) - Method in class org.orekit.time.DateComponents

equals(Object) - Method in class org.orekit.time.DateTimeComponents

equals(Object) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents the same time as another instance.

equals(Object) - Method in class org.orekit.time.TimeComponents

equals(Object) - Method in class org.orekit.utils.units.Unit

Check if the instance represents the same unit as another instance.

EquinoctialOrbit - Class in org.orekit.orbits

This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.

EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Creates a new instance.

EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Creates a new instance.

EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from Cartesian parameters.

EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from Cartesian parameters.

EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from any kind of orbital parameters.

ErrorState - Class in org.orekit.files.ccsds.utils.parsing

Special ProcessingState that always generate an error message.

ErrorState() - Constructor for class org.orekit.files.ccsds.utils.parsing.ErrorState

Empty constructor.

estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodGauss

Estimate and orbit based on Gauss Intial Orbit Determination method.

estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodGauss

Estimate and orbit based on Gauss Intial Orbit Determination method.

estimate(Frame, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodGauss

Estimate and orbit based on Gauss Intial Orbit Determination method.

estimate(Frame, Position, Position, Position) - Method in class org.orekit.estimation.iod.IodGibbs

Give an initial orbit estimation, assuming Keplerian motion.

estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs

Give an initial orbit estimation, assuming Keplerian motion.

estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs

Give an initial orbit estimation, assuming Keplerian motion.

estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three angular observations.

estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three angular observations.

estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three angular observations.

estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three angular observations.

estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three line of sight.

estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding

Estimate orbit from three line of sight.

estimate(Frame, boolean, int, Position, Position) - Method in class org.orekit.estimation.iod.IodLambert

Estimate an initial orbit from two position measurements.

estimate(Frame, boolean, int, PV, PV) - Method in class org.orekit.estimation.iod.IodLambert

Estimate an initial orbit from two PV measurements.

estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert

Estimate a Keplerian orbit given two position vectors and a duration.

estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodLaplace

Estimate the orbit from three angular observations at the same location.

estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodLaplace

Estimate the orbit from three angular observations at the same location.

estimate(Frame, PVCoordinates, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodLaplace

Estimate orbit from three line of sight angles at the same location.

estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Estimate the orbital, propagation and measurements parameters.

estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value of the measurement, with derivatives.

estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Estimate the theoretical value of the measurement, with derivatives.

EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements

Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.

EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Build an estimated Earth frame.

EstimatedIonosphericModel - Class in org.orekit.models.earth.ionosphere

An estimated ionospheric model.

EstimatedIonosphericModel(IonosphericMappingFunction, double) - Constructor for class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Build a new instance.

EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements

Class holding an estimated theoretical value associated to an observed measurement.

EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement

Simple constructor.

EstimatedMeasurementBase<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements

Class holding an estimated theoretical value associated to an observed measurement.

EstimatedMeasurementBase(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurementBase

Simple constructor.

EstimatedMeasurementBase.Status - Enum in org.orekit.estimation.measurements

Enumerate for the status of the measurement.

estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Configure the estimated measurement parameters.

estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder

Configure the estimated measurement parameters.

estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Configure the estimated measurement parameters.

estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Configure the estimated measurement parameters.

EstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere

An estimated tropospheric model.

EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Build a new instance using the given environmental conditions.

EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Build a new instance using a standard atmosphere model.

estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates

Estimate rotation rate between two orientations.

estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates

Estimate rotation rate between two orientations.

estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates

Estimate rotation rate between two orientations.

estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates

Estimate velocity between two positions.

estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates

Estimate velocity between two positions.

estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value of the measurement, without derivatives.

estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Estimate the theoretical value of the measurement, without derivatives.

EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements

Interface for estimated measurements modifiers used for orbit determination.

EstimationsProvider - Interface in org.orekit.estimation.measurements

Interface for retrieving estimated measurements during orbit determination.

estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Process a single measurement.

estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator

Process a single measurement.

estimationTypeChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter estimation type (continuous or step) has been changed.

eta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

eta from SPTRCK #3.

eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta from SPTRCK #3.

etasq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

eta squared.

etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta squared.

Euler - Class in org.orekit.files.ccsds.ndm.adm.apm

Container for Euler rotations entries.

Euler() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Euler

Simple constructor.

EulerFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for EulerFieldIntegrator.

EulerFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder

Constructor.

EulerFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder

Constructor using a "fielded" step.

EulerIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for EulerIntegrator.

EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a new instance.

EulerKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for APM Euler angles entries.

evaluate(Vector3D) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType

Evaluate the cost of the input seen as a 3D control vector.

evaluate(FieldVector3D<T>) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType

Evaluate the cost of the input seen as a 3D control vector.

evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Evaluate the impact of the proposed step on the event detector.

evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Evaluate the impact of the proposed step on the event detector.

evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluateTC(AbsoluteDate, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluateTC(FieldAbsoluteDate<T>) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluateTC(FieldAbsoluteDate<T>, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in interface org.orekit.estimation.leastsquares.BatchLSObserver

Notification callback for the end of each evaluation.

evaluationPerformed(KalmanEstimation) - Method in interface org.orekit.estimation.sequential.KalmanObserver

Notification callback after each one of a Kalman filter estimation.

EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation

Scheduler based on EventDetector for generating measurements sequences.

EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler

Simple constructor.

EventDetector - Interface in org.orekit.propagation.events

This interface represents space-dynamics aware events detectors.

EventDetectorsProvider - Interface in org.orekit.propagation.events

Interface for building event detectors for force models and maneuver parameters.

EventEnablingPredicateFilter - Class in org.orekit.propagation.events

Wrapper used to detect events only when enabled by an external predicated function.

EventEnablingPredicateFilter(EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter

Wrap an event detector.

EventEnablingPredicateFilter(AdaptableInterval, double, int, EventHandler, EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter

Protected constructor with full parameters.

EventHandler - Interface in org.orekit.propagation.events.handlers

An interface defining how to handle events occurring during propagation.

eventIsEnabled(SpacecraftState, EventDetector, double) - Method in interface org.orekit.propagation.events.EnablingPredicate

Compute an event enabling function of state.

eventIsEnabled(FieldSpacecraftState<T>, FieldEventDetector<T>, T) - Method in interface org.orekit.propagation.events.FieldEnablingPredicate

Compute an event enabling function of state.

EventMultipleHandler - Class in org.orekit.propagation.events.handlers

Facade handlers that allows to use several handlers for one detector.

EventMultipleHandler() - Constructor for class org.orekit.propagation.events.handlers.EventMultipleHandler

Constructor with list initialisation.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Handle an event.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Handle an event.

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

Handle an event.

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing

Handle a detection event and choose what to do next.

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing

Handle a detection event and choose what to do next.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing

Handle a detection event and choose what to do next.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing

Handle a detection event and choose what to do next.

EventShifter - Class in org.orekit.propagation.events

Wrapper shifting events occurrences times.

EventShifter(EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter

Build a new instance.

EventShifter(AdaptableInterval, double, int, EventHandler, EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter

Protected constructor with full parameters.

EventsLogger - Class in org.orekit.propagation.events

This class logs events detectors events during propagation.

EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger

Simple constructor.

EventsLogger.LoggedEvent - Class in org.orekit.propagation.events

Class for logged events entries.

EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper used to detect only increasing or decreasing events.

EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter

Wrap an event detector.

EventSlopeFilter(AdaptableInterval, double, int, EventHandler, T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter

Protected constructor with full parameters.

EventState<T extends EventDetector> - Class in org.orekit.propagation.events

This class handles the state for one event detector during integration steps.

EventState(T) - Constructor for class org.orekit.propagation.events.EventState

Simple constructor.

EventState.EventOccurrence - Class in org.orekit.propagation.events

Class to hold the data related to an event occurrence that is needed to decide how to modify integration.

ExceptionalDataContext - Class in org.orekit.data

A data context that always throws a runtime exception when it's methods are used.

ExceptionalDataContext() - Constructor for class org.orekit.data.ExceptionalDataContext

Empty constructor.

exitSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter

Exit the section.

exitSection() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Exit last section.

exitSection() - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Exit last section.

exitSection() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Exit last section.

exitSection() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Exit last section.

expressCovarianceInDesiredOutput(Orbit, StateCovariance) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Express covariance in output configuration defined at this instance construction.

extend(Gradient, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Add zero derivatives.

extend(FieldVector3D<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Add zero derivatives.

extend(FieldRotation<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Add zero derivatives.

ExtendedPVCoordinatesProvider - Interface in org.orekit.utils

Interface for PV coordinates providers that also support fields.

ExtendedPVCoordinatesProviderAdapter - Class in org.orekit.utils

Adapter from ExtendedPVCoordinatesProvider to TransformProvider.

ExtendedPVCoordinatesProviderAdapter(Frame, ExtendedPVCoordinatesProvider, String) - Constructor for class org.orekit.utils.ExtendedPVCoordinatesProviderAdapter

Simple constructor.

extractAccelerationModelRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Extract a range of the AccelerationModel map.

extractBits(int) - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage

Extract the next n bits from the encoded message.

extractBits(int) - Method in interface org.orekit.gnss.metric.parser.EncodedMessage

Extract the next n bits from the encoded message.

extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Extract a range of the DragSensitive map.

extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Extract the proper parameter drivers' values from the array in input of the acceleration method.

extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Extract the proper parameter drivers' values from the array in input of the acceleration method.

extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Extract the proper parameter drivers' values from the array in input of the acceleration method.

extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Extract the proper parameter drivers' values from the array in input of the acceleration method.

extractParameters(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Extract the proper parameter drivers' values from the array in input of the pathDelay method.

extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Extract the proper parameter drivers' values from the array in input of the pathDelay method.

extractParameters(double[], AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms method.

extractParameters(T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms method.

extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Extract a range of the map.

ExtremumApproachDetector - Class in org.orekit.propagation.events

Finder for extremum approach events.

ExtremumApproachDetector(PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector

Constructor with default values.

ExtremumApproachDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector

Constructor.

F

F0 - Static variable in enum org.orekit.gnss.Frequency

Common frequency F0 in MHz (10.23 MHz).

FactoryManagedFrame - Class in org.orekit.frames

Base class for the predefined frames that are managed by Frames.

FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame

Simple constructor.

FDOA - Class in org.orekit.estimation.measurements

Class modeling a Frequency Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.

FDOA(GroundStation, GroundStation, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.FDOA

Simple constructor.

FDOABuilder - Class in org.orekit.estimation.measurements.generation

Builder for FDOA measurements.

FDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.FDOABuilder

Simple constructor.

feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.AbstractListCrawler

Feed a data file loader by browsing the data collection.

feed(DataLoader) - Method in class org.orekit.data.AbstractSelfFeedingLoader

Feed the given loader with AbstractSelfFeedingLoader.getDataProvidersManager() and AbstractSelfFeedingLoader.getSupportedNames().

feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ClasspathCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader, DataProvidersManager) - Method in interface org.orekit.data.DataProvider

Feed a data file loader by browsing the data collection.

feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager

Feed a data file loader by browsing all data providers.

feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.DirectoryCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ZipJarCrawler

Feed a data file loader by browsing the data collection.

FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES C hat and epsilon tides files.

FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Cnm, Snm tides files.

FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Hf tides files.

FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004.dat format.

FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Simple constructor.

FESCnmSnmReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.

FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader

Simple constructor.

fetchByte() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor

Fetch the next byte from the message.

fetchByte() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage

Fetch the next byte from the message.

fetchByte() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage

Fetch the next byte from the message.

fetchByte() - Method in class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage

Fetch the next byte from the message.

fetchByte() - Method in class org.orekit.gnss.metric.parser.InputStreamEncodedMessage

Fetch the next byte from the message.

fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Fetch a measurement that was evaluated during propagation.

FieldAbsoluteDate<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.time

This class represents a specific instant in time.

FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an AbsoluteDate.

FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate

Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).

FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location (parsed from a string) in a time scale.

FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from a location in a time scale.

FieldAbsoluteDate(Field<T>, Instant, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an instant in a time scale.

FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an elapsed duration since to another instant.

FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate

Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.

FieldAbsolutePVCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Field implementation of AbsolutePVCoordinates.

FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Build from position, velocity, acceleration.

FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Build from position and velocity.

FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Build from frame, date and FieldPVA coordinates.

FieldAbsolutePVCoordinates(Frame, TimeStampedFieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Build from frame and TimeStampedFieldPVCoordinates.

FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Multiplicative constructor

FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, FieldAbsolutePVCoordinates<T>, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Subtractive constructor

FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Linear constructor

FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Linear constructor

FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Linear constructor

FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates

Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.

FieldAbsolutePVCoordinatesHermiteInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.utils

Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.

FieldAbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).

FieldAbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Constructor.

FieldAbstractAnalyticalPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical

Common handling of FieldPropagator methods for analytical propagators.

FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Build a new instance.

FieldAbstractDetector<D extends FieldAbstractDetector<D,T>,T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Common parts shared by several orbital events finders.

FieldAbstractDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector

Build a new instance.

FieldAbstractGaussianContributionContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common "field" parameters used in AbstractGaussianContribution.

FieldAbstractIntegratedPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.integration

Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.

FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Build a new instance.

FieldAbstractIntegratedPropagator.MainStateEquations<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration

Differential equations for the main state (orbit, attitude and mass).

FieldAbstractPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation

Common handling of Propagator methods for analytical propagators.

FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator

Build a new instance.

FieldAdaptableInterval<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.events

This interface represents an event checking interval that depends on state.

FieldAdapterDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Base class for adapting an existing detector.

FieldAdapterDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldAdapterDetector

Build an adaptor wrapping an existing detector.

FieldAdditionalDerivativesProvider<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration

Provider for additional derivatives.

FieldAdditionalStateProvider<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation

This interface represents providers for additional state data beyond SpacecraftState.

FieldAltitudeDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite altitude crossing events.

FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Build a new altitude detector.

FieldAltitudeDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector

Protected constructor with full parameters.

FieldAngularCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Simple container for rotation / rotation rate pairs, using CalculusFieldElement.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a rotation/rotation rate pair.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a rotation / rotation rate / rotation acceleration triplet.

FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another one.

FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.

FieldAngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.

FieldApsideDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for apside crossing events.

FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector

Build a new instance.

FieldApsideDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector

Protected constructor with full parameters.

FieldArrayDictionary<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

String → CalculusFieldElement[] mapping, for small number of keys.

FieldArrayDictionary(Field<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary

Constructor with default initial capacity.

FieldArrayDictionary(Field<T>, int) - Constructor for class org.orekit.utils.FieldArrayDictionary

Constructor with specified capacity.

FieldArrayDictionary(FieldArrayDictionary<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary

Constructor from another dictionary.

FieldArrayDictionary(Field<T>, Map<String, T[]>) - Constructor for class org.orekit.utils.FieldArrayDictionary

Constructor from a map.

FieldArrayDictionary.Entry - Class in org.orekit.utils

Entry in a dictionary.

FieldAttitude<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.attitudes

This class handles attitude definition at a given date.

FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude

Creates a new instance.

FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude

Builds an instance for a regular Attitude.

FieldAttitudeInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.attitudes

Class for attitude interpolation.

FieldAttitudeInterpolator(Frame, FieldTimeInterpolator<TimeStampedFieldAngularCoordinates<KK>, KK>) - Constructor for class org.orekit.attitudes.FieldAttitudeInterpolator

Constructor.

FieldAuxiliaryElements<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Container class for common parameters used by all DSST forces.

FieldAuxiliaryElements(FieldOrbit<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Simple constructor.

FieldBodiesElements<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements

Simple constructor.

FieldBooleanDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

This class provides AND and OR operations for event detectors.

FieldBooleanDetector(List<FieldEventDetector<T>>, FieldBooleanDetector.Operator, FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldBooleanDetector

Private constructor with all the parameters.

FieldBoundedPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation

This interface is intended for ephemerides valid only during a time range.

FieldBrouwerLyddanePropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical

This class propagates a FieldSpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).

FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Private helper constructor.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit and potential.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, mass and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, mass and potential.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider and potential.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Private helper constructor.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Build a propagator from orbit, attitude provider, mass and potential.

FieldCartesianOrbit<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.orbits

This class holds Cartesian orbital parameters.

FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Cartesian parameters.

FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Cartesian parameters.

FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from any kind of orbital parameters.

FieldCartesianOrbit(Field<T>, CartesianOrbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Field and CartesianOrbit.

FieldCartesianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit

Constructor from Field and Orbit.

FieldChronologicalComparator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.time

Comparator for FieldTimeStamped instance.

FieldChronologicalComparator() - Constructor for class org.orekit.time.FieldChronologicalComparator

Simple constructor.

FieldCircularOrbit<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.orbits

This class handles circular orbital parameters.

FieldCircularOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Creates a new instance.

FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Creates a new instance.

FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Cartesian parameters.

FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Cartesian parameters.

FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from any kind of orbital parameters.

FieldCircularOrbit(Field<T>, CircularOrbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Field and CircularOrbit.

FieldCircularOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit

Constructor from Field and Orbit.

FieldCjSjCoefficient<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the S_j(k, h) and the C_j(k, h) series and their partial derivatives with respect to k and h.

FieldCjSjCoefficient(T, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

C_j(k, h) and S_j(k, h) constructor.

FieldCombinedDerivatives<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.integration

Container for additional derivatives.

FieldCombinedDerivatives(T[], T[]) - Constructor for class org.orekit.propagation.integration.FieldCombinedDerivatives

Simple constructor.

FieldContinueOnEvent<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent

Empty constructor.

FieldDateDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for date events.

FieldDateDetector(Field<T>, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector

Build a new instance.

FieldDateDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, double, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector

Protected constructor with full parameters.

FieldDeepSDP4<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle

This class contains the methods that compute deep space perturbation terms.

FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4

Constructor for a unique initial TLE.

FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4

Constructor for a unique initial TLE.

FieldDelaunayArguments<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments

Simple constructor.

FieldDSSTJ2SquaredClosedFormContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.

FieldDSSTJ2SquaredClosedFormContext(FieldAuxiliaryElements<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Simple constructor.

FieldDSSTNewtonianAttractionContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common "field" parameters used in DSSTNewtonianAttraction.

FieldDSSTPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst

This class propagates orbits using the DSST theory.

FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Create a new instance of DSSTPropagator.

FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Create a new instance of DSSTPropagator.

FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Create a new instance of DSSTPropagator.

FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Create a new instance of DSSTPropagator.

FieldDSSTTesseralContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common "field" parameters used in DSSTTesseral.

FieldDSSTThirdBodyDynamicContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common "field" parameters used in DSSTThirdBody.

FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T>, CelestialBody, T[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Constructor.

FieldDSSTZonalContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

This class is a container for the common "field" parameters used in DSSTZonal.

FieldEcksteinHechlerPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical

This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Private helper constructor.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, mass and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, mass and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from orbit and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Private helper constructor.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential.

FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Build a propagator from FieldOrbit, attitude provider, mass and potential.

FieldEclipseDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite eclipse related events.

FieldEclipseDetector(Field<T>, ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Build a new eclipse detector.

FieldEclipseDetector(Field<T>, OccultationEngine) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Build a new eclipse detector.

FieldEclipseDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OccultationEngine, T, boolean) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector

Protected constructor with full parameters.

FieldElevationDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.

FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.

FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.

FieldElevationDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector

Protected constructor with full parameters.

FieldElevationExtremumDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Detector for elevation extremum with respect to a ground point.

FieldElevationExtremumDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector

Build a new detector.

FieldElevationExtremumDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector

Build a detector.

FieldElevationExtremumDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector

Protected constructor with full parameters.

FieldEllipse<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.bodies

Model of a 2D ellipse in 3D space.

FieldEllipse(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>, T, T, Frame) - Constructor for class org.orekit.bodies.FieldEllipse

Simple constructor.

FieldEnablingPredicate<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.events

This interface represents an event enabling predicate function.

FieldEphemerisGenerator<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation

Generator for ephemerides.

FieldEquinoctialOrbit<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.orbits

This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.

FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Creates a new instance.

FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Creates a new instance.

FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Cartesian parameters.

FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Cartesian parameters.

FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from any kind of orbital parameters.

FieldEquinoctialOrbit(Field<T>, EquinoctialOrbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Field and EquinoctialOrbit.

FieldEquinoctialOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit

Constructor from Field and Orbit.

FieldEventDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.events

This interface represents space-dynamics aware events detectors.

FieldEventEnablingPredicateFilter<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Wrapper used to detect events only when enabled by an external predicated function.

FieldEventEnablingPredicateFilter(FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Wrap an event detector.

FieldEventEnablingPredicateFilter(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Protected constructor with full parameters.

FieldEventHandler<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.events.handlers

An interface defining how to handle events occurring during propagation..

FieldEventsLogger<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

This class logs events detectors events during propagation.

FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger

Simple constructor.

FieldEventsLogger.FieldLoggedEvent<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Class for logged events entries.

FieldEventSlopeFilter<D extends FieldEventDetector<T>,T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Wrapper used to detect only increasing or decreasing events.

FieldEventSlopeFilter(D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter

Wrap an event detector.

FieldEventSlopeFilter(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter

Protected constructor with full parameters.

FieldEventState<D extends FieldEventDetector<T>,T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

This class handles the state for one event detector during integration steps.

FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState

Simple constructor.

FieldEventState.EventOccurrence<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Class to hold the data related to an event occurrence that is needed to decide how to modify integration.

FieldFixedNumberInterpolationGrid<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.

FieldFixedNumberInterpolationGrid(Field<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid

Constructor.

FieldForceModelContext<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces

Base class for dsst force models parameter containers.

FieldForceModelContext(FieldAuxiliaryElements<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext

Simple constructor.

FieldFunctionalDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

A detector that implements the FieldFunctionalDetector.g(FieldSpacecraftState) function using a lambda that can be set using FieldFunctionalDetector.withFunction(Function).

FieldFunctionalDetector(Field<T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector

Create an event detector with the default values.

FieldFunctionalDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, Function<FieldSpacecraftState<T>, T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector

Private constructor.

FieldGammaMnsFunction<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).

FieldGammaMnsFunction(int, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction

Simple constructor.

FieldGeodeticPoint<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.bodies

Point location relative to a 2D body surface, using CalculusFieldElement.

FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint

Build a new instance.

FieldGHIJjsPolynomials<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_js, H_js, I_js and J_js polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

FieldGHIJjsPolynomials(T, T, T, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Create a set of G_js, H_js, I_js and J_js polynomials.

FieldGHmsjPolynomials<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

FieldGHmsjPolynomials(T, T, T, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Create a set of G_ms^j and H_ms^j polynomials.

FieldHansenTesseralLinear<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t!=0 and n < 0.

FieldHansenTesseralLinear(int, int, int, int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear

Constructor.

FieldHansenThirdBodyLinear<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n > 0.

FieldHansenThirdBodyLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear

Constructor.

FieldHansenZonalLinear<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n < 0.

FieldHansenZonalLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear

Constructor.

Fieldifier - Class in org.orekit.utils

Utility class used to convert class to their Field equivalent.

fieldify(Field<T>, Orbit) - Static method in class org.orekit.utils.Fieldifier

Fieldify given orbit with given field.

fieldify(Field<T>, RealMatrix) - Static method in class org.orekit.utils.Fieldifier

Fieldify given matrix with given field.

fieldify(Field<T>, StateCovariance) - Static method in class org.orekit.utils.Fieldifier

Fieldify given state covariance with given field.

FieldImpulseManeuver<D extends FieldEventDetector<T>,T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.forces.maneuvers

Impulse maneuver model for propagators working with Fields.

FieldImpulseManeuver(D, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver

Build a new instance.

FieldImpulseManeuver(D, AttitudeProvider, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver

Build a new instance.

FieldImpulseManeuver(D, AttitudeProvider, FieldVector3D<T>, T, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver

Build a new instance.

FieldInertia<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.attitudes

Container for inertia of a 3D object.

FieldInertiaAxis<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.attitudes

Container for inertial axis.

FieldInertiaAxis(T, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldInertiaAxis

Simple constructor to pair a moment of inertia with its associated axis.

FieldIntegrableFunction(FieldSpacecraftState<T>, boolean, int, T[], Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction

Build a new instance with a new field.

FieldIntegratedEphemeris<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.integration

This class stores sequentially generated orbital parameters for later retrieval.

FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, FieldArrayDictionary<T>, List<FieldAdditionalStateProvider<T>>, String[], int[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris

Creates a new instance of IntegratedEphemeris.

FieldInterpolationGrid<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities

Interface for interpolation grids.

FieldKeplerianAnomalyUtility - Class in org.orekit.orbits

Utility methods for converting between different Keplerian anomalies.

FieldKeplerianOrbit<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.orbits

This class handles traditional Keplerian orbital parameters.

FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Creates a new instance.

FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Creates a new instance.

FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Cartesian parameters.

FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Cartesian parameters.

FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from any kind of orbital parameters.

FieldKeplerianOrbit(Field<T>, KeplerianOrbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Field and KeplerianOrbit.

FieldKeplerianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit

Constructor from Field and Orbit.

FieldKeplerianPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical

Simple Keplerian orbit propagator.

FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit only.

FieldKeplerianPropagator(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit and central attraction coefficient μ.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit and attitude provider.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build a propagator from orbit, attitude provider and central attraction coefficient μ.

FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator

Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

FieldLatitudeCrossingDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Detector for geographic latitude crossing.

FieldLatitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Build a new detector.

FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Build a detector.

FieldLatitudeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Protected constructor with full parameters.

FieldLegendrePolynomials<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Computes the P_nm(t) coefficients.

FieldLegendrePolynomials(int, int, T) - Constructor for class org.orekit.utils.FieldLegendrePolynomials

Create Legendre polynomials for the given degree and order.

FieldLnsCoefficients<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the L_n^s(γ).

FieldLnsCoefficients(int, int, T[][], SortedMap<CoefficientsFactory.NSKey, Double>, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients

Create a set of L_n^s(γ) coefficients.

FieldLongitudeCrossingDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Detector for geographic longitude crossing.

FieldLongitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Build a new detector.

FieldLongitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Build a detector.

FieldLongitudeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Protected constructor with full parameters.

FieldManeuverTriggersResetter<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.forces.maneuvers.trigger

Resetter for maneuver triggers.

FieldMaxGapInterpolationGrid<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where points obey a maximum time gap.

FieldMaxGapInterpolationGrid(Field<T>, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid

Constructor.

fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Natural to proper correction for aberration of light.

fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Natural to proper correction for aberration of light.

FieldNegateDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

An event detector that negates the sign on another event detector's g function.

FieldNegateDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector

Create a new event detector that negates an existing event detector.

FieldNegateDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector

Private constructor.

FieldNodeDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Finder for node crossing events.

FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector

Build a new instance.

FieldNodeDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector

Protected constructor with full parameters.

FieldNumericalPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.numerical

This class propagates orbits using numerical integration.

FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

FieldODEIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build first order integrators for propagators conversion.

FieldOfView - Interface in org.orekit.geometry.fov

Interface representing a spacecraft sensor Field Of View.

FieldOfViewDetector - Class in org.orekit.propagation.events

Finder for target entry/exit events with respect to a satellite sensor Field Of View.

FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector

Build a new instance.

FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector

Build a new instance.

FieldOfViewDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector

Protected constructor with full parameters.

FieldOrbit<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.orbits

This class handles orbital parameters.

FieldOrbit(Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldOrbit

Default constructor.

FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldOrbit

Set the orbit from Cartesian parameters.

FieldOrbitBlender<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.orbits

Orbit blender.

FieldOrbitBlender(SmoothStepFactory.FieldSmoothStepFunction<KK>, FieldAbstractAnalyticalPropagator<KK>, Frame) - Constructor for class org.orekit.orbits.FieldOrbitBlender

Default constructor.

FieldOrbitHermiteInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.orbits

Class using a Hermite interpolator to interpolate orbits.

FieldOrbitHermiteInterpolator(Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

FieldOrbitHermiteInterpolator(int, Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

FieldOrbitHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator

Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).

FieldOrbitHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator

Constructor.

FieldOrekitFixedStepHandler<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed size step handler.

FieldOrekitStepHandler<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler.

FieldOrekitStepInterpolator<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step interpolator.

FieldOrekitStepNormalizer<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling

This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.

FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Simple constructor.

FieldParameterDrivenDateIntervalDetector<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events

Detector for date intervals that may be offset thanks to parameter drivers.

FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Build a new instance.

FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Build a new instance.

FieldParameterDrivenDateIntervalDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, DateDriver, DateDriver, DateDriver, ParameterDriver) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Protected constructor with full parameters.

FieldPoleCorrection<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.frames

Simple container class for pole correction parameters.

FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection

Simple constructor.

FieldProbabilityOfCollision<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.ssa.metrics

Container for values relative to the probability of collision : Value of the probability of collision. Name of the method with which it was computed. Upper and lower limit of the value if the method provides them (such as Laas2015 for example). Flag defining if the probability was maximized in any way (such as Alfriend1999Max for example).

FieldProbabilityOfCollision(T, String) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Constructor with default values of 0 for the upper/lower limits and default false flag for maximum probability.

FieldProbabilityOfCollision(T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Constructor with default values of 0 for the upper and lower limits.

FieldProbabilityOfCollision(T, T, T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Constructor.

FieldPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation

This interface provides a way to propagate an orbit at any time.

fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Proper to natural correction for aberration of light.

fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Proper to natural correction for aberration of light.

FieldPVCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Simple container for Position/Velocity pairs, using CalculusFieldElement.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet with zero acceleration.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet.

FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates from a field and a regular PVCoordinates.

FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor.

FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Subtractive constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor.

FieldPVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.

FieldPVCoordinatesProvider<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.utils

Interface for PV coordinates providers.

FieldRecordAndContinue<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Handler that will record every time an event occurs and always return Action.CONTINUE.

FieldRecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue

Create a new handler using an ArrayList to store events.

FieldRecordAndContinue(List<FieldRecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue

Create a handler using the given collection to store events.

FieldRecordAndContinue.Event<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

A single event detected during propagation.

FieldSGP4<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle

This class contains methods to compute propagated coordinates with the SGP4 model.

FieldSGP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4

Constructor for a unique initial TLE.

FieldSGP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4

Constructor for a unique initial TLE.

FieldShortPeriodicsInterpolatedCoefficient<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolated short periodics coefficients.

FieldShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient

Simple constructor.

FieldShortPeriodTerms<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.forces

Additive short period terms contributing to the mean to osculating orbit mapping.

FieldShortTermEncounter2DDefinition<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Defines the encounter between two collision object at time of closest approach assuming a short-term encounter model .

FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Constructor.

FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Constructor.

FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Constructor.

FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Constructor.

FieldSpacecraftState<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation

This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.

FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit only.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and attitude.

FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit and mass.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude and mass.

FieldSpacecraftState(FieldOrbit<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and additional states.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit attitude and additional states.

FieldSpacecraftState(FieldOrbit<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit, mass and additional states.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude, mass and additional states.

FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.

FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Convert a FieldSpacecraftState.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit only.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and attitude.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit and mass.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude and mass.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit only.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit and attitude.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Create a new instance from orbit and mass.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude and mass.

FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState

Build a spacecraft state from orbit, attitude and mass.

FieldSpacecraftStateInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.propagation

Generic class for spacecraft state interpolator.

FieldSpacecraftStateInterpolator(Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Simplest constructor to create a default Hermite interpolator for every spacecraft state field.

FieldSpacecraftStateInterpolator(int, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

FieldSpacecraftStateInterpolator(int, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

FieldSpacecraftStateInterpolator(int, double, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

FieldSpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Constructor.

FieldSpacecraftStateInterpolator(Frame, FieldTimeInterpolator<FieldOrbit<KK>, KK>, FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>, FieldTimeInterpolator<FieldAttitude<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator

Constructor.

FieldStateCovariance<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation

This class is the representation of a covariance matrix at a given date.

FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, LOF) - Constructor for class org.orekit.propagation.FieldStateCovariance

Constructor.

FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.FieldStateCovariance

Constructor.

FieldStateMapper<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.integration

This class maps between raw double elements and FieldSpacecraftState instances.

FieldStateMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper

Simple constructor.

FieldStaticTransform<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.frames

A transform that only includes translation and rotation.

FieldStepHandlerMultiplexer<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling

This class gathers several OrekitStepHandler instances into one.

FieldStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Simple constructor.

FieldStopOnDecreasing<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing

Empty constructor.

FieldStopOnEvent<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent

Empty constructor.

FieldStopOnIncreasing<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing

Empty constructor.

FieldTimeDerivativesEquations<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.propagation.numerical

Interface summing up the contribution of several forces into orbit and mass derivatives.

FieldTimeInterpolator<T extends FieldTimeStamped<KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Interface in org.orekit.time

This interface represents objects that can interpolate a time stamped value with respect to time.

FieldTimeShiftable<T extends FieldTimeShiftable<T,KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Interface in org.orekit.time

This interface represents objects that can be shifted in time.

FieldTimeSpanMap<T,D extends org.hipparchus.CalculusFieldElement<D>> - Class in org.orekit.utils

Container for objects that apply to spans of time.

FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap

Create a map containing a single object, initially valid throughout the timeline.

FieldTimeSpanMap.Transition<S,D extends org.hipparchus.CalculusFieldElement<D>> - Class in org.orekit.utils

Local class holding transition times.

FieldTimeStamped<T extends org.hipparchus.CalculusFieldElement<T>> - Interface in org.orekit.time

This interface represents objects that have a AbsoluteDate date attached to them.

FieldTimeStampedCache<T extends FieldTimeStamped<KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Interface in org.orekit.utils

Interface for a data structure that can provide concurrent access to FieldTimeStamped data surrounding a given date.

FieldTimeStampedPair<F extends FieldTimeStamped<KK>,S extends FieldTimeStamped<KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.time

Pair of time stamped values being defined at the same date.

FieldTimeStampedPair(F, S) - Constructor for class org.orekit.time.FieldTimeStampedPair

Constructor.

FieldTimeStampedPair(F, S, double) - Constructor for class org.orekit.time.FieldTimeStampedPair

Constructor.

FieldTLE<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle

This class is a container for a single set of TLE data.

FieldTLE(Field<T>, String, String) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE

Simple constructor from unparsed two lines.

FieldTLE(Field<T>, String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE

Simple constructor from unparsed two lines using the given time scale as UTC.

FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE

Simple constructor from already parsed elements.

FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE

Simple constructor from already parsed elements using the given time scale as UTC.

FieldTLEPropagator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle

This class provides elements to propagate TLE's.

FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Protected constructor for derived classes.

FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Protected constructor for derived classes.

FieldTrackingCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Container for azimut/elevation/range coordinates as seen from a ground point.

FieldTrackingCoordinates(T, T, T) - Constructor for class org.orekit.utils.FieldTrackingCoordinates

Simple constructor.

FieldTransform<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.frames

Transformation class in three-dimensional space.

FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform

Build a transform from a regular transform.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first time derivative.

FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first and second time derivatives.

FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a translation transform, with its first time derivative.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a rotation transform.

FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform

Build a transform by combining two existing ones.

FieldTransformGenerator<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.frames

Generator to use field transforms in GenericTimeStampedCache.

FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator

simple constructor.

FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for 1950 dates: 1950-01-01.

FileFormat - Enum in org.orekit.files.ccsds.utils

Enumerate for file format.

FilesListCrawler - Class in org.orekit.data

Provider for data files in an explicit list.

FilesListCrawler(File...) - Constructor for class org.orekit.data.FilesListCrawler

Build a data classpath crawler.

fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a single vector.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a single vector.

fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in class org.orekit.files.sinex.SinexLoader

Load celestial body.

fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EopHistoryLoader

Load celestial body.

filter(DataSource) - Method in interface org.orekit.data.DataFilter

Filter the data source.

filter(DataSource) - Method in class org.orekit.data.GzipFilter

Filter the data source.

filter(DataSource) - Method in class org.orekit.data.TruncatingFilter

Filter the data source.

filter(DataSource) - Method in class org.orekit.data.UnixCompressFilter

Filter the data source.

filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ElevationFilter

Apply a filter to an observed measurement.

filter(ObservedMeasurement<T>, SpacecraftState) - Method in interface org.orekit.estimation.measurements.filtering.MeasurementFilter

Apply a filter to an observed measurement.

filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ResidualFilter

Apply a filter to an observed measurement.

filter(DataSource) - Method in class org.orekit.files.rinex.HatanakaCompressFilter

Filter the data source.

filter(boolean) - Method in class org.orekit.utils.ParameterDriversList

Filter parameters to keep only one type of selection status.

filterData(ObservationData, ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter

This method filters the provided data given the state of the filter.

filterData(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter

This method filters the provided data given the state of the filter.

filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Applies a Dual Frequency Hatch filter to a list of ObservationDataSet.

filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Applies a Single Frequency Hatch filter to a list of ObservationDataSet.

filterRelevant(ObservedMeasurement<?>, SpacecraftState[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Filter relevant states for a measurement.

FiltersManager - Class in org.orekit.data

Manager for data filters.

FiltersManager() - Constructor for class org.orekit.data.FiltersManager

Build an empty manager.

FilterType - Enum in org.orekit.propagation.events

Enumerate for filtering events.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Finalize data after parsing.

finalizeData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Finalize data after parsing.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.KalmanModel

Finalize estimation.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Finalize estimation.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Finalize estimation.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Finalize estimation.

finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Finalize estimation.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Finalize header after parsing.

finalizeHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Finalize header after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Finalize metadata after parsing.

finalizeMetadata(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Finalize the metadata.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Finalize metadata after parsing.

finalizeMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Finalize metadata after parsing.

finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Finalize estimation operations on the observation grid.

finalizeOperationsObservationGrid() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Finalize estimation operations on the observation grid.

finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Finalize estimation operations on the observation grid.

findByName(String) - Method in class org.orekit.utils.ParameterDriversList

Find a delegating driver by name.

findDelegatingSpanNameBySpanName(String) - Method in class org.orekit.utils.ParameterDriversList

Find a delegating driver by name.

findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory

Retrieve EOP from a frame hierarchy.

findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader

Find the time map for a specific satellite antenna.

finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter

Finalize propagation.

finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter

Finalize propagation.

finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter

Finalize propagation.

finish(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment

Finalize propagation.

finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler

Finalize propagation.

finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler

Finalize propagation.

finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Finalize propagation.

finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Finalize propagation.

finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler

Finalize propagation.

finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler

Finalize propagation.

finish(List<SpacecraftState>) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer

Finalize propagation.

finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Finalize propagation.

finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Finalize propagation.

finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Finalize propagation.

finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Finalize propagation.

finished(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin

FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using finite differences to compute the Jacobian.

FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Simple constructor.

fit(EOPHistory) - Method in class org.orekit.frames.EOPFitter

Fit raw history.

fit(EOPHistory, ToDoubleFunction<EOPEntry>) - Method in class org.orekit.frames.SingleParameterFitter

Perform secular and harmonic fitting.

fit() - Method in class org.orekit.utils.SecularAndHarmonic

Fit parameters.

FixedFrameBuilder - Class in org.orekit.attitudes

Builder that assumes angular coordinates are given in a fixed frame.

FixedFrameBuilder(Frame) - Constructor for class org.orekit.attitudes.FixedFrameBuilder

Creates new instance.

FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.

FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid

Constructor.

FixedPanel - Class in org.orekit.forces

Class representing one panel of a satellite, fixed with respect to satellite body.

FixedPanel(Vector3D, double, boolean, double, double, double, double) - Constructor for class org.orekit.forces.FixedPanel

Simple constructor.

FixedPointTleGenerationAlgorithm - Class in org.orekit.propagation.analytical.tle.generation

Fixed Point method to reverse SGP4 and SDP4 propagation algorithm and generate a usable TLE from a spacecraft state.

FixedPointTleGenerationAlgorithm() - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Default constructor.

FixedPointTleGenerationAlgorithm(double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Constructor.

FixedPointTleGenerationAlgorithm(double, int, double, TimeScale, Frame) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Constructor.

FixedRate - Class in org.orekit.attitudes

This class handles a simple attitude provider at constant rate around a fixed axis.

FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate

Creates a new instance.

FixedStepSelector - Class in org.orekit.time

Selector generating a continuous stream of dates separated by a constant step.

FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector

Simple constructor.

FixedTransformProvider - Class in org.orekit.frames

Transform provider using fixed transform.

FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider

Simple constructor.

FixedTroposphericDelay - Class in org.orekit.models.earth.troposphere

A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.

FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance.

FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.

FixedTroposphericDelay(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the specified data manager.

fixIntegerAmbiguities(int, List<ParameterDriver>, RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Fix integer ambiguities.

FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Parameter name for flow rate.

FLOW_RATE_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Flow rate scaling factor.

FootprintOverlapDetector - Class in org.orekit.propagation.events

Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.

FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector

Build a new instance.

FootprintOverlapDetector(AdaptableInterval, double, int, EventHandler, FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double, List<FootprintOverlapDetector.SamplingPoint>) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector

Protected constructor with full parameters.

ForceModel - Interface in org.orekit.forces

This interface represents a force modifying spacecraft motion.

ForceModelContext - Class in org.orekit.propagation.semianalytical.dsst.forces

Base class for dsst force models attributes containers.

ForceModelContext(AuxiliaryElements) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext

Simple constructor.

forEach(Consumer<T>) - Method in class org.orekit.utils.TimeSpanMap

Performs an action for each non-null element of map.

format(double) - Static method in class org.orekit.utils.AccurateFormatter

Format a double number.

format(int, int, int, int, int, double) - Static method in class org.orekit.utils.AccurateFormatter

Format a date.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Key for format version.

FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm

Key for format version.

formatIntegerOrNaN(int, int) - Static method in class org.orekit.files.ilrs.CRD

Format the integer value as a string, or the string VALUE_NOT_AVAILABLE.

formatUtcOffset() - Method in class org.orekit.time.TimeComponents

Get the UTC offset as a string in ISO8601 format.

Frame - Class in org.orekit.frames

Tridimensional references frames class.

Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

FrameAdapter - Class in org.orekit.utils

Adapter from Frame to ExtendedPVCoordinatesProvider.

FrameAdapter(Frame) - Constructor for class org.orekit.utils.FrameAdapter

Simple constructor.

FrameAlignedProvider - Class in org.orekit.attitudes

This class handles an attitude provider aligned with a frame or a fixed offset to it.

FrameAlignedProvider(Rotation) - Constructor for class org.orekit.attitudes.FrameAlignedProvider

Creates new instance.

FrameAlignedProvider(Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider

Creates new instance aligned with the given frame.

FrameAlignedProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider

Creates new instance with a fixed attitude in the given frame.

FrameAncestorException - Exception in org.orekit.errors

This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.

FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException

Simple constructor.

FrameFacade - Class in org.orekit.files.ccsds.definitions

Facade in front of several frames types in CCSDS messages.

FrameFacade(Frame, CelestialBodyFrame, OrbitRelativeFrame, SpacecraftBodyFrame, String) - Constructor for class org.orekit.files.ccsds.definitions.FrameFacade

Simple constructor.

Frames - Interface in org.orekit.frames

A collection of commonly used Frames.

FramesFactory - Class in org.orekit.frames

Factory for predefined reference frames.

freeze() - Method in class org.orekit.frames.FieldTransform

Get a frozen transform.

freeze() - Method in class org.orekit.frames.Transform

Get a frozen transform.

freezeColumnsNames() - Method in class org.orekit.propagation.AbstractMatricesHarvester

Freeze the names of the Jacobian columns.

freezeColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Freeze the names of the Jacobian columns.

freezeColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Freeze the names of the Jacobian columns.

Frequency - Enum in org.orekit.gnss

Enumerate for GNSS frequencies.

FrequencyPattern - Class in org.orekit.gnss.antenna

Pattern for GNSS antenna model on one frequency.

FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern

Simple constructor.

fromSeconds(int, double, double, int) - Static method in class org.orekit.time.TimeComponents

Build a time from the second number within the day.

fromSI(double) - Method in class org.orekit.utils.units.Unit

Convert a value from SI units.

fromSI(Double) - Method in class org.orekit.utils.units.Unit

Convert a value from SI units.

FrRangeMeasurement(AbsoluteDate, double, int, String, int, int, int, int, int) - Constructor for class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Constructor.

FunctionalDetector - Class in org.orekit.propagation.events

A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).

FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector

Create an event detector with the default values.

FunctionalDetector(AdaptableInterval, double, int, EventHandler, ToDoubleFunction<SpacecraftState>) - Constructor for class org.orekit.propagation.events.FunctionalDetector

Private constructor.

FundamentalNutationArguments - Class in org.orekit.data

Class computing the fundamental arguments for nutation and tides.

FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the future direction.

G

g(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector

The g is positive when the primary object is getting further away from the secondary object and is negative when it is getting closer to it.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAdapterDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector

Compute the value of the detection function.

g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Compute the value of the detection function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Compute the value of the detection function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector

Compute the value of the switching function.

g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector

g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector

Compute the value of the detection function.

G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants

Standard gravity constant, used in maneuvers definition: 9.80665 m/s².

Galileo - Class in org.orekit.gnss.attitude

Attitude providers for Galileo navigation satellites.

Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo

Simple constructor.

GALILEO_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the earth's rotation rate in rad/s for Galileo user.

GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.

GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for Galileo System Time: 1999-08-22.

GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Earth's universal gravitational parameter for Galileo user in m³/s².

GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Number of weeks in the Galileo cycle.

GalileoAlmanac - Class in org.orekit.propagation.analytical.gnss.data

Class for Galileo almanac.

GalileoAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Build a new almanac.

GalileoNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a Galileo navigation message.

GalileoNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Constructor.

GalileoScale - Class in org.orekit.time

Galileo system time scale.

GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).

GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Simple constructor.

GatheringSubscriber - Class in org.orekit.estimation.measurements.generation

Subscriber that gather all generated measurements in a sorted set.

GatheringSubscriber() - Constructor for class org.orekit.estimation.measurements.generation.GatheringSubscriber

Simple constructor.

generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Generate a sequence of measurements.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator

Generate measurements.

generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler

Generate a sequence of measurements.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator

Generate a chronologically sorted list of entries to be cached.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator

Generate a chronologically sorted list of entries to be cached.

generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator

Generate a chronologically sorted list of entries to be cached.

generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(SpacecraftState, TLE) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm

Generate a TLE from a given spacecraft state and a template TLE.

generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator

Generate a chronologically sorted list of entries to be cached.

generateCartesianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Generate a Cartesian orbit.

generateData(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Generate the attitude data corresponding to the attitude type.

generateDataFromEarliestToLatestDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator

Generate a list of parameters between earliest and latest dates.

GeneratedMeasurementSubscriber - Interface in org.orekit.estimation.measurements.generation

Interface for subscribing to generated measurements events.

generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Generate a parse exception for this entry.

generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Generate a keplerian orbit.

generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Generate a keplerian orbit.

generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Generate a keplerian orbit.

generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.

generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.

generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Generate TLE from OMM file.

Generator - Class in org.orekit.estimation.measurements.generation

Main generator for observed measurements.

Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator

Build a generator with no sequences generator.

Generator - Interface in org.orekit.files.ccsds.utils.generation

Generation interface for CCSDS messages.

GenericGNSS - Class in org.orekit.gnss.attitude

Attitude providers for navigation satellites for which no specialized model is known.

GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS

Simple constructor.

GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

Generic thread-safe cache for time-stamped data.

GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache

Simple constructor.

GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, double) - Constructor for class org.orekit.utils.GenericTimeStampedCache

Simple constructor with overriding minimum step.

GeodeticPoint - Class in org.orekit.bodies

Point location relative to a 2D body surface.

GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint

Build a new instance.

geodeticToIsometricLatitude(double) - Method in class org.orekit.bodies.OneAxisEllipsoid

Compute the isometric latitude corresponding to the provided latitude.

geodeticToIsometricLatitude(T) - Method in class org.orekit.bodies.OneAxisEllipsoid

Compute the isometric latitude corresponding to the provided latitude.

GeographicZoneDetector - Class in org.orekit.propagation.events

Detector for entry/exit of a zone defined by geographic boundaries.

GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a new detector.

GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a detector.

GeographicZoneDetector(AdaptableInterval, double, int, EventHandler, BodyShape, SphericalPolygonsSet, EnclosingBall<Sphere2D, S2Point>, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Protected constructor with full parameters.

Geoid - Class in org.orekit.models.earth

A geoid is a level surface of the gravity potential of a body.

Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid

Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.

GeoMagneticElements - Class in org.orekit.models.earth

Contains the elements to represent a magnetic field at a single point.

GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements

Construct a new element with the given field vector.

GeoMagneticField - Class in org.orekit.models.earth

Used to calculate the geomagnetic field at a given geodetic point on earth.

GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField

Create a new geomagnetic field model with the given parameters.

GeoMagneticFieldFactory - Class in org.orekit.models.earth

Factory for different GeoMagneticField models.

GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth

The currently supported geomagnetic field models.

GeoMagneticFields - Interface in org.orekit.models.earth

Methods for obtaining geomagnetic fields.

GeoMagneticModelLoader - Class in org.orekit.models.earth

Loads geomagnetic field models from a given input stream.

GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader

Empty constructor.

GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss

Geometry-free combination.

GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss

Geometry free cycle slip detectors.

GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector

Constructor.

get(String) - Method in class org.orekit.utils.DoubleArrayDictionary

Get the value corresponding to a key.

get(String) - Method in class org.orekit.utils.FieldArrayDictionary

Get the value corresponding to a key.

get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap

Get the entry valid at a specified date.

get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Get the entry valid at a specified date.

get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the last 24H mean geomagnetic index.

get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

The Kp index is derived from the Ap index.

get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Get the last 24H mean geomagnetic index.

getA() - Method in class org.orekit.attitudes.FieldInertiaAxis

Get the inertia axis.

getA() - Method in class org.orekit.attitudes.InertiaAxis

Get the inertia axis.

getA() - Method in class org.orekit.bodies.Ellipse

Get the semi major axis.

getA() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the first semi-axis.

getA() - Method in class org.orekit.bodies.FieldEllipse

Get the semi major axis.

getA() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit semi-major axis.

getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Returns the a coefficients array.

getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Returns the a coefficients array.

getA() - Method in class org.orekit.orbits.CartesianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.CircularOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.FieldOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.KeplerianOrbit

Get the semi-major axis.

getA() - Method in class org.orekit.orbits.Orbit

Get the semi-major axis.

getA() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the semi-major axis.

getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get A = sqrt(μ * a).

getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get A = sqrt(μ * a).

getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get A = sqrt(μ * a).

getA() - Method in class org.orekit.propagation.SpacecraftState

Get the semi-major axis.

getA0() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the constant term of the offset.

getA0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get A0 field.

getA1() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the linear term of the offset.

getA1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get A₁ field.

getA2() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the quadratic term of the offset.

getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Get the semi major axis to the power 4.

getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Get the semi major axis to the power 4.

getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the abscissa grid for the interpolation function.

getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the transition field absolute date.

getAbsorption() - Method in class org.orekit.forces.Panel

Get radiation pressure absorption coefficient.

getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the absolute position-velocity-acceleration.

getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState

Get the absolute position-velocity-acceleration.

getAbsPVAInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get absolute position-velocity-acceleration interpolator.

getAbsPVAInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get absolute position-velocity-acceleration interpolator.

getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get acceleration.

getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the acceleration of the spacecraft during maneuver and in maneuver frame.

getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the acceleration of the spacecraft during maneuver and in maneuver frame.

getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the acceleration of the spacecraft during maneuver and in maneuver frame.

getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the acceleration of the spacecraft during maneuver and in maneuver frame.

getAcceleration() - Method in class org.orekit.frames.FieldTransform

Get the second time derivative of the translation.

getAcceleration() - Method in class org.orekit.frames.Transform

Get the second time derivative of the translation.

getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the acceleration.

getAcceleration() - Method in class org.orekit.utils.PVCoordinates

Gets the acceleration.

getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ angular off-nominal acceleration direction.

getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get interpolation mode between current and next acceleration line.

getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ percent error on acceleration magnitude.

getAccelerationModel(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the AccelerationModel model valid at a date.

getAccelerationModelSpan(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the AccelerationModel TimeSpanMap.Span containing a specified date.

getAccuracy(String) - Method in class org.orekit.files.sp3.SP3Header

Get the formal accuracy.

getAccuracy() - Method in interface org.orekit.gnss.metric.messages.common.AccuracyProvider

Get the accuracy of the ephemeris data from an accuracy index.

getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.GlonassUserRangeAccuracy

Get the accuracy of the ephemeris data from an accuracy index.

getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.SignalInSpaceAccuracy

Get the accuracy of the ephemeris data from an accuracy index.

getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.UserRangeAccuracy

Get the accuracy of the ephemeris data from an accuracy index.

getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData

Get the accuracy provider of the ephemeris message.

getAcmDataElements() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the list of elements of information data blocks included in this message.

getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the user requested action.

getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the user requested action.

getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.

getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get actual time span used for the OD of the object.

getActuatorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get the actuator used.

getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the adapted propagator.

getAdditionalCovMetadataBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the additional covariance metadata logical block.

getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.CombinedDerivatives

Get the derivatives related to the additional state.

getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives

Get the derivatives related to the additional state.

getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the list of additional equations.

getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get an unmodifiable list of providers for additional derivatives.

getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get an unmodifiable list of providers for additional derivatives.

getAdditionalParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the additional parameters logical block.

getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration

Get the additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate

Get the additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Get the additional state.

getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider

Get the additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Get the additional state.

getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Get the additional state.

getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Get an additional state.

getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Get an additional state.

getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the additional state.

getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Get an additional state derivative.

getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState

Get an additional state derivative.

getAdditionalStateInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get additional state interpolator.

getAdditionalStateInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get additional state interpolator.

getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator

Get an unmodifiable list of providers for additional state.

getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator

Get an unmodifiable list of providers for additional state.

getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.FieldSpacecraftState

Get an unmodifiable map of additional states derivatives.

getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.SpacecraftState

Get an unmodifiable map of additional states derivatives.

getAdditionalStatesValues() - Method in class org.orekit.propagation.FieldSpacecraftState

Get an unmodifiable map of additional states.

getAdditionalStatesValues() - Method in class org.orekit.propagation.SpacecraftState

Get an unmodifiable map of additional states.

getAdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Unique identifier of Attitude Data Message linked to this Orbit Data Message.

getAdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.

getADot() - Method in class org.orekit.orbits.CartesianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.CircularOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.FieldOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.orbits.Orbit

Get the semi-major axis derivative.

getADot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for the change rate in semi-major axis.

getADot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for the change rate in semi-major axis.

getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the value of the central body reference radius.

getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the central body reference radius.

getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the value of the central body reference radius.

getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get af₀.

getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get af₀.

getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the the SV Clock Bias Correction Coefficient.

getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the Zeroth Order Clock Correction.

getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get af₁.

getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get af₁.

getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the SV Clock Drift Correction Coefficient.

getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the First Order Clock Correction.

getAF2() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get af₂.

getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Drift Rate Correction Coefficient.

getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Drift Rate Correction Coefficient.

getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the Second Order Clock Correction.

getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the entry valid after transition.

getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the entry valid after transition.

getAgency() - Method in class org.orekit.files.sp3.SP3Header

Returns the agency that prepared this SP3 file.

getAgencyName() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the agency name.

getAgencyName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get name of the agency.

getAGf0() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Gets the Zeroth Order Clock Correction.

getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the Zeroth Order Clock Correction.

getAGf1() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Gets the First Order Clock Correction.

getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the First Order Clock Correction.

getAGoM() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the SGP4-XP solar radiation pressure-like coefficient Aγ/m.

getAi0() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Get aᵢ₀.

getAi1() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Get aᵢ₁.

getAi2() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Get aᵢ₂.

getAlbedoGridSize() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get albedo grid size.

getAlbedoModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get albedo model.

getAlert() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get alert flag.

getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector

Get the alignment angle (rad).

getAll() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get all the data in this cache.

getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get all of the data in this cache.

getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Get all the ambiguity parameters drivers.

getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Get the list of all force models.

getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the list of all force models.

getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get all the force models, perturbing forces and Newtonian attraction included.

getAlmanacs() - Method in class org.orekit.gnss.SEMParser

Gets all the GPS almanacs read from the file.

getAlmanacs() - Method in class org.orekit.gnss.YUMAParser

Gets all the GPS almanacs read from the file.

getAlpha() - Method in class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage

Get the α coefficients.

getAlpha() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Get the α coefficients.

getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Returns the alpha coefficients array.

getAlpha(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit

Get the latitude argument.

getAlpha(PositionAngleType) - Method in class org.orekit.orbits.FieldCircularOrbit

Get the latitude argument.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get direction cosine α for central body.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get direction cosine α for central body.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine α for central body.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get direction cosine α for central body.

getAlpha0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get α₀ field.

getAlpha1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get α₁ field.

getAlpha2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get α₂ field.

getAlpha3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get α₃ field.

getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Get the equatorial radius of the central body to the power 4.

getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Get the equatorial radius of the central body to the power 4.

getAlphaDot(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit

Get the latitude argument derivative.

getAlphaDot(PositionAngleType) - Method in class org.orekit.orbits.FieldCircularOrbit

Get the latitude argument derivative.

getAlphaE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric latitude argument.

getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric latitude argument.

getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric latitude argument derivative.

getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric latitude argument derivative.

getAlphaM() - Method in class org.orekit.orbits.CircularOrbit

Get the mean latitude argument.

getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean latitude argument.

getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit

Get the mean latitude argument derivative.

getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean latitude argument derivative.

getAlphaV() - Method in class org.orekit.orbits.CircularOrbit

Get the true latitude argument.

getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true latitude argument.

getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit

Get the true latitude argument derivative.

getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true latitude argument derivative.

getAltCovRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the value of ALT_COV_REF_FRAME as an Orekit Frame.

getAltCovType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the flag indicating the type of alternate covariance information provided.

getAlternateNames() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the alternate names for this space object.

getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the altitude.

getAltitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the altitude.

getAltitude() - Method in class org.orekit.bodies.Loxodrome

Get the altitude above the reference body.

getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector

Get the threshold altitude value.

getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Get the threshold altitude value.

getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Get the driver for phase ambiguity.

getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Get the driver for phase ambiguity.

getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.Phase

Get the driver for phase ambiguity.

getAmplifierBandwidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the amplifier bandwidth.

getAmplifierGain() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the amplifier gain.

getAmplifierInUse() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the amplifier in use.

getAnalysisCenterID() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the analysis center ID.

getAnalysisCenterName() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the analysis center name.

getAncestor(int) - Method in class org.orekit.frames.Frame

Get the n^th ancestor of the frame.

getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the fixed angle to be crossed (radians).

getAngle() - Method in class org.orekit.utils.units.Unit

Get the angle exponent.

getAnglesData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the angles data for the data block.

getAngleType() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for angleType.

getAngular() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary angular part.

getAngular() - Method in class org.orekit.frames.Transform

Get the underlying elementary angular part.

getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get an unmodifiable list of attitude data lines.

getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData

Get an unmodifiable view of the data points.

getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get an unmodifiable list of attitude data lines.

getAngularCoordinates() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get an unmodifiable list of attitude data lines.

getAngularCoordinates() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get an unmodifiable list of attitude data lines.

getAngularDerivativesFilter() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Get the angular derivative filter corresponding to the attitude data.

getAngularInterpolator() - Method in class org.orekit.attitudes.AttitudeInterpolator

Get time stamped angular coordinates interpolator.

getAngularInterpolator() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator

Get time stamped angular coordinates interpolator.

getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the mean angular velocity of the Earth for the GNSS model.

getAngularVelocity() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the mean angular velocity of the Earth of the GNSS model.

getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates

Get the angular velocity (spin) of this point as seen from the origin.

getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates

Get the angular velocity (spin) of this point as seen from the origin.

getAngularVelocityBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the angular velocity logical block.

getAngVelX() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Get the angular velocity around X axis (rad/s).

getAngVelY() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Get the angular velocity around Y axis (rad/s).

getAngVelZ() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Get the angular velocity around Z axis (rad/s).

getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit anomaly.

getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the anomaly.

getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.KeplerianOrbit

Get the anomaly.

getAnomalyDot(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the anomaly derivative.

getAnomalyDot(PositionAngleType) - Method in class org.orekit.orbits.KeplerianOrbit

Get the anomaly derivative.

getAnomalyType() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the type of anomaly (true or mean).

getAntennaAzimuth() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the azimuth of the zero direction of a fixed antenna.

getAntennaBSight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the antenna B.Sight.

getAntennaHeight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the antenna height.

getAntennaNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the number of the antenna.

getAntennaPhaseCenter() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the antenna phasecenter.

getAntennaReferencePoint() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the position of antenna reference point for antenna on vehicle.

getAntennaType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the type of the antenna.

getAntennaType(AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Get the antenna type for the given epoch.

getAntennaTypeTimeSpanMap() - Method in class org.orekit.files.sinex.Station

Get the TimeSpanMap of site antenna type.

getAntennaZeroDirection() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the zero direction of antenna.

getAntiSpoofing() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get anti-spoofing flag.

getAntiSpoofing(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E

Get the anti-spoofing for a satellite.

getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Getter for the Age Of Data Clock (AODC).

getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Getter for the Age Of Data Ephemeris (AODE).

getAODO() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Age Of data Offset.

getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the A_p geomagnetic indices.

getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the A_p geomagnetic indices.

getAp() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

Get the Ap index.

getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters

Get the A_p geomagnetic indices.

getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the arithmetic average of all eight Ap indices for the current entry.

getApoapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the distance of the furthest point in the objects orbit above the equatorial radius of the central body.

getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the applicable wavelength.

getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the applied voltage.

getApproachAngle() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.

getApproxPos() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the Approximate Marker Position.

getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Get an arbitrary date.

getArea() - Method in class org.orekit.forces.Panel

Get panel area.

getAreaDRG() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the effective area of the object exposed to atmospheric drag.

getAreaPC() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the actual area of the object.

getAreaPCMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the maximum area of the object to be used to compute the collision probability.

getAreaPCMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the minimum area of the object to be used to compute the collision probability.

getAreaSRP() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the effective area of the object exposed to solar radiation pressure.

getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Get astronomical amplitudes map.

getAtmosphere() - Method in class org.orekit.forces.drag.DragForce

Get the atmospheric model.

getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the atmospheric model.

getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get name of atmospheric model.

getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get name of atmospheric model.

getAttBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get basis of this attitude state time history data.

getAttBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get identification number of the orbit determination or simulation upon which this attitude is based.

getAttID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get attitude identification number.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TorqueFree

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TorqueFree

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the attitude corresponding to an orbital state.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the attitude corresponding to an orbital state.

getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm

Get the attitude.

getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the attitude.

getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Compute the attitude corresponding to an orbital state.

getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the attitude.

getAttitude() - Method in class org.orekit.propagation.SpacecraftState

Get the attitude.

getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the type of actuator for attitude control.

getAttitudeBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get attitude state histories logical blocks.

getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the accuracy of attitude control.

getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the attitude control mode.

getAttitudeDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get attitude determination logical block.

getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.

getAttitudeInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get attitude interpolator.

getAttitudeInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get attitude interpolator.

getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the accuracy of attitude knowledge.

getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Get the Attitude Provider to use during maneuver.

getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the Attitude Provider to use during maneuver.

getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the attitude override used for the maneuver.

getAttitudePointingAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the overall accuracy of spacecraft to maintain attitude.

getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the attitude provider for this attitude ephemeris segment.

getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the attitude provider for this attitude ephemeris segment.

getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the attitude provider for this attitude ephemeris segment.

getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Get the attitude provider corresponding to this ephemeris, combining data from all segments.

getAttitudeProvider() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the attitude provider for this attitude ephemeris segment.

getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator

Get attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get attitude provider.

getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator

Get attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the attitude provider.

getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper

Get the attitude provider.

getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator

Get attitude provider.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the attitude-related rotation corresponding to an orbital state.

getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get attitude states.

getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the attitude states.

getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Get the type of the elements.

getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get attitude element set type.

getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the format of the data lines in the message.

getAttPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get identification number of previous attitude.

getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Compute the additional state from the additionalEquations.

getAugmentedInitialState(int) - Method in class org.orekit.utils.AbstractMultipleShooting

Compute the additional state from the additionalEquations.

getAugmentedInitialState(int) - Method in class org.orekit.utils.MultipleShooter

Compute the additional state from the additionalEquations.

getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication

Get the authentication type corresponding to a keyword.

getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the authentication method.

getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the authentication method.

getAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext

Method to get the auxiliary elements related to the ForceModelContext.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Get which derivatives of position are available in this state.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get which derivatives of angular data are available in this attitude ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get which derivatives of angular data are available in this attitude ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Get which derivatives of position are available in this state.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Get the derivatives available in the block.

getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get which derivatives of angular data are available in this attitude ephemeris segment.

getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get which derivatives of angular data are available in this attitude ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the available derivatives.

getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3Segment

Get which derivatives of position are available in this ephemeris segment.

getAvailableDerivatives() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getAvailableObservationPairs() - Method in class org.orekit.files.sinex.Dcb

Get all available observation code pairs for the satellite.

getAvailableSatelliteSystems() - Method in class org.orekit.files.sinex.DcbStation

Get the satellite systems available for the station.

getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the value of the 81 day average of F10.7 solar flux centered on current day.

getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters

Get the value of the 81 day average of F10.7 solar flux centered on current day.

getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get ax2oA = 2 * a / A .

getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get ax2oA = 2 * a / A .

getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.DefaultEncounterLOF

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAxisNormalToCollisionPlane(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAxisNormalToCollisionPlane() - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame

Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.

getAzimuth() - Method in class org.orekit.bodies.Loxodrome

Get the azimuth.

getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the azimuth angle.

getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the azimuth of a point with regards to the topocentric frame center point.

getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the azimuth of a point with regards to the topocentric frame center point.

getAzimuth() - Method in class org.orekit.utils.FieldTrackingCoordinates

Get the azimuth.

getAzimuth() - Method in class org.orekit.utils.TrackingCoordinates

Get the azimuth.

getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the azimuth rate.

getB() - Method in class org.orekit.bodies.Ellipse

Get the semi minor axis.

getB() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the second semi-axis.

getB() - Method in class org.orekit.bodies.FieldEllipse

Get the semi minor axis.

getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).

getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).

getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get B = sqrt(1 - e²).

getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get B = sqrt(1 - e²).

getB1() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the Jacobian matrix B1 (B1 = ∂εη/∂Y).

getB2(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the Jacobian matrix B2 (B2 = ∂Y/∂Y₀).

getB3(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the Jacobian matrix B3 (B3 = ∂Y/∂P).

getB4() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the Jacobian matrix B4 (B4 = ∂εη/∂c).

getBase() - Method in class org.orekit.utils.units.PowerTerm

Get the base term.

getBaseDate() - Method in class org.orekit.utils.DateDriver

Get the base (unshifted) date.

getBaseEquipment() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame

Get the quipment on which the frame is located.

getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation

Get the base frame associated with the station.

getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler

Get the base name of an input.

getBaseName(File) - Method in class org.orekit.data.FilesListCrawler

Get the base name of an input.

getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler

Get the base name of an input.

getBaseOffsets() - Method in class org.orekit.time.UTCScale

Get the base offsets.

getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get a time-independent provider containing base harmonics coefficients.

getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the base system state at given date, without compensation.

getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the base system state at given date, without compensation.

getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the base system state at given date, without compensation.

getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the base system state at given date, without compensation.

getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the base weight associated with the measurement

getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the base weight associated with the measurement

getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the base weight associated with the measurement

getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get state vector dimension without additional parameters.

getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get state vector dimension without additional parameters.

getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get B².

getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get B * B.

getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get B².

getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get B * B.

getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get B³.

getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get B³.

getBDGIMMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the ionosphere BDGIM messages.

getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales

getBDT() - Method in interface org.orekit.time.TimeScales

Get the BeiDou Navigation Satellite System time scale.

getBDT() - Static method in class org.orekit.time.TimeScalesFactory

Get the BeiDou Navigation Satellite System time scale.

getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the beacon at the center of the proximity zone.

getBeamDivergence() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the beam divergence.

getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the entry valid before transition.

getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the entry valid before transition.

getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults

Return the date of validity beginning of the detector.

getBeginTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get start time of actual maneuver, relative to t₀.

getBeidouCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the Beidou navigation messages contained in the file.

getBeidouCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the Beidou navigation messages for the given satellite Id.

getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales

getBeidouEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.

getBeidouLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the Beidou navigation messages contained in the file.

getBeidouLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the Beidou navigation messages for the given satellite Id.

getBeidouNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Get the Beidou navigation message corresponding to the current RTCM data.

getBeidouNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Get the Beidou navigation message corresponding to the current RTCM data.

getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Get the Beidou time of clock.

getBeta() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Get the β coefficients.

getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Returns the beta coefficients array.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get direction cosine β for central body.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get direction cosine β for central body.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine β for central body.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get direction cosine β for central body.

getBeta0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get β₀ field.

getBeta1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get β₁ field.

getBeta2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get β₂ field.

getBeta3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get β₃ field.

getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the E1/E5a broadcast group delay.

getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the the Broadcast Group Delay E5b/E1.

getBiasMode() - Method in class org.orekit.files.sinex.DcbDescription

Get the bias mode

getBinKurtosis() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the bin kurtosis from the mean of raw accepted time-of-flight values minus the trend function.

getBinPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the bin peak - mean value.

getBinRms() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the bin RMS from the mean of raw accepted time-of-flight values minus the trend function.

getBinSkew() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the bin skew from the mean of raw accepted time-of-flight values minus the trend function.

getBitRate() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the bit rate.

getBN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS B_n Word.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get B / A.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get B / A.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get B / A.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get B / A.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get B / A.

getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get B / A.

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get BoABpo = B / A(1 + B).

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get BoABpo = B / A(1 + B).

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get BoABpo = B / A(1 + B).

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get BoABpo = B / A(1 + B).

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get BoABpo = B / A(1 + B).

getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get BoABpo = B / A(1 + B).

getBody(String) - Method in interface org.orekit.bodies.CelestialBodies

Get a celestial body.

getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Get a celestial body.

getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

Get a celestial body.

getBody() - Method in class org.orekit.bodies.Loxodrome

Get the body on which the loxodrome is defined.

getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade

Get the celestial body.

getBody() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get central body.

getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector

Get the body on which the geographic zone is defined.

getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Get third body.

getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing

Get the body frame.

getBodyFrame() - Method in interface org.orekit.bodies.BodyShape

Get body frame related to body shape.

getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get body frame related to body shape.

getBodyFrame() - Method in class org.orekit.models.earth.Geoid

getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody

Get a body oriented, body centered frame.

getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector

Get the body shape.

getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector

Get the body shape.

getBolDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the total ΔV capability at beginning of life.

getBStar() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the SGP/SGP4 drag-like coefficient.

getBStar() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the ballistic coefficient.

getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the ballistic coefficient at tle date.

getBStar(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLE

Get the ballistic coefficient at a specific date.

getBTerm() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the SGP4-XP drag-like coefficient.

getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Get the builder associated with this scheduler.

getBuilder() - Method in interface org.orekit.estimation.measurements.generation.Scheduler

Get the builder associated with this scheduler.

getBuilders() - Method in class org.orekit.estimation.sequential.KalmanModel

Getter for the propagators.

getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the bus model name.

getC() - Method in class org.orekit.bodies.Ellipsoid

Get the length of the third semi-axis.

getC() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Get the cosine of the inclination.

getC() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Get the cosine of the inclination.

getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get C = 1 + p² + q².

getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get C = 1 + p² + q².

getC1cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the code phase bias correction for GLONASS ObservationType.C1C signal.

getC1pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the code phase bias correction for GLONASS ObservationType.C1P signal.

getC2cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the code phase bias correction for GLONASS ObservationType.C2C signal.

getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid

Get the fully normalized coefficient C_2n,0 for the normal gravity potential.

getC2pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the code phase bias correction for GLONASS ObservationType.C2P signal.

getCache() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Get underlying cache.

getCachedPositionAngleType() - Method in class org.orekit.orbits.CircularOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in class org.orekit.orbits.KeplerianOrbit

Get the cached PositionAngleType.

getCachedPositionAngleType() - Method in interface org.orekit.orbits.PositionAngleBased

Get the cached PositionAngleType.

getCachedSamples() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get cached samples.

getCachedSamples() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData

Get cached samples.

getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration

Get the number of slots to use in caches.

getCalendarWeek() - Method in class org.orekit.time.DateComponents

Get the calendar week number.

getCalibrationData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the calibration data for the data block.

getCalibrationDetailData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the calibration detail data for the data block.

getCalibrationDetailRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the CalibrationDetail record(s) related to the default system configuration id.

getCalibrationDetailRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the CalibrationDetail record(s) related to the given systemConfigurationId.

getCalibrationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the Calibration record(s) related to the default system configuration id.

getCalibrationRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the Calibration record(s) related to the given systemConfigurationId.

getCalibrationTargetRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get calibration target configuration record related to the systemRecord.

getCalibrationTargetRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the calibration target configuration record.

getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the number of calls to the differential equations computation method.

getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the number of calls to the differential equations computation method.

getCaOrPFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get C/A or P flag.

getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month

Get the capitalized three letters abbreviation.

getCapitalizedName() - Method in enum org.orekit.time.Month

Get the capitalized full name.

getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase

Get the carrier phase corresponding to a code.

getCarrierPhase() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the carrier phase.

getCartesian() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary Cartesian part.

getCartesian() - Method in class org.orekit.frames.Transform

Get the underlying elementary Cartesian part.

getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getCartesianPoint() - Method in class org.orekit.frames.TopocentricFrame

Get the surface point defining the origin of the frame.

getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable

Get the casters records.

getCatalogName() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the specification of satellite catalog source.

getCatalogName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the satellite catalog used for the object.

getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the specification of satellite catalog source.

getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales

getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):

getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).

getCCSDSName() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType

Get CCSDS compatible name.

getCCSDSType() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType

Get the CCSDS type if used by the SANA registry.

getCDAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the object’s Cd x A/m used to propagate the state vector and covariance to TCA.

getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.

getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,7] in covariance matrix (with index starting at 1).

getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,7] in covariance matrix (with index starting at 1).

getCdrgn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,3] in covariance matrix (with index starting at 1).

getCdrgndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,6] in covariance matrix (with index starting at 1).

getCdrgr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,1] in covariance matrix (with index starting at 1).

getCdrgrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,4] in covariance matrix (with index starting at 1).

getCdrgt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,2] in covariance matrix.

getCdrgtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [7,5] in covariance matrix (with index starting at 1).

getCdrgx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,1] in covariance matrix (with index starting at 1).

getCdrgxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,4] in covariance matrix (with index starting at 1).

getCdrgy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,2] in covariance matrix.

getCdrgydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,5] in covariance matrix (with index starting at 1).

getCdrgz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,3] in covariance matrix (with index starting at 1).

getCdrgzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [7,6] in covariance matrix (with index starting at 1).

getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the instance of CelestialBodies that is called by the static methods in this class.

getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext

getCelestialBodies() - Method in interface org.orekit.data.DataContext

Get a factory constructing CelestialBodys based on the auxiliary data in this context.

getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext

getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext

getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName

Get the celestial body corresponding to the CCSDS constant.

getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName

Get the celestial body corresponding to the CCSDS constant.

getCelestialSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the source and version of celestial body (e.g.

getCenter() - Method in class org.orekit.bodies.Ellipse

Get the center of the 2D ellipse.

getCenter() - Method in class org.orekit.bodies.FieldEllipse

Get the center of the 2D ellipse.

getCenter() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the body at origin of reference frame.

getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the origin of reference frame.

getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the origin of reference frame.

getCenter() - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get the direction of the FOV center, in spacecraft frame.

getCenter() - Method in class org.orekit.models.earth.tessellation.Tile

Get the center point.

getCenterMass() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the current center of mass of vehicle in body fixed coordinate system.

getCenterName() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame

Get the CCSDS center name.

getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse

Find the center of curvature (point on the evolute) at the nadir of a point.

getCenterOfCurvature(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse

Find the center of curvature (point on the evolute) at the nadir of a point.

getCenterOfMassCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the target center of mass.

getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader

Get the approximate center of mass to reflector offset.

getCenterOfPressure() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get the location of center of pressure.

getCenterOfPressureReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get reference frame for center of pressure.

getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Get the central body.

getCentralBodyRotation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get central body angular rotation rate.

getCentralDate(FieldAbsoluteDate<KK>, ImmutableFieldTimeStampedCache<T, KK>, double) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator

Get the central date to use to find neighbors while taking into account extrapolation threshold.

getCentralDate(FieldAbsoluteDate<KK>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get the central date to use to find neighbors while taking into account extrapolation threshold.

getCentralDate(AbsoluteDate, ImmutableTimeStampedCache<T>, double) - Static method in class org.orekit.time.AbstractTimeInterpolator

Get the central date to use to find neighbors while taking into account extrapolation threshold.

getCentralDate(AbsoluteDate) - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData

Get the central date to use to find neighbors while taking into account extrapolation threshold.

getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get Χ².

getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get Χ².

getChildren() - Method in class org.orekit.frames.OrphanFrame

Get all children of the instance.

getCic() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get Cic.

getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Cic parameter.

getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Cic parameter.

getCic() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.

getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients

Get the coefficient C_i^j.

getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients

Get the coefficient C_i^j.

getCircularEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the circular eccentricity vector.

getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the circular eccentricity vector.

getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the circular eccentricity vector derivative.

getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the circular eccentricity vector derivative.

getCircularEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the circular eccentricity vector.

getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the circular eccentricity vector.

getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the circular eccentricity vector derivative.

getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the circular eccentricity vector derivative.

getCIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the CIRF2000 reference frame.

getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the CIRF2000 reference frame.

getCis() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get Cis.

getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Cis parameter.

getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Cis parameter.

getCis() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.

getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the C_j coefficient.

getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the C_j coefficient.

getCk0() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the un-normalized zonal coefficients.

getCk0() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Get the un-normalized zonal coefficients.

getClassification() - Method in class org.orekit.files.ccsds.section.Header

Get the classification/caveats.

getClassification() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the classification.

getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the classification.

getClassificationType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the classification type.

getClkOffset() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the realtime-derived receiver clock offset.

getClockAcceleration() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock acceleration.

getClockAccelerationSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock acceleration sigma.

getClockAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the clock accuracy.

getClockBase() - Method in class org.orekit.files.sp3.SP3Header

Get the base for clock/clock-rate accuracy.

getClockBias() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock bias.

getClockBiasSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock bias sigma.

getClockConstraint() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Getter for the clock constraint.

getClockCorrection() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the clock correction value.

getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData

Get the clock correction data.

getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Get the clock correction data.

getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data

Get the clock correction data.

getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Get the clock correction data.

getClockCount() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get clock count.

getClockData() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for an unmodifiable map of clock data.

getClockDataTypes() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the different clock data types.

getClockDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station clock drift (which is related to measurement date).

getClockDriftDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite

Get the clock drift parameter driver.

getClockID() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Getter for the clock ID.

getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station clock (which is related to measurement date).

getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite

Get the clock offset parameter driver.

getClockRate() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get clock rate.

getClockRate() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock rate.

getClockRateAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the clock rate accuracy.

getClockRateChange() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the clock rate.

getClockRateSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock rate sigma.

getCndotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,3] in covariance matrix (with index starting at 1).

getCndotndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,6] in covariance matrix (with index starting at 1).

getCndotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,1] in covariance matrix (with index starting at 1).

getCndotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,4] in covariance matrix (with index starting at 1).

getCndott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,2] in covariance matrix (with index starting at 1).

getCndottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [6,5] in covariance matrix (with index starting at 1).

getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Get the cosine parameters of spherical harmonics expansion of degree N and order M.

getCnn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [3,3] in covariance matrix (with index starting at 1).

getCnr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [3,1] in covariance matrix (with index starting at 1).

getCnt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [3,2] in covariance matrix (with index starting at 1).

getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get co2AB = C / 2AB.

getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get Co2AB = C / 2AB.

getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get co2AB = C / 2AB.

getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get Co2AB = C / 2AB.

getCodeBias() - Method in class org.orekit.gnss.metric.messages.common.CodeBias

Get the code bias associated to the signal ID.

getCodeBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Get the code bias for a given signal ID.

getCodeBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Get the code biases for the current satellite.

getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Get the load deformation coefficients for ocean tides.

getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Get the coefficients for a given site.

getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients

Computes the coefficients involved in the contributions.

getCoefficients(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients

Computes the coefficients involved in the contributions.

getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms

Computes the coefficients involved in the contributions.

getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Computes the coefficients involved in the contributions.

getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients

Get the prefix for short period coefficients keys.

getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients

Get the prefix for short period coefficients keys.

getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms

Get the prefix for short period coefficients keys.

getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Get the prefix for short period coefficients keys.

getCollisionPercentile() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.

getCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.

getCollisionProbaMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the method that was used to calculate the collision probability.

getCombinationType() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData

Get the type of the combination of measurements used to build the instance.

getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Get the combined frequency of two measurements.

getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination

Get the combined frequency of two measurements.

getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination

Get the combined frequency of two measurements.

getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination

Get the combined frequency of two measurements.

getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination

Get the combined frequency of two measurements.

getCombinedMHzFrequency() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData

Get the value of the combined frequency in MHz.

getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils

Combine two transform providers.

getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get combined radius.

getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get combined radius.

getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Get the combined observed value of two measurements.

getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination

Get the combined observed value of two measurements.

getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination

Get the combined observed value of two measurements.

getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination

Get the combined observed value of two measurements.

getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination

Get the combined observed value of two measurements.

getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination

Get the combined observed value of two measurements.

getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination

Get the combined observed value of two measurements.

getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination

Get the combined observed value of two measurements.

getComment() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get comment for relative metadata.

getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the comments.

getComments() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the comments.

getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm

Get an unmodifiable view of the comments.

getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer

Get the comments.

getComments() - Method in class org.orekit.files.ilrs.CPF

Get the comments contained in the file.

getComments() - Method in class org.orekit.files.ilrs.CRD

Get the comments contained in the file.

getComments() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the comments.

getComments() - Method in class org.orekit.files.rinex.RinexFile

Get an unmodifiable view of the comments.

getComments() - Method in class org.orekit.files.sp3.SP3Header

Get the comments.

getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler

Get the complete name of a input.

getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler

Get the complete name of a input.

getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler

Get the complete name of a input.

getComponents() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Get the components (config ids) for system configuration.

getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components.

getComponents(int) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a local time.

getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a local time.

getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a time zone.

getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Split the instance into date/time components for a time zone.

getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components.

getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a local time.

getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a local time.

getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a time zone.

getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Split the instance into date/time components for a time zone.

getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the compression/encryption algorithm applied.

getConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get confidence metric.

getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader

getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider

Get the ITRF version configuration defined by a given file at specified date.

getConfigurationId() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

Get the configuration ID.

getConfigurationRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get configuration record corresponding to the configId.

getConfigurationRecordMap() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the configuration records map.

getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the system configuration records.

getConjunctionId() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Originator’s ID that uniquely identifies the conjunction to which the message refers.

getConsiderN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of consider parameters.

getConsiderParameters() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get description of consider parameters.

getConstantNormalizedProvider(int, int, AbsoluteDate) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the constant gravity field coefficients provider from the first supported file.

getConstantNormalizedProvider(int, int, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields

Get a constant gravity field normalized coefficients provider frozen at a given epoch.

getConstantNormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get a constant gravity field normalized coefficients provider frozen at a given epoch.

getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the constant gravity field coefficients provider from the first supported file.

getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields

Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.

getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.

getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the name of the constellation this space object belongs to.

getConstituents() - Method in class org.orekit.files.ccsds.ndm.Ndm

Get an unmodifiable view of the constituents.

getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting

Get the map of patch points components which are constrained.

getContentAsBoolean() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a boolean.

getContentAsDouble() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a double.

getContentAsEnum(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as an enum.

getContentAsEnumList(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a list of enum.

getContentAsFreeTextList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a list of free-text strings.

getContentAsInt() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as an integer.

getContentAsNormalizedList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a list of normalized strings.

getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry.

getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as an uppercase character.

getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a list of normalized and uppercased strings.

getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as normalized and uppercased.

getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the content of the entry as a vector.

getContext() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get the current context.

getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get the current context.

getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Get the control vector's cost type.

getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the control vector's cost type.

getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the control vector's cost type.

getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the control vector's cost type.

getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the control vector's cost type.

getControl3DVectorCostType() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the control vector's cost type.

getConventions() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the IERS conventions.

getConventions() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Get IERS conventions.

getConventions() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get IERS conventions.

getConventions() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Get IERS conventions.

getConventions() - Method in class org.orekit.frames.EOPHistory

Get the IERS conventions to which these EOP apply.

getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester

Get the conversion Jacobian between state parameters and parameters used for derivatives.

getConverter(ContextBinding) - Method in enum org.orekit.files.ccsds.definitions.TimeSystem

Get associated TimeConverter.

getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion

Find a converter between specified ITRF frames.

getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion

Find a converter between specified ITRF frames.

getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Get Cartesian coordinates as derivatives.

getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Get an unmodifiable view of the data points.

getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in class org.orekit.files.sp3.SP3Segment

Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

getCoordinates() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3Header

Returns the coordinate system of the entries in this orbit file.

getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the estimated measurement.

getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the estimated measurement.

getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the estimated measurement.

getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the estimated measurement.

getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the estimated measurement.

getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the corrected spacecraft states.

getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the corrected spacecraft states.

getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the corrected spacecraft states.

getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the corrected spacecraft states.

getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the corrected spacecraft states.

getCorrection() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection

Get the Phase Shift Corrections.

getCorrection() - Method in class org.orekit.files.rinex.observation.ScaleFactorCorrection

Get the Scale Factor.

getCorrectionAberrationDiurnal() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the diurnal aberration correction.

getCorrectionAberrationYearly() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the yearly aberration correction.

getCorrectionAngle1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionAngle1.

getCorrectionAngle2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionAngle2.

getCorrectionDoppler() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionDoppler.

getCorrectionMagnitude() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the magnitude correction.

getCorrectionRange(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the raw correction for range in meters.

getCorrectionRcs() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the radar cross section correction.

getCorrectionReceive() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionReceive.

getCorrectionsApplied() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionApplied.

getCorrectionTransmit() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the correctionTransmit.

getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position

Get the correlation coefficients matrix.

getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV

Get the correlation coefficients matrix.

getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get COSPAR ID.

getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the evaluations counter.

getCountry() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the name of the country where the space object owner is based.

getCountry() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the country.

getCountry() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the country.

getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getCovariance(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Get the covariance at given date.

getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the covariance matrix logical block.

getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the covariance matrix logical block.

getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get covariance logical blocks.

getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get covariance logical blocks.

getCovarianceInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris

Get covariance interpolator.

getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Get an unmodifiable view of Covariance Matrices.

getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get an unmodifiable view of Covariance Matrices.

getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position

Get the covariance matrix.

getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV

Get the covariance matrix.

getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Get the Position/Velocity covariance matrix.

getCovarianceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the method name used to calculate covariance during OD.

getCovarianceOrbitType() - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the orbit type in which the covariance matrix is expressed.

getCovariances() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory

Get the covariances.

getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory

Get the covariances.

getCovarianceSource() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the source of the covariance data.

getCovarianceType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get type of attitude error state.

getCovBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get basis of this covariance time history data.

getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get basis of this covariance time history data.

getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get identification number of the orbit determination or simulation upon which this covariance is based.

getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get identification number of the orbit determination or simulation upon which this covariance is based.

getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the measure of the confidence in the covariance errors matching reality.

getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get the measure of confidence in covariance error matching reality.

getCovConfidenceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the method used for the calculation of COV_CONFIDENCE.

getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get epoch of the covariance reference frame.

getCovID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get covariance identification number.

getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get covariance identification number.

getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get identification number of next covariance.

getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get covariance ordering.

getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get identification number of previous covariance.

getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get identification number of previous covariance.

getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get reference frame of the covariance.

getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get reference frame of the covariance.

getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get the maximum scale factor to apply to achieve realism.

getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get the minimum scale factor to apply to achieve realism.

getCovType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Get covariance element set type.

getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get covariance element set type.

getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Get covariance element set units.

getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion

Get the considered CR3BP system.

getCRAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the object’s Cr x A/m used to propagate the state vector and covariance to TCA.

getCrc() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get Crc.

getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Crc parameter.

getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Crc parameter.

getCrc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.

getCrdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [4, 3] in covariance matrix (with index starting at 1) .

getCrdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [4,1] in covariance matrix (with index starting at 1).

getCrdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [4, 4] in covariance matrix (with index starting at 1).

getCrdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [4,2] in covariance matrix (with index starting at 1).

getCreationDate() - Method in class org.orekit.files.ccsds.section.Header

Get the message creation date and time in UTC.

getCreationDate() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the creation date.

getCreationDate() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the creation date.

getCreationDate() - Method in class org.orekit.files.sinex.SinexLoader

Get the creation date of the parsed SINEX file.

getCreationDateComponents() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the creation date of the file as a string.

getCreationDateString() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the creation date of the file as a string.

getCreationTimeString() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the creation time of the file as a string.

getCreationTimeZone() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the creation time zone of the file as a string.

getCreationTimeZoneString() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the creation time zone of the file as a string.

getCrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [1,1] in covariance matrix (with index starting at 1).

getCrs() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Crs.

getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Crs parameter.

getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Crs parameter.

getCrs() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.

getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header

Get the Global/Regional CRS Indicator.

getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header

Get the Global/Regional CRS Indicator.

getcScaleFactor() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the (median) suggested covariance scale factor.

getcScaleFactorMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the maximum suggested covariance scale factor.

getcScaleFactorMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the minimum suggested covariance scale factor.

getCsig3eigvec3() - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance

Get the Sigma/Eigenvectors Covariance data.

getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,7] in covariance matrix (with index starting at 1).

getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,7] in covariance matrix (with index starting at 1).

getCsrpn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,3] in covariance matrix (with index starting at 1).

getCsrpndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,6] in covariance matrix (with index starting at 1).

getCsrpr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,1] in covariance matrix (with index starting at 1).

getCsrprdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,4] in covariance matrix (with index starting at 1).

getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,8] in covariance matrix (with index starting at 1).

getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,8] in covariance matrix (with index starting at 1).

getCsrpt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,2] in covariance matrix (with index starting at 1).

getCsrptdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [8,5] in covariance matrix (with index starting at 1).

getCsrpx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,1] in covariance matrix (with index starting at 1).

getCsrpxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,4] in covariance matrix (with index starting at 1).

getCsrpy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,2] in covariance matrix (with index starting at 1).

getCsrpydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,5] in covariance matrix (with index starting at 1).

getCsrpz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,3] in covariance matrix (with index starting at 1).

getCsrpzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [8,6] in covariance matrix (with index starting at 1).

getCtdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [5,3] in covariance matrix (with index starting at 1).

getCtdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [5, 1] in covariance matrix (with index starting at 1).

getCtdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [5,4] in covariance matrix (with index starting at 1).

getCtdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [5,2] in covariance matrix (with index starting at 1).

getCtdottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [5,5] in covariance matrix (with index starting at 1).

getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,7] in covariance matrix (with index starting at 1).

getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,7] in covariance matrix (with index starting at 1).

getCthrn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,3] in covariance matrix (with index starting at 1).

getCthrndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,6] in covariance matrix (with index starting at 1).

getCthrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,1] in covariance matrix (with index starting at 1).

getCthrrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,4] in covariance matrix (with index starting at 1).

getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,8] in covariance matrix (with index starting at 1).

getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,8] in covariance matrix (with index starting at 1).

getCthrt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,2] in covariance matrix (with index starting at 1).

getCthrtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,5] in covariance matrix (with index starting at 1).

getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [9,9] in covariance matrix (with index starting at 1).

getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,9] in covariance matrix (with index starting at 1).

getCthrx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,1] in covariance matrix (with index starting at 1).

getCthrxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,4] in covariance matrix (with index starting at 1).

getCthry() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,2] in covariance matrix (with index starting at 1).

getCthrydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,5] in covariance matrix (with index starting at 1).

getCthrz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,3] in covariance matrix (with index starting at 1).

getCthrzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [9,6] in covariance matrix (with index starting at 1).

getCtr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [2,1] in covariance matrix (with index starting at 1).

getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the centered 81-day arithmetic average of F10.7 (adjusted).

getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the centered 81-day arithmetic average of F10.7 (observed).

getCtt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the object [2,2] in covariance matrix (with index starting at 1).

getCuc() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Cuc.

getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Cuc parameter.

getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Cuc parameter.

getCuc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.

getCurrent() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Get the current processing state.

getCurrent() - Method in class org.orekit.utils.units.Unit

Get the current exponent.

getCurrentDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the current date.

getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the current date.

getCurrentDate() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the current date.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the current measurement number.

getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the current measurement number.

getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the current measurement number.

getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at previous grid point date.

getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at current grid point date.

getCus() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Cus.

getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the Cus parameter.

getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the Cus parameter.

getCus() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.

getCxdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [4,1] in covariance matrix (with index starting at 1).

getCxdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [4, 4] in covariance matrix (with index starting at 1).

getCxdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [4,2] in covariance matrix (with index starting at 1).

getCxdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [4, 3] in covariance matrix (with index starting at 1) .

getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get (C * χ) / ( 2 * n² * a² ).

getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get (C * χ) / ( 2 * n² * a² ).

getCxx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [1,1] in covariance matrix (with index starting at 1).

getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the duration of the GNSS cycle in seconds.

getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the duration of the GNSS cycle in seconds.

getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the duration of the GNSS cycle in seconds.

getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults

Get the cycle slip Map with contains the results.

getCydotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [5, 1] in covariance matrix (with index starting at 1).

getCydotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [5,4] in covariance matrix (with index starting at 1).

getCydoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [5,2] in covariance matrix (with index starting at 1).

getCydotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [5,5] in covariance matrix (with index starting at 1).

getCydotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [5,3] in covariance matrix (with index starting at 1).

getCyx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [2,1] in covariance matrix (with index starting at 1).

getCyy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [2,2] in covariance matrix (with index starting at 1).

getCzdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,1] in covariance matrix (with index starting at 1).

getCzdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,4] in covariance matrix (with index starting at 1).

getCzdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,2] in covariance matrix (with index starting at 1).

getCzdotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,5] in covariance matrix (with index starting at 1).

getCzdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,3] in covariance matrix (with index starting at 1).

getCzdotzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [6,6] in covariance matrix (with index starting at 1).

getCzx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [3,1] in covariance matrix (with index starting at 1).

getCzy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [3,2] in covariance matrix (with index starting at 1).

getCzz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the object [3,3] in covariance matrix (with index starting at 1).

getD() - Method in class org.orekit.data.DelaunayArguments

Get the mean elongation of the Moon from the Sun.

getD() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean elongation of the Moon from the Sun.

getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the value of the daily F10.7 solar flux for previous day.

getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the daily F10.7 solar flux for previous day.

getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters

Get the value of the daily F10.7 solar flux for previous day.

getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the dark count.

getData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Get the data from the single segment.

getData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm

Get the file data.

getData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Get the data from the single segment.

getData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Get the file data.

getData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get the file data.

getData() - Method in class org.orekit.files.ccsds.section.Segment

Get the segment data.

getData() - Method in class org.orekit.files.ilrs.CRD.Meteo

Get an unmodifiable view of the tabulated meteorological data.

getData() - Method in class org.orekit.gnss.metric.messages.rtcm.RtcmMessage

Get the data.

getData() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage

Get the data.

getData() - Method in class org.orekit.utils.DoubleArrayDictionary

Get an unmodifiable view of the dictionary entries.

getData() - Method in class org.orekit.utils.FieldArrayDictionary

Get an unmodifiable view of the dictionary entries.

getData() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the data valid during this time span.

getDataBlocks() - Method in class org.orekit.files.ilrs.CRD

Get the data blocks contain in the file.

getDataContext() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the data context.

getDataContext() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Get the data context.

getDataContext() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get the data context used for getting frames, time scales, and celestial bodies.

getDataContext() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Get the data context used for getting frames, time scales, and celestial bodies.

getDataFormat(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat

Get the message type corresponding to a keyword.

getDataId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45

Get data ID.

getDataMap() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage

Get the all data parsed in the RTCM correction message.

getDataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get the file data.

getDataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get the file data.

getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader

Get the data provider manager.

getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext

Get the provider of auxiliary data for this data context.

getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop

Get the data providers manager for this instance.

getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the dataQuality.

getDataQulityIndicator() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get the data quality assessment indicator 0=undefined or no comment 1=clear, easily filtered data, with little or no noise 2=clear data with some noise; filtering is slightly compromised by noise level 3=clear data with a significant amount of noise, or weak data with little noise.

getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader

Get the flag indicating the data release.

getDataSet() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet

Get the original observation data set used to compute the smoothed observation data.

getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Get the data set.

getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader

Getter for the data set.

getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Getter for the data set.

getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader

getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Gets the data set.

getDataSource() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the the data source.

getDataStreams() - Method in class org.orekit.gnss.metric.ntrip.SourceTable

Get the data streams records.

getDataType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType

Get the data type for the given indicator.

getDataType() - Method in class org.orekit.files.ilrs.CRDHeader

Get the data type.

getDataType() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the clock data type.

getDataTypes() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get observation data types used.

getDataTypes() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the data types in the data section.

getDataUsed() - Method in class org.orekit.files.sp3.SP3Header

Returns the data used indicator from the SP3 file.

getDate() - Method in class org.orekit.attitudes.Attitude

Get the date of attitude parameters.

getDate() - Method in class org.orekit.attitudes.FieldAttitude

Get the date of attitude parameters.

getDate() - Method in class org.orekit.data.DelaunayArguments

Get the date.

getDate() - Method in class org.orekit.data.FieldDelaunayArguments

Get the date.

getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the date.

getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the date.

getDate() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Get the date.

getDate() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get the date.

getDate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the date.

getDate() - Method in class org.orekit.files.ilrs.CRD.Calibration

getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get the date.

getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get the date.

getDate() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

getDate() - Method in class org.orekit.files.rinex.observation.ObservationDataSet

Get the date.

getDate() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the date.

getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the date of the maneuver.

getDate() - Method in class org.orekit.frames.EOPEntry

Get the date.

getDate() - Method in class org.orekit.frames.FieldTransform

Get the date.

getDate() - Method in class org.orekit.frames.Transform

Get the date.

getDate() - Method in class org.orekit.gnss.DOP

Gets the calculation date of the DOP.

getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity

getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters

getDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters

getDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

getDate() - Method in class org.orekit.orbits.FieldOrbit

Get the date of orbital parameters.

getDate() - Method in class org.orekit.orbits.Orbit

Get the date of orbital parameters.

getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the reference date of the ephemeris.

getDate() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the ephemeris reference date.

getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getDate() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the TLE current date.

getDate() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the TLE current date.

getDate() - Method in class org.orekit.propagation.events.DateDetector

Get the current event date according to the propagator.

getDate() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the date.

getDate() - Method in class org.orekit.propagation.events.FieldDateDetector

Get the current event date according to the propagator.

getDate() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the date.

getDate() - Method in class org.orekit.propagation.FieldStateCovariance

Get the date.

getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the date of the orbit.

getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the date of the orbit.

getDate() - Method in class org.orekit.propagation.SpacecraftState

Get the date.

getDate() - Method in class org.orekit.propagation.StateCovariance

Get the date.

getDate() - Method in class org.orekit.time.AbsoluteDate

Get the date.

getDate() - Method in class org.orekit.time.DateTimeComponents

Get the date component.

getDate() - Method in class org.orekit.time.FieldAbsoluteDate

Get the date.

getDate() - Method in interface org.orekit.time.FieldTimeStamped

Get the date.

getDate() - Method in class org.orekit.time.FieldTimeStampedPair

Get the date.

getDate() - Method in class org.orekit.time.GLONASSDate

getDate() - Method in class org.orekit.time.GNSSDate

Get the date.

getDate() - Method in interface org.orekit.time.TimeStamped

Get the date.

getDate() - Method in class org.orekit.time.TimeStampedDouble

Get the date.

getDate() - Method in class org.orekit.time.TimeStampedField

Get the date.

getDate() - Method in class org.orekit.time.TimeStampedPair

Get the date.

getDate() - Method in class org.orekit.time.UTCTAIOffset

Get the date of the start of the leap.

getDate() - Method in class org.orekit.utils.DateDriver

Get the shifted date.

getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition

Get the transition absolute date.

getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the transition date.

getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get the date.

getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates

Get the date.

getDateAndTime() - Method in class org.orekit.files.ilrs.CRDHeader

Get the date and time as the string value.

getDates() - Method in class org.orekit.propagation.events.DateDetector

Get all event dates currently managed, in chronological order.

getDates() - Method in class org.orekit.propagation.events.FieldDateDetector

Get all event field dates currently managed, in chronological order.

getDay() - Method in class org.orekit.time.DateComponents

Get the day.

getDayFraction() - Method in class org.orekit.files.sp3.SP3Header

Returns the day fraction for this SP3 file.

getDayNumber() - Method in class org.orekit.time.GLONASSDate

Get the number of the current day in a four year interval.

getDayOfWeek() - Method in class org.orekit.time.DateComponents

Get the day of week.

getDayOfYear() - Method in class org.orekit.time.DateComponents

Get the day number in year.

getDcb(String, String, AbsoluteDate) - Method in class org.orekit.files.sinex.Dcb

Get the value of the Differential Code Bias for a given observation pair and a at a given date.

getDcb(ObservationType, ObservationType, AbsoluteDate) - Method in class org.orekit.files.sinex.Dcb

Get the value of the Differential Code Bias for a given observation pair and a at a given date.

getDcbData() - Method in class org.orekit.files.sinex.DcbSatellite

Get the DCB data for the current satellite.

getDcbData(SatelliteSystem) - Method in class org.orekit.files.sinex.DcbStation

Get the DCB data for a given satellite system.

getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get spacecraft body frame in which OrbitManeuverHistoryMetadata.getDcBodyTrigger() is specified.

getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get direction in body frame for triggering duty cycle.

getDcbSatellite(String) - Method in class org.orekit.files.sinex.SinexLoader

Get the DCB data for a given satellite identified by its PRN.

getDcbStation(String) - Method in class org.orekit.files.sinex.SinexLoader

Get the DCB data for a given station.

getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the start time of initial duty cycle-based maneuver execution.

getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the end time of final duty cycle-based maneuver execution.

getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dC_j / dh coefficient.

getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the dC_j / dh coefficient.

getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dC_j / dk coefficient.

getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the dC_j / dk coefficient.

getDcMaxCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the maximum number of "ON" duty cycles.

getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the minimum number of "ON" duty cycles.

getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get phase angle of pulse start.

getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get phase angle of pulse stop.

getDcpSensitivityVectorPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the DCP sensitivity vector (position errors at TCA).

getDcpSensitivityVectorVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the DCP sensitivity vector (velocity errors at TCA).

getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get reference direction for triggering duty cycle.

getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get duty cycle thrust reference time.

getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get duty cycle pulse "ON" duration.

getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get duty cycle elapsed time between start of a pulse and start of next pulse.

getDcType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get type of duty cycle.

getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the end time of duty cycle-based maneuver window.

getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the start time of duty cycle-based maneuver window.

getDdEps() - Method in class org.orekit.frames.EOPEntry

Get the correction for nutation in obliquity δΔε.

getDdim() - Method in class org.orekit.bodies.CR3BPSystem

Get the CR3BP distance between the two bodies.

getDDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean elongation of the Moon from the Sun time derivative.

getDDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean elongation of the Moon from the Sun time derivative.

getDdPsi() - Method in class org.orekit.frames.EOPEntry

Get the correction for nutation in longitude δΔΨ.

getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField

Utility function to get a decimal year for a given day.

getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the declination of the magnetic field in radians.

getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the reference decorrelated ambiguities.

getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter

Get the decreasing events time shift.

getDefault() - Static method in interface org.orekit.data.DataContext

Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.

getDefaultInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Get the default interpolation degree.

getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator

Get a default law using the given frames.

getDefaultMass() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Get the default mass.

getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.

getDefaultTleGenerationAlgorithm(TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the default TLE generation algorithm.

getDefaultVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get the default format version.

getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get the default format version.

getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA

Get the default yaw rate for a satellite.

getDefinedTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the time system defined by this message.

getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide

Get the multipliers for Delaunay arguments (l, l', F, D, Ω).

getDelayShift() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the calibration delay shift.

getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection

Get the delta clock C0.

getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection

Get the delta clock C1.

getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection

Get the delta clock C2.

getDeltai() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get Δi.

getDeltaI() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the correction to the mean value of inclination.

getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Get mass change during maneuver.

getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get mass change.

getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Get mass change during maneuver (value is < 0).

getDeltaN() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Δn.

getDeltaN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the delta of satellite mean motion.

getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for change rate in Δn₀.

getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for change rate in Δn₀.

getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the along-track orbit correction for broadcast ephemeris.

getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the cross-track orbit correction for broadcast ephemeris.

getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the radial orbit correction for broadcast ephemeris.

getDeltaT() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the correction to the mean value of Draconian period.

getDeltaTDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the rate of change of Draconian period.

getDeltaTLs() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get ΔtLS field.

getDeltaTLsf() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get ΔtLSF field.

getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the deltaTauN value.

getDeltaVSat() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Get the velocity increment in satellite frame.

getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the velocity increment in satellite frame.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere

Get the local density.

getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000

Get the local density with initial entries.

getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000

Get the local density with initial entries.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000

Get the local density.

getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the local density.

getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the local density at some position.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the local density at some position.

getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008

Get the local density with initial entries.

getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008

Get the local density with initial entries.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008

Get the local density.

getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput

Get one of the stored densities.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere

Get the local density.

getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere

getDensityForecastUncertainty() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the atmospheric density forecast error.

getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ angular off-nominal deployment vector direction.

getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get velocity increment of deployed "child" object.

getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.

getDeployDvRatio() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get ratio of child-to-host ΔV vectors.

getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ percent error on deployment ΔV magnitude.

getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get identifier of resulting "child" object deployed from this host.

getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get decrement in host mass as a result of deployment.

getDepth() - Method in class org.orekit.frames.Frame

Get the depth of the frame.

getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction

Get Γ function derivative.

getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function derivative.

getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear

Compute the value of the derivative dK_j^{-n-1, s} / de².

getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear

Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.

getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear

Get the dK₀^-n-1,s / dΧ coefficient derivative.

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the derivative dK_j^{-n-1, s} / de².

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Get the dK₀^-n-1,s / dΧ coefficient derivative.

getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get all the drivers with set derivatives.

getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch

Compute derivatives of the state w.r.t epoch.

getDescription() - Method in class org.orekit.files.sinex.DcbSatellite

Get the data contained in "DCB/DESCRIPTION" block of the Sinex file.

getDescription() - Method in class org.orekit.files.sinex.DcbStation

Get the data contained in "DCB/DESCRIPTION" block of the Sinex file.

getDesignator() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver

Getter for the designator.

getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the destination ITRF.

getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter

Get the destination ITRF.

getDetector() - Method in class org.orekit.propagation.events.AdapterDetector

Get the wrapped detector.

getDetector() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Get the wrapped raw detector.

getDetector() - Method in class org.orekit.propagation.events.EventShifter

Get the detector for the raw unshifted event.

getDetector() - Method in class org.orekit.propagation.events.EventSlopeFilter

Get the wrapped raw detector.

getDetector() - Method in class org.orekit.propagation.events.FieldAdapterDetector

Get the wrapped detector.

getDetector() - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Get the wrapped raw detector.

getDetector() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter

Get the wrapped raw detector.

getDetector() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event

Get the detector.

getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Get the detector.

getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the detector channel.

getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get the detector channel.

getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the detector channel.

getDetectorId() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the detector configuration ID.

getDetectorRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the detector configuration record.

getDetectorRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get detector configuration record related to the systemRecord.

getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector

Get the list of original detectors.

getDetectors() - Method in class org.orekit.propagation.events.FieldBooleanDetector

Get the list of original detectors.

getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the detector type.

getDeterminationMethod() - Method in class org.orekit.files.sinex.DcbDescription

Get the determination mode used to generate the bias results.

getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dG_js / dα coefficient.

getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dα coefficient.

getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dG_js / dβ coefficient.

getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dβ coefficient.

getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dG_js / dh coefficient.

getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dh coefficient.

getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dG_js / dk coefficient.

getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dk coefficient.

getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dG_ms^j / d_α coefficient.

getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_α coefficient.

getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dG_ms^j / d_β coefficient.

getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_β coefficient.

getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dG_ms^j / d_h coefficient.

getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_h coefficient.

getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dG_ms^j / d_k coefficient.

getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_k coefficient.

getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dH_js / dα coefficient.

getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dα coefficient.

getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dH_js / dβ coefficient.

getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dβ coefficient.

getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dH_js / dh coefficient.

getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dh coefficient.

getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dH_js / dk coefficient.

getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dk coefficient.

getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dH_ms^j / d_α coefficient.

getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_α coefficient.

getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dH_ms^j / d_β coefficient.

getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_β coefficient.

getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dH_ms^j / d_h coefficient.

getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_h coefficient.

getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the dH_ms^j / d_k coefficient.

getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_k coefficient.

getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get a reference to the diagonal matrix of the decomposition.

getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dI_js / dα coefficient.

getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dα coefficient.

getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dI_js / dβ coefficient.

getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dβ coefficient.

getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dI_js / dh coefficient.

getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dh coefficient.

getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dI_js / dk coefficient.

getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dk coefficient.

getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the dimension of the measurement.

getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the dimension of the measurement.

getDimension() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Get the dimension of the generated column.

getDimension() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider

Get the dimension of the generated derivative.

getDimension() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider

Get the dimension of the generated derivative.

getDimension() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations

Get the dimension of the generated derivative.

getDimension() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Get the dimension of the generated derivative.

getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the direction.

getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the direction.

getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust direction in S/C frame.

getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust direction in S/C frame.

getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the thrust direction in spacecraft frame.

getDirectionFlag() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).

getDiscontinuityCounter() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias

Get the signal phase discontinuity counter.

getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation

Get the displacement models.

getDistance() - Method in class org.orekit.bodies.LoxodromeArc

Compute the distance of the arc along the surface of the ellipsoid.

getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dJ_js / dα coefficient.

getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dα coefficient.

getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dJ_js / dβ coefficient.

getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dβ coefficient.

getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dJ_js / dh coefficient.

getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dh coefficient.

getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the dJ_js / dk coefficient.

getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dk coefficient.

getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients

Get the value of dL_n^s / dγ (γ).

getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of dL_n^s / dγ (γ).

getDn() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get DN field.

getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value D_n^l(Χ).

getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value D_n^l(Χ).

getDockedWith() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the other space objects this object is docked to.

getDoi() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the Digital Object Information.

getDomes() - Method in class org.orekit.files.sinex.Station

Get the site DOMES number.

getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the Doodson number for the wave.

getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide

Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).

getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide

Get the Doodson number.

getDopplerCountBias() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Get the Doppler count bias.

getDopplerCountScale() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Get the Doppler count scale.

getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the velocity of along-track orbit correction for broadcast ephemeris.

getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the velocity of cross-track orbit correction for broadcast ephemeris.

getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection

Get the velocity of radial orbit correction for broadcast ephemeris.

getDrag() - Method in class org.orekit.forces.Panel

Get drag coefficient.

getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get drag force.

getDragArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the drag area.

getDragCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the drag coefficient.

getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get the drag coefficient.

getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the nominal drag coefficient.

getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.

getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the drivers for supported parameters.

getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive

Get the drivers for supported parameters.

getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag

Get the drivers for supported parameters.

getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the DragSensitive model valid at a date.

getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the DragSensitive TimeSpanMap.Span containing a specified date.

getDragUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the drag coefficient 1σ uncertainty.

getDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier

Get the drivers for this modifier.

getDrivers(double, Orbit, PositionAngleType) - Method in enum org.orekit.orbits.OrbitType

Get parameters drivers initialized from a reference orbit.

getDrivers() - Method in class org.orekit.utils.ParameterDriversList

Get delegating drivers for all parameters.

getDryMass() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get the mass without propellant.

getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the mass without propellant.

getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Compute density and its derivatives.

getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dh coefficient.

getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the dS_j / dh coefficient.

getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dk coefficient.

getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the dS_j / dk coefficient.

getDSTDTC() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters

Get the DSTDTC parameter.

getDSTDTC(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the temperature change computed from Dst index.

getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the temperature change computed from Dst index.

getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get duration.

getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Get duration (value is 0 for impulsive maneuver).

getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get duration.

getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Get duration (value is 0 for impulsive maneuver).

getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the duration of the maneuver (s).

getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Get the duration of the maneuver (s).

getDurationDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Get the driver for duration.

getDurationDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Get the driver for duration.

getDut1() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the ΔUT₁.

getDUT1() - Method in class org.orekit.frames.EOPFittedModel

Get the fitted secular and harmonics model for DUT1/LOD.

getDut1Dot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the ΔUT₁ first derivative.

getDut1DotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the ΔUT₁ second derivative.

getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get velocity increment.

getDV() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Get velocity increment.

getDvDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ angular off-nominal ΔV direction.

getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ percent error on ΔV magnitude.

getDx() - Method in class org.orekit.frames.EOPEntry

Get the correction for Celestial Intermediate Pole (CIP) coordinates.

getDx() - Method in class org.orekit.frames.EOPFittedModel

Get the fitted secular and harmonics model for nutation x component.

getDy() - Method in class org.orekit.frames.EOPEntry

Get the correction for Celestial Intermediate Pole (CIP) coordinates.

getDy() - Method in class org.orekit.frames.EOPFittedModel

Get the fitted secular and harmonics model for nutation y component.

getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit eccentricity.

getE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get e.

getE() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get eccentricity.

getE() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.Orbit

Get the eccentricity.

getE() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the eccentricity.

getE() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the Eccentricity.

getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Eccentricity.

getE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the eccentricity.

getE() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the eccentricity.

getE() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the eccentricity.

getE() - Method in class org.orekit.propagation.SpacecraftState

Get the eccentricity.

getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get ecc².

getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get ecc².

getEarliest() - Method in interface org.orekit.utils.FieldTimeStampedCache

Get the earliest entry in this cache.

getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the earliest entry in this cache.

getEarliest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get the earliest entry in this cache.

getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get the earliest entry in this cache.

getEarliest() - Method in interface org.orekit.utils.TimeStampedCache

Get the earliest entry in this cache.

getEarth() - Method in interface org.orekit.bodies.CelestialBodies

Get the Earth singleton body.

getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Earth singleton body.

getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getEarth() - Method in class org.orekit.forces.gravity.DeSitterRelativity

Get the Earth model used to compute De Sitter effect.

getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies

Get the Earth-Moon barycenter singleton bodies pair.

getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Earth-Moon barycenter singleton bodies pair.

getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getEarthMoonBarycenterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants

Get the Earth-Moon barycenter semi-major axis.

getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory

Get the Earth-Moon CR3BP singleton bodies pair.

getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the raw Earth Orientation Angle.

getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the raw Earth Orientation Angle.

getEarthOrientationParameters() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the Earth orientation parameters.

getEarthTides() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get Enum YesNoUnknown that indicates if Earth and ocean tides are taken into account or not.

getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the east of point, expressed in parent shape frame.

getEast() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the east of point, expressed in parent shape frame.

getEast() - Method in class org.orekit.frames.TopocentricFrame

Get the east direction of topocentric frame, expressed in parent shape frame.

getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along East axis.

getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentricity.

getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the eccentricity.

getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric anomaly.

getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric anomaly.

getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric anomaly derivative.

getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric anomaly derivative.

getEccentricities() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the eccentricities of antenna center.

getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Get the station antenna eccentricities for the given epoch.

getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna

Get the phase center eccentricities.

getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern

Get the phase center eccentricities.

getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station

Get the TimeSpanMap of site antenna eccentricities.

getEccentricity() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the first eccentricity of the ellipsoid: e = sqrt(f * (2.0 - f)).

getEccentricitySquared() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the first eccentricity squared of the ellipsoid: e^2 = f * (2.0 - f).

getEccRefSystem() - Method in class org.orekit.files.sinex.Station

Get the reference system used to define the eccentricity vector (local or cartesian).

getEccRefSystem(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem

Get the eccentricity reference system corresponding to the given value.

getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.

getECEF() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the Interface Control Document.

getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.

getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Gets the Earth Centered Inertial frame used to propagate the orbit.

getECI() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Gets the Earth Centered Inertial frame used to propagate the orbit.

getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Gets the Earth Centered Inertial frame used to propagate the orbit.

getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames

getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames

Get the ecliptic frame.

getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the ecliptic frame.

getEDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentricity derivative.

getEDot() - Method in class org.orekit.orbits.Orbit

Get the eccentricity derivative.

getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the differential effects.

getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Get the value of an element.

getElementNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the element number.

getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the element number.

getElements() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Get attitude elements.

getElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Get trajectory elements.

getElementSetNumber() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the element set number for this satellite.

getElevation() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the elevation angle.

getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the elevation of a point with regards to the local point.

getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the elevation of a point with regards to the local point.

getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Get the elevation value.

getElevation(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector

Get the elevation value.

getElevation(double) - Method in class org.orekit.utils.ElevationMask

Get the interpolated elevation for a given azimuth according to the mask.

getElevation() - Method in class org.orekit.utils.FieldTrackingCoordinates

Get the elevation.

getElevation() - Method in class org.orekit.utils.TrackingCoordinates

Get the elevation.

getElevationMask() - Method in class org.orekit.gnss.DOPComputer

Get the elevation mask.

getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured elevation mask.

getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured elevation mask.

getElevationRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the elevation rate.

getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape

Get the underlying ellipsoid model that defines latitude and longitude.

getEllipsoid() - Method in class org.orekit.models.earth.Geoid

getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid

getEME2000() - Method in class org.orekit.frames.AbstractFrames

getEME2000() - Method in interface org.orekit.frames.Frames

Get the unique EME2000 frame.

getEME2000() - Static method in class org.orekit.frames.FramesFactory

Get the unique EME2000 frame.

getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRange

Get the emitter ground station.

getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate

Get the emitter ground station.

getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS E_n Word.

getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get encounter local orbital frame.

getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get encounter local orbital frame.

getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the end of the measurements time span.

getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the end of this time span.

getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults

Return the end date at the given frequency.

getEndDate() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Getter for the validity period end date.

getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the end date.

getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Get the end date.

getEndDate() - Method in class org.orekit.frames.EOPHistory

Get the date of the last available Earth Orientation Parameters.

getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the ending epoch (UTC).

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Get the endpoints (i.e.

getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the endpoints (i.e.

getEndTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get end time of actual maneuver, relative to t₀.

getEndTransition() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the transition at end of this time span.

getEntries() - Method in class org.orekit.frames.EOPHistory

Get a non-modifiable view of the EOP entries.

getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the total number of entries cached.

getEntry(String) - Method in class org.orekit.utils.DoubleArrayDictionary

Get a complete entry.

getEntry(String) - Method in class org.orekit.utils.FieldArrayDictionary

Get a complete entry.

getEnum(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable

Get the enum entry corresponding to the given String.

getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider

Get the EOP history.

getEOPHistory(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get Earth Orientation Parameters history.

getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get Earth Orientation Parameters history.

getEOPHistory() - Method in class org.orekit.frames.GTODProvider

Get the EOP history.

getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop

Get Earth Orientation Parameters history.

getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames

Get Earth Orientation Parameters history.

getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales

Get the EOP history for the given conventions.

getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales

getEOPHistory() - Method in class org.orekit.time.UT1Scale

Get the EOP history.

getEOPHistoryWithoutCachedTidalCorrection() - Method in class org.orekit.frames.EOPHistory

Get version of the instance that does not cache tidal correction.

getEopSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the source and version of Earth Orientation Parameters.

getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions

Get the function computing tidal corrections for Earth Orientation Parameters.

getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing tidal corrections for Earth Orientation Parameters.

getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData

Get the list of Ephemerides data lines.

getEphemeridesDataLines() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the list of Ephemerides data lines.

getEphemeris(int) - Method in class org.orekit.files.sp3.SP3

Get an ephemeris.

getEphemeris(String) - Method in class org.orekit.files.sp3.SP3

Get an ephemeris.

getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage

Get the ephemeris data contain in the ephemeris message.

getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator

Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.

getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for external ephemeris names for participants.

getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the ephemeris type.

getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the type of ephemeris.

getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the type of ephemeris.

getEphemName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the unique name of the external ephemeris used for OD.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the epoch of the data.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Get matrix epoch.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get epoch of state vector, Keplerian elements and covariance matrix data.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get time tag for orbit determination solved-for state.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Get epoch of state vector, Keplerian elements and covariance matrix data.

getEpoch() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation

Getter for the epoch.

getEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Get data line epoch.

getEpoch(TimeScale) - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Get data line epoch.

getEpoch() - Method in class org.orekit.files.sinex.Station

Get the coordinates reference epoch.

getEpoch() - Method in class org.orekit.files.sp3.SP3Header

Returns the start epoch of the orbit file.

getEpoch() - Method in class org.orekit.frames.HelmertTransformation

Get the reference epoch of the transform.

getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the epoch for this magnetic field model.

getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the epoch delay correction.

getEpochEigenInt() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.

getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.

getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.

getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get the indicator for the time event reference.

getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader

Get the epoch identifier.

getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Get epoch ignition.

getEpochInterval() - Method in class org.orekit.files.sp3.SP3Header

Returns the time interval between epochs (in seconds).

getEpochStart() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Get epoch start.

getEpochT0() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the epoch to which all relative times are referenced in data blocks.

getEpochT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the epoch to which all relative times are referenced in data blocks.

getEpochTime1s() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the Epoch Time 1s.

getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the time of clock epoch.

getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the time of clock epoch.

getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the equatorial radius of the body.

getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the central body equatorial radius.

getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Get the central body equatorial radius.

getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get oblate spheroid equatorial radius of central body.

getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get the central body equatorial radius.

getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.orbits.Orbit

Get the first component of the equinoctial eccentricity vector derivative.

getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the first component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState

Get the first component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.orbits.Orbit

Get the second component of the equinoctial eccentricity vector derivative.

getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the second component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState

Get the second component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit

Get the second component of the equinoctial eccentricity vector.

getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for equinox-based paradigm.

getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for equinox-based paradigm.

getERD(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4C

Get an Estimated Range Deviation.

getEstimate() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the current corrected estimate.

getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the current corrected estimate.

getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the current corrected estimate.

getEstimate() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the current corrected estimate.

getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation

Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.

getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider

Get one estimated measurement.

getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement

Get the underlying estimated measurements.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the list of estimated measurements parameters.

getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the list of estimated measurements parameters.

getEstimatedMeasurementsWithoutDerivatives() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement

Get the underlying estimated measurements without derivatives.

getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated orbital parameters.

getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the list of estimated orbital parameters.

getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the list of estimated orbital parameters.

getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the list of estimated orbital parameters.

getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the list of estimated orbital parameters.

getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the list of estimated propagation parameters.

getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the list of estimated propagation parameters.

getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the list of estimated propagation parameters.

getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the list of estimated propagation parameters.

getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the list of estimated propagation parameters.

getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the propagator estimated with the values set in the propagator builder.

getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the propagator estimated with the values set in the propagator builder.

getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the propagators estimated with the values set in the propagators builders.

getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the propagators estimated with the values set in the propagators builders.

getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the estimated UT1 time scale.

getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation

Get the estimated UT1 scale, including the estimated linear models for prime meridian.

getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the estimated value.

getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Get the eta value.

getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Get the eta value.

getEulerBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the Euler angles logical block.

getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get the rotation order for Euler angles.

getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get the rotation order for Euler angles.

getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the rotation order of Euler angles.

getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Get the rotation order of Euler angles.

getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the number of objective function evaluations.

getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Get the evaluations count.

getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the number of evaluations used for last estimation.

getEventDate() - Method in class org.orekit.propagation.events.EventState

Get the occurrence time of the event triggered in the current step.

getEventDate() - Method in class org.orekit.propagation.events.FieldEventState

Get the occurrence time of the event triggered in the current step.

getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the event detector triggered.

getEventDetector() - Method in class org.orekit.propagation.events.EventState

Get the underlying event detector.

getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the event detector triggered.

getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState

Get the underlying event detector.

getEventDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.empirical.ParametricAcceleration

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the discrete events related to the model.

getEventDetectors() - Method in interface org.orekit.forces.ForceModel

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.gravity.OceanTides

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.gravity.SolidTides

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the discrete events related to the model.

getEventDetectors() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Get the discrete events related to the model.

getEventDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Get the discrete events related to the model.

getEventDetectors() - Method in interface org.orekit.propagation.events.EventDetectorsProvider

Get the discrete events related to the model.

getEventDetectors(List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider

Get the discrete events related to the model from a list of ParameterDriver

getEventDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the discrete events related to the model.

getEventDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Get the discrete events related to the model.

getEventFlag() - Method in class org.orekit.files.rinex.observation.ObservationDataSet

Get the event flag.

getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue

Get the events passed to this handler.

getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue

Get the events passed to this handler.

getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get all the events detectors that have been added.

getEventsDetectors() - Method in interface org.orekit.propagation.Propagator

Get all the events detectors that have been added.

getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.KalmanModel

getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

getException() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor

Retrieve exception caught during monitoring.

getExponent() - Method in class org.orekit.utils.units.PowerTerm

Get the fractional exponent.

getExternalClockReference() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the external clock reference.

getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Get the external frame.

getExternalSignalProcessing() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the external signal processing.

getExtrapolationThreshold() - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get the extrapolation threshold.

getExtrapolationThreshold() - Method in class org.orekit.time.AbstractTimeInterpolator

Get the extrapolation threshold.

getExtrapolationThreshold() - Method in interface org.orekit.time.FieldTimeInterpolator

Get the extrapolation threshold.

getExtrapolationThreshold() - Method in interface org.orekit.time.TimeInterpolator

Get the extrapolation threshold.

getF() - Method in class org.orekit.data.DelaunayArguments

Get L - Ω where L is the mean longitude of the Moon.

getF() - Method in class org.orekit.data.FieldDelaunayArguments

Get L - Ω where L is the mean longitude of the Moon.

getF10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).

getF10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).

getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).

getF107() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

Get the F10.0 flux.

getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.

getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the observed (unadjusted) value of F10.7.

getF10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the value of the mean solar flux.

getF10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the value of the mean solar flux.

getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the value of the mean solar flux.

getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame

Get the key of the frame within the factory.

getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the fallback host or IP address.

getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the fallback port number.

getFDot() - Method in class org.orekit.data.DelaunayArguments

Get L - Ω where L is the mean longitude of the Moon time derivative.

getFDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get L - Ω where L is the mean longitude of the Moon time derivative.

getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record

Get one field from the parsed sourcetable.

getField(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get a field.

getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the GeoMagneticField for the given model type and year.

getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields

Get the GeoMagneticField for the given model type and year.

getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields

getField() - Method in class org.orekit.orbits.FieldOrbit

Getter for Field.

getField() - Method in class org.orekit.propagation.FieldAbstractPropagator

Field getter.

getField() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get field.

getField() - Method in class org.orekit.time.FieldAbsoluteDate

Get the field.

getField() - Method in class org.orekit.utils.FieldArrayDictionary

Get the field to which elements belong.

getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext

Method to get the auxiliary elementsrelated to the ForceModelContext.

getFieldDate() - Method in class org.orekit.frames.FieldTransform

Get the date.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.empirical.ParametricAcceleration

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the discrete events related to the model.

getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Get the discrete events related to the model.

getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>, List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider

Get the discrete events related to the model from a list of ParameterDriver

getFieldEventDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the discrete events related to the model.

getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Get the discrete events related to the model.

getFieldOther(Field<T>) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF

Get the field version of other's position and velocity coordinates.

getFieldOther(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get other's position and velocity coordinates.

getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record

Get the number of fields.

getFieldStep(Field<T>) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder

Get "fielded" step size (s).

getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the magnetic field vector in Tesla.

getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales

getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the date of the file from which data at the specified date comes from.

getFileDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

Get the file date.

getFileEpochEndTime() - Method in class org.orekit.files.sinex.SinexLoader

Get the file epoch end time.

getFileEpochStartTime() - Method in class org.orekit.files.sinex.SinexLoader

Get the file epoch start time.

getFileFormat() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Get the file format of the last message parsed.

getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Get the file format of the last message parsed.

getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the name of the file.

getFileType() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Get the file type.

getFilter() - Method in class org.orekit.files.sp3.SP3Header

Get the derivatives filter.

getFilter() - Method in class org.orekit.propagation.events.EventSlopeFilter

Get filter type.

getFilter() - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Get Filter defining if only the state covariance value are used or if first or/and second Keplerian derivatives should be used.

getFilter() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Get the filter for derivatives from the sample to use in interpolation.

getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter

Get the filter corresponding to a maximum derivation order.

getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Get the filter corresponding to a maximum derivation order.

getFilter() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Get filter for derivatives from the sample to use in interpolation.

getFilter() - Method in class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

Get filter for derivatives from the sample to use in interpolation.

getFilter() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

Get filter for derivatives from the sample to use in interpolation.

getFilter() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

filter for derivatives from the sample to use in interpolation.

getFilter() - Method in class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Get filter for derivatives from the sample to use in interpolation.

getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Get the map of the filtered data.

getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Get the map of the filtered data.

getFilterFlag() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get the filter flag.

getFilters() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Get the filters to apply to parse tokens.

getFiltersManager() - Method in class org.orekit.data.DataProvidersManager

Get the manager for filters.

getFinalPoint() - Method in class org.orekit.bodies.LoxodromeArc

Get the final point of the arc.

getFiringIntervalDetector() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Getter for the firing interval detector.

getFirings() - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Get the firings detected during last propagation.

getFirst() - Method in class org.orekit.time.FieldTimeStampedPair

Get first time stamped value.

getFirst() - Method in class org.orekit.time.TimeStampedPair

Get first time stamped value.

getFirstFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter

Get the history of phase values of the first frequency.

getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale

Get the date of the first known leap second.

getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the first time span of the drag sensitive time span map.

getFirstSpan() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the first time span of the acceleration model time span map.

getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Get the first time span of the tropospheric model time span map.

getFirstSpan() - Method in class org.orekit.utils.TimeSpanMap

Get the first (earliest) span.

getFirstTransition() - Method in class org.orekit.utils.TimeSpanMap

Get the first (earliest) transition.

getFitInterval() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get fit interval.

getFitInterval() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the fit interval.

getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic

Get a copy of the last fitted parameters.

getFixedF10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.

getFixedF10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.

getFixedGeomagneticAp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.

getFixedGeomagneticDst() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.

getFixedGeomagneticKp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.

getFixedM10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux daily proxy M10.7.

getFixedM10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.

getFixedS10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux daily proxy S10.7.

getFixedS10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.

getFixedStepHandler() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Get the underlying fixed step handler.

getFixedStepHandler() - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer

Get the underlying fixed step handler.

getFixedStepHandler() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Get the underlying fixed step handler.

getFixedTimeStep() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Get the fixed time step.

getFixedTimeStep() - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer

Get the fixed time step.

getFixedTimeStep() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Get the fixed time step.

getFixedY10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux daily proxy Y10.7.

getFixedY10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.

getFlags() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Get the disturbance flags.

getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the flattening of the body: f = (a-b)/a.

getFlattening() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the central body flattening.

getFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Get the central body flattening.

getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the flow rate at given date.

getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the flow rate.

getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the flow rate (kg/s).

getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the flow rate (kg/s).

getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the Flux Qualifier.

getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

Get first focus in spacecraft frame.

getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

Get second focus in spacecraft frame.

getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView

Get the footprint of the Field Of View on ground.

getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView

Get the footprint of the Field Of View on ground.

getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get the footprint of the Field Of View on ground.

getFormat() - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Get the generated file format.

getFormat() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Get the generated file format.

getFormat() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Get the generated file format.

getFormat() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the file format.

getFormat() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the data format.

getFormatDetails() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the format details.

getFormatVersion() - Method in class org.orekit.files.ccsds.section.Header

Get the CCSDS NDM (ADM, ODM or TDM) format version.

getFormatVersion() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the format version.

getFormatVersion() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the format version.

getFormatVersionKey() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get key for format version.

getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get key for format version.

getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Get key for format version.

getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Get the key for format version.

getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Get the key for format version.

getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector

Get the Field Of View.

getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the Field Of View.

getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Get the Field Of View.

getFrame() - Method in class org.orekit.bodies.Ellipse

Get the defining frame.

getFrame() - Method in class org.orekit.bodies.Ellipsoid

Get the ellipsoid central frame.

getFrame() - Method in class org.orekit.bodies.FieldEllipse

Get the defining frame.

getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Get the frame corresponding to the CCSDS constant.

getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Get frame in which angular velocities are specified.

getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Get frame in which inertia is specified.

getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Get Coordinate system for the torque vector.

getFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).

getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).

getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the reference frame for this ephemeris segment.

getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.rinex.clock.RinexClock

Get the reference frame for the station positions.

getFrame() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the reference frame.

getFrame() - Method in class org.orekit.files.sp3.SP3Segment

Get the reference frame for this ephemeris segment.

getFrame() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames

getFrame(PVCoordinates) - Method in enum org.orekit.frames.encounter.EncounterLOFType

Get encounter local orbital frame associated to this enum.

getFrame(FieldPVCoordinates<T>) - Method in enum org.orekit.frames.encounter.EncounterLOFType

Get encounter local orbital frame associated to this enum.

getFrame(Predefined) - Method in interface org.orekit.frames.Frames

Get one of the predefined frames.

getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory

Get one of the predefined frames.

getFrame() - Method in class org.orekit.frames.OrphanFrame

Get the associated frame.

getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere

Get the frame of the central body.

getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000

Get the frame of the central body.

getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the frame of the central body.

getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008

Get the frame of the central body.

getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00

Get the frame of the central body.

getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere

Get the frame of the central body.

getFrame() - Method in class org.orekit.orbits.FieldOrbit

Get the frame in which the orbital parameters are defined.

getFrame() - Method in class org.orekit.orbits.Orbit

Get the frame in which the orbital parameters are defined.

getFrame() - Method in class org.orekit.propagation.AbstractPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the frame of the initial state.

getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector

Get the frame in which the equator is defined.

getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector

Get the sensor reference frame.

getFrame() - Method in class org.orekit.propagation.events.NodeDetector

Get the frame in which the equator is defined.

getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in interface org.orekit.propagation.FieldPropagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the defining frame.

getFrame() - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance frame.

getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the inertial frame.

getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

getFrame() - Method in class org.orekit.propagation.integration.StateMapper

Get the inertial frame.

getFrame() - Method in interface org.orekit.propagation.Propagator

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the definition frame of the orbit.

getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the definition frame of the orbit.

getFrame() - Method in class org.orekit.propagation.SpacecraftState

Get the defining frame.

getFrame() - Method in class org.orekit.propagation.StateCovariance

Get the covariance frame.

getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates

Get the frame in which the coordinates are defined.

getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get the frame in which the coordinates are defined.

getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Get frame A.

getFrameAngvelFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get frame in which angular velocities are specified.

getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Get frame B.

getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get epoch of reference frame, if not intrinsic to the definition of the reference frame.

getFrameName() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the frame name.

getFrames() - Method in class org.orekit.data.CompositeDataContext

getFrames() - Method in interface org.orekit.data.DataContext

Get a factory constructing Frames based on the auxiliary data in this context.

getFrames() - Method in class org.orekit.data.ExceptionalDataContext

getFrames() - Method in class org.orekit.data.LazyLoadedDataContext

getFrames() - Static method in class org.orekit.frames.FramesFactory

Get the instance of Frames that is called by the static methods in this class.

getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Get the ambiguity parameters drivers that have not been fixed yet.

getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.

getFreeCompsMap() - Method in class org.orekit.utils.AbstractMultipleShooting

Get the map of free state components.

getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Get the number of free state parameters.

getFreqOffset() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the freqOffset.

getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna

Get supported frequencies.

getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType

Get the frequency for a specified satellite system.

getFrequencyChannel() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the frequency channel.

getFrequencyNumber() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Getter for the frequency number.

getFrequencySource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the frequency source.

getFrom() - Method in class org.orekit.utils.units.UnitsConverter

Get the source unit.

getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame

Get a new version of the instance, frozen with respect to a reference frame.

getFT() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS F_T Word.

getFunction() - Method in class org.orekit.propagation.events.FieldFunctionalDetector

Get the switching function.

getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector

Get the switching function.

getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales

getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Dummy date at infinity in the future direction.

getFutureInfinity() - Method in interface org.orekit.time.TimeScales

Dummy date at infinity in the future direction.

getGalileoDataValidityStatus() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Get the Galileo data validity status.

getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales

getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.

getGalileoEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.

getGalileoNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Get the Galileo navigation message corresponding to the current RTCM data.

getGalileoNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Get the Galileo navigation message corresponding to the current RTCM data.

getGalileoNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the Galileo navigation messages contained in the file.

getGalileoNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the Galileo navigation messages for the given satellite Id.

getGalileoToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Get the Galileo time of clock.

getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem

Get the position of the Lagrangian point in the CR3BP Rotating frame.

getGamma() - Method in class org.orekit.data.DelaunayArguments

Get the tide parameter γ = GMST + π.

getGamma() - Method in class org.orekit.data.FieldDelaunayArguments

Get the tide parameter γ = GMST + π.

getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get direction cosine γ for central body.

getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get direction cosine γ for central body.

getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine γ for central body.

getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get direction cosine γ for central body.

getGammaDot() - Method in class org.orekit.data.DelaunayArguments

Get the tide parameter γ = GMST + π time derivative.

getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the tide parameter γ = GMST + π time derivative.

getGammaN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the relative deviation of predicted satellite carrier frequency from nominal value.

getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the relative deviation of predicted satellite carrier frequency from nominal value.

getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich apparent sidereal time, in radians.

getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich apparent sidereal time, in radians.

getGCRF() - Method in class org.orekit.frames.AbstractFrames

getGCRF() - Method in interface org.orekit.frames.Frames

Get the unique GCRF frame.

getGCRF() - Static method in class org.orekit.frames.FramesFactory

Get the unique GCRF frame.

getGdop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get generalize Dilution Of Precision.

getGdop() - Method in class org.orekit.gnss.DOP

Gets the geometric dilution of precision.

getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Get the useful angles for eclipse computation.

getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Get the useful angles for eclipse computation.

getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of calls to the generate method.

getGeneratedEphemeris() - Method in interface org.orekit.propagation.EphemerisGenerator

Get the ephemeris generated during the propagation.

getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldEphemerisGenerator

Get the ephemeris generated during the propagation.

getGeneratedMeasurements() - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber

Get generated measurements.

getGenerator() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the hardware or software generator.

getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the generator.

getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext

getGeoMagneticFields() - Method in interface org.orekit.data.DataContext

Get a factory constructing GeoMagneticFields based on the auxiliary data in this context.

getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext

getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext

getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the instance of GeoMagneticFields that is called by methods in this class.

getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the Geometry-Free combination of measurements.

getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of calls to the TimeStampedCache.getNeighbors(AbsoluteDate) method.

getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the G_js coefficient.

getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the G_js coefficient.

getGlo2UTC() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the correction from GLONASS to UTC.

getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales

getGLONASS() - Method in interface org.orekit.time.TimeScales

Get the GLObal NAvigation Satellite System time scale.

getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory

Get the GLObal NAvigation Satellite System time scale.

getGlonassChannels() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the list of GLONASS satellite/channel associations.

getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales

getGlonassEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.

getGlonassNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the Glonass navigation message corresponding to the current RTCM data.

getGlonassNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the Glonass navigation message corresponding to the current RTCM data.

getGlonassNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the Glonass navigation messages contained in the file.

getGlonassNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the Glonass navigation messages for the given satellite Id.

getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Gets the underlying GLONASS orbital elements.

getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator

Gets the underlying GLONASS orbital elements.

getGloOffset() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the correction of time relative to GLONASS system time.

getGM() - Method in interface org.orekit.bodies.CelestialBody

Get the attraction coefficient of the body.

getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get gravitational coefficient of attracting body.

getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the gravitational parameter that is part of the definition of the reference ellipsoid.

getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext

Get standard gravitational parameter μ for the body in m³/s².

getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTNewtonianAttractionContext

Get standard gravitational parameter μ for the body in m³/s².

getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the G_ms^j coefficient.

getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the G_ms^j coefficient.

getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales

getGMST() - Method in class org.orekit.time.GLONASSDate

Get the Greenwich Mean Sidereal Time.

getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales

getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales

Get the Greenwich Mean Sidereal Time scale.

getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory

Get the Greenwich Mean Sidereal Time scale.

getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time, in radians.

getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time, in radians.

getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time rate, in radians per second.

getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing Greenwich mean sidereal time rate, in radians per second.

getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Get the GNSS IOD.

getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData

Get the GNSS IOD.

getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data

Get the GNSS IOD.

getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Get the GNSS IOD.

getGnssNb() - Method in class org.orekit.gnss.DOP

Gets the number of GNSS satellites taken into account for DOP computation.

getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales

getGPS() - Method in interface org.orekit.time.TimeScales

Get the Global Positioning System scale.

getGPS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Global Positioning System scale.

getGPS2Glo() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the correction to GPS time relative GLONASS.

getGPSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the GPS civilian navigation messages contained in the file.

getGPSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the GPS civilian navigation messages for the given satellite Id.

getGpsCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS code on L2.

getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales

getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.

getGpsEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.

getGpsFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS fit interval.

getGpsL2PDataFlag() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS L2 P-Code data flag.

getGPSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the GPS legacy navigation messages contained in the file.

getGPSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the GPS legacy navigation messages for the given satellite Id.

getGpsNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS navigation message corresponding to the current RTCM data.

getGpsNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS navigation message corresponding to the current RTCM data.

getGpsToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Get the GPS time of clock.

getGpsWeek() - Method in class org.orekit.files.sp3.SP3Header

Returns the GPS week as contained in the SP3 file.

getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the gradient converter related to the analytical orbit propagator.

getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Compute density and its derivatives.

getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the GRAPHIC combination of measurements.

getGravitationalAssist() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the origin of gravitational assist.

getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get degree of the gravity model.

getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get degree of the gravity model.

getGravityFields() - Method in class org.orekit.data.CompositeDataContext

getGravityFields() - Method in interface org.orekit.data.DataContext

Get a factory constructing gravity fields based on the auxiliary data in this context.

getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext

getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext

getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the instance of GravityFields that is called by the static methods of this class.

getGravityModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get gravity model name.

getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get gravity model name.

getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get order of the gravity model.

getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get order of the gravity model.

getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the number of interpolation grid points.

getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the number of interpolation grid points.

getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid

Get grid points that are within the current step.

getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid

Get grid points that are within the current step.

getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid

Get grid points that are within the current step.

getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid

Get grid points that are within the current step.

getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid

Get grid points that are within the current step.

getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid

Get grid points that are within the current step.

getGroundStationCoordinates(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Get the station coordinates for a given frame.

getGroundStationPosition(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Get the station position for a given frame.

getGroupDelayDifference() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get group delay difference.

getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the GRS80 ellipsoid, attached to the given body frame.

getGST() - Method in class org.orekit.time.LazyLoadedTimeScales

getGST() - Method in interface org.orekit.time.TimeScales

Get the Galileo System Time scale.

getGST() - Static method in class org.orekit.time.TimeScalesFactory

Get the Galileo System Time scale.

getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames

getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getGTOD(boolean) - Method in interface org.orekit.frames.Frames

Get the GTOD reference frame.

getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the GTOD reference frame.

getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the GTOD reference frame.

getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the GTOD reference frame.

getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the y component of eccentricity vector.

getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the y component of eccentricity vector.

getH1CrdString() - Method in class org.orekit.files.ilrs.CRDHeader

Get a string representation of the H1 in the CRD format.

getH2CrdString() - Method in class org.orekit.files.ilrs.CRDHeader

Get a string representation of the H2 in the CRD format.

getH3CrdString() - Method in class org.orekit.files.ilrs.CRDHeader

Get a string representation of the H3 in the CRD format.

getH4CrdString() - Method in class org.orekit.files.ilrs.CRDHeader

Get a string representation of the H4 in the CRD format.

getH5CrdString() - Method in class org.orekit.files.ilrs.CRDHeader

Get a string representation of the H5 in the CRD format.

getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView

get the FOV half aperture angle.

getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

get the FOV half aperture angle for spreading along X_ell (i.e.

getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

get the FOV half aperture angle for spreading along Y_ell (i.e.

getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion

Return the orbital period of the Halo Orbit.

getHandler() - Method in class org.orekit.propagation.events.AbstractDetector

Get the handler.

getHandler() - Method in class org.orekit.propagation.events.AdapterDetector

Get the handler.

getHandler() - Method in interface org.orekit.propagation.events.EventDetector

Get the handler.

getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get the handler.

getHandler() - Method in class org.orekit.propagation.events.FieldAdapterDetector

Get the handler.

getHandler() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get the handler.

getHandlers() - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Retrieve managed handlers list.

getHandlers() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Get an unmodifiable view of all handlers.

getHandlers() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Get an unmodifiable view of all handlers.

getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic

Get an upper bound of the fitted harmonic amplitude.

getHarvester() - Method in class org.orekit.propagation.AbstractPropagator

Get the harvester.

getHasCreatableBody() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.

getHbr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the object hard body radius.

getHdop() - Method in class org.orekit.gnss.DOP

Gets the horizontal dilution of precision.

getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Get the header.

getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Get file header to fill.

getHeader() - Method in class org.orekit.files.ilrs.CPF

Get the CPF file header.

getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the header of the current data block.

getHeader() - Method in class org.orekit.files.rinex.RinexFile

Get the header.

getHeader() - Method in class org.orekit.files.sp3.SP3

Get the header.

getHeader() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage

Get the header.

getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage

Get the header.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the health status.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac

Gets the Health status.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for health.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the Health status.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets the Health status.

getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Gets the Health status.

getHealthE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Gets the E1-B/C signal health status.

getHealthE5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Gets the E5a signal health status.

getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Gets the E5b signal health status.

getHealthFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get health flags.

getHeightIonosphericLayer() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Get the height of the ionospheric layer.

getHighRateClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data

Get the high rate clock correction to be added to the polynomial clock correction.

getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the H_js coefficient.

getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the H_js coefficient.

getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get h * k.

getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get h * k.

getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials

Get the H_ms^j coefficient.

getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the H_ms^j coefficient.

getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).

getHost() - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Get the caster host.

getHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the host or IP address.

getHour() - Method in class org.orekit.time.TimeComponents

Get the hour number.

getHumidity() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get the relative humidity at the surface.

getHumiSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the humidity sensor manufacturer.

getHumiSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the humidity sensor model.

getHumiSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the humidity sensor serial number.

getHx() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.orbits.Orbit

Get the first component of the inclination vector.

getHx() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the first component of the inclination vector (as per equinoctial parameters).

getHx() - Method in class org.orekit.propagation.SpacecraftState

Get the first component of the inclination vector (as per equinoctial parameters).

getHxDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.FieldOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the first component of the inclination vector derivative.

getHxDot() - Method in class org.orekit.orbits.Orbit

Get the first component of the inclination vector derivative.

getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get hXXX = h * Χ³.

getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get hXXX = h * Χ³.

getHy() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.orbits.Orbit

Get the second component of the inclination vector.

getHy() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the second component of the inclination vector (as per equinoctial parameters).

getHy() - Method in class org.orekit.propagation.SpacecraftState

Get the second component of the inclination vector (as per equinoctial parameters).

getHyDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.FieldOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the second component of the inclination vector derivative.

getHyDot() - Method in class org.orekit.orbits.Orbit

Get the second component of the inclination vector derivative.

getI() - Method in class org.orekit.attitudes.FieldInertiaAxis

Get the moment of inertia.

getI() - Method in class org.orekit.attitudes.InertiaAxis

Get the moment of inertia.

getI() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit inclination.

getI() - Method in class org.orekit.orbits.CartesianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.CircularOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.FieldOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.KeplerianOrbit

Get the inclination.

getI() - Method in class org.orekit.orbits.Orbit

Get the inclination.

getI() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the inclination.

getI() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the inclination.

getI() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the inclination.

getI() - Method in class org.orekit.propagation.SpacecraftState

Get the inclination.

getI0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get i₀.

getI0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the inclination angle at reference time.

getI0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Inclination Angle at Reference Time.

getICRF() - Method in class org.orekit.frames.AbstractFrames

getICRF() - Method in interface org.orekit.frames.Frames

Get the unique ICRF frame.

getICRF() - Static method in class org.orekit.frames.FramesFactory

Get the unique ICRF frame.

getId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get identification number.

getID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get maneuver identification number.

getId() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get identification number.

getId() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Get the satellite ID.

getId() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Get the satellite ID.

getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the satellite ID.

getId() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage

Get message id.

getId() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get sub-frame id.

getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter

Get the regular expression for identifying line.

getIdentity(Field<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Get the identity static transform.

getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform

Get the identity transform.

getIdentity() - Static method in interface org.orekit.frames.StaticTransform

Get the identity static transform.

getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates

Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).

getIDot() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get dot(i).

getIDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.CircularOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.FieldOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.orbits.Orbit

Get the inclination derivative.

getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the rate of inclination angle.

getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the rate of inclination angle.

getIDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Rate of Inclination Angle.

getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the IERS2003 ellipsoid, attached to the given body frame.

getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the IERS2010 ellipsoid, attached to the given body frame.

getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the IERS96 ellipsoid, attached to the given body frame.

getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the IGRF model for the given year.

getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields

Get the IGRF model for the given year.

getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields

getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the I_js coefficient.

getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the I_js coefficient.

getIlrsSatelliteId() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the IRLS satellite ID (based on COSPAR ID).

getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the imaginary part of a nominal Love numbers.

getInclination() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the angle between the objects orbit plane and the orbit centers equatorial plane.

getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the inclination of the magnetic field in radians.

getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter

Get the increasing events time shift.

getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.DataType

Get the data type indicator.

getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType

Get the range type indicator.

getIndices() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get derivatives indices map.

getInertia() - Method in class org.orekit.attitudes.TorqueFree

Get the spacecraft inertia.

getInertiaAxis1() - Method in class org.orekit.attitudes.FieldInertia

Get inertia along first axis.

getInertiaAxis1() - Method in class org.orekit.attitudes.Inertia

Get inertia along first axis.

getInertiaAxis2() - Method in class org.orekit.attitudes.FieldInertia

Get inertia along second axis.

getInertiaAxis2() - Method in class org.orekit.attitudes.Inertia

Get inertia along second axis.

getInertiaAxis3() - Method in class org.orekit.attitudes.FieldInertia

Get inertia along third axis.

getInertiaAxis3() - Method in class org.orekit.attitudes.Inertia

Get inertia along third axis.

getInertiaBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the inertia logical block.

getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the inertial velocity increment of the maneuver.

getInertialFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the inertial reference frame for this ephemeris segment.

getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the inertial reference frame for this ephemeris segment.

getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the inertial reference frame for this ephemeris segment.

getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Get the inertial frame in which the velocity increment is defined.

getInertialFrame() - Method in class org.orekit.frames.LocalMagneticFieldFrame

Get interlai frame.

getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody

Get an inertially oriented, body centered frame.

getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get the inertia matrix.

getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Get the inertia matrix.

getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the inertia matrix.

getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get reference frame for inertia.

getInitialAttitude() - Method in class org.orekit.attitudes.TorqueFree

Get the initial attitude.

getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider

Get the initial covariance matrix.

getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider

Get the initial covariance matrix.

getInitialFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the initial flow rate.

getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the initial state for integration.

getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the initial state for integration.

getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the initial state for integration.

getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get the initial state for integration.

getInitialJacobianColumn(String) - Method in class org.orekit.propagation.AbstractMatricesHarvester

Get the initial column of Jacobian matrix with respect to named parameter.

getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the date of the initial orbit.

getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the date of the initial orbit.

getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit

Return the initialPV on the libration orbit.

getInitialState() - Method in class org.orekit.propagation.AbstractPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the propagator initial state.

getInitialState() - Method in interface org.orekit.propagation.FieldPropagator

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the propagator initial state.

getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the propagator initial state.

getInitialState() - Method in interface org.orekit.propagation.Propagator

Get the propagator initial state.

getInitialStateTransitionMatrix() - Method in class org.orekit.propagation.AbstractMatricesHarvester

Get the initial State Transition Matrix.

getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the initial thrust vector.

getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the total mass at beginning of life.

getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.KalmanModel

getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

getInputs() - Method in class org.orekit.data.AbstractListCrawler

Get the list of inputs supported by the instance.

getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the value of the instantaneous solar flux.

getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the instantaneous solar flux.

getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Get the value of the instantaneous solar flux.

getIntegrationInterval() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the integrationInterval.

getIntegrationRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the integrationRef.

getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the integrator used by the propagator.

getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the integrator used by the propagator.

getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Get the integrator builder.

getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the integrator builder.

getIntegratorName() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the integrator's name.

getIntegratorName() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the integrator's name.

getIntegrityFlags() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for B1C integrity flags.

getIntegrityStatus() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get integrity status flag.

getInternationalDes() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the international designator for the object.

getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the international designator for the object.

getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the international designator for the object.

getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the interpolation method for Earth Orientation Parameters.

getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get the interpolation method for Space Weather data.

getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile

Get an interpolated point inside the tile.

getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at interpolated date.

getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at interpolated date.

getInterpolationDate() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get interpolation date.

getInterpolationDate() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData

Get interpolation date.

getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the interpolation degree.

getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the interpolation degree.

getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get the interpolation degree.

getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Get the interpolation degree.

getInterpolationDegree() - Method in class org.orekit.frames.EOPHistory

Get interpolation degree.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Get the interpolation method to be used.

getInterpolationMethod() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the interpolation method to be used.

getInterpolationMethod() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the interpolation method to be used.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the number of points to use for interpolation.

getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3Segment

Get the number of samples to use in interpolation.

getInterpolationSamples() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Get the intersection point of a line with the surface of the body.

getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid

Get the intersection point of a line with the surface of the body.

getInterval() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the observation interval in seconds.

getIntervalNumber() - Method in class org.orekit.time.GLONASSDate

Get the number of the current four year interval.

getIntrackThrust() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get Enum YesNoUnknown that indicates if intrack thrust modeling was into account or not.

getInverse() - Method in interface org.orekit.frames.FieldStaticTransform

Get the inverse transform of the instance.

getInverse() - Method in class org.orekit.frames.FieldTransform

Get the inverse transform of the instance.

getInverse() - Method in interface org.orekit.frames.StaticTransform

Get the inverse transform of the instance.

getInverse() - Method in class org.orekit.frames.Transform

Get the inverse transform of the instance.

getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Gets the Issue of Data (IOD).

getIOD() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Gets the GLONASS Issue Of Data (IOD).

getIODC() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get IODC.

getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for the Issue Of Data Clock (IODC).

getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the Issue Of Data Clock (IODC).

getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Issue Of Data (ephemeris).

getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get Issue Of Data (ephemeris).

getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for the Issue Of Data Ephemeris (IODE).

getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the Issue Of Data Ephemeris (IODE).

getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Getter for the Issue Of Data Ephemeris and Clock (IODEC).

getIODN() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Gets the Issue Of Data Navigation (IODN).

getIODN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the Issue Of Data Navigation (IODN).

getIODNav() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the the Issue Of Data (IOD).

getIodSsr() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the IOD SSR.

getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the IOD SSR.

getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier

Get the ionospheric delay model.

getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier

Get the ionospheric delay model.

getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the Ionosphere-Free combination of measurements.

getIonosphericCorrectionType() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Getter for the ionospheric correction type.

getIonosphericModel() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201

Get the ionospheric model adapted to the current IM201 message.

getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales

getIRNSS() - Method in interface org.orekit.time.TimeScales

Get the Indian Regional Navigation Satellite System time scale.

getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Indian Regional Navigation Satellite System time scale.

getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales

getIrnssEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.

getIRNSSNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the IRNSS navigation messages contained in the file.

getIRNSSNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the IRNSS navigation messages for the given satellite Id.

getIscB1CD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for inter Signal Delay for B1 CD.

getIscB1CP() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for inter Signal Delay for B1 CP.

getIscB2AD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for inter Signal Delay for B2 AD.

getIscL1CA() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L1 C/A.

getIscL1CD() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L1 CD.

getIscL1CP() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L1 CP.

getIscL2C() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L2 C.

getIscL5I5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L5I.

getIscL5Q5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for inter Signal Delay for L5Q.

getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Get the specific impulse.

getIsp() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Get the specific impulse.

getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the specific impulse at given date.

getIsp() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the specific impulse.

getIsp() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Get the specific impulse.

getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the specific impulse.

getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the specific impulse.

getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the specific impulse at given date.

getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the specific impulse (s).

getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the iteration number.

getIterationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Get the iterations count.

getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the number of iterations used for last estimation.

getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get an unspecified International Terrestrial Reference Frame.

getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get an specific International Terrestrial Reference Frame.

getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get an unspecified International Terrestrial Reference Frame.

getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get a specific International Terrestrial Reference Frame.

getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the equinox-based ITRF reference frame.

getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the equinox-based ITRF reference frame.

getITRFType() - Method in class org.orekit.frames.EOPEntry

Get the ITRF version this entry defines.

getITRFVersion() - Method in class org.orekit.files.sinex.SinexLoader

Get the ITRF version used for the EOP entries processing.

getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the ITRF version.

getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion

Find an ITRF version from its reference year.

getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion

Find an ITRF version from its name.

getITRFVersion() - Method in class org.orekit.frames.VersionedITRF

Get the ITRF version.

getJ2000Day() - Method in class org.orekit.time.DateComponents

Get the day number with respect to J2000 epoch.

getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales

getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

getJ2000Epoch() - Method in interface org.orekit.time.TimeScales

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

getJacobian(Orbit, PositionAngleType, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the Jacobian of the orbit with respect to maneuver parameters.

getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform

Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.

getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform

Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.

getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in interface org.orekit.propagation.MatricesHarvester

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).

getJacobianWrtCartesian(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.

getJacobianWrtCartesian(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.

getJacobianWrtParameters(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit

Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.

getJacobianWrtParameters(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.

getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales

getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

getJavaEpoch() - Method in interface org.orekit.time.TimeScales

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

getJD0() - Method in class org.orekit.time.GLONASSDate

Get the current Julian date JD0.

getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials

Get the J_js coefficient.

getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the J_js coefficient.

getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales

getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

getJulianEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

getJupiter() - Method in interface org.orekit.bodies.CelestialBodies

Get the Jupiter singleton body.

getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Jupiter singleton body.

getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getJupiterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants

Get the Jupiter semi-major axis.

getK() - Method in class org.orekit.files.rinex.observation.GlonassSatelliteChannel

Get the channel frequency multiplier.

getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the x component of eccentricity vector.

getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the x component of eccentricity vector.

getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get k² - h².

getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get k² - h².

getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get (k² - h²) / 2.

getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get (k² - h²) / 2.

getKalmanEstimation() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the provider for kalman filter estimations.

getKalmanEstimation() - Method in class org.orekit.estimation.sequential.KalmanEstimator

Get the provider for kalman filter estimations.

getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator

Get the provider for kalman filter estimations.

getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator

Get the provider for kalman filter estimations.

getKalmanEstimation() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator

Get the provider for kalman filter estimations.

getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the Keplerian elements logical block.

getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the Keplerian elements logical block.

getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the Keplerian mean motion.

getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState

Get the Keplerian mean motion.

getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the Keplerian period.

getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState

Get the Keplerian period.

getKey() - Method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType

Get the key for the system.

getKey() - Method in enum org.orekit.files.sp3.DataUsed

Get the key for the data used.

getKey() - Method in enum org.orekit.files.sp3.SP3FileType

Get the key for the file type.

getKey() - Method in enum org.orekit.gnss.SatelliteSystem

Get the key for the system.

getKey() - Method in enum org.orekit.gnss.TimeSystem

Get the 3 letters key of the time system.

getKey() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Get the entry key.

getKey() - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Get the entry key.

getKlobucharAlpha() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the "alpha" ionospheric parameters.

getKlobucharBeta() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the "beta" ionospheric parameters.

getKlobucharMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the ionosphere Klobuchar messages.

getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the sum of all eight Kp indices for the current entry.

getKurtosis() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the kurtosis of raw system delay values from the mean.

getKurtosis() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get the session kurtosis from the mean of raw accepted time-of-flight values minus the trend function.

getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get kXXX = h * Χ³.

getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get kXXX = h * Χ³.

getL() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Moon.

getL() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Moon.

getL(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit

Get the longitude argument.

getL(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the longitude argument.

getL2PDataFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get L2 P data flag.

getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame

Get the frame label.

getLabel() - Method in enum org.orekit.files.rinex.section.RinexLabels

Get the first label.

getLabel(String) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Get the trimmed label from a header line.

getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion

Get the considered lagrangian point.

getLambda() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getLambda() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the longitude of ascending node of orbit.

getLaserId() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the laser configuration ID.

getLaserRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the laser configuration record.

getLaserRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get laser configuration record related to the systemRecord.

getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the laser type.

getLast() - Static method in enum org.orekit.frames.ITRFVersion

Get last supported ITRF version.

getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader

Gets the day (at data start) of the last daily data entry.

getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the last estimations performed.

getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale

Get the date of the last known leap second.

getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader

Gets the day (at data start) of the last observed data entry.

getLastSpan() - Method in class org.orekit.utils.TimeSpanMap

Get the last (latest) span.

getLastSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the system configuration record.

getLastTransition() - Method in class org.orekit.utils.TimeSpanMap

Get the last (latest) transition.

getLatest() - Method in interface org.orekit.utils.FieldTimeStampedCache

Get the latest entry in this cache.

getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the latest entry in this cache.

getLatest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get the latest entry in this cache.

getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get the latest entry in this cache.

getLatest() - Method in interface org.orekit.utils.TimeStampedCache

Get the latest entry in this cache.

getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the latitude.

getLatitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the latitude.

getLatitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the latitude.

getLatitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the latitude.

getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector

Get the fixed latitude to be crossed (radians).

getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector

Get the fixed latitude to be crossed (radians).

getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the launch number.

getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the launch number.

getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata

Get the launch number.

getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the launch number.

getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch number.

getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the piece of launch.

getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the piece of launch.

getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata

Get the piece of launch.

getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the launch piece.

getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch piece.

getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the launch year.

getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the launch year.

getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata

Get the launch year.

getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the launch year.

getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the launch year.

getLDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Moon time derivative.

getLDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Moon time derivative.

getLDot(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit

Get the longitude argument derivative.

getLDot(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the longitude argument derivative.

getLE() - Method in class org.orekit.data.BodiesElements

Get the mean Earth longitude.

getLE() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Earth longitude.

getLE() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.orbits.Orbit

Get the eccentric longitude argument.

getLE() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the eccentric latitude argument (as per equinoctial parameters).

getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the eccentric longitude.

getLE() - Method in class org.orekit.propagation.SpacecraftState

Get the eccentric latitude argument (as per equinoctial parameters).

getLeap() - Method in class org.orekit.files.ilrs.CPF.CPFCoordinate

Get the leap second flag (= 0 or the value of the new leap second).

getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Get the value of the previous leap.

getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Get the value of the previous leap.

getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the value of the previous leap.

getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Get the value of the previous leap.

getLeap() - Method in class org.orekit.time.UTCTAIOffset

Get the value of the leap at offset validity start (in seconds).

getLeapSeconds() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the Number of leap seconds since 6-Jan-1980.

getLeapSecondsDayNum() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the respective leap second day number.

getLeapSecondsFuture() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the future or past leap seconds.

getLeapSecondsWeekNum() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the respective leap second week number.

getLEDot() - Method in class org.orekit.data.BodiesElements

Get the mean Earth longitude time derivative.

getLEDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Earth longitude time derivative.

getLEDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.FieldOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric longitude argument derivative.

getLEDot() - Method in class org.orekit.orbits.Orbit

Get the eccentric longitude argument derivative.

getLength() - Method in class org.orekit.utils.units.Unit

Get the length exponent.

getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentric longitude.

getLicense() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the license of use.

getLiftRatio() - Method in class org.orekit.forces.Panel

Get drag lift ratio.

getLightingRatio(SpacecraftState) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the lighting ratio ([0-1]).

getLightingRatio(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the lighting ratio ([0-1]).

getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles

Get limb radius in occulting/occulted plane.

getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles

Get limb radius in occulting/occulted plane.

getLine1() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the first line.

getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the first line.

getLine2() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the second line.

getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the second line.

getLinearInterpolation(AbsoluteDate, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.

getLinearInterpolation(AbstractSolarActivityData<L, D>.LocalSolarActivity, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.

getLineNumber() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the number of the line in the CCSDS data message.

getLineNumber() - Method in class org.orekit.files.rinex.section.RinexComment

Get the line number.

getListAppliedDCBS() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the applied differential code bias corrections.

getListAppliedDCBS() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the list of applied differential code bias corrections.

getListAppliedPCVS() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the applied phase center variations.

getListAppliedPCVS() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the list of antenna center variation corrections.

getLJu() - Method in class org.orekit.data.BodiesElements

Get the mean Jupiter longitude.

getLJu() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Jupiter longitude.

getLJuDot() - Method in class org.orekit.data.BodiesElements

Get the mean Jupiter longitude time derivative.

getLJuDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Jupiter longitude time derivative.

getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Compute the limits in L, the true longitude, for integration.

getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Compute the limits in L, the true longitude, for integration.

getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Compute the limits in L, the true longitude, for integration.

getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Compute the limits in L, the true longitude, for integration.

getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Compute the limits in L, the true longitude, for integration.

getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Compute the limits in L, the true longitude, for integration.

getLM() - Method in class org.orekit.orbits.CartesianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.CircularOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.FieldOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.orbits.Orbit

Get the mean longitude argument.

getLM() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the mean longitude argument (as per equinoctial parameters).

getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the mean longitude.

getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the mean longitude.

getLM() - Method in class org.orekit.propagation.SpacecraftState

Get the mean longitude argument (as per equinoctial parameters).

getLMa() - Method in class org.orekit.data.BodiesElements

Get the mean Mars longitude.

getLMa() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mars longitude.

getLMaDot() - Method in class org.orekit.data.BodiesElements

Get the mean Mars longitude time derivative.

getLMaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mars longitude time derivative.

getLMDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.CircularOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.FieldOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean longitude argument derivative.

getLMDot() - Method in class org.orekit.orbits.Orbit

Get the mean longitude argument derivative.

getLMe() - Method in class org.orekit.data.BodiesElements

Get the mean Mercury longitude.

getLMe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mercury longitude.

getLMeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Mercury longitude time derivative.

getLMeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Mercury longitude time derivative.

getLNe() - Method in class org.orekit.data.BodiesElements

Get the mean Neptune longitude.

getLNe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Neptune longitude.

getLNeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Neptune longitude time derivative.

getLNeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Neptune longitude time derivative.

getLNFifthString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS l_n Word extracted from fifth string of the subframe.

getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients

Get the value of L_n^s(γ).

getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of L_n^s(γ).

getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS l_n Word extracted from third string of the subframe.

getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get astronomical unit.

getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get a constant defined in the ephemerides headers.

getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager

Get an unmodifiable view of the set of data file names that have been loaded.

getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get Earth/Moon mass ratio.

getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get the gravitational coefficient of a body.

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException

getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException

getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages

getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the local timing system configuration ID.

getLocation() - Method in class org.orekit.gnss.DOP

Gets the location with respect to the Earth where DOP was calculated.

getLod() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the length of day.

getLOD() - Method in class org.orekit.frames.EOPEntry

Get the LoD (Length of Day) value.

getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the LoD (Length of Day) value.

getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the LoD (Length of Day) value.

getLOF() - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance LOF type.

getLOF() - Method in class org.orekit.propagation.StateCovariance

Get the covariance LOF type.

getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the lofCartesianOrbitalParametersEvolution.

getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the lofType.

getLofType() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame

Get the type of Local Orbital frame.

getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger

Get an immutable copy of the logged events.

getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger

Get an immutable copy of the logged events.

getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the longitude.

getLongitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the longitude.

getLongitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the longitude.

getLongitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the longitude.

getLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Get the fixed longitude to be crossed (radians).

getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Get the fixed longitude to be crossed (radians).

getLossOfLockIndicator() - Method in class org.orekit.files.rinex.observation.ObservationData

Get the Loss of Lock Indicator.

getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions

Get the Love numbers.

getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Get the low elevation threshold value for path delay computation.

getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month

Get the lower case three letters abbreviation.

getLowerCaseName() - Method in enum org.orekit.time.Month

Get the lower case full name.

getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get ω.

getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get ω.

getLowerLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Get lower limit of the probability of collision value.

getLowerLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision

Get lower limit of the probability of collision value.

getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get a reference to the lower triangular matrix of the decomposition.

getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem

Get the position of the Lagrangian point in the CR3BP Rotating frame.

getLPrime() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Sun.

getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Sun.

getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean anomaly of the Sun time derivative.

getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean anomaly of the Sun time derivative.

getLSa() - Method in class org.orekit.data.BodiesElements

Get the mean Saturn longitude.

getLSa() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Saturn longitude.

getLSaDot() - Method in class org.orekit.data.BodiesElements

Get the mean Saturn longitude time derivative.

getLSaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Saturn longitude time derivative.

getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the last 81-day arithmetic average of F10.7 (adjusted).

getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the last 81-day arithmetic average of F10.7 (observed).

getLUr() - Method in class org.orekit.data.BodiesElements

Get the mean Uranus longitude.

getLUr() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Uranus longitude.

getLUrDot() - Method in class org.orekit.data.BodiesElements

Get the mean Uranus longitude time derivative.

getLUrDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Uranus longitude time derivative.

getLv() - Method in class org.orekit.orbits.CartesianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.CircularOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.FieldOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true longitude argument.

getLv() - Method in class org.orekit.orbits.Orbit

Get the true longitude argument.

getLv() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the true latitude argument (as per equinoctial parameters).

getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the true longitude.

getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the true longitude.

getLv() - Method in class org.orekit.propagation.SpacecraftState

Get the true latitude argument (as per equinoctial parameters).

getLvDot() - Method in class org.orekit.orbits.CartesianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.CircularOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.FieldOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true longitude argument derivative.

getLvDot() - Method in class org.orekit.orbits.Orbit

Get the true longitude argument derivative.

getLVe() - Method in class org.orekit.data.BodiesElements

Get the mean Venus longitude.

getLVe() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Venus longitude.

getLVeDot() - Method in class org.orekit.data.BodiesElements

Get the mean Venus longitude time derivative.

getLVeDot() - Method in class org.orekit.data.FieldBodiesElements

Get the mean Venus longitude time derivative.

getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion

Return the orbital period of the Halo Orbit.

getM() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS M Word.

getM0() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get M₀.

getM0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get M₀.

getM0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the mean anomaly at reference time.

getM0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Mean Anomaly at Reference Time.

getM2() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the value of the M2 drag parameter.

getM2() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Get the value of the M2 drag parameter.

getM2(AbsoluteDate) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Get the value of the M2 drag parameter.

getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get m2aoA = -2 * a / A.

getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get m2aoA = -2 * a / A.

getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get m2aoA = -2 * a / A.

getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get m2aoA = -2 * a / A.

getMagneticField() - Method in class org.orekit.frames.LocalMagneticFieldFrame

Get geomagnetid field.

getMahalanobisDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Mahalanobis Distance.

getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.CombinedDerivatives

Get the derivatives increments related to the main state.

getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives

Get the derivatives increments related to the main state.

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get the differential equations to integrate (for main state only).

getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get all the names of all managed states.

getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator

Get all the names of all managed states.

getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get basis of this maneuver history data.

getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get identification number of the orbit determination or simulation upon which this maneuver is based.

getManComposition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get maneuver elements of information.

getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get identifier of the device used for this maneuver.

getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get a maneuver.

getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get a maneuver.

getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get a maneuver.

getManeuverable() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the ability of object to maneuver or not.

getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Attitude provider to use.

getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get maneuvers logical blocks.

getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get maneuvers logical blocks.

getManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get a list of all maneuvers.

getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory

Get the maneuvers.

getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get a list of all maneuvers.

getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get a list of all maneuvers.

getManeuversFrequency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).

getManeuversPerYear() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the average number of orbit or attitude maneuvers per year.

getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the maneuver triggers.

getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get epoch of the maneuver reference frame.

getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get maneuver identification number.

getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit

Return a manifold direction from one position on a libration Orbit.

getManNextEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get start time of next maneuver.

getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get identification number of next maneuver.

getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get prediction source on which this maneuver is based.

getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get completion time of previous maneuver.

getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get identification number of previous maneuver.

getManPurpose() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get purpose of maneuver.

getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get the purposes of the maneuver.

getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get reference frame of the maneuver.

getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get manufacturer name.

getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Get maneuver elements of information units.

getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother

Get the map storing the filters for each observation type.

getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Get the map storing the filters for each observation type.

getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView

Get the angular margin to apply (radians).

getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView

Get the angular margin to apply (radians).

getMargin() - Method in class org.orekit.propagation.events.EclipseDetector

Get the angular margin used for eclipse detection.

getMargin() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the angular margin used for eclipse detection.

getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the angular margin to apply (radians).

getMarkerName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get name of the antenna marker.

getMarkerNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get number of the antenna marker.

getMarkerType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get type of the antenna marker.

getMars() - Method in interface org.orekit.bodies.CelestialBodies

Get the Mars singleton body.

getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Mars singleton body.

getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the mass of the object.

getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the mass.

getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the mass.

getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the spacecraft mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Get the mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the mass.

getMass() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Get the mass.

getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the mass.

getMass() - Method in class org.orekit.propagation.FieldSpacecraftState

Gets the current mass.

getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the mass.

getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the mass.

getMass() - Method in class org.orekit.propagation.SpacecraftState

Gets the current mass.

getMass() - Method in class org.orekit.utils.units.Unit

Get the mass exponent.

getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Get the mass depletion effect processor.

getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the mass derivative (i.e.

getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the mass derivative (i.e.

getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the mass derivative (i.e.

getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the mass derivative (i.e.

getMassInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get mass interpolator.

getMassInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get mass interpolator.

getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem

Get the CR3BP mass ratio of the system mu2/(mu1+mu2).

getMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance

Get the covariance matrix.

getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance

Get the covariance matrix.

getMatrix() - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance matrix.

getMatrix() - Method in class org.orekit.propagation.StateCovariance

Get the covariance matrix.

getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Get a line of the matrix.

getMaxAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the maximal altitude for the model.

getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext

Get the value of max power for a/R3 in the serie expansion.

getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the maximum cross-sectional area for collision probability estimation purposes.

getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the maximal degree available in the last file parsed.

getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the maximal degree available in the last file parsed.

getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the maximal order available in the last file parsed.

getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the maximal order available in the last file parsed.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAdapterDetector

Get maximal time interval between switching function checks.

getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get maximal time interval between switching function checks.

getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get the maximal chunks duration.

getMaxCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get max collision probability.

getMaxCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get max collision probability method.

getMaxDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

Get the last date of the range.

getMaxDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider

Get the last date of the range.

getMaxDate() - Method in class org.orekit.attitudes.TabulatedLofOffset

Get the last date of the range.

getMaxDate() - Method in class org.orekit.attitudes.TabulatedProvider

Get the last date of the range.

getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the last date of the range.

getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator

Get the last date of the range.

getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator

Get the last date of the range.

getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the last date of the range.

getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the last date of the range.

getMaxDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider

Get the last date of the range.

getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the maximal supported degree.

getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the maximum supported degree.

getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the maximal supported degree.

getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the maximum of distance among the solutions found.

getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext

Get the value of max power for e in the serie expansion.

getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext

Get the value of max frequency of F.

getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get maximum time between observations in the OD of the object.

getMaximumValidDateForObservationPair(String, String) - Method in class org.orekit.files.sinex.Dcb

Get the maximum valid date for a given observation pair.

getMaximumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.Dcb

Get the maximum valid date for a given observation pair.

getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAdapterDetector

Get maximal number of iterations in the event time search.

getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get maximal number of iterations in the event time search.

getMaxNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).

getMaxNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).

getMaxNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache

Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).

getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the maximal supported order.

getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the maximum supported order.

getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the maximal supported order.

getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter

Get the maximum derivation order.

getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter

Get the maximum derivation order.

getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the degree limit for the next file parsing.

getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the degree limit for the next file parsing.

getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the order limit for the next file parsing.

getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the order limit for the next file parsing.

getMaxPredictedEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.

getMaxRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the maximum radar cross-section.

getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the value of the outlier detection limit.

getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the maximum number of independent cached time slots.

getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the maximum number of solutions seeked.

getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the maximum duration span in seconds of one slot.

getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the maximum composite thrust the spacecraft can accomplish.

getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.

getMaxValue() - Method in class org.orekit.utils.ParameterDriver

Get maximum parameter value.

getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get mCo2AB = -C / 2AB.

getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get mCo2AB = -C / 2AB.

getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get mCo2AB = -C / 2AB.

getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get mCo2AB = -C / 2AB.

getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean anomaly.

getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean anomaly.

getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the mean anomaly.

getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean anomaly.

getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the mean anomaly derivative.

getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the mean anomaly derivative.

getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.FieldOrbit

Get the derivative of the mean anomaly with respect to the semi major axis.

getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.Orbit

Get the derivative of the mean anomaly with respect to the semi major axis.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, AbstractGaussianContribution.GaussQuadrature, T, T, FieldAbstractGaussianContributionContext<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementTheory() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Get the description of the Mean Element Theory.

getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the value of the mean solar flux.

getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the mean solar flux.

getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Get the value of the mean solar flux.

getMeanMotion() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit mean motion.

getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac

Getter for the mean motion.

getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for the mean motion.

getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Mean Motion.

getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the mean motion.

getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the Keplerian mean motion.

getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the Keplerian mean motion.

getMeanMotionDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the first time derivative of the mean motion.

getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the second time derivative of the mean motion.

getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the mean motion first derivative.

getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion first derivative.

getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the mean motion second derivative.

getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the mean motion second derivative.

getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing mean obliquity of the ecliptic.

getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing mean obliquity of the ecliptic.

getMeasurement() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation

Getter for the measurement.

getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement

Get the underlying measurements.

getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the measurements parameters supported by this estimator (including measurements and modifiers).

getMeasurementsParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the measurementsParametersEvolution.

getMeasurementType() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData

Get the measurement type.

getMeasurementType() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the type of measurement.

getMeasurementType() - Method in enum org.orekit.gnss.ObservationType

Get the measurement type.

getMedianDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Get the driver for median date.

getMedianDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Get the driver for median date.

getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the Melbourne-Wübbena combination of measurements.

getMercury() - Method in interface org.orekit.bodies.CelestialBodies

Get the Mercury singleton body.

getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Mercury singleton body.

getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getMergedFiles() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Getter for the number of merged files.

getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException

Gets the message in a specified locale.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitException

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException

getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitInternalError

getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitIOException

getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitParseException

getMessage() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get telemetry message.

getMessageFor() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader

Get the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.

getMessageId() - Method in class org.orekit.files.ccsds.section.Header

Get the ID that uniquely identifies a message from a given originator.

getMessageType(String) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser

Get the message type corresponding to the message number.

getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Get the message type corresponding to a message number.

getMessageType(String) - Method in class org.orekit.gnss.metric.parser.MessagesParser

Get the message type corresponding to the message number.

getMessageType(String) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser

Get the message type corresponding to the message number.

getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType

Get the message type corresponding to a message number.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Get the metadata from the single segment.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory

Get metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm

Get the file metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Get the metadata from the single segment.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory

Get metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory

Get metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Get the file metadata.

getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get the file metadata.

getMetadata() - Method in class org.orekit.files.ccsds.section.Segment

Get the segment metadata.

getMetadataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get the file metadata.

getMetadataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get the file metadata.

getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo

Get the meteorological parameters at a given date.

getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the meteorological data for the data block.

getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the meteorological configuration ID.

getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the meteorological record.

getMeteorologicalRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get meteorological configuration record related to the systemRecord.

getMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get attitude determination method.

getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get orbit determination method.

getMethod() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType

Get probability of collision method.

getMethodType() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType

Get a probability of collision computing method type based on the short term encounter model.

getMHzFrequency() - Method in enum org.orekit.gnss.Frequency

Get the value of the frequency in MHz.

getMilliInWeek() - Method in class org.orekit.time.GNSSDate

Get the number of milliseconds since week start.

getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the minimal altitude for the model.

getMinAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the minimum cross-sectional area for collision probability estimation purposes.

getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider

getMinDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider

Get the first date of the range.

getMinDate() - Method in class org.orekit.attitudes.TabulatedLofOffset

Get the first date of the range.

getMinDate() - Method in class org.orekit.attitudes.TabulatedProvider

Get the first date of the range.

getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris

Get the first date of the range.

getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator

Get the first date of the range.

getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator

Get the first date of the range.

getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the first date of the range.

getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the first date of the range.

getMinDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider

Get the first date of the range.

getMinElevation() - Method in class org.orekit.gnss.DOPComputer

Get the minimum elevation.

getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured minimum valid elevation value.

getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured minimum valid elevation value.

getMinimumValidDateForObservationPair(String, String) - Method in class org.orekit.files.sinex.Dcb

Get the minimum valid date for a given observation pair.

getMinimumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.Dcb

Get the minimum valid date for a given observation pair.

getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.

getMinPredictedEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.

getMinRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the minimum radar cross-section.

getMinute() - Method in class org.orekit.time.TimeComponents

Get the minute number.

getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents

Get the offset between the specified date and UTC.

getMinValue() - Method in class org.orekit.utils.ParameterDriver

Get minimum parameter value.

getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record

Get miscellaneous information.

getMissDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the norm of relative position vector at TCA.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser

Get reference date for Mission Elapsed Time and Mission Relative Time time systems.

getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser

Get reference date for Mission Elapsed Time and Mission Relative Time time systems.

getMjd() - Method in class org.orekit.frames.EOPEntry

Get the entry date (modified julian day, 00h00 UTC scale).

getMJD() - Method in class org.orekit.time.DateComponents

Get the modified julian day.

getMJD() - Method in class org.orekit.time.UTCTAIOffset

Get the date of the start of the leap as Modified Julian Day.

getMJDRef() - Method in class org.orekit.time.OffsetModel

Get the reference date of the linear model as a modified julian day.

getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get μ / a .

getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get μ / a .

getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames

getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames

getMOD(boolean) - Method in interface org.orekit.frames.Frames

Get the MOD reference frame.

getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames

Get the MOD reference frame.

getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the MOD reference frame.

getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the MOD reference frame.

getMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the mode.

getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getModelName() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the model name.

getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Returns a Collection of the GeoMagneticField models that have been successfully loaded.

getModifiedJulianDay() - Method in class org.orekit.files.sp3.SP3Header

Returns the modified julian day for this SP3 file.

getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales

getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates

Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.

getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates

Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.

getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the modifiers that apply to a measurement.

getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the modifiers that apply to a measurement.

getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Get the modifiers that apply to a measurement.

getModifiers() - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Get the modifiers that apply to a measurement.

getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the modifiers that apply to a measurement.

getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the momentum.

getMomentum() - Method in class org.orekit.utils.PVCoordinates

Gets the momentum.

getMomentumAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the right ascension of angular momentum vector (rad).

getMomentumDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the declination of the angular momentum vector (rad).

getMonth() - Method in class org.orekit.time.DateComponents

Get the month.

getMonth(int) - Static method in enum org.orekit.time.Month

Get the month corresponding to a number.

getMonthEnum() - Method in class org.orekit.time.DateComponents

Get the month as an enumerate.

getMoon() - Method in interface org.orekit.bodies.CelestialBodies

Get the Moon singleton body.

getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Moon singleton body.

getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getMoonSemiMajorAxis() - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants

Get the Moon semi-major axis.

getMountPoint() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the mount point.

getMu() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the gravitational coefficient.

getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Get the gravitational coefficient.

getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the standard gravitational parameter for the satellite.

getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.sp3.SP3Segment

Get the standard gravitational parameter for the satellite.

getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the central attraction coefficient μ.

getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the central attraction coefficient μ.

getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the central attraction coefficient μ.

getMu(Field<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the central body attraction coefficient.

getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the central body attraction coefficient.

getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the central body attraction coefficient.

getMu() - Method in class org.orekit.orbits.FieldOrbit

Get the central attraction coefficient used for position and velocity conversions (m³/s²).

getMu() - Method in class org.orekit.orbits.Orbit

Get the central acceleration constant.

getMu() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the Earth's universal gravitational parameter.

getMu() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Earth's universal gravitational parameter.

getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Get the Earth gravity coefficient used for GLONASS propagation.

getMU() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Gets the Earth gravity coefficient used for GNSS propagation.

getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Get the Earth gravity coefficient used for SBAS propagation.

getMU() - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the Earth gravity coefficient used for TLE propagation.

getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the Earth gravity coefficient used for TLE propagation.

getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the central attraction coefficient (µ - m³/s²) value.

getMu() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the central attraction coefficient (µ - m³/s²) value.

getMu() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the central attraction coefficient.

getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.integration.StateMapper

Get the central attraction coefficient μ.

getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get central attraction coefficient.

getMu(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Get the central attraction coefficient μ at specific date.

getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get central attraction coefficient.

getMu() - Method in class org.orekit.propagation.SpacecraftState

Get the central attraction coefficient.

getMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the Multiple Message Indicator.

getMultiplexer() - Method in class org.orekit.propagation.AbstractPropagator

Get the multiplexer holding all step handlers.

getMultiplexer() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the multiplexer holding all step handlers.

getMultiplexer() - Method in interface org.orekit.propagation.FieldPropagator

Get the multiplexer holding all step handlers.

getMultiplexer() - Method in interface org.orekit.propagation.Propagator

Get the multiplexer holding all step handlers.

getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get μ / a .

getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get μ / a .

getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get muoR3 = mu3 / R3.

getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get muoR3 = mu3 / R3.

getMuSet() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser

Get the gravitational coefficient set at construction.

getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Get n.

getN4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the four-year interval number starting from 1996.

getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getN4() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the number of the current four year interval.

getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS N^A Word.

getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getNa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the number of the current day in a four year interval.

getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction below the point, expressed in parent shape frame.

getNadir() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction below the point, expressed in parent shape frame.

getNadir() - Method in class org.orekit.frames.TopocentricFrame

Get the nadir direction of topocentric frame, expressed in parent shape frame.

getName() - Method in interface org.orekit.bodies.CelestialBody

Get the name of the body.

getName() - Method in class org.orekit.bodies.CR3BPSystem

Get the name of the CR3BP system.

getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin

getName() - Method in class org.orekit.data.DataSource

Get the name of the data.

getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Get the name of the combination of measurements.

getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination

Get the name of the combination of measurements.

getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType

Get the name of the combination of measurements.

getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination

Get the name of the combination of measurements.

getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination

Get the name of the combination of measurements.

getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade

Get the CCSDS name for the body.

getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Get the name of celestial body frame.

getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the CCSDS name for the frame.

getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade

Get the name of the method.

getName() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade

Get the name of the method.

getName(double) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Get the type name for a given format version.

getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the name of the block or entry.

getName() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the satellite target name.

getName() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the receiver/satellite name.

getName() - Method in enum org.orekit.files.sinex.Station.ReferenceSystem

Get the name used to define the reference system in SINEX file.

getName() - Method in class org.orekit.forces.maneuvers.jacobians.Duration

Get the name of the additional state.

getName() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Get the name of the additional derivatives (which will become state once integrated).

getName() - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate

Get the name of the additional state.

getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Get the name of the additional state.

getName() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the name of the maneuver.

getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the maneuver name.

getName() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the maneuver name.

getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Get the maneuver name.

getName() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Get the maneuver name.

getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Get the maneuver name.

getName() - Method in class org.orekit.frames.encounter.DefaultEncounterLOF

Get name of the local orbital frame.

getName() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame

Get name of the local orbital frame.

getName() - Method in class org.orekit.frames.Frame

Get the name.

getName() - Method in enum org.orekit.frames.ITRFVersion

Get the name the frame version.

getName() - Method in class org.orekit.frames.LocalMagneticFieldFrame

Get name of the local orbital frame.

getName() - Method in interface org.orekit.frames.LOF

Get name of the local orbital frame.

getName() - Method in enum org.orekit.frames.LOFType

Get name of the local orbital frame.

getName() - Method in enum org.orekit.frames.Predefined

Get the name of the frame.

getName() - Method in enum org.orekit.gnss.antenna.SatelliteType

Get the IGS name for the antenna code.

getName() - Method in enum org.orekit.gnss.Frequency

Get the RINEX name for the frequency.

getName() - Method in interface org.orekit.propagation.AdditionalStateProvider

Get the name of the additional state.

getName() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the name of the additional state.

getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider

Get the name of the additional state.

getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Get the name of the additional state.

getName() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider

Get the name of the additional derivatives (which will become state once integrated).

getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider

Get the name of the additional derivatives (which will become state once integrated).

getName() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations

Get the name of the additional derivatives (which will become state once integrated).

getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Get the name of the additional derivatives (which will become state once integrated).

getName() - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the name of the additional state.

getName() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Get name of the method.

getName() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Get name of the method.

getName() - Method in class org.orekit.time.BDTScale

Get the name time scale.

getName() - Method in class org.orekit.time.GalileoScale

Get the name time scale.

getName() - Method in class org.orekit.time.GLONASSScale

Get the name time scale.

getName() - Method in class org.orekit.time.GMSTScale

Get the name time scale.

getName() - Method in class org.orekit.time.GPSScale

Get the name time scale.

getName() - Method in class org.orekit.time.IRNSSScale

Get the name time scale.

getName() - Method in class org.orekit.time.QZSSScale

Get the name time scale.

getName() - Method in class org.orekit.time.SatelliteClockScale

Get the name time scale.

getName() - Method in class org.orekit.time.TAIScale

Get the name time scale.

getName() - Method in class org.orekit.time.TCBScale

Get the name time scale.

getName() - Method in class org.orekit.time.TCGScale

Get the name time scale.

getName() - Method in class org.orekit.time.TDBScale

Get the name time scale.

getName() - Method in interface org.orekit.time.TimeScale

Get the name time scale.

getName() - Method in class org.orekit.time.TTScale

Get the name time scale.

getName() - Method in class org.orekit.time.UT1Scale

Get the name time scale.

getName() - Method in class org.orekit.time.UTCScale

Get the name time scale.

getName() - Method in class org.orekit.utils.ParameterDriver

Get parameter driver general name.

getName() - Method in class org.orekit.utils.units.Unit

Get the name of the unit.

getNameSpan(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get name of the parameter span for a specific date.

getNamesSpanMap() - Method in class org.orekit.utils.ParameterDriver

Get current name span map of the parameterDriver, cut in interval in accordance with value span map and validity period.

getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the Narrow-Lane combination of measurements.

getNavigationMessageType() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage

Get navigation message type.

getNavigationSystem(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem

Get the navigation system corresponding to a keyword.

getNavigationSystems() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the navigation systems.

getNbInterpolationPoints() - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get the number of interpolation points.

getNbInterpolationPoints() - Method in class org.orekit.time.AbstractTimeInterpolator

Get the number of interpolation points.

getNbInterpolationPoints() - Method in interface org.orekit.time.FieldTimeInterpolator

Get the number of interpolation points.

getNbInterpolationPoints() - Method in interface org.orekit.time.TimeInterpolator

Get the number of interpolation points.

getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the number of maneuvers present in the APM.

getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get the number of maneuvers present in the OPM.

getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the number of maneuvers present in the APM.

getNbObsPerSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get an unmodifiable view of the map of number of observations per satellites.

getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get n-body perturbation bodies.

getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get n-body perturbation bodies.

getNbOfValues() - Method in class org.orekit.utils.ParameterDriver

Get the number of values to estimate that is to say the number.

getNbParametersDriversValue() - Method in interface org.orekit.utils.ParameterDriversProvider

Get total number of spans for all the parameters driver.

getNbParams() - Method in class org.orekit.utils.ParameterDriversList

Get the number of parameters with different names.

getNbSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get number of satellites.

getNbSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Get number of noise elements for sensor.

getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the number of species.

getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get number of states for AdMethodType.EKF, AdMethodType.BATCH or AdMethodType.FILTER_SMOOTHER.

getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get the number of data states included (attitude components plus rates components).

getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the number of tides for one species.

getNbValuesToEstimate() - Method in class org.orekit.utils.ParameterDriversList

Get the number of values to estimate for parameters with different names.

getNdFilterValue() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the neutral density (ND) filter value.

getNeighborList() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get neighbor list.

getNeighborList() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData

Get neighbor list.

getNeighbors(AbsoluteDate, int) - Method in class org.orekit.frames.EOPHistory

Get the entries surrounding a central date.

getNeighbors(FieldAbsoluteDate<KK>) - Method in interface org.orekit.utils.FieldTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.GenericTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(FieldAbsoluteDate<KK>) - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.ImmutableTimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache

Get the entries surrounding a central date.

getNeighbors(AbsoluteDate, int) - Method in interface org.orekit.utils.TimeStampedCache

Get the entries surrounding a central date.

getNeighborsSize() - Method in interface org.orekit.utils.FieldTimeStampedCache

Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).

getNeighborsSize() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).

getNeptune() - Method in interface org.orekit.bodies.CelestialBodies

Get the Neptune singleton body.

getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Neptune singleton body.

getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getNeQuickAlpha() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the "alpha" ionospheric parameters.

getNequickGMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the ionosphere Nequick-G messages.

getNetwork() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the network.

getNetworkIdentifier() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the network identifier.

getNetworkInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the web address for network information.

getNetworks() - Method in class org.orekit.gnss.metric.ntrip.SourceTable

Get the networks records.

getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache

Get quantum gap above which a new slot is created instead of extending an existing one.

getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the new state for a reset action.

getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the new state for a reset action.

getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the epoch of next leap second.

getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the epoch of next leap second.

getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the difference (TAI – UTC) in seconds incorporated at epoch AcmMetadata.getNextLeapEpoch().

getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().

getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.

getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the creation date of next message from a given originator.

getNextMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the unique ID identifying next message from a given originator.

getNextParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity

getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the body Q Node direction in ICRF frame.

getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the body Q Node direction in ICRF frame.

getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Generate a noise vector.

getNominalFireRate() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the nominal fire rate.

getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions

Get the nominal values of the displacement numbers.

getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider

Get a version of the provider that does not cache tidal corrections.

getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider

Get a version of the provider that does not cache tidal corrections.

getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory

Get the transform between two frames, suppressing all interpolation.

getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory

Get the transform between two frames, suppressing all interpolation.

getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries

Get the number of different terms in the non-polynomial part.

getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for Non-Rotating Origin paradigm.

getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for Non-Rotating Origin paradigm.

getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the NORAD Catalog Number ("Satellite Number").

getNoradId() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the satellite NORAD ID (i.e.

getNormal(SpacecraftState) - Method in class org.orekit.forces.FixedPanel

Get panel normal in spacecraft frame.

getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.FixedPanel

Get panel normal in spacecraft frame.

getNormal(SpacecraftState) - Method in class org.orekit.forces.Panel

Get panel normal in spacecraft frame.

getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.Panel

Get panel normal in spacecraft frame.

getNormal(SpacecraftState) - Method in class org.orekit.forces.PointingPanel

Get panel normal in spacecraft frame.

getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.PointingPanel

Get panel normal in spacecraft frame.

getNormal(SpacecraftState) - Method in class org.orekit.forces.SlewingPanel

Get panel normal in spacecraft frame.

getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.SlewingPanel

Get panel normal in spacecraft frame.

getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.

getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.

getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.

getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields

Get a gravity field normalized coefficients provider.

getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get a gravity field normalized coefficients provider.

getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic sine coefficient.

getNormalizedValue(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get normalized value at specific date.

getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver

Get normalized value.

getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the north of point, expressed in parent shape frame.

getNorth() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the north of point, expressed in parent shape frame.

getNorth() - Method in class org.orekit.frames.TopocentricFrame

Get the north direction of topocentric frame, expressed in parent shape frame.

getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along North axis.

getNt() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the current date.

getNtripFlags() - Method in class org.orekit.gnss.metric.ntrip.SourceTable

Get the flags set by server.

getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider

Get the number of evaluations available.

getNumber() - Method in enum org.orekit.time.Month

Get the month number.

getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Get the number of biases processed for the current satellite.

getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Get the number of biases processed for the current satellite.

getNumberOfClockDataTypes() - Method in class org.orekit.files.rinex.clock.RinexClock

Get the number of different clock data types in the file.

getNumberOfConstraints() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Get the total number of constraints.

getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting

Get the total number of constraints.

getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3Header

Returns the number of epochs contained in this orbit file.

getNumberOfFreeComponents() - Method in class org.orekit.utils.AbstractMultipleShooting

Get the number of free state components.

getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header

Get the number of ionospheric layers.

getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the number of leap seconds.

getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Getter for the current number of leap seconds.

getNumberOfLeapSecondsGNSS() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the number of leap second for GNSS time scales.

getNumberOfPointsRecorded() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the number of data points recorded.

getNumberOfPointsUsed() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the number of data points used.

getNumberOfRawRanges() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the umber of raw ranges (after editing) compressed into the normal point.

getNumberOfReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock

Get the number of receivers that are considered in the file.

getNumberOfSatellites() - Method in class org.orekit.files.rinex.clock.RinexClock

Get the number of satellites that are considered in the file.

getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the number of satellites for the current IGM message.

getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader

Get the number of satellites for the current IGM message.

getNumberOfValues() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine

Getter for the number of values to follow.

getNumberSelectedMeasurementDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the number of estimated measurement parameters.

getNumberSelectedOrbitalDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the number of estimated orbital parameters.

getNumberSelectedPropagationDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the number of estimated propagation parameters.

getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the nutation angle of spin axis (rad).

getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the fundamental nutation arguments.

getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the fundamental nutation arguments.

getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the fundamental nutation arguments.

getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions

Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.

getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.

getNutationFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the nutation angles.

getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the nutation angles.

getNutationPeriod() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the body nutation period of the spin axis (s).

getNutationPhase() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the inertial nutation phase (rad).

getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions

Get the reference epoch for fundamental nutation arguments.

getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the reference epoch for fundamental nutation arguments.

getNutationVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the angular velocity of spin vector around angular momentum vector.

getNutLn() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the nutation correction in longitude.

getNutOb() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the nutation correction in obliquity.

getNutX() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the nutation correction X.

getNutY() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the nutation correction Y.

getObject() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the object name for which metadata are given.

getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the unique satellite identification designator for the object.

getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the object satellite catalog designator for which metadata are given.

getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the unique satellite identification designator for the object.

getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the spacecraft ID for which the attitude data are provided.

getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the spacecraft ID for which the orbit state is provided.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the function computing position/velocity at sample points.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Get the function computing position/velocity at sample points.

getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter

Get the function computing position/velocity at sample points.

getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Get the spacecraft name for which the attitude data are provided.

getObjectName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the spacecraft name for the object.

getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata

Get the spacecraft name for which the orbit state is provided.

getObjectOrbitFromCdm(CdmRelativeMetadata, CdmData, CdmMetadata, DataContext) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Extract collision object spacecraft state from given Conjunction Data Message data.

getObjectStateCovarianceFromCdm(CdmRelativeMetadata, CdmData) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Get collision object state covariance from given Conjunction Data Message data.

getObjectType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the type of object.

getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the type of object.

getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get central body oblate spheroid oblateness.

getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the number of observations available for the OD of the object.

getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of observations available within the actual OD span.

getObsBeforeNextMessage() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.

getObservationCode() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the observation code of the average phasecenter position w/r to antenna reference point.

getObservationData() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Get list of observation data.

getObservationData() - Method in class org.orekit.files.rinex.observation.ObservationDataSet

Get list of observation data.

getObservationDataSets() - Method in class org.orekit.files.rinex.observation.RinexObservation

Get an unmodifiable view of the observations.

getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock

Get the list of Observations data lines.

getObservationSampling() - Method in class org.orekit.files.sinex.DcbDescription

Get the observation sampling interval used for data analysis.

getObservationTimeScale() - Method in enum org.orekit.gnss.SatelliteSystem

Get observation time scale for satellite system.

getObservationType() - Method in class org.orekit.files.rinex.observation.ObservationData

Get the observation type.

getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularAzEl

Calculate the Line Of Sight of the given measurement.

getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularRaDec

Calculate the Line Of Sight of the given measurement.

getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the associated observed measurement.

getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

Get the observed measurement.

getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the observed value.

getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement

Get the observed value.

getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the observed value.

getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the observer for Kalman Filter estimations.

getObserver() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Get the observer for Kalman Filter estimations.

getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the observer for Kalman Filter estimations.

getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the observer for the spacecraft.

getObserverName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get name of the observer.

getObservers() - Method in class org.orekit.utils.ParameterDriver

Get the observers for this driver.

getObsUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the number of observations accepted for the OD of the object.

getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of observations accepted within the actual OD span.

getOccultationEngine() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occultation engine.

getOccultationEngine() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the occultation engine.

getOcculted() - Method in class org.orekit.utils.OccultationEngine

Getter for the occulted body.

getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles

Get apparent radius of occulted body.

getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles

Get apparent radius of occulted body.

getOccultedRadius() - Method in class org.orekit.utils.OccultationEngine

Getter for the occultedRadius.

getOcculting() - Method in class org.orekit.utils.OccultationEngine

Getter for the occulting body.

getOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel

Get all occulting bodies to consider.

getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the configured ocean load deformation coefficients.

getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get the configured ocean load deformation coefficients.

getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).

getOceanTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get ocean tides model.

getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the ocean tides waves from the first supported file.

getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields

Get the ocean tides waves.

getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get the ocean tides waves.

getOcmDataElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the list of elements of information data blocks included in this message.

getOdEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the epoch of the orbit determination used for this message.

getOdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the Unique identifier of Orbit Data Message linked to this Attitude Data Message.

getOdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.

getODParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the OD parameters logical block.

getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.

getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.

getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.

getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the intermediate physical dimension of the OEB.

getOebMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the maximum physical dimension of the OEB.

getOebMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the minimum physical dimension of the OEB.

getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the Optimally Enclosing Box parent reference frame.

getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the Optimally Enclosing Box parent reference frame epoch.

getOebQ() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the quaternion defining Optimally Enclosing Box.

getOffset() - Method in class org.orekit.time.OffsetModel

Offset at reference date in seconds (TAI minus UTC).

getOffset(AbsoluteDate) - Method in class org.orekit.time.UTCTAIOffset

Get the TAI - UTC offset in seconds.

getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCTAIOffset

Get the TAI - UTC offset in seconds.

getOffset(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCTAIOffset

Get the TAI - UTC offset in seconds.

getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation

Get the geodetic point at the center of the offset frame.

getOffsetToInertial(Frame, AbsoluteDate, boolean) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame.

getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame with derivatives.

getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation

Get the transform between offset frame and inertial frame with derivatives.

getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get transform between station and inertial frame.

getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get transform between station and inertial frame.

getOmega() - Method in class org.orekit.data.DelaunayArguments

Get the mean longitude of the ascending node of the Moon.

getOmega() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean longitude of the ascending node of the Moon.

getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the longitude of ascending node of orbit plane at weekly epoch.

getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.

getOmegaDot() - Method in class org.orekit.data.DelaunayArguments

Get the mean longitude of the ascending node of the Moon time derivative.

getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments

Get the mean longitude of the ascending node of the Moon time derivative.

getOmegaDot() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get dot(Ω).

getOmegaDot() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get dot(Ω).

getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the rate of right ascension.

getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Rate of Right Ascension.

getOne() - Method in class org.orekit.orbits.FieldOrbit

Getter for Field-valued one.

getOne() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get one.

getOneWayDistance() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the one-way target distance (nominal).

getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get ooA = 1 / A.

getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get ooA = 1 / A.

getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get ooAB = 1 / (A * B).

getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get ooAB = 1 / (A * B).

getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get ooAB = 1 / (A * B).

getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get ooBpo = 1 / (B + 1).

getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get ooBpo = 1 / (B + 1).

getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get ooMu = 1 / mu.

getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get ooMu = 1 / mu.

getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get 1 / (n² * a²).

getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get 1 / (n² * a²).

getOpener() - Method in class org.orekit.data.DataSource

Get the data stream opener.

getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the operator of the space object.

getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the institution/agency/company operating the caster.

getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the institution/agency/company operating the caster.

getOperatorContactPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the contact position of the owner / operator of the object.

getOperatorEmail() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the email of the operator of the object.

getOperatorOrganization() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the contact organisation of the object.

getOperatorPhone() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the contact phone of the operator of the object.

getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the operational status.

getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the optimum found.

getOrbAveraging() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get type of averaging (Osculating, mean Brouwer, other.

getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the current orbit.

getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the orbit.

getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the orbit.

getOrbit() - Method in class org.orekit.propagation.SpacecraftState

Get the current orbit.

getOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Get the underlying GNSS orbital elements.

getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the orbital parameters supported by this estimator.

getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the orbital parameters supported by this estimator.

getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the drivers for the configurable orbital parameters.

getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the drivers for the configurable orbital parameters.

getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection

Get the orbital period of the required orbit.

getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit

Return the orbital period of the libration orbit.

getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the orbit category.

getOrbitCenter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the central body for object 1 and 2.

getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Get the orbit correction data.

getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData

Get the orbit correction data.

getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data

Get the orbit correction data.

getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Get the orbit correction data.

getOrbitDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get orbit determination logical block.

getOrbitInterpolator() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Get orbit interpolator.

getOrbitInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get orbit interpolator.

getOrbitInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get orbit interpolator.

getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get the Keplerian period.

getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get the Keplerian period.

getOrbitType() - Method in class org.orekit.files.sp3.SP3Header

Returns the SP3OrbitType for this SP3 file.

getOrbitType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the orbit type used for the matrix computation.

getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the orbit type defining the angle type.

getOrbitType() - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance orbit type.

getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper

Get propagation parameter type.

getOrbitType() - Method in interface org.orekit.propagation.MatricesHarvester

Get the orbit type used for the matrix computation.

getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the orbit type used for the matrix computation.

getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get propagation parameter type.

getOrbitType() - Method in class org.orekit.propagation.StateCovariance

Get the covariance orbit type.

getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3Header

Returns the orbit type key for this SP3 file.

getOrbRevNum() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the integer orbit revolution number.

getOrbRevNumBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the basis for orbit revolution number.

getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the ordinate grid for the interpolation function.

getOrientation() - Method in class org.orekit.attitudes.Attitude

Get the complete orientation including spin.

getOrientation() - Method in class org.orekit.attitudes.FieldAttitude

Get the complete orientation including spin.

getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the origin ITRF.

getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter

Get the origin ITRF.

getOriginal() - Method in class org.orekit.propagation.events.FieldNegateDetector

Get the delegate event detector.

getOriginal() - Method in class org.orekit.propagation.events.NegateDetector

Get the delegate event detector.

getOriginator() - Method in class org.orekit.files.ccsds.section.Header

Get the message originator.

getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the address of Programmatic Point Of Contact at originator.

getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the address of Programmatic Point Of Contact at originator.

getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the email address of Programmatic Point Of Contact at originator.

getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the email address of Programmatic Point Of Contact at originator.

getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the phone number of Programmatic Point Of Contact at originator.

getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the phone number of Programmatic Point Of Contact at originator.

getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the programmatic Point Of Contact at originator.

getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the programmatic Point Of Contact at originator.

getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the position of Programmatic Point Of Contact at originator.

getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the position of Programmatic Point Of Contact at originator.

getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the angle origin indicator.

getOriginOfValues() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get the origin of values.

getOther() - Method in class org.orekit.frames.encounter.AbstractEncounterLOF

Get the normal version of other's position and velocity coordinates.

getOther() - Method in interface org.orekit.frames.encounter.EncounterLOF

Get other's position and velocity coordinates.

getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get other's orbit at time of closest approach.

getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get other's orbit at time of closest approach.

getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get other's covariance.

getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get other's covariance.

getOutFrame() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Get output frame.

getOutLOF() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Get output local orbital frame.

getOutOrbitType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Get output orbit type.

getOutPositionAngleType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Get output position angle type.

getOutputFrame() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get output frame.

getOutputFrame() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get output frame.

getOutputFrame() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Get output frame for the interpolated instance.

getOutputFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Get output frame for the interpolated instance.

getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractFieldOrbitInterpolator

Get output inertial frame.

getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractOrbitInterpolator

Get output inertial frame.

getOutputName() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Get the name of the output (for error messages).

getOutputName() - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Get the name of the output (for error messages).

getOutputPulseType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the output pulse type.

getOutputPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the output pulse width.

getOwner() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the owner of the space object.

getP() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS P Word.

getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the y component of inclination vector.

getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the y component of inclination vector.

getP1() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS P1 Word.

getP2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS P2 Word.

getP3() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS P3 Word.

getP4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS P4 Word.

getPa() - Method in class org.orekit.data.BodiesElements

Get the general accumulated precession in longitude.

getPa() - Method in class org.orekit.data.FieldBodiesElements

Get the general accumulated precession in longitude.

getPa() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit argument of pericenter.

getPa() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the argument of perigee.

getPa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the Argument of Perigee.

getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Argument of Perigee.

getPaDot() - Method in class org.orekit.data.BodiesElements

Get the general accumulated precession in longitude time derivative.

getPaDot() - Method in class org.orekit.data.FieldBodiesElements

Get the general accumulated precession in longitude time derivative.

getPanels() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the panels composing the body.

getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the partial derivatives of the simulated measurement with respect to a parameter.

getParameterDerivatives(ParameterDriver, AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the partial derivatives of the simulated measurement with respect to a parameter.

getParameterDriver(String) - Method in interface org.orekit.utils.ParameterDriversProvider

Get parameter value from its name.

getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined

Get all user defined parameters.

getParameters(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Get the parametric model parameters, return gradient values for each span of each driver (several gradient values for each parameter).

getParameters() - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters.

getParameters(AbsoluteDate) - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters.

getParameters(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters.

getParameters(Field<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters.

getParametersAllValues() - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters, return a list a all span values of all parameters.

getParametersAllValues(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider

Get model parameters.

getParametersAtStateDate(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Get the parametric model parameters, return gradient values at state date for each driver (only 1 gradient value for each parameter).

getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier

Get the drivers for this modifier parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel

getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel

getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the parameters driver for propagation model.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the drivers for TLE propagation SGP4 and SDP4.

getParametersDrivers() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Get the drivers for parameters.

getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Get the drivers for parameters.

getParametersDrivers() - Method in interface org.orekit.utils.ParameterDriversProvider

Get the drivers for parameters.

getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Get the drivers for force model parameters except the one for the central attraction coefficient.

getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the drivers for force model parameters except the one for the central attraction coefficient.

getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get the drivers for force model parameters except the one for the central attraction coefficient.

getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester

Get the Jacobian with respect to propagation parameters.

getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the Jacobian with respect to propagation parameters.

getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester

Get the Jacobian with respect to propagation parameters.

getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the Jacobian with respect to propagation parameters.

getParameterSpacing() - Method in class org.orekit.files.sinex.DcbDescription

Get the parameter spacing interval between the bias value.

getParent() - Method in class org.orekit.frames.Frame

Get the parent frame.

getParentShape() - Method in class org.orekit.frames.TopocentricFrame

Get the body shape on which the local point is defined.

getParsedEop() - Method in class org.orekit.files.sinex.SinexLoader

Get the parsed EOP data.

getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Get the behavior to adopt for handling parsed units.

getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get the behavior to adopt for handling parsed units.

getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Get the behavior to adopt for handling parsed units.

getParser(List<Integer>) - Method in enum org.orekit.gnss.metric.ntrip.Type

Get the message parser associated to the SSR type.

getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the coordinates of the measurements participants in signal travel order.

getParticipants() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the participants.

getParts() - Method in interface org.orekit.errors.LocalizedException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitInternalError

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitIOException

Get the variable parts of the error message.

getParts() - Method in exception org.orekit.errors.OrekitParseException

Get the variable parts of the error message.

getPastInfinity() - Method in class org.orekit.time.AbstractTimeScales

getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Dummy date at infinity in the past direction.

getPastInfinity() - Method in interface org.orekit.time.TimeScales

Dummy date at infinity in the past direction.

getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting

Get the list of patched spacecraft states.

getPatchPoint(int) - Method in class org.orekit.utils.AbstractMultipleShooting

Get a patch point.

getPath() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the path.

getPath1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the path1.

getPath2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the path2.

getPattern(Frequency) - Method in class org.orekit.gnss.antenna.Antenna

Get a frequency pattern.

getPattern() - Method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Get the message number.

getPattern() - Method in enum org.orekit.gnss.metric.parser.RtcmMessageType

Get the message number.

getPdop() - Method in class org.orekit.gnss.DOP

Gets the position dilution of precision.

getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the system delay peak – mean value.

getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get the session peak – mean value.

getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState

Get PendingEvent.

getPeriapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the distance of the closest point in the objects orbit above the equatorial radius of the central body.

getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the perigee argument.

getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit

Get the perigee argument.

getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the argument of perigee.

getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the argument of perigee.

getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the perigee argument derivative.

getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the perigee argument derivative.

getPermanentTide() - Method in enum org.orekit.utils.IERSConventions

Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.

getPerturbationsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get perturbations logical block.

getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide

Get the phase of the tide.

getPhaseBias() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias

Get the phase bias associated to the signal ID.

getPhaseBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Get the phase bias for a given signal ID.

getPhaseBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Get the phase biases for the current satellite.

getPhaseCenterSystem() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get satellite system for average phase center.

getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna

Get the value of the phase center variation in a signal direction.

getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern

Get the value of the phase center variation in a signal direction.

getPhaseCenterVariationFunction() - Method in class org.orekit.gnss.antenna.FrequencyPattern

Get the phase center variation function.

getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the phase minus code combination of measurements.

getPhaseShiftCorrections() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.

getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the covariances matrix in space flight dynamics physical units.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the "physical" estimated covariance matrix (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the "physical" estimated state (i.e.

getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the "physical" estimated state (i.e.

getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical innovation covariance matrix.

getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the physical innovation covariance matrix.

getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the physical innovation covariance matrix.

getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the physical innovation covariance matrix.

getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the physical innovation covariance matrix.

getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical Kalman gain matrix.

getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the physical Kalman gain matrix.

getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the physical Kalman gain matrix.

getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the physical Kalman gain matrix.

getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the physical Kalman gain matrix.

getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the physical Jacobian of the measurement with respect to the state (H matrix).

getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get physical state transition matrix between previous state and estimated (but not yet corrected) state.

getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get physical properties logical block.

getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get physical properties logical block.

getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.

getPlaneSection(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid

Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.

getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the real part of a nominal Love numbers.

getPluto() - Method in interface org.orekit.bodies.CelestialBodies

Get the Pluto singleton body.

getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Pluto singleton body.

getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getPnm(int, int) - Method in class org.orekit.utils.FieldLegendrePolynomials

Return the coefficient P_nm.

getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials

Return the coefficient P_nm.

getPoint() - Method in class org.orekit.bodies.Loxodrome

Get the geodetic point defining the loxodrome.

getPoint() - Method in class org.orekit.frames.TopocentricFrame

Get the surface point defining the origin of the frame.

getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the surface point defining the origin of the frame.

getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar drift along X.

getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar drift along X.

getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar drift along Y.

getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar drift along Y.

getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar offset along X.

getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar offset along X.

getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a polar offset along Y.

getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a polar offset along Y.

getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Get the radius of this ellipsoid at the poles.

getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the body North pole direction in ICRF frame.

getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the body North pole direction in ICRF frame.

getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the pole IERS Reference Pole correction.

getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the pole IERS Reference Pole correction.

getPolynomial() - Method in class org.orekit.data.PoissonSeries

Get the polynomial part of the series.

getPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the port number.

getPort() - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Get the port to use for connection.

getPosition() - Method in class org.orekit.estimation.measurements.Position

Get the position.

getPosition() - Method in class org.orekit.estimation.measurements.PV

Get the position.

getPosition() - Method in class org.orekit.files.sinex.Station

Get the station position.

getPosition(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame

Get the position of the body in the selected frame.

getPosition(Frame) - Method in class org.orekit.orbits.FieldOrbit

Get the position in a specified frame.

getPosition() - Method in class org.orekit.orbits.FieldOrbit

Get the position in definition frame.

getPosition(Frame) - Method in class org.orekit.orbits.Orbit

Get the position in a specified frame.

getPosition() - Method in class org.orekit.orbits.Orbit

Get the position in definition frame.

getPosition() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the position in orbit definition frame.

getPosition(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState

Get the position in given output frame.

getPosition() - Method in class org.orekit.propagation.SpacecraftState

Get the position in orbit definition frame.

getPosition(Frame) - Method in class org.orekit.propagation.SpacecraftState

Get the position in given output frame.

getPosition(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates

Get the position in a specified frame.

getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider

getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider

getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider

Get the position of the body in the selected frame.

getPosition(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get the position in a specified frame.

getPosition() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the position.

getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider

Get the position of the body in the selected frame.

getPosition() - Method in class org.orekit.utils.PVCoordinates

Gets the position.

getPosition(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider

Get the position of the body in the selected frame.

getPositionAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the position accuracy.

getPositionAngleType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the positionAngle.

getPositionAngleType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Get the position angle used for the matrix computation.

getPositionAngleType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getPositionAngleType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).

getPositionAngleType() - Method in class org.orekit.propagation.events.PositionAngleDetector

Get the type of position angle.

getPositionAngleType() - Method in class org.orekit.propagation.FieldStateCovariance

Get the covariance angle type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper

Get propagation parameter type.

getPositionAngleType() - Method in interface org.orekit.propagation.MatricesHarvester

Get the position angle used for the matrix computation.

getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Get the position angle used for the matrix computation.

getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get propagation parameter type.

getPositionAngleType() - Method in class org.orekit.propagation.StateCovariance

Get the covariance angle type.

getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the position scale.

getPositionVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Get object Position Vector.

getPosVelBase() - Method in class org.orekit.files.sp3.SP3Header

Get the base for position/velocity accuracy.

getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Calculate spacecraft potential.

getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Calculate spacecraft potential.

getPreamble() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get telemetry preamble.

getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the precession angles.

getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the precession angles.

getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the predicted measurement.

getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the predicted measurement.

getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the predicted measurement.

getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the predicted measurement.

getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the predicted measurement.

getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation

Get the predicted spacecraft states.

getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.KalmanModel

Get the predicted spacecraft states.

getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Get the predicted spacecraft states.

getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Get the predicted spacecraft states.

getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel

Get the predicted spacecraft states.

getPredictionProvider() - Method in class org.orekit.files.ilrs.CRDHeader

Get the prediction provider.

getPredictionType() - Method in class org.orekit.files.ilrs.CRDHeader

Get the prediction type (CPF or TLE).

getPressSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the pressure sensor manufacturer.

getPressSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the pressure sensor model.

getPressSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the pressure sensor serial number.

getPressure() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get the surface pressure.

getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Get the local pressure at the evaluation location.

getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Returns the pressure at the station [hPa].

getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel

Get the atmospheric pressure of the station depending its position.

getPrevId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get identification of previous orbit determination.

getPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get identification number of previous maneuver.

getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get identification of previous orbit determination.

getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.

getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the creation date of previous message from a given originator.

getPreviousMessageId() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the ID of previous CDM issued for event identified by CONJUNCTION_ID.

getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the unique ID identifying previous message from a given originator.

getPreviousParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity

getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the state at previous grid point date.

getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the state at previous grid point date.

getPrf() - Method in class org.orekit.files.ilrs.CPFHeader

Get the Pulse Repetition Frequency (PRF).

getPrimary() - Method in class org.orekit.bodies.CR3BPSystem

Get the primary CelestialBody.

getPrimary() - Method in class org.orekit.estimation.measurements.gnss.Dipole

Get the primary dipole vector.

getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Get the primaryObject, at the center of the proximity zone.

getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange

Get the primary ground station from which measurement is performed.

getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the primary wavelength.

getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the prime meridian angle.

getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole

Get the prime meridian angle.

getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a prime meridian rotation rate.

getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a prime meridian rotation rate.

getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a driver allowing to add a prime meridian rotation.

getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to add a prime meridian rotation.

getPrimeStation() - Method in class org.orekit.estimation.measurements.FDOA

Get the prime ground station, the one that gives the date of the measurement.

getPrimeStation() - Method in class org.orekit.estimation.measurements.TDOA

Get the prime ground station, the one that gives the date of the measurement.

getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.

getPrn() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage

Get satellite number.

getPRN() - Method in class org.orekit.files.sinex.DcbSatellite

Return the satellite PRN, as a String.

getPRN() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get the PRN code phase of the SV.

getPRN() - Method in class org.orekit.gnss.SatInSystem

Get the Pseudo Random Number of the satellite.

getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the PRN number of the satellite.

getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the PRN number of the satellite.

getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the PRN number of the GNSS satellite.

getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the PRN number of the SBAS satellite.

getPrnNumber() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Get PRN number.

getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get PRN number.

getPRNNumbers() - Method in class org.orekit.gnss.SEMParser

Gets the PRN numbers of all the GPS almanacs read from the file.

getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser

Gets the PRN numbers of all the GPS almanacs read from the file.

getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Get name of the probability computing method with which this probability was computed.

getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision

Get name of the probability computing method with which this probability was computed.

getProcessingSoftwareName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the processing software name.

getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get the processing softwares.

getProcessingSoftwareVersion() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the processing software version.

getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get the processing software versions.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise

Get the process noise matrix between previous and current states.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider

Get the process noise matrix between previous and current states.

getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Get the process noise matrix between previous and current states.

getProductionEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the date component of the ephemeris production.

getProductionHour() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the hour of ephemeris production (UTC).

getProgDCBS() - Method in class org.orekit.files.rinex.AppliedDCBS

Get the program name used to apply DCBs.

getProgPCVS() - Method in class org.orekit.files.rinex.AppliedPCVS

Get the program name used to apply PCVs.

getProgramName() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the program name.

getProgramName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the program name.

getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator

Get the propagator parameters supported by this estimator.

getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the drivers for the configurable propagation parameters.

getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the drivers for the configurable propagation parameters.

getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise

Getter for the propagationParametersEvolution.

getPropagationType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Get the type of the orbit used for the propagation (mean or osculating).

getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the propagation type.

getPropagationType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Get the propagation type.

getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator

Get a registered propagator.

getPropagator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get the orbit propagator used to generate this trajectory.

getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

View this ephemeris segment as a propagator.

getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

View this ephemeris segment as a propagator.

getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

View this ephemeris as a propagator, combining data from all segments.

getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

View this ephemeris as a propagator, combining data from all segments.

getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

View this ephemeris as a propagator, combining data from all segments.

getPropagator(AttitudeProvider) - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

View this ephemeris as a propagator, combining data from all segments.

getPropagator() - Method in class org.orekit.files.sp3.SP3Segment

View this ephemeris segment as a propagator.

getPropagator(AttitudeProvider) - Method in class org.orekit.files.sp3.SP3Segment

View this ephemeris segment as a propagator.

getPropagator(FieldSpacecraftState<Gradient>, Gradient[]) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter

Get the converted analytical orbit propagator.

getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the reference propagator.

getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the propagator corresponding to the navigation message.

getPropagator(DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the propagator corresponding to the navigation message.

getPropagator(DataContext, AttitudeProvider, Frame, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Get the propagator corresponding to the navigation message.

getPropagator(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagator(double, DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagator(double, DataContext, AttitudeProvider, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagator() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Get the propagator corresponding to the navigation message.

getPropagator(Frames) - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Get the propagator corresponding to the navigation message.

getPropagator(Frames, AttitudeProvider, Frame, Frame, double) - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Get the propagator corresponding to the navigation message.

getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagator(Frames) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagator(Frames, AttitudeProvider, Frame, Frame, double, double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Get the propagator corresponding to the navigation message.

getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite

Get the index of the propagator related to this satellite.

getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Get the propagator parameters supported by this estimator.

getPropagators() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

Get an unmodifiable view of the propagators map.

getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer

Get an unmodifiable list of the underlying mono-satellite propagators.

getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver

Get the propulsion model.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Get the spherical harmonics provider.

getProviders() - Method in class org.orekit.data.DataProvidersManager

Get an unmodifiable view of the list of supported providers.

getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector

Get the proximity angle (rad).

getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Get the proximity angle (rad).

getProxy() - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Get proxy.

getPulsations() - Method in class org.orekit.utils.SecularAndHarmonic

Get the pulsations of harmonic part.

getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the pulse energy.

getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the pulse energy.

getPulseInOutgoingSemiTrain() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the number of pulses in outgoing semi-train.

getPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get the pulse width (FWHM in ps).

getPVAFilter() - Method in class org.orekit.orbits.FieldOrbitHermiteInterpolator

Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.

getPVAFilter() - Method in class org.orekit.orbits.OrbitHermiteInterpolator

Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.

getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Get the position/velocity coordinates contained in the OPM.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame

Get the PVCoordinates of the topocentric frame origin in the selected frame.

getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit

Get the TimeStampedPVCoordinates in definition frame.

getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in definition frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

getPVCoordinates(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the extrapolated position and velocity from an initial TLE.

getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the extrapolated position and velocity from an initial TLE.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState

Get the TimeStampedFieldPVCoordinates in orbit definition frame.

getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState

Get the TimeStampedFieldPVCoordinates in given output frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in orbit definition frame.

getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in given output frame.

getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates

Get the TimeStampedPVCoordinates.

getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.InvalidPVProvider

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get the TimeStampedFieldPVCoordinates.

getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get the TimeStampedFieldPVCoordinates in a specified frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.FrameAdapter

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FrameAdapter

Get the FieldPVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider

Get the PVCoordinates of the body in the selected frame.

getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector

Get the body to align.

getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Get PV coordinates provider.

getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Get PV coordinates provider.

getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector

Get the position/velocity provider of the target .

getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.

getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.

getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the x component of inclination vector.

getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the x component of inclination vector.

getQualityIndicator() - Method in class org.orekit.files.ilrs.CRDHeader

Get the data quality indicator.

getQuantumEfficiency() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the quantum efficiency at applicable wavelength.

getQuaternion() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Get the quaternion.

getQuaternionBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the quaternion logical block.

getQuaternionDot() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Get the quaternion derivative.

getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales

getQZSS() - Method in interface org.orekit.time.TimeScales

Get the Quasi-Zenith Satellite System time scale.

getQZSS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Quasi-Zenith Satellite System time scale.

getQZSSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the QZSS navigation messages contained in the file.

getQZSSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the QZSS navigation messages for the given satellite Id.

getQzssCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Get the QZSS code on L2 Channel.

getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales

getQzssEpoch() - Method in interface org.orekit.time.TimeScales

Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.

getQzssFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Get the QZSS fit interval.

getQZSSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the QZSS navigation messages contained in the file.

getQZSSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the QZSS navigation messages for the given satellite Id.

getQzssNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Get the QZSS navigation message corresponding to the current RTCM data.

getQzssNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Get the QZSS navigation message corresponding to the current RTCM data.

getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Get the QZSS time of clock.

getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get the distance from center of mass of the central body to the 3rd body.

getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get the distance from center of mass of the central body to the 3rd body.

getRaan() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Get the orbit right ascension of ascending node.

getRaan() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get Right Ascension of the Ascending node.

getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE

Get Right Ascension of the Ascending node.

getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Get the drivers for supported parameters.

getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive

Get the drivers for supported parameters.

getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the range of a point with regards to the topocentric frame center point.

getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the range of a point with regards to the topocentric frame center point.

getRange() - Method in class org.orekit.utils.FieldTrackingCoordinates

Get the range.

getRange() - Method in class org.orekit.utils.TrackingCoordinates

Get the range.

getRange1() - Method in class org.orekit.estimation.iod.IodGooding

Get range for observation (1).

getRange2() - Method in class org.orekit.estimation.iod.IodGooding

Get range for observation (2).

getRange3() - Method in class org.orekit.estimation.iod.IodGooding

Get range for observation (3).

getRangeData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the range data for the data block.

getRangeMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the rangeMode.

getRangeModulus(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the range modulus in meters.

getRangeRate() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the range rate.

getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the range rate of a point with regards to the topocentric frame center point.

getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the range rate of a point with regards to the topocentric frame center point.

getRangeSupplementData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the range supplement data for the data block.

getRangeType() - Method in class org.orekit.files.ilrs.CRDHeader

Get the range type.

getRangeType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType

Get the range type for the given indicator.

getRangeUnits() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the rangeUnits.

getRangeUnitsConverter() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Get the converter for Range Units.

getRate() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage

Get refresh rate.

getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide

Get the angular rate of the tide.

getRateElementsType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Get the type of the elements rates.

getRateProcessNoiseStdDev() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get process noise standard deviation if AttitudeDetermination.rateStates is RateElementsType.ANGVEL.

getRateStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get attitude rate states.

getRateType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Get attitude rate element set type.

getRatio() - Method in enum org.orekit.gnss.Frequency

Get the ratio f/f0, where f0 is the common frequency.

getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get the ratio of satellite period to central body rotation period.

getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get the ratio of satellite period to central body rotation period.

getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getRawContent() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the raw content of the entry.

getRawCorrectionRange() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the raw correction for range.

getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver

Get the raw drivers to which this one delegates.

getRawPosition(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position at date.

getRawPosition(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position at date.

getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the underlying provider for raw (non-interpolated) transforms.

getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the underlying provider for raw (non-interpolated) transforms.

getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position-velocity at date.

getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider

Get the position-velocity at date.

getRawRangeModulus() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the raw range modulus.

getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics

Get a spherical harmonic sine coefficient.

getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get the critical distance.

getRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the typical (50th percentile) radar cross-section.

getRcvrClkOffset() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Get receiver clock offset.

getRcvrClkOffset() - Method in class org.orekit.files.rinex.observation.ObservationDataSet

Get receiver clock offset.

getRdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Unique identifier of Reentry Data Message linked to this Orbit Data Message.

getReal(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the real part of a nominal Love numbers.

getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem

Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.

getReceiveAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get the receive amplitude.

getReceiveBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the receiveBand.

getReceiveDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for receiveDelays.

getReceiverIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver

Getter for the receiver identifier.

getReceiverNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the number of the receiver.

getReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the receivers.

getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader

Get parsed receivers antennas.

getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRange

Get the receiver ground station.

getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate

Get the receiver ground station.

getReceiverType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the type of the receiver.

getReceiverVersion() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the version of the receiver.

getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the recommended OD time span calculated for the object.

getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get time span of observation recommended for the OD of the object.

getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the type of record.

getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the type of record.

getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the type of record.

getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record

Get the type of record.

getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get reduction theory used for precession and nutation modeling.

getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get reference's orbit at time of closest approach.

getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get reference's orbit at time of closest approach.

getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate

Get the reference attitude.

getReferenceClocks() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the reference clocks.

getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get reference's covariance.

getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get reference's covariance.

getReferenceDate() - Method in class org.orekit.files.ccsds.definitions.TimeConverter

Get the reference date for relative dates (may be null if no relative dates are used).

getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get initial date.

getReferenceDate() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection

Getter for the reference date of the time system correction polynomial.

getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the reference date for the harmonics.

getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the reference date for the harmonics.

getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper

Get reference date.

getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper

Get reference date.

getReferenceDate() - Method in class org.orekit.utils.ParameterDriver

Get current reference date.

getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic

Get the reference date.

getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the reference epoch.

getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the reference epoch.

getReferenceFrame() - Method in class org.orekit.attitudes.Attitude

Get the reference frame.

getReferenceFrame() - Method in class org.orekit.attitudes.AttitudeInterpolator

Get reference frame from which attitude is defined.

getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude

Get the reference frame.

getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator

Get reference frame from which attitude is defined.

getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec

Get the reference frame in which the right ascension - declination angles are given.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the reference frame from which attitude is defined.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the reference frame from which attitude is defined.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Get the reference frame.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Get the value of REF_FRAME as an Orekit Frame.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Get Coordinate system for velocity increment vector.

getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Get the the value of REFERENCE_FRAME as an Orekit Frame.

getReferenceFrame() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the reference frame from which attitude is defined.

getReferenceFrame() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the reference frame from which attitude is defined.

getReferenceName() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Getter for the name of the receiver/satellite embedding the reference clock.

getReferenceRadius() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Get the reference radius of the central body attraction model.

getReferenceRadius() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Get the reference radius of the central body attraction model.

getReferenceTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the time system used as a reference to define a time system.

getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.KalmanModel

Getter for the reference trajectories.

getReferenceValue() - Method in class org.orekit.utils.ParameterDriver

Get reference parameter value.

getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame

Get the CCSDS reference frame.

getRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the value of REF_FRAME as an Orekit Frame.

getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader

Get the reference frame.

getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader

Get the reference frame identifier.

getReflectance() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the typical (50th percentile) coefficient of reflectance.

getReflection() - Method in class org.orekit.forces.Panel

Get radiation pressure specular reflection coefficient.

getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel

Compute the refraction angle from the true (geometrical) elevation.

getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured refraction model.

getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured refraction model.

getRegionCode() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Get the region code.

getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the web or mail address for registration.

getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get the file metadata.

getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get the relative metadata following header, they are the common metadata for the CDM.

getRelativePosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Object2’s position vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.

getRelativeSpeed() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the norm of relative velocity vector at TCA.

getRelativeVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Object2’s velocity vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.

getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the total ΔV remaining for spacecraft.

getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 3.

getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 3.

getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the reserved field in word 4.

getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 4.

getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 4.

getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the reserved field in word 5.

getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 5.

getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 5.

getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the reserved field in word 6.

getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 6.

getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 6.

getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the reserved field in word 7.

getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 7.

getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 7.

getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 8.

getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 8.

getReserved09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 9.

getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field in word 10.

getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B

Get the reserved field in word 10.

getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get reserved field in word 10.

getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E

Get the reserved field in word 10.

getReserved8() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E

Get the reserved field in word 8.

getReservedA09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field A in word 9.

getReservedA10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B

Get the reserved field A in word 10.

getReservedB09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A

Get the reserved field B in word 9.

getReservedB10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B

Get the reserved field B in word 10.

getResetAtEnd() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Getter for the resetting flag regarding initial state.

getResetAtEnd() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Getter for the resetting flag regarding initial state.

getResidualsAccepted() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the percentage of residuals accepted in the OD of the object (from 0 to 100).

getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Get on all the results computed by the detector (e.g.: dates of cycle-slip).

getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the retrograde factor.

getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the retrograde factor.

getReturnRate() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the return rate.

getReturnRate() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the return rate.

getRevAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Get the revolution rumber.

getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils

Reverse a transform provider.

getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the revolution number.

getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the revolution number.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit

Get the right ascension of the ascending node.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the right ascension of the ascending node derivative.

getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the right ascension of the ascending node derivative.

getRms() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the rms of raw system delay.

getRms() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get the session RMS from the mean of raw accepted time-of-flight values minus the trend function.

getRms() - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Get the Root Mean Square of the TLE estimation.

getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the Root Mean Square Deviation of the fitting.

getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value R^ε_n,m,l(γ).

getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value R^ε_n,m,l(γ).

getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get roa = R / a.

getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get roa = R / a.

getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get roa = R / a.

getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get roa = R / a.

getRolloverReference() - Static method in class org.orekit.time.GNSSDate

Get the reference date ensuring continuity across GNSS week rollover.

getRoot() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get root element for XML files.

getRoot() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get root element for XML files.

getRoot() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Get root element for XML files.

getRoot() - Static method in class org.orekit.frames.Frame

Get the unique root frame.

getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem

Get the CR3BP Rotating Frame.

getRotation() - Method in class org.orekit.attitudes.Attitude

Get the attitude rotation.

getRotation() - Method in class org.orekit.attitudes.FieldAttitude

Get the attitude rotation.

getRotation() - Method in interface org.orekit.frames.FieldStaticTransform

Get the underlying elementary rotation.

getRotation() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary rotation.

getRotation() - Method in interface org.orekit.frames.StaticTransform

Get the underlying elementary rotation.

getRotation() - Method in class org.orekit.frames.Transform

Get the underlying elementary rotation.

getRotation() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation.

getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation.

getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude

Get the satellite rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude

Get the satellite rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform

Get the second time derivative of the rotation.

getRotationAcceleration() - Method in class org.orekit.frames.Transform

Get the second time derivative of the rotation.

getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation acceleration.

getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation acceleration.

getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader

Get the rotation angle type.

getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Get the coordinates of the Euler angles.

getRotationRate() - Method in class org.orekit.frames.FieldTransform

Get the first time derivative of the rotation.

getRotationRate() - Method in class org.orekit.frames.Transform

Get the first time derivative of the rotation.

getRotationRate() - Method in class org.orekit.utils.AngularCoordinates

Get the rotation rate.

getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates

Get the rotation rate.

getRotationRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Get the rates of the Euler angles.

getRTNCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the covariance matrix logical block.

getRTNCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Get the RTN covariance matrix.

getRunByName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the run/by name.

getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Get s.

getS10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the EUV index (26-34 nm) scaled to F10.

getS10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the EUV index (26-34 nm) scaled to F10.

getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the EUV index (26-34 nm) scaled to F10.

getS10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the EUV 81-day averaged centered index.

getS10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the EUV 81-day averaged centered index.

getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the EUV 81-day averaged centered index.

getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext

Get the sine of the inclination to the power 2.

getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext

Get the sine of the inclination to the power 2.

getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the states sample.

getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets the satellite configuration.

getSatellite() - Method in class org.orekit.files.rinex.observation.GlonassSatelliteChannel

Get the satellite identifier.

getSatellite() - Method in class org.orekit.files.rinex.observation.ObservationDataSet

Get observed satellite.

getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite code.

getSatelliteCount() - Method in class org.orekit.files.sp3.SP3

Get the number of satellites contained in this orbit file.

getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData

Get the satellite ID.

getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData

Get the satellite ID.

getSatelliteID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData

Get the satellite ID.

getSatelliteId(SatelliteSystem, int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Transform the satellite ID parsed from the IGS SSR message to the real ID.

getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults

Get the satellite name.

getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get the satellite id.

getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the satellite id.

getSatelliteReferenceDatum() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader

Get the satellite reference datum.

getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the number of satellite revolutions to use for converting osculating to mean elements.

getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get the number of satellite revolutions to use for converting osculating to mean elements.

getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the satellites related to this measurement.

getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the satellites related to this measurement.

getSatellites() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Get the satellites related to this measurement.

getSatellites() - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Get the satellites related to this measurement.

getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the satellites related to this measurement.

getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in interface org.orekit.files.general.AttitudeEphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in interface org.orekit.files.general.EphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.ilrs.CPF

Get the loaded ephemeris for each satellite in the file.

getSatellites() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the satellites.

getSatellites() - Method in class org.orekit.files.sp3.SP3

getSatellites() - Method in class org.orekit.files.stk.STKEphemerisFile

Get the loaded ephemeris for each satellite in the file.

getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader

Get parsed satellites antennas.

getSatelliteSystem() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet

Get Satellite System.

getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedDCBS

Get the satellite system.

getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedPCVS

Get the satellite system.

getSatelliteSystem() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the satellite system.

getSatelliteSystem() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection

Get the Satellite System.

getSatelliteSystem() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the satellite system.

getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite system.

getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency

Get the satellite system for which this frequency is defined.

getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage

Get the satellite system associated to the message.

getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage

Get the satellite system associated to the message.

getSatelliteSytem() - Method in class org.orekit.files.sinex.DcbSatellite

Get the satellite sytem corresponding to the satellite.

getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get satellite type.

getSatelliteType() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for satellite type.

getSatIds() - Method in class org.orekit.files.sp3.SP3Header

Get the satellite identifiers.

getSatsCorrected() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection

Get the list of satellites involved.

getSaturn() - Method in interface org.orekit.bodies.CelestialBodies

Get the Saturn singleton body.

getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Saturn singleton body.

getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getSbasId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the SBAS Id.

getSBASNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get all the SBAS navigation messages contained in the file.

getSBASNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the SBAS navigation messages for the given satellite Id.

getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Get the underlying SBAS orbital elements.

getScale() - Method in class org.orekit.utils.ParameterDriver

Get scale.

getScale() - Method in class org.orekit.utils.units.PowerTerm

Get the scaling factor.

getScale() - Method in class org.orekit.utils.units.Unit

Get the scaling factor to SI units.

getScaleFactor() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier

Get the scale factor used to compute relativistic effect.

getScaleFactorCorrections(SatelliteSystem) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the list of scale factor correction.

getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the spacecraft clock count at OcmMetadata.getEpochT0().

getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the number of spacecraft clock seconds occurring during one SI second.

getScreenEntryTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the time in UTC when Object2 enters the screening volume.

getScreenExitTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the time in UTC when Object2 exits the screening volume.

getScreeningDataSource() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Get the source (or origin) of the specific orbital data for this object.

getScreenPcThreshold() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the collision probability screening threshold used to identify this conjunction.

getScreenType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the type of screening to be used.

getScreenVolumeFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the name of the Object1 centered reference frame in which the screening volume data are given.

getScreenVolumeRadius() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the screen volume radius.

getScreenVolumeShape() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the shape of the screening volume.

getScreenVolumeX() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.

getScreenVolumeY() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.

getScreenVolumeZ() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the N component size of the screening volume in the corresponding frame.

getSecInDay() - Method in class org.orekit.time.GLONASSDate

Get the number of seconds since N_a start.

getSecond() - Method in class org.orekit.time.FieldTimeStampedPair

Get second time stamped value.

getSecond() - Method in class org.orekit.time.TimeComponents

Get the seconds number.

getSecond() - Method in class org.orekit.time.TimeStampedPair

Get second time stamped value.

getSecondary() - Method in class org.orekit.bodies.CR3BPSystem

Get the secondary CelestialBody.

getSecondary() - Method in class org.orekit.estimation.measurements.gnss.Dipole

Get the secondary dipole vector.

getSecondary() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Get the provider for the secondary satellite.

getSecondaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector

Get the secondaryObject.

getSecondaryPVProvider() - Method in class org.orekit.propagation.events.ExtremumApproachDetector

Get the secondary position-velocity provider stored in this instance.

getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange

Get the secondary ground station reflecting the signal.

getSecondFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter

Get the history of phase values of the second frequency.

getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents

Get the second number within the local day, without applying the offset from UTC.

getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents

Get the second number within the UTC day, applying the offset from UTC.

getSecondsInWeek() - Method in class org.orekit.time.GNSSDate

Get the number of seconds since week start.

getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3Header

Returns the seconds of the GPS week as contained in the SP3 file.

getSecondStation() - Method in class org.orekit.estimation.measurements.FDOA

Get the second ground station, the one that gives the measurement.

getSecondStation() - Method in class org.orekit.estimation.measurements.TDOA

Get the second ground station, the one that gives the measurement.

getSecularDegree() - Method in class org.orekit.utils.SecularAndHarmonic

Get degree of polynomial secular part.

getSedr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the amount of energy being removed from the object’s orbit by atmospheric drag.

getSedr() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get Specific Energy Dissipation Rate.

getSefiCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Space Environment Fragmentation Impact probability.

getSefiCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Space Environment Fragmentation Impact probability method.

getSefiFragmentationModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Space Environment Fragmentation Impact fragmentation model.

getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris

Get the segments of the attitude ephemeris.

getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

Get the segments of the attitude ephemeris.

getSegments() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Get the segments.

getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Get the segments of the ephemeris.

getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Get the segments of the ephemeris.

getSegments() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Get the segments of the attitude ephemeris.

getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the segments of the ephemeris.

getSegments() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Get the segments of the attitude ephemeris.

getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Get the segments of the ephemeris.

getSegments() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Returns a list containing only this.

getSegments() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the segments of the ephemeris.

getSegments() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the selected short periodic coefficients that must be stored as additional states.

getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Get the selected short periodic coefficients that must be stored as additional states.

getSelectedMu() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser

Select the gravitational coefficient to use.

getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Get the current value of selected normalized parameters.

getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Get the current value of selected normalized parameters.

getSelectedOrbitalParametersDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Get the selected orbital drivers for a propagatorBuilder.

getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Get the selected propagation drivers for a propagatorBuilder.

getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Get the dates selector.

getSensorFrequency() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Get frequency of sensor data for sensor.

getSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Get standard deviation of sensor noise for sensor.

getSensorNumber() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Get number of the sensor.

getSensors() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get description of sensors used.

getSensorsN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of sensors used.

getSensorsUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get sensors used.

getSensorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Get sensor used.

getSeparation() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles

Get apparent separation between occulting and occulted directions.

getSeparation() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles

Get apparent separation between occulting and occulted directions.

getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the ephemeris sequence number.

getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna

Get the serial number.

getSessionStatisticsData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the session statistics data for the data block.

getSessionStatisticsRecord() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the default (the first if there are many records) SessionStat record.

getSessionStatisticsRecord(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the session statistics record related to the systemConfigurationId.

getShadowBodies() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get celestial bodies casting shadows.

getShadowModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get shadow model used for solar radiation pressure.

getShiftTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the calibration shift type indicator.

getShortPeriodTerms() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the short periodic terms.

getShortPeriodTermsValue(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the short period terms value.

getSic() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the SIC ID.

getSig3EigVec3CovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the Sigma / Eigenvector covariance logical block.

getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Get the current value of sigma.

getSigmaU() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get rate random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.

getSigmaV() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get angle random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.

getSignal() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for signal.

getSignalCode() - Method in enum org.orekit.gnss.ObservationType

Get the signal code.

getSignalID() - Method in class org.orekit.gnss.metric.messages.common.CodeBias

Get the GNSS signal and tracking mode identifier.

getSignalID() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias

Get the GNSS signal and tracking mode identifier.

getSignalStrength() - Method in class org.orekit.files.rinex.observation.ObservationData

Get the signal strength.

getSignalStrengthUnit() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the unit of the carrier to noise ratio observables.

getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias

Get the signal Wide-Lane integer indicator.

getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients

Get the coefficient S_i^j.

getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients

Get the coefficient S_i^j.

getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna

Get the sinex code of the antenna.

getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming

Get points at which aiming direction cannot be computed.

getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming

Get points at which aiming direction cannot be computed.

getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming

Get points at which aiming direction cannot be computed.

getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming

Get points at which aiming direction cannot be computed.

getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the signal in space accuracy (m).

getSisaiOc1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for Signal In Space Accuracy Index (clock drift accuracy).

getSisaiOc2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for Signal In Space Accuracy Index (clock drift rate accuracy).

getSisaiOcb() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for Signal In Space Accuracy Index (radial and clock).

getSisaiOe() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for Signal In Space Accuracy Index (along track and across track).

getSismai() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for Signal In Space Monitoring Accuracy Index.

getSiteCode() - Method in class org.orekit.files.sinex.DcbStation

Get the site code (station identifier).

getSiteCode() - Method in class org.orekit.files.sinex.Station

Get the site code (station identifier).

getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the site location.

getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the site name.

getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.

getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the size of the problem.

getSize() - Method in class org.orekit.utils.LoveNumbers

Get the size of the arrays.

getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the S_j coefficient.

getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient

Get the S_j coefficient.

getSkew() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the skew of raw system delay values from the mean.

getSkewness() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get the session skewness from the mean of raw accepted time-of-flight values minus the trend function.

getSkimmingAltitude() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Get the skimming altitude.

getSlope() - Method in class org.orekit.time.OffsetModel

Offset slope in seconds per UTC day (TAI minus UTC / dUTC).

getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots in use.

getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots evictions.

getSma() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the semi-major axis.

getSma() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Semi-Major Axis.

getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the semi-major axis.

getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get the semi-major axis.

getSmoothedData() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet

Get the smoothed observation data.

getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Get the sine parameters of spherical harmonics expansion of degree N and order M.

getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get the signal to noise ratio.

getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get the software configuration ID.

getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the software configuration record.

getSoftwareRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get software configuration record related to the systemRecord.

getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the solar radiation pressure area.

getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the solar radiation pressure coefficient.

getSolarRadiationPressure() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Get Enum YesNoUnknown that indicates if Solar Radiation Pressure is taken into account or not.

getSolarSystemBarycenter() - Method in interface org.orekit.bodies.CelestialBodies

Get the solar system barycenter aggregated body.

getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the solar system barycenter aggregated body.

getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions

Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).

getSolidTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get solid tides model.

getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution

Get the solution array.

getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the number of solutions found.

getSolveN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of solved-for states.

getSolveStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get description of state elements solved-for.

getSource() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Get source of attitude estimate.

getSource() - Method in class org.orekit.files.ilrs.CPFHeader

Get the ephemeris source.

getSource() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets the source of this GPS almanac.

getSource() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Gets the source of this QZSS almanac.

getSourceDCBS() - Method in class org.orekit.files.rinex.AppliedDCBS

Get the source of corrections.

getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord

Get the source identifier.

getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Get the source identifier.

getSourcePCVS() - Method in class org.orekit.files.rinex.AppliedPCVS

Get the source of corrections.

getSourceString() - Method in enum org.orekit.errors.OrekitMessages

getSourceTable() - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Get a sourcetable.

getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the south of point, expressed in parent shape frame.

getSouth() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the south of point, expressed in parent shape frame.

getSouth() - Method in class org.orekit.frames.TopocentricFrame

Get the south direction of topocentric frame, expressed in parent shape frame.

getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along South axis.

getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along South axis.

getSpacecraft() - Method in class org.orekit.forces.drag.DragForce

Get spacecraft that are sensitive to atmospheric drag forces.

getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Get spacecraft shape.

getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Get spacecraft shape.

getSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Get the spacecraft body frame.

getSpacecraftClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the spacecraft clock offset and drift applied indicator.

getSpacecraftEpochTimeScale() - Method in class org.orekit.files.ilrs.CRDHeader

Get the spacecraft epoch time scale.

getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the spacecraft parameters logical block.

getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the spacecraft parameters logical block.

getSpaceWeatherEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get epoch of the Space Weather data.

getSpaceWeatherSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get Space Weather data source.

getSpan() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the calibration span.

getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap

Get the time span containing a specified date.

getSpanAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the TimeSpanMap.Span valid after transition.

getSpanBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the TimeSpanMap.Span valid before transition.

getSpansNumber() - Method in class org.orekit.utils.TimeSpanMap

Get the number of spans.

getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the spatial filter.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.NdmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Get the non-default token builders for special XML elements.

getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Get the non-default token builders for special XML elements.

getSpecifier() - Method in interface org.orekit.errors.LocalizedException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitIOException

Get the localizable specifier of the error message.

getSpecifier() - Method in exception org.orekit.errors.OrekitParseException

Get the localizable specifier of the error message.

getSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the spectral filter.

getSphericalHarmonicsDegree() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Get the degree of spherical harmonic expansion.

getSphericalHarmonicsOrder() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Get the order of spherical harmonic expansion.

getSpin() - Method in class org.orekit.attitudes.Attitude

Get the satellite spin.

getSpin() - Method in class org.orekit.attitudes.FieldAttitude

Get the satellite spin.

getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid

Gets the rotation of the ellipsoid about its axis.

getSpinAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the right ascension of spin axis vector (rad).

getSpinAngle() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the phase of the satellite about the spin axis (rad).

getSpinAngleVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the angular velocity of satellite around spin axis (rad/s).

getSpinDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Get the declination of the spin axis vector (rad).

getSpinStabilizedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get the spin-stabilized logical block.

getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get √a.

getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get √a.

getSqrtA() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for Square Root of Semi-Major Axis (√m).

getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution

Get the squared distance to the corresponding float solution.

getSrpCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the nominal SRP coefficient.

getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.

getSrpModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Get Solar Radiation Pressure model.

getSrpUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the SRP coefficient 1σ uncertainty.

getSsrEpoch1s() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the SSR Epoch Time 1s.

getSsrIgm01Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01

Get the SSR IGM01 data parsed in the SSR message.

getSsrIgm02Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02

Get the SSR IGM02 data parsed in the SSR message.

getSsrIgm03Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03

Get the SSR IGM03 data parsed in the SSR message.

getSsrIgm04Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04

Get the SSR IGM04 data parsed in the SSR message.

getSsrIgm05Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05

Get the SSR IGM05 data parsed in the SSR message.

getSsrIgm06Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06

Get the SSR IGM06 data parsed in the SSR message.

getSsrIgm07Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07

Get the SSR IGM07 data parsed in the SSR message.

getSsrMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the SSR Multiple Message Indicator.

getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the SSR Provider ID.

getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the SSR Provider ID.

getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the SSR Solution ID.

getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the SSR Solution ID.

getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Get the SSR Update Interval.

getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Get the SSR Update Interval.

getSsrUra() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data

Get the SSR User Range Accuracy (URA).

getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel

Create a new Marini-Murray model using a standard atmosphere model.

getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel

Create a new Mendes-Pavlis model using a standard atmosphere model.

getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Create a new Saastamoinen model using a standard atmosphere model.

getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the start of the measurements time span.

getStart() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the start date of this ephemeris segment.

getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the start date of this ephemeris segment.

getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Get the start date of the ephemeris.

getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the start date of this ephemeris segment.

getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the start date of the ephemeris.

getStart() - Method in class org.orekit.files.sp3.SP3Segment

Get the start date of this ephemeris segment.

getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getStart() - Method in class org.orekit.time.OffsetModel

Get the date of the offset start.

getStart() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the start of this time span.

getStartDate() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Getter for the validity period start date.

getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the start date.

getStartDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers

Get the start date.

getStartDate() - Method in class org.orekit.frames.EOPHistory

Get the date of the first available Earth Orientation Parameters.

getStartDate() - Method in class org.orekit.propagation.AbstractPropagator

Get the start date.

getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator

Get the start date.

getStartDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Getter for the firing start detector.

getStartDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Get the driver for start date.

getStartDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Get the driver for start date.

getStartEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the starting epoch (UTC).

getStartScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the start time in UTC of the screening period for the conjunction assessment.

getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the time of the earliest data contained in the OCM.

getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get start of total time span covered by attitude data.

getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the time of the earliest data contained in the OCM.

getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get start of total time span covered by ephemerides data and covariance data.

getStartTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the startTime.

getStartTransition() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the transition at start of this time span.

getState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get spacecraft state.

getState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get spacecraft state.

getState() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter

Get the state with the number of parameters consistent with the propagation model.

getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the triggering state.

getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the triggering state.

getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event

Get the spacecraft's state at the event.

getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Get the spacecraft's state at the event.

getState(ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Get the state with the number of parameters consistent with parametric model.

getStateCovariance(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the state covariance in the same frame/local orbital frame, orbit type and position angle as the initial covariance.

getStateCovariance(SpacecraftState, Frame) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the state covariance expressed in a given frame.

getStateCovariance(SpacecraftState, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Get the state covariance expressed in a given orbit type.

getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.

getStateInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris

Get state interpolator.

getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the states of the spacecrafts.

getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Get state size.

getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester

Extract state transition matrix from state.

getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Extract state transition matrix from state.

getStateTransitionMatrix(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester

Extract state transition matrix from state.

getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations

Method returning the State Transition Matrix.

getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Extract state transition matrix from state.

getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Get the type of the elements used to define the orbital state (mean or osculating).

getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the state vector logical block.

getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the state vector logical block.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider

Get a transform for only rotations and translations on the specified date.

getStaticTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame

Get the static portion of the transform from the instance to another frame.

getStaticTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame

Get the static portion of the transform from the instance to another frame.

getStation() - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Get the ground station from which measurement is performed.

getStation(String) - Method in class org.orekit.files.sinex.SinexLoader

Get the station corresponding to the given site code.

getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the station clock offset and drift applied indicator.

getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get station position in inertial frame at end of the downlink leg.

getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get station position in inertial frame at end of the downlink leg.

getStationIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the station identifier.

getStationInformation() - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Getter for the station information.

getStationName() - Method in class org.orekit.files.ilrs.CRDHeader

Get the station name from official list.

getStationName() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the station name.

getStationNetword() - Method in class org.orekit.files.ilrs.CRDHeader

Get the station network.

getStationOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the estimated station oscillator drift in parts in 10¹⁵.

getStations() - Method in class org.orekit.files.sinex.SinexLoader

Get the parsed station data.

getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the estimated station UTC offset.

getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the status.

getStatusFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get status flags.

getStep() - Method in class org.orekit.files.ilrs.CPFHeader

Get the time between table entries.

getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the grid points time step.

getStep() - Method in class org.orekit.frames.ShiftingTransformProvider

Get the grid points time step.

getSTKVersion() - Method in class org.orekit.files.stk.STKEphemerisFile

Returns the STK version string.

getStm(Orbit, double) - Static method in class org.orekit.propagation.StateCovariance

Get the state transition matrix considering Keplerian contribution only.

getStmName() - Method in class org.orekit.propagation.AbstractMatricesHarvester

Get the State Transition Matrix state name.

getStop() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Get the end date of this ephemeris segment.

getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment

Get the end date of this ephemeris segment.

getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

Get the end date of the ephemeris.

getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment

Get the end date of this ephemeris segment.

getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.sp3.SP3Ephemeris

Get the end date of the ephemeris.

getStop() - Method in class org.orekit.files.sp3.SP3Segment

Get the end date of this ephemeris segment.

getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence

Get the new time for a stop action.

getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence

Get the new time for a stop action.

getStopDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Getter for the firing stop detector.

getStopDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Get the driver for stop date.

getStopDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Get the driver for stop date.

getStopNumber() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get the stop number.

getStopScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the stop time in UTC of the screening period for the conjunction assessment.

getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the time of the latest data contained in the OCM.

getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get end of total time span covered by attitude data.

getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the time of the latest data contained in the OCM.

getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get end of total time span covered by ephemerides data and covariance data.

getStopTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the stopTime.

getStream(T) - Method in class org.orekit.data.AbstractListCrawler

Get the stream to read from an input.

getStream(File) - Method in class org.orekit.data.FilesListCrawler

Get the stream to read from an input.

getStream(URL) - Method in class org.orekit.data.NetworkCrawler

Get the stream to read from an input.

getStreamInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord

Get the web address for stream information.

getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the strength level for activity.

getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Get the stuff (all the things needed for, the detector).

getSubDailySequenceNumber() - Method in class org.orekit.files.ilrs.CPFHeader

Get the sub-daily ephemeris sequence number.

getSubInterpolators() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSubInterpolators() - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSubInterpolators() - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSubInterpolators() - Method in class org.orekit.time.AbstractTimeInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSubInterpolators() - Method in interface org.orekit.time.FieldTimeInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSubInterpolators() - Method in interface org.orekit.time.TimeInterpolator

Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

getSumOfAllConstantDelays() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the sum of all constant delays (electronic, geometric, optical) that are not included in the time of flight measurements or time- variant or point angle-variant delays in the “42” record below (m, one way).

getSun() - Method in interface org.orekit.bodies.CelestialBodies

Get the Sun singleton body.

getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Sun singleton body.

getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getSun() - Method in class org.orekit.forces.gravity.DeSitterRelativity

Get the sun model used to compute De Sitter effect.

getSunEarthCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory

Get the Sun-Earth CR3BP singleton bodies pair.

getSunJupiterCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory

Get the Sun-Jupiter CR3BP singleton bodies pair.

getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader

Get the supported names regular expression.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the regular expression for supported files names.

getSupportedNames() - Method in class org.orekit.gnss.SEMParser

getSupportedNames() - Method in class org.orekit.gnss.YUMAParser

getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Get the supported names regular expression.

getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

getSurveyedTargetDistance() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the surveyed target distance.

getSurveyError() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the survey error.

getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Getter for the user SV accuray (meters).

getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for the user SV accuray (meters).

getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the user SV accuray (meters).

getSvHealth() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Get the satellite health status.

getSvHealth() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get SV health.

getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E

Get the Sv health for a satellite.

getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame5B

Get the SV Health for a satellite.

getSvHealth() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get SV health.

getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for the satellite health status.

getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Getter for the SV health status.

getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Getter for the satellite health status.

getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the satellite health status.

getSvId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45

Get SV (page) ID.

getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets the satellite "SVN" reference number.

getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory

Get the corresponding CR3BP System.

getSystem() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage

Get satellite system.

getSystem() - Method in class org.orekit.gnss.SatInSystem

Get the system this satellite belongs to.

getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the system configuration id.

getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get the system configuration id.

getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the system configuration id.

getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get system configuration id.

getSystemConfigurationIds() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get a set of configuration ids.

getSystemConfigurationRecords() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get a list of system configurations.

getSystemDelay() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the calibration system delay.

getSystemId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Get the system configuration ID.

getSystemIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader

Get the system identifier.

getSystemNumber() - Method in class org.orekit.files.ilrs.CRDHeader

Get the system number.

getSystemObservationTypes() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the different observation type for each satellite system.

getSystemOccupancy() - Method in class org.orekit.files.ilrs.CRDHeader

Get the system occupancy.

getSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the system configuration record.

getSystemRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get system configuration record.

getSystemTimeOffsets() - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Get the system time offsets.

getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester

Get the current density table.

getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset

Get an unmodifiable view of the tabulated attitudes.

getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales

getTAI() - Method in interface org.orekit.time.TimeScales

Get the International Atomic Time scale.

getTAI() - Static method in class org.orekit.time.TimeScalesFactory

Get the International Atomic Time scale.

getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Get the difference (TAI – UTC) in seconds at epoch AcmMetadata.getEpochT0().

getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().

getTargetAttitude() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get target attitude (if purpose is attitude adjustment).

getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the target class.

getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the target location.

getTargetMomentum() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get target momentum (if purpose is momentum desaturation).

getTargetMomFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get reference frame for AttitudeManeuver.getTargetMomentum().

getTargetName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get the target name or ID.

getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position in specified frame.

getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the target point position/velocity in specified frame.

getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the target point position/velocity in specified frame.

getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering

Compute the target point position/velocity in specified frame.

getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the size of the target.

getTargetSpinRate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Get target spin rate (if purpose is spin rate adjustment).

getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS time scale correction to UTC time.

getTauD() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get downlink delay.

getTauD() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get downlink delay.

getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the correction to GPS time relative to GLONASS time.

getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide

Get the multiplier for the τ Doodson argument.

getTC() - Method in class org.orekit.data.DelaunayArguments

Get the offset in Julian centuries.

getTC() - Method in class org.orekit.data.FieldDelaunayArguments

Get the offset in Julian centuries.

getTca() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the date and time in UTC of the closest approach.

getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get the Time of Closest Approach.

getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Get the Time of Closest Approach.

getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales

getTCB() - Method in interface org.orekit.time.TimeScales

Get the Barycentric Coordinate Time scale.

getTCB() - Static method in class org.orekit.time.TimeScalesFactory

Get the Barycentric Coordinate Time scale.

getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales

getTCG() - Method in interface org.orekit.time.TimeScales

Get the Geocentric Coordinate Time scale.

getTCG() - Static method in class org.orekit.time.TimeScalesFactory

Get the Geocentric Coordinate Time scale.

getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales

getTDB() - Method in interface org.orekit.time.TimeScales

Get the Barycentric Dynamic Time scale.

getTDB() - Static method in class org.orekit.time.TimeScalesFactory

Get the Barycentric Dynamic Time scale.

getTdim() - Method in class org.orekit.bodies.CR3BPSystem

Get the CR3BP orbital period of m2 around m1.

getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.

getTdop() - Method in class org.orekit.gnss.DOP

Gets the time dilution of precision.

getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the address of Technical Point Of Contact at originator.

getTechEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the email address of Technical Point Of Contact at originator.

getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the creating agency or operator.

getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the phone number of Technical Point Of Contact at originator.

getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the Technical Point Of Contact at originator.

getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the position of Technical Point Of Contact at originator.

getTEME() - Method in class org.orekit.frames.AbstractFrames

getTEME() - Method in interface org.orekit.frames.Frames

Get the TEME reference frame.

getTEME() - Static method in class org.orekit.frames.FramesFactory

Get the TEME reference frame.

getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get the surface temperature.

getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Get the local temperature at the evaluation location.

getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Returns the temperature at the station [K].

getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel

Get the atmospheric temperature of the station depending its position.

getTemplateTLE() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Getter for the template TLE.

getTempSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the temperature sensor manufacturer.

getTempSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the temperature sensor model.

getTempSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get the temperature sensor serial number.

getText() - Method in class org.orekit.files.rinex.section.RinexComment

Get the text.

getTFirstObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the time of First observation record.

getTGD() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the TGD.

getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for the Group Delay Differential (s).

getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the estimated group delay differential TGD for L1-L2 correction.

getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets for the Group Delay Differential (s).

getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Getter for the estimated group delay differential TGD for L5-S correction.

getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Getter for the Group Delay Differential (s).

getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Getter for the estimated group delay differential TGD1 for B1I signal.

getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Getter for the estimated group delay differential TGD for B2I signal.

getTgdB1Cp() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for B1/B3 Group Delay Differential (s).

getTgdB2ap() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for B2 AP Group Delay Differential (s).

getTgdB2bI() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Getter for B2B_i / B3I Group Delay Differential (s).

getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Get the theoretical standard deviation.

getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Get the theoretical standard deviation.

getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Get the theoretical standard deviation.

getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext

Get Central body rotation angle θ.

getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext

Get Central body rotation angle θ.

getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Get the station elevation angle under free-space propagation .

getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction

Get the station minimal elevation angle.

getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the three-hourly Ap index at index i from the threeHourlyAp array.

getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the array of the eight three-hourly Ap indices for the current entry.

getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData

Get the value of the 3 hours geomagnetic index.

getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the three-hourly Kp index at index i from the threeHourlyKp array.

getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Gets the array of the eight three-hourly Kp indices for the current entry.

getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Get the value of the 3 hours geomagnetic index.

getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters

Get the value of the 3 hours geomagnetic index.

getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in interface org.orekit.propagation.events.EventDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in class org.orekit.propagation.events.FieldAdapterDetector

Get the convergence threshold in the event time search.

getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector

Get the convergence threshold in the event time search.

getThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get thrust.

getThrustAcceleration() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.

getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Getter on Thrust direction and spacecraft attitude provided by an external object.

getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ angular off-nominal thrust direction.

getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get thrust efficiency η.

getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider

Thruster axis in satellite frame.

getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get interpolation mode between current and next thrust line.

getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get thrust specific impulse.

getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Get the thrust magnitude.

getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver

Get the thrust magnitude.

getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust magnitude.

getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust magnitude.

getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust magnitude (N).

getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust magnitude (N) at given date.

getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Get one σ percent error on thrust magnitude.

getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust vector (N) in S/C frame.

getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust vector (N) in S/C frame.

getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment

Get thrust vector at a specified date.

getThrustVector(FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment

Get thrust vector at a specified date.

getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel

Get the thrust vector in spacecraft frame (N).

getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for diurnal tides.

getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for diurnal tides.

getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for zonal tides.

getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions

Get the correction function for tidal displacement for zonal tides.

getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the tide.

getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions

Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).

getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).

getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the TideSystem used in the gravity field.

getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider

Get the TideSystem used in the gravity field.

getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getTime() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the reference time of the GNSS orbit as a duration from week start.

getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the Reference Time.

getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the Reference Time.

getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Reference Time of the GNSS orbit as a duration from week start.

getTime() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Gets the Reference Time of the SBAS orbit in GPS seconds of the week.

getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the Reference Time of the SBAS orbit in GPS seconds of the week.

getTime() - Method in class org.orekit.time.DateTimeComponents

Get the time component.

getTime() - Method in class org.orekit.utils.units.Unit

Get the time exponent.

getTimeBiasApplied() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the time bias applied.

getTimeConverter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get the current time converter.

getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get the current time converter.

getTimeLastObsEnd() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the start of a time interval (UTC) that contains the time of the last accepted observation.

getTimeLastObsStart() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the start of a time interval (UTC) that contains the time of the last accepted observation.

getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get the time-of-flight.

getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Get the time offset from first state date to measurement date.

getTimeParameter(FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.

getTimeParameter(AbsoluteDate, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.AbstractTimeInterpolator

Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.

getTimer() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the timer name.

getTimerSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the timer serial number.

getTimeScale() - Method in class org.orekit.files.ccsds.definitions.TimeConverter

Get the base time scale.

getTimeScale() - Method in class org.orekit.files.ilrs.CPF

Get the time scale used in CPF file.

getTimeScale() - Method in class org.orekit.files.ilrs.CRDParser

Get the time scale used to read the file.

getTimeScale() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the data time scale.

getTimeScale(TimeScales) - Method in enum org.orekit.gnss.ObservationTimeScale

Get time scale.

getTimeScale(TimeScales) - Method in enum org.orekit.gnss.TimeSystem

Get the time scale corresponding to time system.

getTimeScales() - Method in class org.orekit.data.CompositeDataContext

getTimeScales() - Method in interface org.orekit.data.DataContext

Get a factory for constructing TimeScales based on the auxiliary data in this context.

getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext

getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext

getTimeScales() - Method in class org.orekit.frames.AbstractFrames

Get the time scales.

getTimeScales() - Method in class org.orekit.frames.EOPHistory

Get the time scales used in computing EOP corrections.

getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory

Get the instance of TimeScales that is called by all of the static methods in this class.

getTimeSinceFirstObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get time elapsed between first accepted observation on epoch.

getTimeSinceLastObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get time elapsed between last accepted observation on epoch.

getTimeSource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get the time source.

getTimeSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the span of time in seconds that the OCM covers.

getTimeSystem() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Get the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.

getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata

Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.

getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get the time system.

getTimeSystem() - Method in class org.orekit.files.rinex.clock.RinexClock

Getter for the file time system.

getTimeSystem() - Method in class org.orekit.files.sinex.DcbDescription

Get the time system for DCB data.

getTimeSystem() - Method in class org.orekit.files.sp3.SP3Header

Returns the TimeSystem used to time-stamp position entries.

getTimeSystemCorrectionA0() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection

Getter for the A0 coefficient of the time system correction.

getTimeSystemCorrectionA1() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection

Getter for the A1 coefficient of the time system correction.

getTimeSystemCorrections() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Getter for the time system corrections contained in the file header.

getTimeSystemCorrectionType() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection

Getter for the time system correction type.

getTimetagRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the timetagRef.

getTimingRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the timing system configuration record.

getTimingRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get timing system configuration record related to the systemRecord.

getTIRF(IERSConventions) - Method in class org.orekit.frames.AbstractFrames

getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames

Get the TIRF reference frame, ignoring tidal effects.

getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the TIRF reference frame.

getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the TIRF reference frame, ignoring tidal effects.

getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TIRF reference frame.

getTk() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the time referenced to the beginning of the frame within the current day.

getTLastObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get the time of last observation record.

getTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Get the underlying TLE.

getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the underlying TLE.

getTLEBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the TLE logical block.

getTN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Get the correction to the satellite time relative to GLONASS system time.

getTN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the correction to the satellite time relative to GLONASS system time.

getTo() - Method in class org.orekit.utils.units.UnitsConverter

Get the destination unit.

getTOA() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B

Get Time of Almanac.

getToaA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get Time Of Almanac.

getTOC() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get the TOC.

getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements

Gets the clock correction reference time toc.

getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the clock correction reference time toc.

getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames

getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames

getTOD(boolean) - Method in interface org.orekit.frames.Frames

Get the TOD reference frame.

getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames

Get the TOD reference frame.

getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TOD reference frame.

getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the TOD reference frame.

getToe() - Method in class org.orekit.gnss.rflink.gps.SubFrame2

Get Time Of Ephemeris.

getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

Get ton2a = 2 / (n² * a).

getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

Get ton2a = 2 / (n² * a).

getTool() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade

Get the tool used for OD.

getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured topocentric frame definitions.

getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector

Returns the topocentric frame centered on ground point.

getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector

Returns the currently configured topocentric frame definitions.

getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector

Returns the topocentric frame centered on ground point.

getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Get the torque vector (N.m).

getTot() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get TOT field.

getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector

Get the total eclipse detection flag.

getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Get the total eclipse detection flag.

getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the total intensity of the magnetic field (= norm of the field vector).

getTotalNumberOfDataLines() - Method in class org.orekit.files.rinex.clock.RinexClock

Get the total number of complete data lines in the file.

getTow() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Get Time Of Week of next 12 second message.

getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the tracking data identifier.

getTrackingCoordinates(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the tracking coordinates of a point with regards to the local point.

getTrackingCoordinates(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame

Get the tracking coordinates of a point with regards to the local point.

getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get the tracking softwares.

getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get the tracking software versions.

getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the number of sensor tracks available for the OD of the object.

getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of sensors tracks available for the OD within the actual OD span.

getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the number of sensor tracks used for the OD of the object.

getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get number of sensors tracks accepted for the OD within the actual OD span.

getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get basis of this trajectory state time history data.

getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get identification number of the orbit determination or simulation upon which this trajectory is based.

getTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get trajectory state histories logical blocks.

getTrajectoryStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Get the trajectory states.

getTrajFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get epoch of the trajectory reference frame.

getTrajID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get trajectory identification number.

getTrajNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get identification number of next trajectory.

getTrajPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get identification number of previous trajectory.

getTrajReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get reference frame of the trajectory.

getTrajType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get trajectory element set type.

getTrajUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get trajectory element set units.

getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the FieldTransform corresponding to specified date.

getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider

Get the transform with derivatives.

getTransform(FrameFacade, FrameFacade, Frame, AbsoluteDate, PVCoordinatesProvider) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade

Get the transform between CCSDS frames.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider

getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider

Get the FieldTransform corresponding to specified date.

getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider

Get the Transform corresponding to specified date.

getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider

Get the FieldTransform corresponding to specified date.

getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the underlying HelmertTransformation.

getTransformation(TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Get the underlying HelmertTransformation.

getTransformProvider() - Method in class org.orekit.frames.Frame

Get the provider for transform from parent frame to instance.

getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame

Get the transform from the instance to another frame.

getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame

Get the transform from the instance to another frame.

getTransitionDates() - Method in class org.orekit.utils.ParameterDriver

Get the dates of the transitions for the drag sensitive models TimeSpanMap.

getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap

Get an unmodifiable view of the sorted transitions.

getTransitPV() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get transit position/velocity.

getTransitPV() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get transit position/velocity.

getTransitState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Get transit state.

getTransitState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Get transit state.

getTranslation() - Method in interface org.orekit.frames.FieldStaticTransform

Get the underlying elementary translation.

getTranslation() - Method in class org.orekit.frames.FieldTransform

Get the underlying elementary translation.

getTranslation() - Method in interface org.orekit.frames.StaticTransform

Get the underlying elementary translation.

getTranslation() - Method in class org.orekit.frames.Transform

Get the underlying elementary translation.

getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get the percentage of transmission of spectral filter.

getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the message transmission time.

getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the message transmission time.

getTransmissionTime() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Getter for transmission time.

getTransmitAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get the transmit amplitude.

getTransmitBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the transmitBand.

getTransmitDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the transmitDelays.

getTransmitTime() - Method in class org.orekit.files.rinex.navigation.IonosphereBaseMessage

Get the transmit time.

getTranspClkRef() - Method in class org.orekit.files.ilrs.CPFHeader

Get the transponder Clock Reference Time.

getTranspClkRefTime() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the transponder clock reference time.

getTransponderId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the transponder configuration ID.

getTransponderRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration

Get the transponder configuration record.

getTransponderRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration

Get transponder configuration record related to the systemRecord.

getTranspOscDrift() - Method in class org.orekit.files.ilrs.CPFHeader

Get the transponder Oscillator Drift in parts in 10^15.

getTranspOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the estimated transponder oscillator drift in parts in 10¹⁵.

getTranspTransmitDelay() - Method in class org.orekit.files.ilrs.CPFHeader

Get the transponder transmit delay.

getTranspUtcOffset() - Method in class org.orekit.files.ilrs.CPFHeader

Get the transponder UTC offset.

getTranspUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the estimated transponder UTC offset.

getTrigger() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Get the triggering event.

getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the triggering event.

getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType

Get the increasing status of triggered events.

getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier

Get the tropospheric delay model.

getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier

Get the tropospheric delay model.

getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Get the EstimatedTroposphericModel model valid at a date.

getTroposphericRefractionCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get the tropospheric refraction correction.

getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true anomaly.

getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true anomaly.

getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the true anomaly derivative.

getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit

Get the true anomaly derivative.

getTT() - Method in class org.orekit.time.LazyLoadedTimeScales

getTT() - Method in interface org.orekit.time.TimeScales

Get the Terrestrial Time scale.

getTT() - Static method in class org.orekit.time.TimeScalesFactory

Get the Terrestrial Time scale.

getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the turnaroundDenominator.

getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Getter for the turnaroundNumerator.

getTwoDigitsRinexPRN() - Method in class org.orekit.gnss.SatInSystem

Get a 2-digits Pseudo Random Number for RINEX files.

getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.

getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade

Get the method type.

getType() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade

Get the method type.

getType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance

Get the type of the elements.

getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance

Get the type of the elements.

getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Get the type of the elements.

getType() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation

Get the type of observation.

getType() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the type of the token.

getType() - Method in class org.orekit.files.sp3.SP3Header

Returns the SP3FileType associated with this SP3 file.

getType() - Method in class org.orekit.gnss.antenna.Antenna

Get the type of the antenna.

getType() - Method in class org.orekit.orbits.CartesianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.CircularOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.EquinoctialOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldCartesianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldCircularOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.FieldOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.KeplerianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.Orbit

Get the orbit type.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005

Get type of the method.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999

Get type of the method.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max

Get type of the method.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997

Get type of the method.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Get type of the method.

getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005

Get type of the method.

getType() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Get type of the method.

getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage

Get the code for the message type.

getTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the calibration type indicator.

getTypeObs() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection

Get the Carrier Phase Observation Code.

getTypeObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Get an unmodifiable view of the map of observation types.

getTypeOfData() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get the type of data.

getTypesObsScaled() - Method in class org.orekit.files.rinex.observation.ScaleFactorCorrection

Get the list of Observation Types scaled.

getU() - Method in class org.orekit.bodies.Ellipse

Get the unit vector along the major axis.

getU() - Method in class org.orekit.bodies.FieldEllipse

Get the unit vector along the major axis.

getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients

Get the coefficient U₁^j for Fourier index i.

getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients

Get the coefficient U₁^j for Fourier index i.

getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients

Get the coefficient U₂^j for Fourier index = 1 (i == 0).

getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients

Get the coefficient U₂^j for Fourier index = 1 (i == 0).

getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier

Get the underlying attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized

Get the underlying attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation

Get the underlying (ground pointing) attitude provider.

getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering

Get the underlying (ground pointing) attitude provider.

getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Gets the Undulation of the Geoid, N at the given position.

getUnit() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Get the field unit.

getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType

Get the elements units.

getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType

Get the elements units.

getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType

Get the elements units.

getUnits() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

Get the elements units.

getUnits() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Get the units.

getUnits(String) - Method in class org.orekit.utils.units.UnitsCache

Get units from a string specification.

getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get a un-normalization factors array.

getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.

getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.

getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields

Get a gravity field unnormalized coefficients provider.

getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Get a gravity field unnormalized coefficients provider.

getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics

Get a spherical harmonic sine coefficient.

getUpdateInterval() - Method in class org.orekit.gnss.metric.messages.common.SsrUpdateInterval

Get the update interval.

getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month

Get the upper case three letters abbreviation.

getUpperCaseName() - Method in enum org.orekit.time.Month

Get the upper case full name.

getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3

Get Ω₀.

getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac

Get Ω₀.

getUpperLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Get upper limit of the probability of collision value.

getUpperLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision

Get upper limit of the probability of collision value.

getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Getter for the user range accuray (meters).

getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Gets the average URA number.

getURA() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Getter for the user range accuray (meters).

getURA() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Getter for the user range accuray (meters).

getUraiEd() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for Elevation-Dependent User Range Accuracy.

getUraIndex() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get URA index.

getUraiNed0() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for term 0 of Non-Elevation-Dependent User Range Accuracy.

getUraiNed1() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for term 1 of Non-Elevation-Dependent User Range Accuracy.

getUraiNed2() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Getter for term 2 of Non-Elevation-Dependent User Range Accuracy.

getUranus() - Method in interface org.orekit.bodies.CelestialBodies

Get the Uranus singleton body.

getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Uranus singleton body.

getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get start of useable time span covered by attitude data.

getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get end of useable time span covered by ephemerides data.

getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

getUsedObservationData() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData

Get the list of observation data used to perform the combination of measurements.

getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Get user defined parameters logical block.

getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the user defined logical block.

getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Get user defined parameters logical block.

getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Get the user defined parameters logical block.

getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get the user defined parameters logical block.

getUserDefinedParameters() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm

Get user defined parameters.

getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales

Get the Universal Time 1 scale.

getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales

getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales

getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales

Get the Universal Time 1 scale.

getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales

Get the Universal Time 1 scale.

getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUt1MinusUtc() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the UT1-UTC offset.

getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry

Get the UT1-UTC value.

getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the UT1-UTC value.

getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory

Get the UT1-UTC value.

getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Get the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().

getUtc() - Method in class org.orekit.frames.AbstractEopLoader

Get the UTC time scale.

getUTC() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Get the UTC timescale.

getUTC() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Get the UTC timescale.

getUtc() - Method in class org.orekit.propagation.analytical.tle.TLE

Get the UTC time scale used to create this TLE.

getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales

getUTC() - Method in interface org.orekit.time.TimeScales

Get the Universal Time Coordinate scale.

getUTC() - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time Coordinate scale.

getUtcId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Get the UTC Id.

getUTCScale() - Method in class org.orekit.time.UT1Scale

Get the associated UTC scale.

getUTCTAIOffsets() - Method in class org.orekit.time.UTCScale

Returns the UTC-TAI offsets underlying this UTC scale.

getV() - Method in class org.orekit.bodies.Ellipse

Get the unit vector along the minor axis.

getV() - Method in class org.orekit.bodies.FieldEllipse

Get the unit vector along the minor axis.

getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients

Get the coefficient V₁^j for Fourier index i.

getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients

Get the coefficient V₁^j for Fourier index i.

getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients

Get the coefficient V₂^j for Fourier index = 1 (i == 0).

getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients

Get the coefficient V₂^j for Fourier index = 1 (i == 0).

getValidFrom() - Method in class org.orekit.files.sinex.Station

Get start of validity.

getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get start of validity.

getValidityStart() - Method in class org.orekit.time.UTCTAIOffset

Get the start time of validity for this offset.

getValidUntil() - Method in class org.orekit.files.sinex.Station

Get end of validity.

getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna

Get end of validity.

getValue() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData

Get the combined observed value.

getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator

getValue() - Method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable

Get the String representation of the enum.

getValue() - Method in class org.orekit.files.rinex.observation.ObservationData

Get the observed value.

getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction

Get Γ function value.

getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function value.

getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear

Compute the value of the Hansen coefficient K_j^{-n-1, s}.

getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear

Compute the value of the Hansen coefficient K₀^{n, s}.

getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear

Get the K₀^-n-1,s coefficient value.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the Hansen coefficient K_j^{-n-1, s}.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the value of the Hansen coefficient K₀^{n, s}.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Get the K₀^-n-1,s coefficient value.

getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials

Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.

getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials

Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.

getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators

Get the Newcomb operator evaluated at n, s, ρ, σ.

getValue() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Get value of the probability of collision.

getValue() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision

Get value of the probability of collision.

getValue() - Method in class org.orekit.time.TimeStampedDouble

Get value.

getValue() - Method in class org.orekit.time.TimeStampedField

Get value.

getValue() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Get the value.

getValue() - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Get the value.

getValue() - Method in class org.orekit.utils.ParameterDriver

Get current parameter value.

getValue(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get current parameter value at specific date, depending on isContinuousEstimation value, the value returned will be obtained by step estimation or continuous estimation.

getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver

Get the value as a gradient at special date.

getValue(int, Map<String, Integer>, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get the value as a gradient at special date.

getValueAndDerivative(int, int, int, double) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials

Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.

getValueContinuousEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get current parameter value at specific date with continuous estimation.

getValues() - Method in class org.orekit.utils.ParameterDriver

Get all values of the valueSpanMap in the chronological order.

getValueSpanMap() - Method in class org.orekit.utils.ParameterDriver

Get value time span map for parameterDriver.

getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the values samples for the interpolation function.

getValueStepEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Get current parameter value at specific date with step estimation.

getVdim() - Method in class org.orekit.bodies.CR3BPSystem

Get the CR3BP orbital velocity of m2.

getVdop() - Method in class org.orekit.gnss.DOP

Gets the vertical dilution of precision.

getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector f.

getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get equinoctial frame vector f.

getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector g.

getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get equinoctial frame vector g.

getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get equinoctial frame vector w.

getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Get equinoctial frame vector w.

getVeis1950() - Method in class org.orekit.frames.AbstractFrames

getVeis1950() - Method in interface org.orekit.frames.Frames

Get the VEIS 1950 reference frame.

getVeis1950() - Static method in class org.orekit.frames.FramesFactory

Get the VEIS 1950 reference frame.

getVelocity() - Method in class org.orekit.estimation.measurements.PV

Get the velocity.

getVelocity() - Method in class org.orekit.files.sinex.Station

Get the station velocity.

getVelocity() - Method in class org.orekit.frames.FieldTransform

Get the first time derivative of the translation.

getVelocity() - Method in class org.orekit.frames.Transform

Get the first time derivative of the translation.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere

Get the inertial velocity of atmosphere molecules.

getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere

Get the inertial velocity of atmosphere molecules.

getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates

Gets the velocity.

getVelocity() - Method in class org.orekit.utils.PVCoordinates

Gets the velocity.

getVelocityAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate

Get the velocity accuracy.

getVelocityVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Get object Velocity Vector.

getVenus() - Method in interface org.orekit.bodies.CelestialBodies

Get the Venus singleton body.

getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Venus singleton body.

getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies

getVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Get current format version.

getVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Get current format version.

getVersion() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Get current format version.

getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader

Get the format version.

getVersion() - Method in class org.orekit.files.sp3.SP3Header

Get the file version.

getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration

Get ITRF version.

getVertices() - Method in class org.orekit.models.earth.tessellation.Tile

Get the four vertices.

getVmAbsolute() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the typical (50th percentile) visual magnitude.

getVmApparent() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the typical (50th percentile) apparent visual magnitude.

getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the maximum apparent visual magnitude.

getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Get the minimum apparent visual magnitude.

getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Get the V_n,s^m coefficient from V_n,s.

getVtecQualityIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header

Get the VTEC quality indicator.

getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Get the value of warmup iterations.

getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Returns the water vapor pressure at the station [hPa].

getWavelength() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Get the wavelength.

getWavelength() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Get the wavelength.

getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase

Get the wavelength.

getWavelength(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Get the wavelength related to the given RangeMeasurement.

getWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Get the transmit wavelength.

getWavelength() - Method in enum org.orekit.gnss.Frequency

Get the wavelength in meters.

getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the loaded waves.

getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Getter for the reference week of the GNSS orbit.

getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements

Gets the Reference Week of the GNSS orbit.

getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Gets the Reference Week of the SBAS orbit.

getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Gets the Reference Week of the SBAS orbit.

getWeekNumber() - Method in class org.orekit.gnss.rflink.gps.SubFrame1

Get Week Number.

getWeekNumber() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B

Get the almanac week number.

getWeekNumber() - Method in class org.orekit.time.GNSSDate

Get the week number since the GNSS reference epoch.

getWeekNumberLsf() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get Week Number LSF field.

getWeekNumberT() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D

Get Week Number T field.

getWeightedRMS() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Get the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.

getWeightedRms() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Get weighted RMS residual ratio.

getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction to the west of point, expressed in parent shape frame.

getWest() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction to the west of point, expressed in parent shape frame.

getWest() - Method in class org.orekit.frames.TopocentricFrame

Get the west direction of topocentric frame, expressed in parent shape frame.

getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along west axis.

getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along West axis.

getWetMass() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Get the total mass at T₀.

getWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the total mass at T₀.

getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid

Get the WGS84 ellipsoid, attached to the given body frame.

getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory

Get the Wide-Lane combination of measurements.

getWindowLength() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get the normal point window length.

getWindUp(SatelliteSystem, int, Dipole, SatelliteSystem, int, Dipole) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUpFactory

Get a modifier for an emitter/receiver pair.

getWindUp(SatelliteSystem, int, Dipole, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory

Get a modifier for a satellite/receiver pair.

getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the WMM model for the given year.

getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields

Get the WMM model for the given year.

getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields

getX() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver

Getter for the X coordinate in meters in considered Earth centered frame.

getX() - Method in class org.orekit.frames.EOPEntry

Get the X component of the pole motion.

getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get the X axis defining FoV boundary.

getX() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite X position.

getX() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getX() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-X component of satellite coordinates in PZ-90 datum.

getX() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-X component of satellite coordinates.

getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get Χ = 1 / sqrt(1 - e²) = 1 / B.

getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get (χ²) / (n² * a² * (χ + 1 ) ).

getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get (χ²) / (n² * a² * (χ + 1 ) ).

getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get χ³ / (n² * a).

getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get χ³ / (n² * a).

getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite X velocity.

getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-X component of satellite velocity vector in PZ-90 datum.

getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-X component of satellite velocity vector.

getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite X acceleration.

getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.

getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-X component of satellite acceleration vector.

getXM10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the MG2 index scaled to F10.

getXM10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the MG2 index scaled to F10.

getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the MG2 index scaled to F10.

getXM10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the MG2 81-day average centered index.

getXM10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the MG2 81-day average centered index.

getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the MG2 81-day average centered index.

getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get χ / (n² * a²).

getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get χ / (n² * a²).

getXp() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the X component of the pole.

getXp() - Method in class org.orekit.frames.EOPFittedModel

Get the fitted secular and harmonics model for pole x component.

getXp() - Method in class org.orekit.frames.FieldPoleCorrection

Get the x_p parameter.

getXp() - Method in class org.orekit.frames.PoleCorrection

Get the x_p parameter.

getXpDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the X component of the pole first derivative.

getXpDotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the X component of the pole second derivative.

getXPo() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the X polar motion.

getXRate() - Method in class org.orekit.frames.EOPEntry

Get the X component of the pole motion rate.

getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext

Get Χ².

getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get Χ².

getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext

Get Χ².

getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get Χ².

getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext

Get Χ³.

getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext

Get Χ³.

getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.

getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions

Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.

getXYZCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Get the Covariance Matrix in the XYZ Coordinate Frame (defined by value of CdmMetadataKey.ALT_COV_REF_FRAME).

getXYZCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the XYZ covariance matrix.

getY() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver

Getter for the Y coordinate in meters in considered Earth centered frame.

getY() - Method in class org.orekit.frames.EOPEntry

Get the Y component of the pole motion.

getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get the Y axis defining FoV boundary.

getY() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Y position.

getY() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getY() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-Y component of satellite coordinates in PZ-90 datum.

getY() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Y component of satellite coordinates.

getY10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the Solar X-Ray & Lya index scaled to F10.

getY10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the Solar X-Ray & Lya index scaled to F10.

getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the Solar X-Ray & Lya index scaled to F10.

getY10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Get the Solar X-Ray & Lya 81-day ave.

getY10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Get the Solar X-Ray & Lya 81-day ave.

getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters

Get the Solar X-Ray & Lya 81-day ave.

getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the yaw compensation angle at date.

getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the yaw compensation angle at date.

getYawAngle() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Get the yaw angle used for computation of phase wind-up correction.

getYawRate() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Get the yaw rate.

getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Y velocity.

getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.

getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Y component of satellite velocity vector.

getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Y acceleration.

getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.

getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Y component of satellite acceleration vector.

getYear() - Method in enum org.orekit.frames.ITRFVersion

Get the reference year of the frame version.

getYear() - Method in class org.orekit.time.DateComponents

Get the year number.

getYearOfCentury() - Method in class org.orekit.files.ilrs.CRDHeader

Get the year of century from CPF or TLE.

getYp() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the Y component of the pole.

getYp() - Method in class org.orekit.frames.EOPFittedModel

Get the fitted secular and harmonics model for pole y component.

getYp() - Method in class org.orekit.frames.FieldPoleCorrection

Get the y_p parameter.

getYp() - Method in class org.orekit.frames.PoleCorrection

Get the y_p parameter.

getYpDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the Y component of the pole first derivative.

getYpDotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Get the Y component of the pole second derivative.

getYPo() - Method in class org.orekit.files.sinex.SinexEopEntry

Get the Y polar motion.

getYRate() - Method in class org.orekit.frames.EOPEntry

Get the Y component of the pole motion rate.

getZ() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver

Getter for the Z coordinate in meters in considered Earth centered frame.

getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView

Get the Z axis defining FoV boundary.

getZ() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Z position.

getZ() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-Z component of satellite coordinates in PZ-90 datum.

getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Z component of satellite coordinates.

getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Z velocity.

getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.

getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Z component of satellite velocity vector.

getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Getter for the satellite Z acceleration.

getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements

Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.

getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements

Get the ECEF-Z component of satellite acceleration vector.

getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint

Get the direction above the point, expressed in parent shape frame.

getZenith() - Method in class org.orekit.bodies.GeodeticPoint

Get the direction above the point, expressed in parent shape frame.

getZenith() - Method in class org.orekit.frames.TopocentricFrame

Get the zenith direction of topocentric frame, expressed in parent shape frame.

getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the amplitude along zenith axis.

getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Returns the zenith delay array.

getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation

Get a driver allowing to change station position along Zenith axis.

getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Get the phase along zenith axis.

getZero() - Method in class org.orekit.orbits.FieldOrbit

Getter for Field-valued zero.

getZero() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Get zero.

getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates

Get fixed position/velocity at origin (both p, v and a are zero vectors).

getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get a reference to the Z inverse transformation matrix.

getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler

Get a zip/jar crawler for an input.

getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler

Get a zip/jar crawler for an input.

getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler

Get a zip/jar crawler for an input.

getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView

Get the interior zone.

getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector

Get the geographic zone triggering the events.

getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the geographic zone.

GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_js, H_js, I_js and J_js polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Create a set of G_js, H_js, I_js and J_js polynomials.

GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.

GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Create a set of G_ms^j and H_ms^j polynomials.

GillFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for GillFieldIntegrator.

GillFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillFieldIntegratorBuilder

Constructor.

GillFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.GillFieldIntegratorBuilder

Constructor using a "fielded" step.

GillIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for GillIntegrator.

GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder

Build a new instance.

GLOBAL_DRAG_FACTOR - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for global multiplicative factor.

GLOBAL_RADIATION_FACTOR - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for global multiplicative factor.

GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere

Global Ionosphere Map (GIM) model.

GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

Constructor with supported names given by user.

GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

Constructor that uses user defined supported names and data context.

GlobalIonosphereMapModel(TimeScale, DataSource...) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

Constructor that uses user defined data sources.

GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere

The Global Mapping Function model for radio techniques.

GlobalMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel

Build a new instance.

GlobalMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel

Build a new instance.

GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather

The Global Pressure and Temperature 2 (GPT2) model.

GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Constructor with supported names given by user.

GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Constructor with supported names and source of GPT2 auxiliary data given by user.

GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

Constructor with default supported names.

GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather

The Global Pressure and Temperature model.

GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel

Build a new instance.

GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel

Build a new instance.

Glonass - Class in org.orekit.gnss.attitude

Attitude providers for Glonass navigation satellites.

Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass

Simple constructor.

GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.

GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for GLONASS four-year interval number: 1996-01-01.

GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².

GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of Pi for conversion from semicircles to radian.

GLONASSAlmanac - Class in org.orekit.propagation.analytical.gnss.data

This class holds a GLONASS almanac as read from .agl files.

GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Constructor.

GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac

Constructor.

GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss

This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.

GLONASSAnalyticalPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss

This nested class aims at building a GLONASSAnalyticalPropagator.

GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Initializes the builder.

GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Initializes the builder.

GLONASSDate - Class in org.orekit.time

Container for date in GLONASS form.

GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate

Build an instance corresponding to a GLONASS date.

GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate

Build an instance corresponding to a GLONASS date.

GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate

Build an instance from an absolute date.

GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate

Build an instance from an absolute date.

GLONASSEphemeris - Class in org.orekit.propagation.analytical.gnss.data

Class for GLONASS ephemeris used by the GLONASSNumericalPropagator.

GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

Build a new instance.

GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris

Build a new instance.

GLONASSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a Glonass navigation message.

GLONASSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Constructor.

GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical

This class propagates GLONASS orbits using numerical integration.

GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator

Private constructor.

GLONASSNumericalPropagatorBuilder - Class in org.orekit.propagation.numerical

This nested class aims at building a GLONASSNumericalPropagator.

GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Initializes the builder.

GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean, DataContext) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Initializes the builder.

GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data

This interface provides the minimal set of orbital elements needed by the GLONASSAnalyticalPropagator and the GLONASSNumericalPropagator.

GlonassSatelliteChannel - Class in org.orekit.files.rinex.observation

Container for association between GLONASS satellites and frequency channels (f = f₀ + k Δf with k ranging-7 to +6).

GlonassSatelliteChannel(SatInSystem, int) - Constructor for class org.orekit.files.rinex.observation.GlonassSatelliteChannel

Simple constructor.

GLONASSScale - Class in org.orekit.time

GLONASS time scale.

GlonassUserRangeAccuracy - Class in org.orekit.gnss.metric.messages.common

Enumerate for GLONASS User Range Accuracy.

GlonassUserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.GlonassUserRangeAccuracy

Simple constructor.

GMSTScale - Class in org.orekit.time

Greenwich Mean Sidereal Time.

GNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of Pi for conversion from semicircles to radians in GNSS.

GNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Duration of the GNSS week in seconds.

GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude

Attitude providers for navigation satellites.

GNSSClockElements - Interface in org.orekit.propagation.analytical.gnss.data

This interface provides the minimal set of orbital elements needed by the ClockCorrectionsProvider.

GNSSConstants - Interface in org.orekit.propagation.analytical.gnss.data

Set of useful physical constants used in Global Navigation Satellite Systems (GNSS).

GnssData - Class in org.orekit.gnss.metric.ntrip

GNSS data retrieved from Ntrip caster.

GnssData(byte[], int) - Constructor for class org.orekit.gnss.metric.ntrip.GnssData

Build a GNSS data bloc.

GNSSDate - Class in org.orekit.time

Container for date in GNSS form.

GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate

Build an instance corresponding to a GNSS date.

GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate

Build an instance corresponding to a GNSS date.

GNSSDate(int, double, SatelliteSystem, DateComponents, TimeScales) - Constructor for class org.orekit.time.GNSSDate

Build an instance corresponding to a GNSS date.

GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate

Build an instance from an absolute date.

GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate

Build an instance from an absolute date.

GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data

This interface provides the minimal set of orbital elements needed by the GNSSPropagator.

GNSSPropagator - Class in org.orekit.propagation.analytical.gnss

Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.

GNSSPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss

This nested class aims at building a GNSSPropagator.

GNSSPropagatorBuilder(GNSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Initializes the builder.

GNSSPropagatorBuilder(GNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Initializes the builder.

GPS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the earth's rotation rate in rad/s for GPS user.

GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.

GPS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for GPS weeks: 1980-01-06.

GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².

GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Number of weeks in the GPS cycle.

GPSAlmanac - Class in org.orekit.propagation.analytical.gnss.data

This class holds a GPS almanac as read from SEM or YUMA files.

GPSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Constructor.

GPSBlockIIA - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIA navigation satellites.

GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA

Simple constructor.

GPSBlockIIF - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIF navigation satellites.

GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF

Simple constructor.

GPSBlockIIR - Class in org.orekit.gnss.attitude

Attitude providers for GPS block IIR navigation satellites.

GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR

Simple constructor.

GPSCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a GPS navigation message.

GPSCivilianNavigationMessage(boolean) - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSCivilianNavigationMessage

Constructor.

GPSLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a GPS navigation message.

GPSLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSLegacyNavigationMessage

Constructor.

GPSScale - Class in org.orekit.time

GPS time scale.

gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the gradient of the non-central part of the gravity field.

gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the gradient of the non-central part of the gravity field.

GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for GraggBulirschStoerIntegrator.

GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder

Build a new instance.

GRAM - Static variable in class org.orekit.utils.units.Unit

Gram unit.

GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss

GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.

GravityFieldFactory - Class in org.orekit.forces.gravity.potential

Factory used to read gravity field files in several supported formats.

GravityFields - Interface in org.orekit.forces.gravity.potential

Defines methods for obtaining gravity fields.

greatCircleBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder

Construct a waypoint builder interpolating points using a great-circle.

GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for GRGS files.

GRGSFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the GRGS gravity field format.

GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader

Simple constructor.

GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader

Simple constructor.

GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.

GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.

GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.

GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.

GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.

GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.

GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from GRIM5C1 model: 6378136.46 m.

GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from GRIM5C1 model: 1.0 / 298.25765.

GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².

GroundAtNightDetector - Class in org.orekit.propagation.events

Detector for ground location being at night.

GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector

Simple constructor.

GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector

Private constructor.

GroundFieldOfViewDetector - Class in org.orekit.propagation.events

Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.

GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector

Build a new instance.

GroundFieldOfViewDetector(AdaptableInterval, double, int, EventHandler, Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector

Protected constructor with full parameters.

GroundPointing - Class in org.orekit.attitudes

Base class for ground pointing attitude providers.

GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing

Default constructor.

GroundReceiverCommonParametersWithDerivatives - Class in org.orekit.estimation.measurements

Common intermediate parameters used to estimate measurements where receiver is a ground station.

GroundReceiverCommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, FieldTransform<Gradient>, TimeStampedFieldPVCoordinates<Gradient>, Gradient, SpacecraftState, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives

Simple constructor.

GroundReceiverCommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements

Common intermediate parameters used to estimate measurements where receiver is a ground station.

GroundReceiverCommonParametersWithoutDerivatives(SpacecraftState, Transform, TimeStampedPVCoordinates, double, SpacecraftState, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives

Simple constructor.

GroundReceiverMeasurement<T extends GroundReceiverMeasurement<T>> - Class in org.orekit.estimation.measurements

Base class modeling a measurement where receiver is a ground station.

GroundReceiverMeasurement(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.GroundReceiverMeasurement

Simple constructor.

GroundReceiverMeasurement(GroundStation, boolean, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.GroundReceiverMeasurement

Simple constructor.

GroundStation - Class in org.orekit.estimation.measurements

Class modeling a ground station that can perform some measurements.

GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation

Build a ground station ignoring station displacements.

GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation

Simple constructor.

GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.

GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.

GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from GRS80 model: 6378137.0 m.

GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from GRS80 model: 1.0 / 298.257222101.

GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².

GTODProvider - Class in org.orekit.frames

Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).

GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider

Simple constructor.

guessCenter(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName

Guess the name of the center of the reference frame.

guessFrame(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Guesses names from ODM Table 5-3 and Annex A.

GzipFilter - Class in org.orekit.data

Filter for gzip compressed data.

GzipFilter() - Constructor for class org.orekit.data.GzipFilter

Empty constructor.

H

H00 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 00:00:00.

H12 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 12:00:00.

H_X - Static variable in enum org.orekit.orbits.OrbitType

Name for inclination vector first component.

H_Y - Static variable in enum org.orekit.orbits.OrbitType

Name for inclination vector second component .

HaloOrbit - Class in org.orekit.orbits

Class calculating different parameters of a Halo Orbit.

HaloOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.HaloOrbit

Simple Constructor.

HaloOrbit(RichardsonExpansion, double, LibrationOrbitFamily) - Constructor for class org.orekit.orbits.HaloOrbit

Simple Constructor.

HaloXZPlaneCrossingDetector - Class in org.orekit.propagation.events

Detector for XZ Plane crossing.

HaloXZPlaneCrossingDetector(double, double) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector

Simple Constructor.

HaloXZPlaneCrossingDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector

Protected constructor with full parameters.

handleGeneratedMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber

Handle a generated measurement.

handleGeneratedMeasurement(ObservedMeasurement<?>) - Method in interface org.orekit.estimation.measurements.generation.GeneratedMeasurementSubscriber

Handle a generated measurement.

handleNaN(String) - Static method in class org.orekit.files.ilrs.CRD

Replace all " NaN" with " na".

handleStep(OrekitStepInterpolator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler

Handle the current step.

handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter

Handle the current step.

handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter

Handle the current step.

handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter

Handle the current step.

handleStep(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment

Handle the current step.

handleStep(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Handle the current step.

handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Handle the current step.

handleStep(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler

Handle the current step.

handleStep(List<OrekitStepInterpolator>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler

Handle the current step.

handleStep(List<OrekitStepInterpolator>) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer

Handle the current step.

handleStep(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Handle the current step.

handleStep(OrekitStepInterpolator) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Handle the current step.

handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Handle the last accepted step.

handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Handle the current step.

HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t!=0 and n < 0.

HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Constructor.

HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n > 0.

HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Constructor.

HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Utilities class.

HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n < 0.

HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Constructor.

HarmonicAccelerationModel - Class in org.orekit.forces.empirical

Harmonic acceleration model.

HarmonicAccelerationModel(String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.empirical.HarmonicAccelerationModel

Simple constructor.

HarrisPriester - Class in org.orekit.models.earth.atmosphere

This atmosphere model is the realization of the Modified Harris-Priester model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester

Simple constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

hasAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Check if state contains acceleration data.

hasAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Check if an additional state is available.

hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Check if an additional state is available.

hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState

Check if an additional state derivative is available.

hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState

Check if an additional state derivative is available.

hasAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Check if the logical block includes angles.

hasClockEvent() - Method in class org.orekit.files.sp3.SP3Coordinate

Get clock event flag.

hasClockPrediction() - Method in class org.orekit.files.sp3.SP3Coordinate

Get clock prediction flag.

hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().

hasDerivatives() - Method in class org.orekit.orbits.CartesianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldCartesianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldCircularOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.FieldOrbit

Check if orbit includes derivatives.

hasDerivatives() - Method in class org.orekit.orbits.Orbit

Check if orbit includes derivatives.

hasDopplerCountRollover() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Check if there is a Doppler count rollover.

hashCode() - Method in class org.orekit.bodies.FieldGeodeticPoint

hashCode() - Method in class org.orekit.bodies.GeodeticPoint

hashCode() - Method in class org.orekit.estimation.measurements.ObservableSatellite

hashCode() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

hashCode() - Method in class org.orekit.gnss.SatInSystem

hashCode() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters

Get a hashcode for this date.

hashCode() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Get a hashcode for this date.

hashCode() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters

Get a hashcode for this date.

hashCode() - Method in class org.orekit.models.earth.displacement.Tide

hashCode() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get a hashcode for this tle.

hashCode() - Method in class org.orekit.propagation.analytical.tle.TLE

Get a hashcode for this tle.

hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

hashCode() - Method in class org.orekit.time.AbsoluteDate

Get a hashcode for this date.

hashCode() - Method in class org.orekit.time.DateComponents

hashCode() - Method in class org.orekit.time.DateTimeComponents

hashCode() - Method in class org.orekit.time.FieldAbsoluteDate

Get a hashcode for this date.

hashCode() - Method in class org.orekit.time.TimeComponents

hashCode() - Method in class org.orekit.utils.units.Unit

Get a hashcode for this unit.

hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Get boolean testing whether the APM contains at least one maneuver.

hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm

check whether the OPM contains at least one maneuver.

hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Get boolean testing whether the APM contains at least one maneuver.

hasMomentum() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Check if the logical block includes momentum.

hasNonKeplerianAcceleration(FieldPVCoordinates<T>, T) - Static method in class org.orekit.orbits.FieldOrbit

Check if Cartesian coordinates include non-Keplerian acceleration.

hasNonKeplerianAcceleration(PVCoordinates, double) - Static method in class org.orekit.orbits.Orbit

Check if Cartesian coordinates include non-Keplerian acceleration.

hasNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Check if the logical block includes nutation.

hasOrbitManeuverEvent() - Method in class org.orekit.files.sp3.SP3Coordinate

Get orbit maneuver event flag.

hasOrbitPrediction() - Method in class org.orekit.files.sp3.SP3Coordinate

Get orbit prediction flag.

hasParityErrors() - Method in class org.orekit.gnss.rflink.gps.SubFrame

Check if the sub-frame has parity errors.

hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Check if the logical block includes rates.

hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Check if the logical block includes rates.

hasRates() - Method in class org.orekit.orbits.CircularOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in class org.orekit.orbits.EquinoctialOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in class org.orekit.orbits.FieldCircularOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in class org.orekit.orbits.KeplerianOrbit

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasRates() - Method in interface org.orekit.orbits.PositionAngleBased

Tells whether the instance holds rates (first-order time derivatives) for dependent variables.

hasZeroField() - Method in class org.orekit.time.FieldAbsoluteDate

Check if the Field is semantically equal to zero.

HatanakaCompressFilter - Class in org.orekit.files.rinex

Decompression filter for Hatanaka compressed RINEX files.

HatanakaCompressFilter() - Constructor for class org.orekit.files.rinex.HatanakaCompressFilter

Empty constructor.

Header - Class in org.orekit.files.ccsds.section

Header of a CCSDS Navigation Data Message.

Header(double, double) - Constructor for class org.orekit.files.ccsds.section.Header

Constructor.

HeaderKey - Enum in org.orekit.files.ccsds.section

Keywords allowed in Header.

HeaderProcessingState - Class in org.orekit.files.ccsds.section

ProcessingState for NDM header.

HeaderProcessingState(AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.HeaderProcessingState

Simple constructor.

HECTO_PASCAL - Static variable in class org.orekit.files.ccsds.definitions.Units

HectoPascal unit.

HelmertTransformation - Class in org.orekit.frames

Transformation class for geodetic systems.

HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation

Build a transform from its primitive operations.

HelmertTransformation.Predefined - Enum in org.orekit.frames

Enumerate for predefined Helmert transformations.

HERTZ - Static variable in class org.orekit.utils.units.Unit

Hertz unit.

HexadecimalSequenceEncodedMessage - Class in org.orekit.gnss.metric.parser

Encoded message as an hexadecimal characters sequence.

HexadecimalSequenceEncodedMessage(CharSequence) - Constructor for class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage

Simple constructor.

HighamHall54FieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for HighamHall54Integrator.

HighamHall54FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder

Build a new instance.

HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for HighamHall54Integrator.

HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a new instance.

HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity

This class represents the gravitational field of a celestial body.

HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Creates a new instance.

HOUR - Static variable in class org.orekit.utils.units.Unit

Hour unit.

hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic mean anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic mean anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic true anomaly from the hyperbolic eccentric anomaly.

hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic true anomaly from the hyperbolic eccentric anomaly.

hyperbolicMeanToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic eccentric anomaly from the hyperbolic mean anomaly.

hyperbolicMeanToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic eccentric anomaly from the hyperbolic mean anomaly.

hyperbolicMeanToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic true anomaly from the hyperbolic mean anomaly.

hyperbolicMeanToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic true anomaly from the hyperbolic mean anomaly.

hyperbolicTrueToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic eccentric anomaly from the hyperbolic true anomaly.

hyperbolicTrueToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic eccentric anomaly from the hyperbolic true anomaly.

hyperbolicTrueToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility

Computes the hyperbolic mean anomaly from the hyperbolic true anomaly.

hyperbolicTrueToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility

Computes the hyperbolic mean anomaly from the hyperbolic true anomaly.

HZ_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Hertz per second unit.

I

i - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

final inclination.

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final inclination.

IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.

IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).

IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants

Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).

IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).

IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).

IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants

Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).

IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).

IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants

Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.

IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants

Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).

IAUPole - Interface in org.orekit.bodies

Interface for IAU pole and prime meridian orientations.

ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for ICGEM files.

ICGEMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the ICGEM gravity field format.

ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader

Simple constructor.

ICGEMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader

Simple constructor.

IDENTITY - Static variable in class org.orekit.frames.Transform

Identity transform.

IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates

Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).

IDENTITY - Static variable in class org.orekit.utils.units.UnitsConverter

Identity converter.

IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils

Identity provider.

IdentityConverter - Class in org.orekit.files.ccsds.ndm.tdm

Identity converter for Range Units.

IdentityConverter() - Constructor for class org.orekit.files.ccsds.ndm.tdm.IdentityConverter

Empty constructor.

IERS2003_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from IERS2003 model: 7.292115e-5 rad/s.

IERS2003_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from IERS2003 model: -1.0826359e-3.

IERS2003_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from IERS2003 model: 6378136.6 m.

IERS2003_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from IERS2003 model: 1.0 / 298.25642.

IERS2003_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from IERS2003 model: 3.986004418e14 m³/s².

IERS2010_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from IERS2010 model: 7.292115e-5 rad/s.

IERS2010_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from IERS2010 model: -1.0826359e-3.

IERS2010_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from IERS2010 model: 6378136.6 m.

IERS2010_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from IERS2010 model: 1.0 / 298.25642.

IERS2010_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from IERS2010 model: 3.986004418e14 m³/s².

IERS96_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from IERS96 model: 7.292115e-5 rad/s.

IERS96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from IERS96 model: -1.0826359e-3.

IERS96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from IERS96 model: 6378136.49 m.

IERS96_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from IERS96 model: 1.0 / 298.25642.

IERS96_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from IERS96 model: 3.986004418e14 m³/s².

IERSConventions - Enum in org.orekit.utils

Supported IERS conventions.

IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils

Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.

IgsSsrDataField - Enum in org.orekit.gnss.metric.parser

Enum containing all intermediate level data fields that can be parsed to build an IGS SSR message.

IgsSsrMessagesParser - Class in org.orekit.gnss.metric.parser

Parser for SSR encoded messages.

IgsSsrMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.IgsSsrMessagesParser

Constructor.

IgsSsrMessageType - Enum in org.orekit.gnss.metric.parser

Enum containing the supported IGS SSR messages types.

ILRSHeader - Class in org.orekit.files.ilrs

Container for common data contains in International Laser Ranging Service (ILRS) files header.

ILRSHeader() - Constructor for class org.orekit.files.ilrs.ILRSHeader

Empty constructor.

ImmutableFieldTimeStampedCache<T extends FieldTimeStamped<KK>,KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.utils

A cache of TimeStamped data that provides concurrency through immutability.

ImmutableFieldTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableFieldTimeStampedCache

Create a new cache with the given neighbors size and data.

ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

A cache of TimeStamped data that provides concurrency through immutability.

ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache

Create a new cache with the given neighbors size and data.

ImpulseManeuver - Class in org.orekit.forces.maneuvers

Impulse maneuver model.

ImpulseManeuver(EventDetector, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

ImpulseManeuver(EventDetector, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

ImpulseManeuver(EventDetector, AttitudeProvider, Vector3D, double, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

ImpulseManeuver(AdaptableInterval, double, int, EventHandler, EventDetector, AttitudeProvider, Vector3D, double, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Protected constructor with full parameters.

INC - Static variable in enum org.orekit.orbits.OrbitType

Name for inclination.

increment(double[]) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Increment the value.

increment(T[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Increment the value.

increment(double[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Increment the value.

incrementTrajID(String) - Static method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Increments a trajectory ID.

inData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Acknowledge data parsing has started.

inData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Acknowledge data parsing has started.

indexAccuracy(Unit, double, double) - Static method in class org.orekit.files.sp3.SP3Utils

Convert an accuracy from SI units.

Inertia - Class in org.orekit.attitudes

Container for inertia of a 3D object.

Inertia - Class in org.orekit.files.ccsds.ndm.adm.apm

Inertia.

Inertia() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Simple constructor.

InertiaAxis - Class in org.orekit.attitudes

Container for inertial axis.

InertiaKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for inertia entries.

InertialForces - Class in org.orekit.forces.inertia

Inertial force model.

InertialForces(Frame) - Constructor for class org.orekit.forces.inertia.InertialForces

Simple constructor.

inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Acknowledge header parsing has started.

inHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Acknowledge header parsing has started.

init(JavacTask, String...) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

Initialize builder at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Initialize scheduler at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber

Initialize subscriber at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.GeneratedMeasurementSubscriber

Initialize subscriber at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder

Initialize builder at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Initialize builder at the start of a measurements generation.

init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler

Initialize scheduler at the start of a measurements generation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.empirical.AccelerationModel

Initialize the acceleration model at the start of the propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel

Initialize the acceleration model at the start of the propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.ParametricAcceleration

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel

Initialize the acceleration model at the start of the propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel

Initialize the force model at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.ForceModel

Initialize the force model at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Initialize the generator at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Initialize the additional state provider at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.Maneuver

Initialize the force model at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.Maneuver

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Initialization method.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel

Initialization method.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Initialization method called at propagation start.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Initialization method called at propagation start.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter

Initialization method called at propagation start.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Initialization method called at propagation start.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Initialization method called at propagation start.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter

Initialization method called at propagation start.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Initialization method called at propagation start.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.AdditionalStateProvider

Initialize the additional state provider at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAdapterDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector

init(SpacecraftState, AbsoluteDate, EventDetector) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, EventDetector) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, FieldEventDetector<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.MagneticFieldDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector

Initialize event handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Initialize the additional state provider at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations

Initialize the equations at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider

Initialize the generator at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations

Initialize the equations at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider

Initialize the generator at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Initialize step handler at the start of a propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Initialize step handler at the start of a propagation.

init(List<SpacecraftState>, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler

Initialize step handler at the start of a propagation.

init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler

Initialize step handler at the start of a propagation.

init(List<SpacecraftState>, AbsoluteDate) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Initialize the force model at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Initialize the force model at the start of propagation.

init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Initialize the force model at the start of propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Initialize the additional state provider at the start of propagation.

initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Check if the initial state is provided in osculating elements.

initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Check if the initial state is provided in osculating elements.

initializeAdditionalStates(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Initialize the additional state providers at the start of propagation.

initializeAdditionalStates(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Initialize the additional state providers at the start of propagation.

initializeFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Initialize the short periodic terms for the "field" elements.

initializePropagation() - Method in class org.orekit.propagation.AbstractPropagator

Initialize propagation.

initializePropagation() - Method in class org.orekit.propagation.FieldAbstractPropagator

Initialize propagation.

initializeResetters(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Initialize resetters.

initializeResetters(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Initialize resetters.

initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Initialize the short periodic terms for the Kalman Filter.

initializeShortPeriodicTerms(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Initialize the short periodic terms for the Kalman Filter.

initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Initialize the short periodic terms for the Kalman Filter.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Performs initialization prior to propagation for the current force model.

initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Performs initialization prior to propagation for the current force model.

initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Initialize the mapper.

initMapper(Field<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Initialize the mapper.

initPosition() - Method in class org.orekit.orbits.CartesianOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.CircularOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.FieldCartesianOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.FieldOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the position coordinates from the canonical parameters.

initPosition() - Method in class org.orekit.orbits.Orbit

Compute the position coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.Orbit

Compute the position/velocity coordinates from the canonical parameters.

initStates(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.integration.AbstractGradientConverter

Initialize first state with 0 parameters.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Acknowledge metada parsing has started.

inMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Acknowledge metada parsing has started.

InputStreamEncodedMessage - Class in org.orekit.gnss.metric.parser

Encoded message from an input stream.

InputStreamEncodedMessage(InputStream) - Constructor for class org.orekit.gnss.metric.parser.InputStreamEncodedMessage

Simple constructor.

insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Check if date is within a leap second introduction in this time scale.

insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Check if date is within a leap second introduction in this time scale.

insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Check if date is within a leap second introduction in this time scale.

insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Check if date is within a leap second introduction in this time scale.

intArrayToString(int[]) - Method in class org.orekit.files.ccsds.section.AbstractWriter

Convert an array of integer to a comma-separated list.

IntegerBootstrapping - Class in org.orekit.estimation.measurements.gnss

Bootstrapping engine for ILS problem solving.

IntegerBootstrapping(double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerBootstrapping

Constructor for the bootstrapping ambiguity estimator.

integerGaussTransformation(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Perform one integer Gauss transformation.

IntegerLeastSquareComparator - Class in org.orekit.estimation.measurements.gnss

Comparator for IntegerLeastSquareSolution instance.

IntegerLeastSquareComparator() - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator

Simple constructor.

IntegerLeastSquareSolution - Class in org.orekit.estimation.measurements.gnss

Class holding a solution to an Integer Least Square problem.

IntegerLeastSquareSolution(long[], double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution

Simple constructor.

IntegerLeastSquareSolver - Interface in org.orekit.estimation.measurements.gnss

Interface for algorithms solving integer least square problems.

integrate(UnivariateVectorFunction, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature

Integrates a given function on the given interval.

integrate(CalculusFieldUnivariateVectorFunction<T>, T, T, Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature

Integrates a given function on the given interval.

IntegratedEphemeris - Class in org.orekit.propagation.integration

This class stores sequentially generated orbital parameters for later retrieval.

IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List<AdditionalStateProvider>, String[], int[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris

Creates a new instance of IntegratedEphemeris.

IntegrationReference - Enum in org.orekit.files.ccsds.ndm.tdm

Relationship between time tag and integration interval.

INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation

Suffix for ground station intermediate frame name.

interpolate(AbstractTimeInterpolator<Attitude>.InterpolationData) - Method in class org.orekit.attitudes.AttitudeInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<FieldAttitude<KK>, KK>.InterpolationData) - Method in class org.orekit.attitudes.FieldAttitudeInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<SP3Coordinate>.InterpolationData) - Method in class org.orekit.files.sp3.SP3CoordinateHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform

Interpolate a transform from a sample set of existing transforms.

interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform

Interpolate a transform from a sample set of existing transforms.

interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform

Interpolate a transform from a sample set of existing transforms.

interpolate(FieldAbsoluteDate<KK>, Collection<FieldOrbit<KK>>) - Method in class org.orekit.orbits.AbstractFieldOrbitInterpolator

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.AbstractOrbitInterpolator

Get an interpolated instance.

interpolate(AbstractFieldTimeInterpolator<FieldOrbit<KK>, KK>.InterpolationData) - Method in class org.orekit.orbits.FieldOrbitBlender

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<FieldOrbit<KK>, KK>.InterpolationData) - Method in class org.orekit.orbits.FieldOrbitHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<Orbit>.InterpolationData) - Method in class org.orekit.orbits.OrbitBlender

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<Orbit>.InterpolationData) - Method in class org.orekit.orbits.OrbitHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>.InterpolationData) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Interpolate orbit and associated covariance.

interpolate(FieldAbsoluteDate<KK>, Collection<FieldSpacecraftState<KK>>) - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Get an interpolated instance.

interpolate(AbstractFieldTimeInterpolator<FieldSpacecraftState<KK>, KK>.InterpolationData) - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator

Interpolate instance from given interpolation data.

interpolate(AbsoluteDate, Collection<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Get an interpolated instance.

interpolate(AbstractTimeInterpolator<SpacecraftState>.InterpolationData) - Method in class org.orekit.propagation.SpacecraftStateInterpolator

Interpolate instance from given interpolation data.

interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get an interpolated instance.

interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Get an interpolated instance.

interpolate(AbstractFieldTimeInterpolator<T, KK>.InterpolationData) - Method in class org.orekit.time.AbstractFieldTimeInterpolator

Interpolate instance from given interpolation data.

interpolate(AbsoluteDate, Stream<T>) - Method in class org.orekit.time.AbstractTimeInterpolator

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<T>) - Method in class org.orekit.time.AbstractTimeInterpolator

Get an interpolated instance.

interpolate(AbstractTimeInterpolator<T>.InterpolationData) - Method in class org.orekit.time.AbstractTimeInterpolator

Interpolate instance from given interpolation data.

interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolator

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolator

Get an interpolated instance.

interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolator

Get an interpolated instance.

interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolator

Get an interpolated instance.

interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolator

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolator

Get an interpolated instance.

interpolate(AbstractTimeInterpolator<TimeStampedDouble>.InterpolationData) - Method in class org.orekit.time.TimeStampedDoubleHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<TimeStampedField<KK>, KK>.InterpolationData) - Method in class org.orekit.time.TimeStampedFieldHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<AbsolutePVCoordinates>.InterpolationData) - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>, KK>.InterpolationData) - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<TimeStampedAngularCoordinates>.InterpolationData) - Method in class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<TimeStampedFieldAngularCoordinates<KK>, KK>.InterpolationData) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractFieldTimeInterpolator<TimeStampedFieldPVCoordinates<KK>, KK>.InterpolationData) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolate(AbstractTimeInterpolator<TimeStampedPVCoordinates>.InterpolationData) - Method in class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Interpolate instance from given interpolation data.

interpolateOrbit(AbsoluteDate, List<TimeStampedPair<Orbit, StateCovariance>>) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Interpolate orbit at given interpolation date.

InterpolatingTransformProvider - Class in org.orekit.frames

Transform provider using thread-safe interpolation on transforms sample.

InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider

Simple constructor.

InterpolationData(FieldAbsoluteDate<KK>, Collection<T>) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData

Constructor.

InterpolationData(AbsoluteDate, Collection<T>) - Constructor for class org.orekit.time.AbstractTimeInterpolator.InterpolationData

Constructor.

InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities

Interface for interpolation grids.

InterpolationMethod - Enum in org.orekit.files.ccsds.ndm.odm.oem

OEM interpolation method.

InterpolationTableLoader - Class in org.orekit.utils

Used to read an interpolation table from a data file.

InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader

Empty constructor.

InterSatDirectViewDetector - Class in org.orekit.propagation.events

Detector for inter-satellites direct view (i.e.

InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector

simple constructor.

InterSatDirectViewDetector(OneAxisEllipsoid, double, PVCoordinatesProvider, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector

Private constructor.

InterSatellitesPhase - Class in org.orekit.estimation.measurements.gnss

Phase measurement between two satellites.

InterSatellitesPhase(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Constructor.

InterSatellitesPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites phase measurement with ambiguity.

InterSatellitesPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier

Constructor.

InterSatellitesPhaseBuilder - Class in org.orekit.estimation.measurements.generation

Builder for InterSatellitesPhase measurements.

InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder

Simple constructor.

InterSatellitesRange - Class in org.orekit.estimation.measurements

One-way or two-way range measurements between two satellites.

InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange

Simple constructor.

InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for InterSatellitesRange measurements.

InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder

Simple constructor.

InterSatellitesWindUp - Class in org.orekit.estimation.measurements.gnss

Modifier for wind-up effect in GNSS inter-satellites phase measurements.

InterSatellitesWindUpFactory - Class in org.orekit.estimation.measurements.gnss

Factory for wind-up modifiers.

InterSatellitesWindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesWindUpFactory

Simple constructor.

IntervalEventTrigger<T extends AbstractDetector<T>> - Class in org.orekit.forces.maneuvers.trigger

Maneuver triggers based on a single event detector that defines firing intervals.

IntervalEventTrigger(T) - Constructor for class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Simple constructor.

intValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField

Get the value of the field as an integer.

invalidAfter(AbsoluteDate) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Indicate the date after which the resulting PVCoordinatesProvider is invalid.

invalidAfter() - Method in class org.orekit.utils.WaypointPVBuilder

Indicate the resulting PVCoordinatesProvider should be invalid after the last waypoint.

invalidBefore(AbsoluteDate) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder

Indicate the date before which the resulting PVCoordinatesProvider is invalid.

invalidBefore() - Method in class org.orekit.utils.WaypointPVBuilder

Indicate the resulting PVCoordinatesProvider should be invalid before the first waypoint.

InvalidPVProvider() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.InvalidPVProvider

Empty constructor.

inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Inverse the decomposition.

inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod

Inverse the decomposition.

inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Inverse the decomposition.

IodGauss - Class in org.orekit.estimation.iod

Gauss angles-only Initial Orbit Determination (IOD) algorithm.

IodGauss(double) - Constructor for class org.orekit.estimation.iod.IodGauss

Constructor.

IodGibbs - Class in org.orekit.estimation.iod

Gibbs position-based Initial Orbit Determination (IOD) algorithm.

IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs

Creator.

IodGooding - Class in org.orekit.estimation.iod

Gooding angles only Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.

IodGooding(double) - Constructor for class org.orekit.estimation.iod.IodGooding

Constructor.

IodLambert - Class in org.orekit.estimation.iod

Lambert position-based Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.

IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert

Creator.

IodLaplace - Class in org.orekit.estimation.iod

Laplace angles-only Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.

IodLaplace(double) - Constructor for class org.orekit.estimation.iod.IodLaplace

Constructor.

IonosphereBaseMessage - Class in org.orekit.files.rinex.navigation

Base container for data contained in a ionosphere message.

IonosphereBaseMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereBaseMessage

Simple constructor.

IonosphereBDGIMMessage - Class in org.orekit.files.rinex.navigation

Container for data contained in a ionosphere BDGIM message.

IonosphereBDGIMMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage

Simple constructor.

IonosphereFreeCombination - Class in org.orekit.estimation.measurements.gnss

Ionosphere-free combination.

IonosphereKlobucharMessage - Class in org.orekit.files.rinex.navigation

Container for data contained in a ionosphere Klobuchar message.

IonosphereKlobucharMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Simple constructor.

IonosphereNequickGMessage - Class in org.orekit.files.rinex.navigation

Container for data contained in a ionosphere Nequick G message.

IonosphereNequickGMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Simple constructor.

IonosphericCorrectionType - Enum in org.orekit.files.rinex.navigation

Ionospheric correction type.

IonosphericMappingFunction - Interface in org.orekit.models.earth.ionosphere

Interface for mapping functions used in the ionospheric delay computation.

IonosphericModel - Interface in org.orekit.models.earth.ionosphere

Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

IRNSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the earth's rotation rate in rad/s for IRNSS user.

IRNSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.

IRNSS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for IRNSS weeks: 1999-08-22.

IRNSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².

IRNSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Number of weeks in the IRNSS cycle.

IRNSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data

Class for IRNSS almanac.

IRNSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac

Constructor.

IRNSSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in an IRNSS navigation message.

IRNSSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Constructor.

IRNSSScale - Class in org.orekit.time

IRNSS time scale (also called IRNWT for IRNSS NetWork Time).

isA2b() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Check if rotation direction is from frame A to frame B.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator

Check if an additional state is managed.

isAfter(TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is strictly after another.

isAfter(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is strictly after another.

isAfterOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is after or equal to another.

isAfterOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is after or equal to another.

isAltCovFlagSet() - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance

Get the flag indicating whether the alternate covariance type set in the CDM Object metadata section is Sigma/Eigenvectors Covariance.

isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod

Get flag that defines if the method is a maximum probability of collision computing method.

isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999

Get flag that defines if the method is a maximum probability of collision computing method.

isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max

Get flag that defines if the method is a maximum probability of collision computing method.

isAMaximumProbabilityOfCollisionMethod() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod

Get flag that defines if the method is a maximum probability of collision computing method.

isBefore(TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is strictly before another.

isBefore(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is strictly before another.

isBeforeOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is before or equal to another.

isBeforeOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is before or equal to another.

isBetween(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.

isBetween(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.

isBetweenOrEqualTo(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.

isBetweenOrEqualTo(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.

isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CPFHeader

Get the flag telling if the center of mass correction is applied.

isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader

Get the center of mass correction applied indicator.

isChildOf(Frame) - Method in class org.orekit.frames.Frame

Determine if a Frame is a child of another one.

isCloseTo(TimeStamped, double) - Method in class org.orekit.time.AbsoluteDate

Check if the instance time is close to another.

isCloseTo(FieldTimeStamped<T>, double) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance time is close to another.

isCnv2() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Check it message is a CNV2 message.

isCompatibleWith(AttitudeEndpoints) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Check if a endpoint is compatible with another one.

isCompatibleWithTIVs() - Method in class org.orekit.files.ilrs.CPFHeader

Get the flag for compatibility with TIVs.

isConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header

Get the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.

isContinuousEstimation() - Method in class org.orekit.utils.ParameterDriver

Check if parameter estimation is continuous, that is to say when a value wants to be known at date t, the value returned will be an interpolation between start value on span corresponding for date t and end value (which corresponds to the start of the next span), continuous estimation.

isCovXYZset() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Get the flag indicating whether the alternate covariance type set in the CDM Object metadata section is XYZ.

isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.

isDoubleSided() - Method in class org.orekit.forces.Panel

Check if the panel is double-sided (typically solar arrays).

isDSStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Check if a field state corresponds to derivatives with respect to state.

isElliptical() - Method in class org.orekit.orbits.FieldOrbit

Returns true if and only if the orbit is elliptical i.e.

isElliptical() - Method in class org.orekit.orbits.Orbit

Returns true if and only if the orbit is elliptical i.e.

isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Check if a measurement is enabled.

isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Check if a measurement is enabled.

isEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represents the same time as another.

isEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate

Check if the instance represents the same time as another.

isExternal2SpacecraftBody() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Check if attitude is from external frame to spacecraft body frame.

isFiring(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Check if maneuvering is on.

isFiring(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Check if maneuvering is on.

isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Check if maneuvering is on.

isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Find out if the maneuver is firing or not.

isFiring(FieldAbsoluteDate<S>, S[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Find out if the maneuver is firing or not.

isFiring(AbsoluteDate, double[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Find out if the maneuver is firing or not.

isFiring(FieldAbsoluteDate<T>, T[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers

Find out if the maneuver is firing or not.

isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Method to check if the thruster is firing on initialization.

isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger

Method to check if the thruster is firing on initialization.

isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Method to check if the thruster is firing on initialization.

isFirst() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Get the flag for the placement of the quaternion QC in the attitude data.

isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE

Check the lines format validity.

isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE

Check the lines format validity.

isForward() - Method in class org.orekit.propagation.events.AbstractDetector

Check if the current propagation is forward or backward.

isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector

Check if the current propagation is forward or backward.

isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Check is integration direction is forward in date.

isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Check is integration direction is forward in date.

isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Return the forward propagation flag.

isGradientStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Check if a field state corresponds to derivatives with respect to state.

isHealthAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the flag indicating if GLONASS almanac health is available.

isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the Increasing/decreasing status of the event.

isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent

Get the Increasing/decreasing status of the event.

isIncreasing() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event

Is the g() function increasing?

isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

Is the g() function increasing?

isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Check if a point is inside the ellipsoid.

isInside(FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid

Check if a point is inside the ellipsoid.

isMaxProbability() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision

Get flag that defines if this probability of collision can be considered a maximum probability of collision.

isMaxProbability() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision

Get flag that defines if this probability of collision can be considered a maximum probability of collision.

isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Check if only the mean elements should be used in a semi-analytical propagation.

isMelbourneWubbenaConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header

Get the flag indicating if consistency between code and phase biases is maintained for the MW combinations.

isNetworked() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Check if the stream is generated from a network of stations.

isNMEARequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord

Check if NMEA message must be sent to caster.

isOn() - Method in enum org.orekit.files.ccsds.definitions.OnOff

Check if status is "on".

isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Check if fitting uses only sample positions.

isOrbitDefined() - Method in class org.orekit.propagation.FieldSpacecraftState

Check if the state contains an orbit part.

isOrbitDefined() - Method in class org.orekit.propagation.SpacecraftState

Check if the state contains an orbit part.

IsotropicDrag - Class in org.orekit.forces.drag

This class models isotropic drag effects.

IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag

Constructor with drag coefficient min/max set to ±∞.

IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag

Constructor with drag coefficient min/max set by user.

IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Simple constructor.

IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Simple constructor.

IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation

This class represents the features of a simplified spacecraft.

IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Constructor with reflection coefficient min/max set to ±∞.

IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Constructor with reflection coefficient min/max set by user.

isPositionAngleBased() - Method in enum org.orekit.orbits.OrbitType

Tells if the orbit type is based on position angles or not.

isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.

isPseudoInertial() - Method in class org.orekit.frames.Frame

Check if the frame is pseudo-inertial.

isQuasiInertial() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame

Check if frame should be treated as inertial.

isQuasiInertial() - Method in interface org.orekit.frames.encounter.EncounterLOF

Get flag that indicates if current local orbital frame shall be treated as pseudo-inertial.

isQuasiInertial() - Method in interface org.orekit.frames.LOF

Get flag that indicates if current local orbital frame shall be treated as pseudo-inertial.

isReceiveAmplitudeCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader

Get the receive amplitude correction applied indicator.

isRefractionCorrected() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get the flag indicating if the refraction is corrected.

isSelected() - Method in class org.orekit.utils.ParameterDriver

Check if parameter is selected.

isSignalInteger() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias

Get the flag indicating is signal has integer property.

isSimpleEOP() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Check if tidal effects are ignored when interpolating EOP.

isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.ContextBinding

Get EOP interpolation method.

isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Get EOP interpolation method.

isSimpleEop() - Method in class org.orekit.frames.EOPHistory

Determine if this history uses simplified EOP corrections.

isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Check if rates are specified in spacecraft body frame.

isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Check if rates are specified in spacecraft body frame.

isSpacecraftTimeSimplified() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get the spacecraft time simplified flag.

isStart() - Method in class org.orekit.utils.DateDriver

Check if driver corresponds to a start date.

isStationSystemDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader

Get the station system delay applied indicator.

isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Check if some provider is supported.

isSupported(String) - Method in interface org.orekit.utils.ParameterDriversProvider

Check if a parameter is supported.

isTime() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Check if a field is a time field.

isTransponderDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader

Get the spacecraft system delay applied (transponders) indicator.

isTroposphericRefractionApplied() - Method in class org.orekit.files.ilrs.CRDHeader

Get the tropospheric refraction correction applied indicator.

isTwoWay() - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement

Check if the instance represents a two-way measurement.

isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange

Check if the instance represents a two-way measurement.

isValid(int) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration

Check if configuration entry is valid for a date.

isVariable(DerivativeStructure, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Check if a derivative represents a specified variable.

isVariable(Gradient, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel

Check if a derivative represents a specified variable.

ITRFVersion - Enum in org.orekit.frames

Enumerate for ITRF versions.

ITRFVersion.Converter - Class in org.orekit.frames

Specialized transform provider between ITRF frames.

ITRFVersionConfiguration(String, ITRFVersion, int, int) - Constructor for class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration

Simple constructor.

ITRFVersionLoader - Class in org.orekit.frames

Loader for ITRF version configuration file.

ITRFVersionLoader(String) - Constructor for class org.orekit.frames.ITRFVersionLoader

Build a loader for ITRF version configuration file.

ITRFVersionLoader(String, DataProvidersManager) - Constructor for class org.orekit.frames.ITRFVersionLoader

Build a loader for ITRF version configuration file.

ITRFVersionLoader() - Constructor for class org.orekit.frames.ITRFVersionLoader

Build a loader for ITRF version configuration file using the default name.

ITRFVersionLoader.ITRFVersionConfiguration - Class in org.orekit.frames

ITRF version configuration entry.

ItrfVersionProvider - Interface in org.orekit.frames

Interface for retrieving the ITRF version for a given set of EOP data.

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

J2000_EPOCH - Static variable in class org.orekit.time.DateComponents

J2000.0 Reference epoch: 2000-01-01.

J2DifferentialEffect - Class in org.orekit.propagation.analytical

Analytical model for J2 effect.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2SquaredModel - Interface in org.orekit.propagation.semianalytical.dsst.forces

Semi-analytical J2-squared model.

JacobianPropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using the real Jacobian.

JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter

Simple constructor.

JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Provider of the Jacobi polynomials P_l^v,w.

JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents

Java Reference epoch: 1970-01-01.

JB2008 - Class in org.orekit.models.earth.atmosphere

This is the realization of the Jacchia-Bowman 2008 atmospheric model.

JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.JB2008

Constructor with space environment information for internal computation.

JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.JB2008

Constructor with space environment information for internal computation.

JB2008InputParameters - Interface in org.orekit.models.earth.atmosphere

Interface for solar activity and magnetic activity data.

JB2008SpaceEnvironmentData - Class in org.orekit.models.earth.atmosphere.data

This class provides a container for the solar indices data required by the JB2008 atmospheric model.

JB2008SpaceEnvironmentData(String, String) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Simple constructor.

JB2008SpaceEnvironmentData(String, String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Constructor that allows specifying the source of the SOLFSMY space weather file.

JB2008SpaceEnvironmentData(DataSource, DataSource) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Simple constructor.

JB2008SpaceEnvironmentData(DataSource, DataSource, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData

Constructor that allows specifying the source of the SOLFSMY space weather file.

JOULE - Static variable in class org.orekit.utils.units.Unit

Joule unit.

JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical Unit: 149597870691 m.

JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants

Earth attraction coefficient (m³/s²).

JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Earth/Moon mass ratio: 81.30059.

JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) attraction coefficient (m³/s²).

JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants

Gaussian gravitational constant: 0.01720209895 √(AU³/d²).

JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) ttraction coefficient (m³/s²).

JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) attraction coefficient (m³/s²).

JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants

Sun/Mercury attraction coefficient (m³/s²).

JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants

Moon attraction coefficient (m³/s²).

JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) attraction coefficient (m³/s²).

JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) ttraction coefficient (m³/s²).

JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) attraction coefficient (m³/s²).

JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) mass ratio: 328900.56.

JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants

Sun attraction coefficient (m³/s²).

JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) mass ratio: 1047.3486.

JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) mass ratio: 3098708.0.

JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Mercury mass ratio: 6023600.

JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) mass ratio: 19412.24.

JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) mass ratio: 1.35e8.

JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) mass ratio: 3497.898.

JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) mass ratio: 22902.98.

JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Venus mass ratio: 408523.71.

JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) attraction coefficient (m³/s²).

JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants

Sun/Venus attraction coefficient (m³/s²).

JPLEphemeridesLoader - Class in org.orekit.bodies

Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).

JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader

Create a loader for JPL ephemerides binary files.

JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType, DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader

Create a loader for JPL ephemerides binary files.

JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies

List of supported ephemerides types.

JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies

Interface for raw position-velocity retrieval.

JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants

Duration of a Julian century: 36525 Constants.JULIAN_DAY.

JULIAN_DAY - Static variable in interface org.orekit.utils.Constants

Duration of a mean solar day: 86400.0 s.

JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for julian dates: -4712-01-01.

JULIAN_EPOCH - Static variable in class org.orekit.time.DateTimeComponents

The Julian Epoch.

JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Julian year: 365.25 Constants.JULIAN_DAY.

JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Jupiter.

K

K1 - Static variable in class org.orekit.models.earth.displacement.Tide

K₁ tide.

K2 - Static variable in class org.orekit.models.earth.displacement.Tide

K₂ tide.

KalmanEstimation - Interface in org.orekit.estimation.sequential

Interface for accessing Kalman filter estimations.

KalmanEstimator - Class in org.orekit.estimation.sequential

Implementation of a Kalman filter to perform orbit determination.

KalmanEstimatorBuilder - Class in org.orekit.estimation.sequential

Builder for a Kalman filter estimator.

KalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.KalmanEstimatorBuilder

Default constructor.

KalmanEstimatorUtil - Class in org.orekit.estimation.sequential

Utility class for Kalman Filter.

KalmanModel - Class in org.orekit.estimation.sequential

Class defining the process model dynamics to use with a KalmanEstimator.

KalmanModel(List<PropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.KalmanModel

Kalman process model constructor.

KalmanObserver - Interface in org.orekit.estimation.sequential

Observer for Kalman filter estimations.

KeplerianAnomalyUtility - Class in org.orekit.orbits

Utility methods for converting between different Keplerian anomalies.

KeplerianElements - Class in org.orekit.files.ccsds.ndm.odm

Container for Keplerian elements.

KeplerianElements() - Constructor for class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Simple constructor.

KeplerianElementsKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for Keplerian elements entries.

KeplerianOrbit - Class in org.orekit.orbits

This class handles traditional Keplerian orbital parameters.

KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Creates a new instance.

KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Creates a new instance.

KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from Cartesian parameters.

KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from Cartesian parameters.

KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from any kind of orbital parameters.

KeplerianPropagator - Class in org.orekit.propagation.analytical

Simple Keplerian orbit propagator.

KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit only.

KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and attitude provider.

KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit, attitude provider and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Keplerian propagator.

KeplerianPropagatorBuilder(Orbit, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a new instance.

KeplerianPropagatorBuilder(Orbit, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a new instance.

KG_M2 - Static variable in class org.orekit.files.ccsds.definitions.Units

kg.m² unit.

KILOGRAM - Static variable in class org.orekit.utils.units.Unit

Kilogram unit.

KILOMETRE - Static variable in class org.orekit.utils.units.Unit

Kilometre unit.

KILOMETRES_2_TO_METRES_2 - Static variable in class org.orekit.utils.units.UnitsConverter

Square kilometres to square metres converter.

KILOMETRES_TO_METRES - Static variable in class org.orekit.utils.units.UnitsConverter

Kilometres to metres converter.

KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth.ionosphere

Loads Klobuchar-Style ionospheric coefficients a given input stream.

KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Constructor with supported names given by user.

KlobucharIonoCoefficientsLoader(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Constructor that uses user defined supported names and data context.

KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Constructor with default supported names.

KlobucharIonoModel - Class in org.orekit.models.earth.ionosphere

Klobuchar ionospheric delay model.

KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

KlobucharIonoModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

KM2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Square kilometers units.

KM2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Square kilometers per second units.

KM2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Square kilometers per square second units.

KM3_P_S2_TO_M3_P_S2 - Static variable in class org.orekit.utils.units.UnitsConverter

km³/s² to m³/s² converter.

KM3_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units

km³/s² unit.

KM_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Kilometers per second units.

KM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units

Kilometers par second units.

KM_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Kilometers per square second units.

KM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units

Kilometers par square second units.

KnockeRediffusedForceModel - Class in org.orekit.forces.radiation

The Knocke Earth Albedo and IR emission force model.

KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel

Default Constructor.

KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double, TimeScale) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel

General constructor.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter

Padding width for aligning the '=' sign.

KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter

Padding width for aligning the '=' sign.

KvnGenerator - Class in org.orekit.files.ccsds.utils.generation

Generator for Key-Value Notation CCSDS messages.

KvnGenerator(Appendable, int, String, double, int) - Constructor for class org.orekit.files.ccsds.utils.generation.KvnGenerator

Simple constructor.

KvnLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical

Lexical analyzer for Key-Value Notation CCSDS messages.

KvnLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer

Simple constructor.

KvnStructureKey - Enum in org.orekit.files.ccsds.section

Keys for FileFormat.KVN format structure.

KvnStructureProcessingState - Class in org.orekit.files.ccsds.section

ProcessingState for structure of FileFormat.KVN CCSDS Messages.

KvnStructureProcessingState(AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.KvnStructureProcessingState

Simple constructor.

L

L1Frame - Class in org.orekit.frames

Class to create a L1 centered frame with L1TransformProvider.

L1Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1Frame

Simple constructor.

L1TransformProvider - Class in org.orekit.frames

L1 Transform provider for a frame on the L1 Lagrange point of two celestial bodies.

L1TransformProvider(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1TransformProvider

Simple constructor.

L2Frame - Class in org.orekit.frames

Class to create a L2 centered frame with L2TransformProvider.

L2Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L2Frame

Simple constructor.

Laas2015 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision using the method described in : "SERRA, Romain, ARZELIER, Denis, JOLDES, Mioara, et al.

Laas2015() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Default constructor.

Laas2015(double, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015

Simple constructor.

LABEL_INDEX - Static variable in class org.orekit.files.rinex.utils.parsing.RinexUtils

Index of label in header lines.

LagrangianPoints - Enum in org.orekit.utils

Enumerate for selecting which Lagrangian Point to consider in different classes.

LambdaMethod - Class in org.orekit.estimation.measurements.gnss

Decorrelation/reduction engine for LAMBDA method.

LambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.LambdaMethod

Empty constructor.

LaserConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Empty constructor.

LatitudeCrossingDetector - Class in org.orekit.propagation.events

Detector for geographic latitude crossing.

LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector

Build a new detector.

LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector

Build a detector.

LatitudeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector

Protected constructor with full parameters.

LatitudeExtremumDetector - Class in org.orekit.propagation.events

Detector for geographic latitude extremum.

LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector

Build a new detector.

LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector

Build a detector.

LatitudeExtremumDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector

Protected constructor with full parameters.

LazyLoadedCelestialBodies - Class in org.orekit.bodies

This class lazily loads auxiliary data when it is needed by a requested body.

LazyLoadedCelestialBodies(DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.LazyLoadedCelestialBodies

Create a celestial body factory with the given auxiliary data sources.

LazyLoadedDataContext - Class in org.orekit.data

A data context that aims to match the behavior of Orekit 10.0 regarding auxiliary data.

LazyLoadedDataContext() - Constructor for class org.orekit.data.LazyLoadedDataContext

Create a new data context that only loads auxiliary data when it is first accessed and allows configuration of the auxiliary data sources until then.

LazyLoadedEop - Class in org.orekit.frames

Loads Earth Orientation Parameters (EOP) from a configured set of EopHistoryLoaders on demand.

LazyLoadedEop(DataProvidersManager) - Constructor for class org.orekit.frames.LazyLoadedEop

Create a new instance for loading EOP data from multiple EopHistoryLoaders.

LazyLoadedFrames - Class in org.orekit.frames

This class lazily loads auxiliary data when it is needed by a requested frame.

LazyLoadedFrames(LazyLoadedEop, TimeScales, CelestialBodies) - Constructor for class org.orekit.frames.LazyLoadedFrames

Create a collection of frames from the given auxiliary data.

LazyLoadedGeoMagneticFields - Class in org.orekit.models.earth

Loads magnetic fields on request and can be configured after creation.

LazyLoadedGeoMagneticFields(DataProvidersManager) - Constructor for class org.orekit.models.earth.LazyLoadedGeoMagneticFields

Create a factory for magnetic fields that uses the given data manager to load magnetic field files.

LazyLoadedGravityFields - Class in org.orekit.forces.gravity.potential

Loads gravity fields when first requested and can be configured until then.

LazyLoadedGravityFields(DataProvidersManager, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Create a factory for gravity fields that uses the given data manager to load the gravity field files.

LazyLoadedTimeScales - Class in org.orekit.time

An implementation of TimeScales that loads auxiliary data, leap seconds and UT1-UTC, when it is first accessed.

LazyLoadedTimeScales(LazyLoadedEop) - Constructor for class org.orekit.time.LazyLoadedTimeScales

Create a new set of time scales with the given sources of auxiliary data.

LeastSquaresTleGenerationAlgorithm - Class in org.orekit.propagation.analytical.tle.generation

Least squares method to generate a usable TLE from a spacecraft state.

LeastSquaresTleGenerationAlgorithm() - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Default constructor.

LeastSquaresTleGenerationAlgorithm(int) - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Default constructor.

LeastSquaresTleGenerationAlgorithm(int, TimeScale, Frame) - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm

Constructor.

LegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a GPS/QZNSS legacy navigation message.

LegacyNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Constructor.

LegendrePolynomials - Class in org.orekit.utils

Computes the P_nm(t) coefficients.

LegendrePolynomials(int, int, double) - Constructor for class org.orekit.utils.LegendrePolynomials

Create Legendre polynomials for the given degree and order.

LenseThirringRelativity - Class in org.orekit.forces.gravity

Lense-Thirring post-Newtonian correction force due to general relativity.

LenseThirringRelativity(double, Frame) - Constructor for class org.orekit.forces.gravity.LenseThirringRelativity

Constructor.

LexicalAnalyzer - Interface in org.orekit.files.ccsds.utils.lexical

Interface for CCSDS messages lexical analysis.

LexicalAnalyzerSelector - Class in org.orekit.files.ccsds.utils.lexical

Utility class for selecting either XmlLexicalAnalyzer or KvnLexicalAnalyzer depending on data first bytes.

LibrationOrbit - Class in org.orekit.orbits

Base class for libration orbits.

LibrationOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LibrationOrbit

Constructor.

LibrationOrbitFamily - Enum in org.orekit.orbits

Enumerate for Libration Orbit family.

LibrationOrbitType - Enum in org.orekit.orbits

Enumerate for Libration Orbit type.

LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for lift ration enabling Jacobian processing.

lIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the index of an entry in the lower triangular matrix.

LineParameters(AbsoluteDate) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters

Constructor.

LineParameters(AbsoluteDate, double[], double, double[], double, double, int, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters

Constructor.

LineParameters(AbsoluteDate, double) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters

Constructor.

LineParameters(AbsoluteDate, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters

Constructor.

LNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Identifier for message type.

LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the L_n^s(γ).

LnsCoefficients(int, int, double[][], SortedMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Create a set of L_n^s(γ) coefficients.

loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader

Load celestial body.

loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Load celestial body.

loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Load data from a stream.

loadData() - Method in class org.orekit.gnss.SEMParser

Loads almanacs.

loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser

loadData() - Method in class org.orekit.gnss.YUMAParser

Loads almanacs.

loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser

loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Load Klobuchar-Style ionospheric coefficients read from some file.

loadData(InputStream, String) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader

Loads an bi-variate interpolation table from the given InputStream.

loadKlobucharIonosphericCoefficients() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Load the data using supported names .

loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Load the data for a given day.

loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions

Load the Love numbers.

loadOffsets() - Method in class org.orekit.time.AGILeapSecondFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in class org.orekit.time.TAIUTCDatFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in class org.orekit.time.UTCTAIBulletinAFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in class org.orekit.time.UTCTAIHistoryFilesLoader

Load UTC-TAI offsets entries.

loadOffsets() - Method in interface org.orekit.time.UTCTAIOffsetsLoader

Load UTC-TAI offsets entries.

loadViennaCoefficients() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Load the data using supported names .

loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Load the data for a given day.

LocalizedException - Interface in org.orekit.errors

This interface specified methods implemented by localized exception classes.

LocalMagneticFieldFrame - Class in org.orekit.frames

This class handles a magnetic field variation attitude provider.

LocalMagneticFieldFrame(Frame, GeoMagneticField, Frame) - Constructor for class org.orekit.frames.LocalMagneticFieldFrame

Constructor with default definition of the local orbital frame: x: Magnetic field y: Completes orthonormal frame z: Cross product of the magnetic field with the orbital momentum .

LocalMagneticFieldFrame(Frame, GeoMagneticField, LocalMagneticFieldFrame.LOFBuilderVector, Frame) - Constructor for class org.orekit.frames.LocalMagneticFieldFrame

Constructor with custom definition of the local orbital frame: x: Magnetic field y: Completes orthonormal frame z: Cross product of the magnetic field with chosen vector For near-polar orbits, it is suggested to use the orbital momentum to define the local orbital frame.

LocalMagneticFieldFrame.LOFBuilderVector - Enum in org.orekit.frames

Enum defining how the +j axis of the local orbital frame will be defined.

LocalOrbitalFrame - Class in org.orekit.frames

Class for frames moving with an orbiting satellite.

LocalOrbitalFrame(Frame, LOF, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame

Build a new instance.

LocalSolarActivity(AbsoluteDate) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity

Constructor.

LOF - Interface in org.orekit.frames

Interface for local orbital frame.

LofOffset - Class in org.orekit.attitudes

Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.

LofOffset(Frame, LOF) - Constructor for class org.orekit.attitudes.LofOffset

Create a LOF-aligned attitude.

LofOffset(Frame, LOF, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset

Creates new instance.

LofOffsetPointing - Class in org.orekit.attitudes

This class provides a default attitude provider.

LofOffsetPointing(Frame, BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing

Creates new instance.

LOFType - Enum in org.orekit.frames

Enumerate for different types of Local Orbital Frames.

LongitudeCrossingDetector - Class in org.orekit.propagation.events

Detector for geographic longitude crossing.

LongitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector

Build a new detector.

LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector

Build a detector.

LongitudeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector

Protected constructor with full parameters.

LongitudeExtremumDetector - Class in org.orekit.propagation.events

Detector for geographic longitude extremum.

LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector

Build a new detector.

LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector

Build a detector.

LongitudeExtremumDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector

Protected constructor with full parameters.

LoveNumbers - Class in org.orekit.utils

Container for Love numbers.

LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers

Simple constructor.

lowestAltitudeIntermediate(Vector3D, Vector3D) - Method in class org.orekit.bodies.OneAxisEllipsoid

Find intermediate point of lowest altitude along a line between two endpoints.

lowestAltitudeIntermediate(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Find intermediate point of lowest altitude along a line between two endpoints.

Loxodrome - Class in org.orekit.bodies

Perform calculations on a loxodrome (commonly, a rhumb line) on an ellipsoid.

Loxodrome(GeodeticPoint, double, OneAxisEllipsoid) - Constructor for class org.orekit.bodies.Loxodrome

Constructor building a loxodrome from an initial point and an azimuth-off-local-north heading.

Loxodrome(GeodeticPoint, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.bodies.Loxodrome

Constructor building a loxodrome from an initial point and an azimuth-off-local-north heading.

LoxodromeArc - Class in org.orekit.bodies

Loxodrome defined by a start and ending point.

LoxodromeArc(GeodeticPoint, GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.bodies.LoxodromeArc

Class constructor where the arc's altitude is the average of the initial and final points.

LoxodromeArc(GeodeticPoint, GeodeticPoint, OneAxisEllipsoid, double) - Constructor for class org.orekit.bodies.LoxodromeArc

Class constructor.

loxodromeBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder

Construct a waypoint builder interpolating points using a loxodrome (or Rhumbline).

ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Perform Lᵀ.D.L = Q decomposition of the covariance matrix.

ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod

Perform Lᵀ.D.L = Q decomposition of the covariance matrix.

ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Compute the LᵀDL factorization with symmetric pivoting decomposition of Q (symmetric definite positive matrix) with a minimum symmetric pivoting: Q = ZᵀLᵀDLZ.

luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.DeepSDP4

Computes luni - solar terms from initial coordinates and epoch.

luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4

Computes luni - solar terms from initial coordinates and epoch.

LutherFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for LutherFieldIntegrator.

LutherFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder

Constructor.

LutherFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder

Constructor using a "fielded" step.

LutherIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for LutherIntegrator.

LutherIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherIntegratorBuilder

Build a new instance.

LyapunovOrbit - Class in org.orekit.orbits

Class calculating different parameters of a Lyapunov Orbit.

LyapunovOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LyapunovOrbit

Simple Constructor.

LyapunovOrbit(RichardsonExpansion, double) - Constructor for class org.orekit.orbits.LyapunovOrbit

Simple Constructor.

M

M2 - Static variable in class org.orekit.files.ccsds.definitions.Units

m² unit.

M2 - Static variable in class org.orekit.models.earth.displacement.Tide

M₂ tide.

M2 - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Default value for M2 coefficient.

M2_NAME - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Parameter name for M2 coefficient.

M2_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units

m² per kilograms units.

M2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Square meters per second units.

M2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Square meters per square second units.

M2_PER_S3 - Static variable in class org.orekit.files.ccsds.definitions.Units

Square meters per cube second units.

M2_PER_S4 - Static variable in class org.orekit.files.ccsds.definitions.Units

Square meters per s⁴ units.

M3_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units

m³ per kilograms units.

M3_PER_KGS - Static variable in class org.orekit.files.ccsds.definitions.Units

Cubic meters per kilograms second units.

M3_PER_KGS2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Cubic meters per kilograms (square second) units.

M4 - Static variable in class org.orekit.files.ccsds.definitions.Units

m⁴ unit.

M4_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units

m⁴ per kilograms units.

M4_PER_KG2 - Static variable in class org.orekit.files.ccsds.definitions.Units

m⁴ per square kilograms units.

M_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Meters per second units.

M_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units

Meters per square second units.

MagneticFieldDetector - Class in org.orekit.propagation.events

Detector for Earth magnetic field strength.

MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector

Build a new detector.

MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector

Build a new detector.

MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector

Build a detector.

MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector

Build a detector.

MagneticFieldDetector(AdaptableInterval, double, int, EventHandler, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector

Protected constructor with full parameters.

MAN_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Maneuver line element for XML messages.

manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

The method is in charge of collecting the measurements, manage them, and call the detection method.

manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector

The method is in charge of collecting the measurements, manage them, and call the detection method.

manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector

The method is in charge of collecting the measurements, manage them, and call the detection method.

ManBasis - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Basis of maneuver used in CCSDS Orbit Comprehensive Messages.

Maneuver - Class in org.orekit.files.ccsds.ndm.adm.apm

Maneuver in an APM file.

Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Simple constructor.

Maneuver - Class in org.orekit.files.ccsds.ndm.odm.opm

Maneuver in an OPM file.

Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Simple constructor.

Maneuver - Class in org.orekit.forces.maneuvers

A generic model for maneuvers with finite-valued acceleration magnitude, as opposed to instantaneous changes in the velocity vector which are defined via detectors (in ImpulseManeuver and FieldImpulseManeuver).

Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel) - Constructor for class org.orekit.forces.maneuvers.Maneuver

Generic maneuver constructor.

ManeuverFieldType - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Maneuver field type used in CCSDS Orbit Comprehensive Messages.

ManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for APM maneuver entries.

ManeuverKey - Enum in org.orekit.files.ccsds.ndm.odm.opm

Keys for OPM maneuver entries.

maneuverTriggered(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Observe a maneuver trigger.

maneuverTriggered(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter

Observe a maneuver trigger.

maneuverTriggered(SpacecraftState, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter

Observe a maneuver trigger.

ManeuverTriggers - Interface in org.orekit.forces.maneuvers.trigger

Generic interface for the maneuver triggers used in a Maneuver.

ManeuverTriggersResetter - Interface in org.orekit.forces.maneuvers.trigger

Resetter for maneuver triggers.

Maneuvrable - Enum in org.orekit.files.ccsds.ndm.cdm

Maneuvrable possibilities used in CCSDS Conjunction Data Messages.

map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Map an Orekit frame to a CCSDS frame.

map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName

Map an Orekit frame to a CCSDS center.

map(Frame) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade

Map an Orekit frame to a CCSDS frame facade.

mapArrayToOrbit(double[], double[], PositionAngleType, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType

Convert state array to orbital parameters.

mapArrayToOrbit(T[], T[], PositionAngleType, FieldAbsoluteDate<T>, T, Frame) - Method in enum org.orekit.orbits.OrbitType

Convert state array to orbital parameters.

mapArrayToState(T, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(FieldAbsoluteDate<T>, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(double, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double components to a spacecraft state.

mapArrayToState(AbsoluteDate, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double components to a spacecraft state.

mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map a date to a raw double time offset.

mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper

Map a date to a raw double time offset.

mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double time offset to a date.

mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map the raw double time offset to a date.

mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double time offset to a date.

mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double time offset to a date.

mapOrbitToArray(Orbit, PositionAngleType, double[], double[]) - Method in enum org.orekit.orbits.OrbitType

Convert orbit to state array.

mapOrbitToArray(FieldOrbit<T>, PositionAngleType, T[], T[]) - Method in enum org.orekit.orbits.OrbitType

Convert orbit to state array.

mappingFactor(double) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction

This method allows the computation of the ionospheric mapping factor.

mappingFactor(T) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction

This method allows the computation of the ionospheric mapping factor.

mappingFactor(double) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction

This method allows the computation of the ionospheric mapping factor.

mappingFactor(T) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction

This method allows the computation of the ionospheric mapping factor.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.MappingFunction

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

This method allows the computation of the hydrostatic and wet mapping functions.

mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

This method allows the computation of the hydrostatic and wet mapping functions.

MappingFunction - Interface in org.orekit.models.earth.troposphere

Interface for mapping functions used in the tropospheric delay computation.

mappingFunction(double, double, double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils

Compute the mapping function related to the coefficient values and the elevation.

mappingFunction(T, T, T, T) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils

Compute the mapping function related to the coefficient values and the elevation.

mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper

Map a spacecraft state to raw double components.

mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper

Map a spacecraft state to raw double components.

MariniMurrayModel - Class in org.orekit.models.earth.troposphere

The Marini-Murray tropospheric delay model for laser ranging.

MariniMurrayModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel

Create a new Marini-Murray model for the troposphere using the given environmental conditions.

MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mars.

MarshallSolarActivityFutureEstimation - Class in org.orekit.models.earth.atmosphere.data

This class provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.

MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Simple constructor.

MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Constructor that allows specifying the source of the MSAFE auxiliary data files.

MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Constructor that allows specifying the source of the MSAFE auxiliary data files and customizable thread safe cache configuration.

MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Simple constructor which use the default data context.

MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Simple constructor.

MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation

Constructor with customizable thread safe cache configuration.

MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.models.earth.atmosphere.data

Strength level of activity.

MarshallSolarActivityFutureEstimationLoader - Class in org.orekit.models.earth.atmosphere.data

This class reads solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.

MarshallSolarActivityFutureEstimationLoader(MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader

Simple constructor.

MarshallSolarActivityFutureEstimationLoader(MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader

Constructor that allows specifying the source of the MSAFE auxiliary data files.

MarshallSolarActivityFutureEstimationLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data

Container class for Solar activity indexes.

mass(double) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder

Sets the mass.

mass(double) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder

Sets the mass.

mass(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Sets the mass.

mass(double) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder

Sets the mass.

MASS_RATIO_SUFFIX - Static variable in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel

Suffix for parameter name for Mass Ratio enabling Jacobian processing.

MassDepletionDelay - Class in org.orekit.forces.maneuvers.jacobians

Generator for effect of delaying mass depletion when delaying a maneuver.

MassDepletionDelay(String, boolean, Maneuver) - Constructor for class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Simple constructor.

matches(String) - Method in enum org.orekit.files.rinex.section.RinexLabels

Check if label matches.

matchesLabel(String, String) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Check if a header line matches an expected label.

MatricesHarvester - Interface in org.orekit.propagation

Interface for extracting State Transition Matrices and Jacobians matrices from spacecraft state.

MAX_EPOCH - Static variable in class org.orekit.time.DateComponents

Maximum supported date.

MAX_ITERATIONS_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Default value for maxIterations.

MAX_POWER - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Max power for summation.

MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where points obey a maximum time gap.

MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid

Constructor.

maxStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder

Maximum step size (s).

maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter maximum value has been changed.

MEAN_ANOM - Static variable in enum org.orekit.orbits.OrbitType

Name for mean anomaly.

MEAN_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for mean argument of latitude.

MEAN_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for mean argument of longitude.

meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean derivative, truncated to first components.

meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean second derivative, truncated to first components.

meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the eccentric latitude argument from the mean latitude argument.

meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the eccentric longitude argument from the mean longitude argument.

meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the eccentric latitude argument from the mean latitude argument.

meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the eccentric longitude argument from the mean longitude argument.

meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean value, truncated to first components.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.AngularAzEl

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.AngularRaDec

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.BistaticRange

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.BistaticRangeRate

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.FDOA

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.Phase

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.InterSatellitesRange

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.MultiplexedMeasurement

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.Position

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.PV

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.Range

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.RangeRate

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.TDOA

Type of the measurement.

MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.TurnAroundRange

Type of the measurement.

MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation

Interface for generating individual measurements.

MeasurementCombination - Interface in org.orekit.estimation.measurements.gnss

Interface for combination of measurements.

MeasurementCombinationFactory - Class in org.orekit.estimation.measurements.gnss

Factory for predefined combination of measurements.

MeasurementDecorator - Class in org.orekit.estimation.sequential

Decorator adding Measurement API to an ObservedMeasurement.

MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator

Simple constructor.

MeasurementFilter<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.filtering

Interface for measurement pre-processing filter.

measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler

Check if a measurement is feasible at some date.

measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler

Check if a measurement is feasible at some date.

measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler

Check if a measurement is feasible at some date.

measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic

Check if measurement is feasible.

MeasurementType - Enum in org.orekit.gnss

Enumerate for measurement type.

MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Default suffix for median driver.

MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Default suffix for median driver.

MedianDate - Class in org.orekit.forces.maneuvers.jacobians

Generator for one column of a Jacobian matrix for special case of maneuver median date.

MedianDate(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.MedianDate

Simple constructor.

MelbourneWubbenaCombination - Class in org.orekit.estimation.measurements.gnss

Melbourne-Wübbena combination.

MendesPavlisModel - Class in org.orekit.models.earth.troposphere

The Mendes - Pavlis tropospheric delay model for optical techniques.

MendesPavlisModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel

Create a new Mendes-Pavlis model for the troposphere.

MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mercury.

messageAvailable(String, ParsedMessage) - Method in interface org.orekit.gnss.metric.ntrip.MessageObserver

Notify that an encoded message is available.

messageNumberToSatelliteSystem(int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Find the satellite system corresponding to the sub-type message number.

MessageObserver - Interface in org.orekit.gnss.metric.ntrip

Interface for objects that needs to be notified when new encoded messages are available.

MessageParser<T> - Interface in org.orekit.files.ccsds.utils.lexical

Parser for CCSDS messages.

MessagesParser - Class in org.orekit.gnss.metric.parser

Parser for IGS encoded messages.

MessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.MessagesParser

Constructor.

MessageType - Interface in org.orekit.gnss.metric.parser

Interface for encoded message types.

MessageVersionXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical

Builder for the root element with CCSDS message version.

MessageVersionXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder

Empty constructor.

MessageWriter<H extends Header,S extends Segment<?,?>,F extends NdmConstituent<H,S>> - Interface in org.orekit.files.ccsds.utils.generation

Interface for writing Navigation Data Message (NDM) files.

Metadata - Class in org.orekit.files.ccsds.section

This class gathers the meta-data present in the Navigation Data Message (ADM, ODM and TDM).

Metadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.section.Metadata

Simple constructor.

MetadataKey - Enum in org.orekit.files.ccsds.section

Keys for NDM Metadata entries.

Meteo(SortedSet<CRD.MeteorologicalMeasurement>) - Constructor for class org.orekit.files.ilrs.CRD.Meteo

Constructor.

MeteorologicalConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Empty constructor.

MeteorologicalMeasurement(AbsoluteDate, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Constructor.

MeteorologicalMeasurement(AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Constructor.

metersToRu(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter

Convert a range expressed in meters.

metersToRu(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter

Convert a range expressed in meters.

METRE - Static variable in class org.orekit.utils.units.Unit

Metre unit.

MF - Static variable in class org.orekit.models.earth.displacement.Tide

Mf tide.

MHZ_TO_HZ - Static variable in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination

Mega Hertz to Hertz converter.

MidpointFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for MidpointFieldIntegrator.

MidpointFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder

Constructor.

MidpointFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder

Constructor using a "fielded" step.

MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for MidpointIntegrator.

MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a new instance.

MILLI_ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter

Milli arcseconds to radians converter.

MILLI_SECONDS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter

Milli seconds to seconds converter.

MIN_EPOCH - Static variable in class org.orekit.time.DateComponents

Maximum supported date.

minStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder

Minimum step size (s).

MINUTE - Static variable in class org.orekit.utils.units.Unit

Minute unit.

minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Check length of the current minute in this time scale.

minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Check length of the current minute in this time scale.

minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Check length of the current minute in this time scale.

minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Check length of the current minute in this time scale.

MINUTES_PER_DAY - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Time units per julian day.

minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter minimum value has been changed.

missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if missing coefficients are allowed in the input data.

MM - Static variable in class org.orekit.gnss.metric.parser.Units

Millimetres units.

MM - Static variable in class org.orekit.models.earth.displacement.Tide

Mm tide.

MM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units

Millimetres per second units.

MM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units

Millimetres per square second units.

modelCalled(Orbit[], Map<ObservedMeasurement<?>, EstimatedMeasurement<?>>) - Method in interface org.orekit.estimation.leastsquares.ModelObserver

Notification callback for orbit changes.

ModelObserver - Interface in org.orekit.estimation.leastsquares

Observer for model calls.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for modified julian dates: 1858-11-17.

ModifiedFrame - Class in org.orekit.files.ccsds.definitions

A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.

ModifiedFrame(Frame, CelestialBodyFrame, CelestialBody, String) - Constructor for class org.orekit.files.ccsds.definitions.ModifiedFrame

Create a CCSDS reference frame by changing the origin of an existing frame.

ModifiedLambdaMethod - Class in org.orekit.estimation.measurements.gnss

Decorrelation/reduction engine for Modified LAMBDA method.

ModifiedLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Empty constructor.

ModifierGradientConverter - Class in org.orekit.estimation.measurements.modifiers

Converter for states and parameters arrays.

ModifierGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.ModifierGradientConverter

Simple constructor.

modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<AngularRaDec>) - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier

modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier

modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier

Apply a modifier to an estimated measurement.

modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Apply a modifier to an estimated measurement.

modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<AngularRaDec>) - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil

Apply a modifier to an estimated measurement.

modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil

Apply a modifier to an estimated measurement.

modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Apply a modifier to an estimated measurement without derivatives.

momentum(FieldVector3D<T>) - Method in class org.orekit.attitudes.FieldInertia

Compute angular momentum.

momentum(Vector3D) - Method in class org.orekit.attitudes.Inertia

Compute angular momentum.

monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger

Monitor an event detector.

monitorDetector(FieldEventDetector<T>) - Method in class org.orekit.propagation.events.FieldEventsLogger

Monitor an event detector.

Month - Enum in org.orekit.time

Enumerate representing a calendar month.

MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Moon.

MOON_DRACONIC_PULSATION - Static variable in class org.orekit.frames.SingleParameterFitter

Moon pulsation (one Moon draconic period).

MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Moon equatorial radius: 1737400 m.

mu(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Sets the Earth gravity coefficient.

MU - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Earth gravity coefficient in m³/s².

MultipleShooter - Class in org.orekit.utils

Multiple shooting method applicable for trajectories, in an ephemeris model.

MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<EpochDerivativesEquations>, double, int) - Constructor for class org.orekit.utils.MultipleShooter

Simple Constructor.

MultipleShooting - Interface in org.orekit.utils

Interface for Multiple shooting methods.

MultiplexedMeasurement - Class in org.orekit.estimation.measurements

Class multiplexing several measurements as one.

MultiplexedMeasurement(List<ObservedMeasurement<?>>) - Constructor for class org.orekit.estimation.measurements.MultiplexedMeasurement

Simple constructor.

MultiplexedMeasurementBuilder - Class in org.orekit.estimation.measurements.generation

Builder for MultiplexedMeasurement measurements.

MultiplexedMeasurementBuilder(List<MeasurementBuilder<?>>) - Constructor for class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder

Simple constructor.

multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Multiply the argument matrix with the current matrix.

multiply(String, Unit) - Method in class org.orekit.utils.units.Unit

Create product of units.

MultiSatFixedStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed step handler for multi-sat propagation.

MultiSatStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler for multi-sat propagation.

MultisatStepNormalizer - Class in org.orekit.propagation.sampling

This class wraps an object implementing MultiSatFixedStepHandler into a MultiSatStepHandler.

MultisatStepNormalizer(double, MultiSatFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.MultisatStepNormalizer

Simple constructor.

N

N2 - Static variable in class org.orekit.models.earth.displacement.Tide

N₂ tide.

N_M - Static variable in class org.orekit.files.ccsds.definitions.Units

Newton metre unit.

N_M_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Newton metre second unit.

N_NEIGHBORS - Static variable in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData

Size of the list.

NadirPointing - Class in org.orekit.attitudes

This class handles nadir pointing attitude provider.

NadirPointing(Frame, BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing

Creates new instance.

nameChanged(String, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter name has been changed.

NANO_TESLA - Static variable in class org.orekit.files.ccsds.definitions.Units

Nano Tesla unit.

NANO_TESLAS_TO_TESLAS - Static variable in class org.orekit.utils.units.UnitsConverter

Nano Teslas to Tesla converter.

NarrowLaneCombination - Class in org.orekit.estimation.measurements.gnss

Narrow-Lane combination.

naturalToProper(double[], GroundStation, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Natural to proper correction for aberration of light.

naturalToProper(double[], GroundStation, AbsoluteDate, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Natural to proper correction for aberration of light.

NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector

Sun elevation at nautical dawn/dusk (12° below horizon).

NavigationSystem - Enum in org.orekit.gnss.metric.ntrip

Enumerate for navigation system in DataStreamRecord.

NB_AS - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4E

Number of Anti-spoofing entries.

NB_ERD - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4C

Number of Estimated Range Deviations.

NB_PER_Y - Static variable in class org.orekit.files.ccsds.definitions.Units

#/year unit.

NB_SVH - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4E

Number of SV health entries.

Ndm - Class in org.orekit.files.ccsds.ndm

CCSDS Navigation Data Message.

Ndm(List<String>, List<NdmConstituent<?, ?>>) - Constructor for class org.orekit.files.ccsds.ndm.Ndm

Simple constructor.

NDM_XML_V3_SCHEMA_LOCATION - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator

NDM/XML version 3 location.

NdmConstituent<H extends Header,S extends Segment<?,?>> - Class in org.orekit.files.ccsds.ndm

Constituents of a CCSDS Navigation Data Message.

NdmConstituent(H, List<S>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.NdmConstituent

Constructor.

NdmParser - Class in org.orekit.files.ccsds.ndm

A parser for the CCSDS NDM (Navigation Data Message).

NdmParser(ParserBuilder, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.NdmParser

Simple constructor.

NdmWriter - Class in org.orekit.files.ccsds.ndm

Writer for CCSDS Navigation Data Message.

NdmWriter(WriterBuilder) - Constructor for class org.orekit.files.ccsds.ndm.NdmWriter

Simple constructor.

negate() - Method in class org.orekit.attitudes.FieldInertiaAxis

Reverse the inertia axis.

negate() - Method in class org.orekit.attitudes.InertiaAxis

Reverse the inertia axis.

negate() - Method in class org.orekit.utils.FieldPVCoordinates

Get the opposite of the instance.

negate() - Method in class org.orekit.utils.PVCoordinates

Get the opposite of the instance.

NegateDetector - Class in org.orekit.propagation.events

An event detector that negates the sign on another event detector's g function.

NegateDetector(EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector

Create a new event detector that negates an existing event detector.

NegateDetector(AdaptableInterval, double, int, EventHandler, EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector

Private constructor.

NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Neptune.

NeQuickModel - Class in org.orekit.models.earth.ionosphere

NeQuick ionospheric delay model.

NeQuickModel(double[]) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel

Build a new instance.

NeQuickModel(double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel

Build a new instance.

NetworkCrawler - Class in org.orekit.data

Provider for data files directly fetched from network.

NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler

Build a data classpath crawler.

NetworkRecord - Class in org.orekit.gnss.metric.ntrip

Network record in source table.

NetworkRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.NetworkRecord

Build a data stream record by parsing a source table line.

newBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter

Create a writer for a new OCM trajectory state history block.

newBulletinBParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser

Create a new parser for EOP data in the Bulletin B format.

newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control

NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities

Implementation of the Modified Newcomb Operators.

newEopC04Parser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser

Create a new parser for EOP data in the EOP C04 format.

newFinalsColumnsParser(IERSConventions, ItrfVersionProvider, TimeScales, boolean) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser

Create a new parser for EOP data in the rapid and predicted columnar format.

newFinalsXmlParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser

Create a new parser for EOP data in the rapid and predicted XML format.

newLine() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Finish current line.

newLine() - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Finish current line.

newSegment() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter

Create a writer for a new AEM attitude ephemeris segment.

newSegment() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter

Create a writer for a new OEM ephemeris segment.

newSegment(Frame) - Method in class org.orekit.files.ilrs.StreamingCpfWriter

Create a writer for a new CPF ephemeris segment.

newTLE(KeplerianOrbit, TLE, double, TimeScale) - Static method in class org.orekit.propagation.analytical.tle.generation.TleGenerationUtil

Builds a new TLE from Keplerian parameters and a template for TLE data.

newTLE(FieldKeplerianOrbit<T>, FieldTLE<T>, T, TimeScale) - Static method in class org.orekit.propagation.analytical.tle.generation.TleGenerationUtil

Builds a new TLE from Keplerian parameters and a template for TLE data.

NEWTON - Static variable in class org.orekit.utils.units.Unit

Newton unit.

NewtonianAttraction - Class in org.orekit.forces.gravity

Force model for Newtonian central body attraction.

NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction

Simple constructor.

next() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the next time span.

next() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the next transition.

NiellMappingFunctionModel - Class in org.orekit.models.earth.troposphere

The Niell Mapping Function model for radio wavelengths.

NiellMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel

Builds a new instance.

NiellMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel

Builds a new instance.

NO_PARAMETER - Static variable in exception org.orekit.errors.UnsupportedParameterException

String for empty parameter drivers' list.

NodeDetector - Class in org.orekit.propagation.events

Finder for node crossing events.

NodeDetector(Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NodeDetector(AdaptableInterval, double, int, EventHandler, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Protected constructor with full parameters.

nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the non-central part of the gravity field.

NONE - Static variable in class org.orekit.utils.units.Unit

No unit.

normalize(FieldOrbit<T>, FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType

Normalize one orbit with respect to a reference one.

normalize(Orbit, Orbit) - Method in enum org.orekit.orbits.OrbitType

Normalize one orbit with respect to a reference one.

normalize() - Method in class org.orekit.utils.FieldPVCoordinates

Normalize the position part of the instance.

normalize() - Method in class org.orekit.utils.PVCoordinates

Normalize the position part of the instance.

normalizeCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Normalize a covariance matrix.

NORMALIZED_EQUATORIAL_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Equatorial radius rescaled (1.0).

NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide normalized spherical harmonics coefficients.

NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The normalized geopotential coefficients at a specific instance in time.

NORTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint

North pole.

notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that negates the g function of another detector.

notCombine(FieldEventDetector<T>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector

Create a new event detector that negates the g function of another detector.

notifyResetters(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Notify resetters.

notifyResetters(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers

Notify resetters.

NptRangeMeasurement(AbsoluteDate, double, int, double, String) - Constructor for class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Constructor.

NptRangeMeasurement(AbsoluteDate, double, int, double, String, double, int, double, double, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Constructor.

NRLMSISE00 - Class in org.orekit.models.earth.atmosphere

This class implements the mathematical representation of the 2001 Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere (NRLMSISE-00) of the MSIS® class model.

NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00

Constructor.

NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00

Constructor.

NRLMSISE00.FieldOutput<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.models.earth.atmosphere

This class is a placeholder for the computed densities and temperatures.

NRLMSISE00InputParameters - Interface in org.orekit.models.earth.atmosphere

Container for solar activity data, compatible with NRLMSISE-00 atmosphere model.

NS - Static variable in class org.orekit.gnss.metric.parser.Units

Nanoseconds units.

NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Simple constructor.

nSteps - Variable in class org.orekit.propagation.conversion.AbstractLimitedVariableStepFieldIntegratorBuilder

Number of steps.

NtripClient - Class in org.orekit.gnss.metric.ntrip

Source table for ntrip streams retrieval.

NtripClient(String, int) - Constructor for class org.orekit.gnss.metric.ntrip.NtripClient

Build a client for NTRIP.

NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection

Null correction (xp = 0, yp = 0).

numberOfCandidates() - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance

Get the number of candidate solutions to search for.

numberOfCandidates() - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance

Get the number of candidate solutions to search for.

numberOfObsTypes(SatelliteSystem) - Method in class org.orekit.files.rinex.clock.RinexClock

Get the number of observation types for a given system.

NumericalPropagator - Class in org.orekit.propagation.numerical

This class propagates orbits using numerical integration.

NumericalPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

NumericalPropagator(ODEIntegrator, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for numerical propagator.

NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a new instance.

NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a new instance.

O

O1 - Static variable in class org.orekit.models.earth.displacement.Tide

O₁ tide.

ObjectType - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Object type used in CCSDS Orbit Comprehensive Messages.

ObservableSatellite - Class in org.orekit.estimation.measurements

Class modeling a satellite that can be observed.

ObservableSatellite(int) - Constructor for class org.orekit.estimation.measurements.ObservableSatellite

Simple constructor.

Observation - Class in org.orekit.files.ccsds.ndm.tdm

The Observation class contains the data from an observation line.

Observation(ObservationType, AbsoluteDate, double) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Observation

Simple constructor.

ObservationData - Class in org.orekit.files.rinex.observation

Observation Data.

ObservationData(ObservationType, double, int, int) - Constructor for class org.orekit.files.rinex.observation.ObservationData

Simple constructor.

ObservationDataSet - Class in org.orekit.files.rinex.observation

Observation Data set.

ObservationDataSet(SatInSystem, AbsoluteDate, int, double, List<ObservationData>) - Constructor for class org.orekit.files.rinex.observation.ObservationDataSet

Simple constructor.

ObservationsBlock - Class in org.orekit.files.ccsds.ndm.tdm

The Observations Block class contain metadata and the list of observation data lines.

ObservationsBlock() - Constructor for class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock

ObservationsBlock constructor.

ObservationTimeScale - Enum in org.orekit.gnss

Observation time scales.

ObservationType - Enum in org.orekit.files.ccsds.ndm.tdm

Keys for TDM observations entries.

ObservationType - Enum in org.orekit.gnss

Enumerate for all the Observation Types for Rinex 2 and 3.

ObservedMeasurement<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements

Interface for measurements used for orbit determination.

OccultationEngine - Class in org.orekit.utils

Computation engine for occultation events.

OccultationEngine(ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.utils.OccultationEngine

Build a new occultation engine.

OccultationEngine.FieldOccultationAngles<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

Container for occultation angles.

OccultationEngine.OccultationAngles - Class in org.orekit.utils

Container for occultation angles.

OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential

Supported Ocean load Deformation coefficients (Love numbers k'_i).

OceanLoading - Class in org.orekit.models.earth.displacement

Modeling of displacement of reference points due to ocean loading.

OceanLoading(OneAxisEllipsoid, OceanLoadingCoefficients) - Constructor for class org.orekit.models.earth.displacement.OceanLoading

Simple constructor.

OceanLoadingCoefficients - Class in org.orekit.models.earth.displacement

Site specific coefficients for ocean loading.

OceanLoadingCoefficients(String, GeodeticPoint, Tide[][], double[][], double[][], double[][], double[][], double[][], double[][]) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficients

Simple constructor.

OceanLoadingCoefficientsBLQFactory - Class in org.orekit.models.earth.displacement

Factory for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.

OceanLoadingCoefficientsBLQFactory(String) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

Simple constructor.

OceanLoadingCoefficientsBLQFactory(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory

This constructor allows specification of the source of the BLQ auxiliary data files.

OceanTides - Class in org.orekit.forces.gravity

Ocean tides force model.

OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale, GravityFields) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTidesReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides coefficients.

OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader

Simple constructor.

OceanTidesWave - Class in org.orekit.forces.gravity.potential

Container for ocen tides coefficients for one tide wave.

OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave

Simple constructor.

Ocm - Class in org.orekit.files.ccsds.ndm.odm.ocm

This class gathers the informations present in the Orbit Comprehensive Message (OCM).

Ocm(OdmHeader, List<Segment<OcmMetadata, OcmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Simple constructor.

OcmData - Class in org.orekit.files.ccsds.ndm.odm.ocm

Data container for Orbit Comprehensive Messages.

OcmData(List<TrajectoryStateHistory>, OrbitPhysicalProperties, List<OrbitCovarianceHistory>, List<OrbitManeuverHistory>, Perturbations, OrbitDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Simple constructor.

OcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keywords for OCM data sub-structure.

OcmElements - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Data elements types used in CCSDS Orbit Comprehensive Messages.

OcmMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm

Meta-data for Orbit Comprehensive Message.

OcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Create a new meta-data.

OcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for OCM container entries.

OcmParser - Class in org.orekit.files.ccsds.ndm.odm.ocm

A parser for the CCSDS OCM (Orbit Comprehensive Message).

OcmParser(IERSConventions, double, double, boolean, DataContext, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Complete constructor.

OcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.ocm

OCM ephemeris blocks for a single satellite.

OcmSatelliteEphemeris(String, double, List<TrajectoryStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris

Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

OcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm

Writer for CCSDS Orbit Comprehensive Message.

OcmWriter(IERSConventions, double, double, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Complete constructor.

ODEIntegratorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build first order integrators for propagators conversion.

OdmCommonMetadata - Class in org.orekit.files.ccsds.ndm.odm

Common metadata for Orbit Parameter/Ephemeris/Mean Messages.

OdmCommonMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Simple constructor.

OdMethodFacade - Class in org.orekit.files.ccsds.definitions

Facade in front of several orbit determination methods in CCSDS messages.

OdMethodFacade(String, OdMethodType, String) - Constructor for class org.orekit.files.ccsds.definitions.OdMethodFacade

Simple constructor.

OdMethodType - Enum in org.orekit.files.ccsds.definitions

Type of orbit determination method used in CCSDS Orbit Comprehensive Messages.

OdmHeader - Class in org.orekit.files.ccsds.ndm.odm

Header of a CCSDS Orbit Data Message.

OdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmHeader

Constructor.

OdmMetadata - Class in org.orekit.files.ccsds.ndm.odm

This class gathers the meta-data present in the Orbital Data Message (ODM).

OdmMetadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmMetadata

Simple constructor.

OdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for ODM metadata entries.

OdmParser<T extends NdmConstituent<OdmHeader,?>,P extends OdmParser<T,?>> - Class in org.orekit.files.ccsds.ndm.odm

Common parser for Orbit Parameter/Ephemeris/Mean/Comprehensive Messages.

OdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmParser

Complete constructor.

ODParameters - Class in org.orekit.files.ccsds.ndm.cdm

Container for OD parameters data block.

ODParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.ODParameters

Simple constructor.

ODParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM OD parameters entries.

ODParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for OD parameters data block for CCSDS Conjunction Data Messages.

Oem - Class in org.orekit.files.ccsds.ndm.odm.oem

This class stores all the information of the OEM File parsed by OEMParser.

Oem(OdmHeader, List<OemSegment>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.Oem

Simple constructor.

OemData - Class in org.orekit.files.ccsds.ndm.odm.oem

The Ephemerides data blocks class contain list of orbital data points.

OemData() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemData

EphemeridesBlock constructor.

OemMetadata - Class in org.orekit.files.ccsds.ndm.odm.oem

Metadata for Orbit Ephemeris Messages.

OemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Simple constructor.

OemMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.oem

Keys for OEM container entries.

OemParser - Class in org.orekit.files.ccsds.ndm.odm.oem

A parser for the CCSDS OEM (Orbit Ephemeris Message).

OemParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, int, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Complete constructor.

OemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.oem

OEM ephemeris blocks for a single satellite.

OemSatelliteEphemeris(String, double, List<OemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris

Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

OemSegment - Class in org.orekit.files.ccsds.ndm.odm.oem

The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).

OemSegment(OemMetadata, OemData, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSegment

Simple constructor.

OemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem

A writer for Orbit Ephemeris Message (OEM) files.

OemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemWriter

Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.

of(Frame) - Static method in class org.orekit.attitudes.FrameAlignedProvider

Creates an attitude provider aligned with the given frame.

of(FieldAbsoluteDate<T>, FieldRotation<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Create a new static transform from a rotation and zero translation.

of(FieldAbsoluteDate<T>, FieldVector3D<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Create a new static transform from a translation and rotation.

of(FieldAbsoluteDate<T>, StaticTransform) - Static method in interface org.orekit.frames.FieldStaticTransform

Create a new static transform from an FieldAbsoluteDate and a StaticTransform.

of(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldRotation<T>) - Static method in interface org.orekit.frames.FieldStaticTransform

Create a new static transform from a translation and rotation.

of(TimeScales, CelestialBodies) - Static method in interface org.orekit.frames.Frames

Create a set of frames from the given data.

of(TimeScales, Supplier<Frame>) - Static method in interface org.orekit.frames.Frames

Create a set of frames from the given data.

of(AbsoluteDate, Rotation) - Static method in interface org.orekit.frames.StaticTransform

Create a new static transform from a rotation and zero translation.

of(AbsoluteDate, Vector3D) - Static method in interface org.orekit.frames.StaticTransform

Create a new static transform from a translation and rotation.

of(AbsoluteDate, Vector3D, Rotation) - Static method in interface org.orekit.frames.StaticTransform

Create a new static transform from a translation and rotation.

of(Collection<? extends OffsetModel>, BiFunction<? super IERSConventions, ? super TimeScales, ? extends Collection<? extends EOPEntry>>) - Static method in interface org.orekit.time.TimeScales

Create a set of time scales where all the data is loaded from the given functions.

offset(StaticTransform, StaticTransform) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersOffsetComputer

Compute distance offset to be added to the distance between antennas reference points.

offset(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter

Generate relative offset.

OFFSET_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation

Suffix for ground station position and clock offset parameters names.

offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the apparent clock offset between two instant in the perspective of a specific time scale.

offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

Compute the seconds offset between two instances.

offsetFrom(FieldAbsoluteDate<T>, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the apparent clock offset between two instant in the perspective of a specific time scale.

offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.CircularFieldOfView

Get the offset of target body with respect to the Field Of View Boundary.

offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

Get the offset of target body with respect to the Field Of View Boundary.

offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in interface org.orekit.geometry.fov.FieldOfView

Get the offset of target body with respect to the Field Of View Boundary.

offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView

Get the offset of target body with respect to the Field Of View Boundary.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.SatelliteClockScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from TAIScale to instance.

OffsetModel - Class in org.orekit.time

TAI UTC offset model.

OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel

Constructor for a linear offset model.

OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel

Constructor for a constant offset model.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.BDTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GLONASSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.IRNSSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.QZSSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.SatelliteClockScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from instance to TAIScale.

OHM - Static variable in class org.orekit.utils.units.Unit

Ohm unit.

omega - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

final perigee argument.

omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final perigee argument.

omgdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

common parameter for perigee argument (omega) computation.

omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for perigee argument (omega) computation.

Omm - Class in org.orekit.files.ccsds.ndm.odm.omm

This class gathers the informations present in the Orbital Mean-Elements Message (OMM).

Omm(OdmHeader, List<Segment<OmmMetadata, OmmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.Omm

Simple constructor.

OmmData - Class in org.orekit.files.ccsds.ndm.odm.omm

Container for Orbit Mean-elements Message data.

OmmData(KeplerianElements, SpacecraftParameters, OmmTle, CartesianCovariance, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Simple constructor.

OmmMetadata - Class in org.orekit.files.ccsds.ndm.odm.omm

Metadata for Orbit Mean Messages.

OmmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Empty constructor.

OmmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.omm

Keys for OMM container entries.

OmmParser - Class in org.orekit.files.ccsds.ndm.odm.omm

A parser for the CCSDS OMM (Orbiter Mean-Elements Message).

OmmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Complete constructor.

OmmTle - Class in org.orekit.files.ccsds.ndm.odm.omm

Container for TLE data.

OmmTle() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Create an empty data set.

OmmTleKey - Enum in org.orekit.files.ccsds.ndm.odm.omm

Keys for TLE entries.

OmmWriter - Class in org.orekit.files.ccsds.ndm.odm.omm

Writer for CCSDS Orbit Mean Mean-Elements Message.

OmmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter

Complete constructor.

OnBoardAntennaInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on inter-satellites phase measurements.

OnBoardAntennaInterSatellitesPhaseModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier

Simple constructor.

OnBoardAntennaInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on inter-satellites range measurements.

OnBoardAntennaInterSatellitesRangeModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier

Simple constructor.

OnBoardAntennaOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on one-way GNSS phase measurements.

OnBoardAntennaOneWayGNSSPhaseModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier

Simple constructor.

OnBoardAntennaOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on one-way GNSS range measurements.

OnBoardAntennaOneWayGNSSRangeModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier

Simple constructor.

OnBoardAntennaTurnAroundRangeModifier - Class in org.orekit.estimation.measurements.modifiers

On-board antenna offset effect on turn around range measurements.

OnBoardAntennaTurnAroundRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier

Simple constructor.

onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider

Get the raw spherical harmonic coefficients on a specific date.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider

Get the un-normalized spherical harmonic coefficients at a specific instance in time.

ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

1 represented as a polynomial.

ONE - Static variable in class org.orekit.utils.units.Unit

Dimensionless unit.

ONE_PER_ER - Static variable in class org.orekit.files.ccsds.definitions.Units

Earth radii reciprocal unit.

ONE_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units

Seconds reciprocal unit.

ONE_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Constant 1.0 / 3.0.

OneAxisEllipsoid - Class in org.orekit.bodies

Modeling of a one-axis ellipsoid.

OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid

Simple constructor.

OneDVariation - Class in org.orekit.gnss.antenna

Interpolator for 1D phase center variation data.

OneDVariation(double, double, double[]) - Constructor for class org.orekit.gnss.antenna.OneDVariation

Simple constructor.

oneWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier

Compute distance modification for one way measurement.

OneWayGNSSPhase - Class in org.orekit.estimation.measurements.gnss

One-way GNSS phase measurement.

OneWayGNSSPhase(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Simple constructor.

OneWayGNSSPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical one-way GNSS phase measurement with ambiguity.

OneWayGNSSPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier

Constructor.

OneWayGNSSPhaseBuilder - Class in org.orekit.estimation.measurements.generation

Builder for OneWayGNSSPhase measurements.

OneWayGNSSPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, ToDoubleFunction<AbsoluteDate>, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder

Simple constructor.

OneWayGNSSRange - Class in org.orekit.estimation.measurements.gnss

One-way GNSS range measurement.

OneWayGNSSRange(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRange

Simple constructor.

OneWayGNSSRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for OneWayGNSSRange measurements.

OneWayGNSSRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, ToDoubleFunction<AbsoluteDate>, double, double) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder

Simple constructor.

OnOff - Enum in org.orekit.files.ccsds.definitions

On/Off status for various elements.

ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

1 / A .

ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

1 / A .

ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

1 / (A * B) .

ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

1 / (A * B) .

ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

1 / (1 + B) .

ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

1 / (1 + B) .

ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

1 / μ .

ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

1 / μ .

openOnce() - Method in interface org.orekit.data.DataSource.ReaderOpener

Open the stream once.

openOnce() - Method in interface org.orekit.data.DataSource.StreamOpener

Open the stream once.

openReaderOnce() - Method in interface org.orekit.data.DataSource.Opener

Open a characters stream reader once.

openStreamOnce() - Method in interface org.orekit.data.DataSource.Opener

Open a bytes stream once.

Opm - Class in org.orekit.files.ccsds.ndm.odm.opm

This class gathers the informations present in the Orbital Parameter Message (OPM).

Opm(OdmHeader, List<Segment<OdmCommonMetadata, OpmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Opm

Simple constructor.

OpmData - Class in org.orekit.files.ccsds.ndm.odm.opm

Container for Orbit Parameter Message data.

OpmData(StateVector, KeplerianElements, SpacecraftParameters, CartesianCovariance, List<Maneuver>, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Simple constructor.

OpmParser - Class in org.orekit.files.ccsds.ndm.odm.opm

A parser for the CCSDS OPM (Orbit Parameter Message).

OpmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Complete constructor.

OpmWriter - Class in org.orekit.files.ccsds.ndm.odm.opm

Writer for CCSDS Orbit Parameter Message.

OpmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter

Complete constructor.

OpsStatus - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Operational status used in CCSDS Orbit Comprehensive Messages.

Orbit - Class in org.orekit.orbits

This class handles orbital parameters.

Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit

Default constructor.

Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit

Set the orbit from Cartesian parameters.

OrbitBlender - Class in org.orekit.orbits

Orbit blender.

OrbitBlender(SmoothStepFactory.SmoothStepFunction, Propagator, Frame) - Constructor for class org.orekit.orbits.OrbitBlender

Default constructor.

OrbitCategory - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Orbit category used in CCSDS Orbit Comprehensive Messages.

OrbitCorrection - Class in org.orekit.gnss.metric.messages.common

Container for SSR orbit correction data.

OrbitCorrection(double, double, double, double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.OrbitCorrection

Constructor.

OrbitCovariance - Class in org.orekit.files.ccsds.ndm.odm.ocm

Covariance entry.

OrbitCovariance(OrbitElementsType, Ordering, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance

Simple constructor.

OrbitCovarianceHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm

Covariance history.

OrbitCovarianceHistory(OrbitCovarianceHistoryMetadata, List<OrbitCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory

Simple constructor.

OrbitCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm

Metadata for covariance history.

OrbitCovarianceHistoryMetadata(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Simple constructor.

OrbitCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for covariance history container entries.

OrbitDetermination - Class in org.orekit.files.ccsds.ndm.odm.ocm

Orbit determination data.

OrbitDetermination() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Simple constructor.

OrbitDeterminationKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for orbit determination data entries.

OrbitElementsType - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Orbit element set type used in CCSDS Orbit Comprehensive Messages.

OrbitHermiteInterpolator - Class in org.orekit.orbits

Class using a Hermite interpolator to interpolate orbits.

OrbitHermiteInterpolator(Frame) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

OrbitHermiteInterpolator(int, Frame) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

OrbitHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator

Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).

OrbitHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator

Constructor.

OrbitManeuver - Class in org.orekit.files.ccsds.ndm.odm.ocm

Maneuver entry.

OrbitManeuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Build an uninitialized maneuver.

OrbitManeuverHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm

Maneuver history.

OrbitManeuverHistory(OrbitManeuverHistoryMetadata, List<OrbitManeuver>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory

Simple constructor.

OrbitManeuverHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm

Metadata for maneuver history.

OrbitManeuverHistoryMetadata(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Simple constructor.

OrbitManeuverHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for maneuver history container entries.

OrbitPhysicalProperties - Class in org.orekit.files.ccsds.ndm.odm.ocm

Spacecraft physical properties.

OrbitPhysicalProperties(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Simple constructor.

OrbitPhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for physical properties data entries.

OrbitRelativeFrame - Enum in org.orekit.files.ccsds.definitions

Frames used in CCSDS Orbit Data Messages.

OrbitType - Enum in org.orekit.orbits

Enumerate for Orbit and FieldOrbit parameters types.

orCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical OR of the given event detectors.

orCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector

Create a new event detector that is the logical OR of the given event detectors.

orCombine(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector

Create a new event detector that is the logical OR of the given event detectors.

orCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector

Create a new event detector that is the logical OR of the given event detectors.

Ordering - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for OrbitCovariance elements ordering.

OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager

Name of the property defining the root directories or zip/jar files path for default configuration.

OrekitAttitudeEphemerisFile - Class in org.orekit.files.general

A class for encapsulating Orekit propagators within an AttitudeEphemerisFile complaint object that makes for easy serialization to external ephemeris formats like AEM.

OrekitAttitudeEphemerisFile() - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile

Standard default constructor.

OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment - Class in org.orekit.files.general

Ephemeris segment.

OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris - Class in org.orekit.files.general

Inner class of OrekitAttitudeEphemerisFile that defines the OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris corresponding object for this ephemeris type.

OrekitAttitudeEphemerisSegment(List<TimeStampedAngularCoordinates>, String, int, Frame, AngularDerivativesFilter) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment

Constructor for OrekitAttitudeEphemerisSegment.

OrekitConfiguration - Class in org.orekit.utils

Utility class for setting global configuration parameters.

OrekitEphemerisFile - Class in org.orekit.files.general

A class for encapsulating Orekit propagators within an EphemerisFile complaint object that makes for easy serialization to external ephemeris formats like OEM.

OrekitEphemerisFile() - Constructor for class org.orekit.files.general.OrekitEphemerisFile

Standard default constructor.

OrekitEphemerisFile.OrekitEphemerisSegment - Class in org.orekit.files.general

Ephemeris segment.

OrekitEphemerisFile.OrekitSatelliteEphemeris - Class in org.orekit.files.general

Inner class of OrekitEphemerisFile that defines the OrekitEphemerisFile.OrekitSatelliteEphemeris corresponding object for this ephemeris type.

OrekitEphemerisSegment(List<TimeStampedPVCoordinates>, Frame, double, int) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment

constructor for OrekitEphemerisSegment.

OrekitException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by the Orekit classes.

OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException

Copy constructor.

OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed size step handler.

OrekitIllegalArgumentException - Exception in org.orekit.errors

Extension of IllegalArgumentException with localized message.

OrekitIllegalArgumentException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalArgumentException

Create an exception with localized message.

OrekitIllegalStateException - Exception in org.orekit.errors

Extension of IllegalStateException with localized message.

OrekitIllegalStateException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalStateException

Create an exception with localized message.

OrekitInternalError - Exception in org.orekit.errors

Extension of Runtime with localized message for internal errors only.

OrekitInternalError(Throwable) - Constructor for exception org.orekit.errors.OrekitInternalError

Create an exception with localized message.

OrekitIOException - Exception in org.orekit.errors

Extension of IOException with localized message.

OrekitIOException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIOException

Create an exception with localized message.

OrekitMessages - Enum in org.orekit.errors

Enumeration for localized messages formats.

OrekitMessages.UTF8Control - Class in org.orekit.errors

Control class loading properties in UTF-8 encoding.

OrekitParseException - Exception in org.orekit.errors

Extension of ParseException with localized message.

OrekitParseException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitParseException

Create an exception with localized message.

OrekitSatelliteAttitudeEphemeris(String) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris

Standard constructor for building the satellite Ephemeris object.

OrekitSatelliteEphemeris(String) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris

Standard constructor for building the satellite Ephemeris object.

OrekitStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler.

OrekitStepInterpolator - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step interpolator.

OrekitStepNormalizer - Class in org.orekit.propagation.sampling

This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.

OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer

Simple constructor.

org.orekit.annotation - package org.orekit.annotation

This package is the top level package for Orekit's specific annotations.

org.orekit.attitudes - package org.orekit.attitudes

This package provides classes to represent simple attitudes.

org.orekit.bodies - package org.orekit.bodies

This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.

org.orekit.compiler.plugin - package org.orekit.compiler.plugin

This package provides elements to handle data context plugin.

org.orekit.data - package org.orekit.data

This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.

org.orekit.errors - package org.orekit.errors

This package provides classes to generate and handle exceptions.

org.orekit.estimation - package org.orekit.estimation

This package is the top level package for orbit determination.

org.orekit.estimation.iod - package org.orekit.estimation.iod

This package provides initial orbit determination methods.

org.orekit.estimation.leastsquares - package org.orekit.estimation.leastsquares

The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.

org.orekit.estimation.measurements - package org.orekit.estimation.measurements

The measurements package defines everything that is related to orbit determination measurements.

org.orekit.estimation.measurements.filtering - package org.orekit.estimation.measurements.filtering

This package provides measurement pre-processing filters.

org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation

This package provides Orbit Determination measurements generation.

org.orekit.estimation.measurements.gnss - package org.orekit.estimation.measurements.gnss

This package provides methods to handle GNSS measurements.

org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers

This package provides measurement modifier.

org.orekit.estimation.sequential - package org.orekit.estimation.sequential

The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.

org.orekit.files - package org.orekit.files

Top level package for various parsers.

org.orekit.files.ccsds - package org.orekit.files.ccsds

This package is gathers sub-packages providing parsers/writers for various CCSDS messages.

org.orekit.files.ccsds.definitions - package org.orekit.files.ccsds.definitions

This package contains definitions for CCSDS objects (frames, time systems...).

org.orekit.files.ccsds.ndm - package org.orekit.files.ccsds.ndm

This package contains the base hierarchy for CCSDS ADM, ODM and TDM.

org.orekit.files.ccsds.ndm.adm - package org.orekit.files.ccsds.ndm.adm

This package contains class managing CCSDS Attitude Data Message.

org.orekit.files.ccsds.ndm.adm.acm - package org.orekit.files.ccsds.ndm.adm.acm

This package contains class managing CCSDS Attitude Comprehensive Message.

org.orekit.files.ccsds.ndm.adm.aem - package org.orekit.files.ccsds.ndm.adm.aem

This package contains class managing CCSDS Attitude Ephemeris Message.

org.orekit.files.ccsds.ndm.adm.apm - package org.orekit.files.ccsds.ndm.adm.apm

This package contains class managing CCSDS Attitude Parameter Message.

org.orekit.files.ccsds.ndm.cdm - package org.orekit.files.ccsds.ndm.cdm

This package contains class managing CCSDS Conjunction Data Message.

org.orekit.files.ccsds.ndm.odm - package org.orekit.files.ccsds.ndm.odm

This package contains class managing CCSDS Orbit Data Message.

org.orekit.files.ccsds.ndm.odm.ocm - package org.orekit.files.ccsds.ndm.odm.ocm

This package contains class managing CCSDS Orbit Comprehensive Message.

org.orekit.files.ccsds.ndm.odm.oem - package org.orekit.files.ccsds.ndm.odm.oem

This package contains class managing CCSDS Orbit Ephemeris Message.

org.orekit.files.ccsds.ndm.odm.omm - package org.orekit.files.ccsds.ndm.odm.omm

This package contains class managing CCSDS Orbit Mean-Elements Message.

org.orekit.files.ccsds.ndm.odm.opm - package org.orekit.files.ccsds.ndm.odm.opm

This package contains class managing CCSDS Orbit Parameter Message.

org.orekit.files.ccsds.ndm.tdm - package org.orekit.files.ccsds.ndm.tdm

This package contains class managing CCSDS Tracking Data Message.

org.orekit.files.ccsds.section - package org.orekit.files.ccsds.section

This package contains class managing the sections in CCSDS Messages.

org.orekit.files.ccsds.utils - package org.orekit.files.ccsds.utils

This package contains utilities shared by many CCSDS messages parsers/writers.

org.orekit.files.ccsds.utils.generation - package org.orekit.files.ccsds.utils.generation

This package contains utilities for CCSDS messages generation.

org.orekit.files.ccsds.utils.lexical - package org.orekit.files.ccsds.utils.lexical

This package contains utilities for CCSDS messages lexical analysis.

org.orekit.files.ccsds.utils.parsing - package org.orekit.files.ccsds.utils.parsing

This package contains classes related to the processing of parse tokens using the state design pattern.

org.orekit.files.general - package org.orekit.files.general

This package provides interfaces for orbit file representations and corresponding parsers.

org.orekit.files.ilrs - package org.orekit.files.ilrs

This package provides parsers for laser ranging data stored in CDR and CPF formats.

org.orekit.files.rinex - package org.orekit.files.rinex

This package is gathers sub-packages providing parsers/writers for various RINEX files.

org.orekit.files.rinex.clock - package org.orekit.files.rinex.clock

This package provides classes related to navigation clock files.

org.orekit.files.rinex.navigation - package org.orekit.files.rinex.navigation

This package provides classes related to RINEX navigation files.

org.orekit.files.rinex.observation - package org.orekit.files.rinex.observation

This package provides classes related to RINEX observation files.

org.orekit.files.rinex.section - package org.orekit.files.rinex.section

This package contains class managing the sections in RINEX files.

org.orekit.files.rinex.utils - package org.orekit.files.rinex.utils

This package contains utilities shared by many RINEX parsers/writers.

org.orekit.files.rinex.utils.parsing - package org.orekit.files.rinex.utils.parsing

This package contains classes related to the parsing of RINEX files.

org.orekit.files.sinex - package org.orekit.files.sinex

This package provides classes related to station data.

org.orekit.files.sp3 - package org.orekit.files.sp3

This package provides a parser for orbit data stored in SP3 format.

org.orekit.files.stk - package org.orekit.files.stk

This package provides a parser for STK ephemeris files.

org.orekit.forces - package org.orekit.forces

This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).

org.orekit.forces.drag - package org.orekit.forces.drag

This package provides all drag-related forces.

org.orekit.forces.empirical - package org.orekit.forces.empirical

This package provides empirical forces.

org.orekit.forces.gravity - package org.orekit.forces.gravity

This package provides all gravity-related forces.

org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential

This package provides classes to read gravity field files and supports several different formats.

org.orekit.forces.inertia - package org.orekit.forces.inertia

This package provides inertial force model.

org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers

This package provides models of simple maneuvers.

org.orekit.forces.maneuvers.jacobians - package org.orekit.forces.maneuvers.jacobians

Generators for columns of Jacobian matrices related to maneuver parameters.

org.orekit.forces.maneuvers.propulsion - package org.orekit.forces.maneuvers.propulsion

This package provides propulsion models intended to be used with class Maneuver.

org.orekit.forces.maneuvers.trigger - package org.orekit.forces.maneuvers.trigger

This package provides maneuver triggers' models intended to be used with class Maneuver.

org.orekit.forces.radiation - package org.orekit.forces.radiation

This package provides all radiation pressure related forces.

org.orekit.frames - package org.orekit.frames

This package provides classes to handle frames and transforms between them.

org.orekit.frames.encounter - package org.orekit.frames.encounter

Package specific to encounter local orbital frame.

org.orekit.geometry.fov - package org.orekit.geometry.fov

This package provides classes for representing a spacecraft sensor Field Of View.

org.orekit.gnss - package org.orekit.gnss

This package provides classes related to GNSS applications.

org.orekit.gnss.antenna - package org.orekit.gnss.antenna

This package provides classes related to receiver and satellites antenna modeling.

org.orekit.gnss.attitude - package org.orekit.gnss.attitude

This package provides classes related to navigation satellites attitude modeling.

org.orekit.gnss.metric - package org.orekit.gnss.metric

This package provides classes related to IGS binary formats.

org.orekit.gnss.metric.messages - package org.orekit.gnss.metric.messages

This package provides all supported IGS binary messages.

org.orekit.gnss.metric.messages.common - package org.orekit.gnss.metric.messages.common

This package contains utility classes relate to RTCM ephemeris messages.

org.orekit.gnss.metric.messages.rtcm - package org.orekit.gnss.metric.messages.rtcm

This package provides all supported RTCM messages.

org.orekit.gnss.metric.messages.rtcm.correction - package org.orekit.gnss.metric.messages.rtcm.correction

This package provides all supported RTCM correction messages.

org.orekit.gnss.metric.messages.rtcm.ephemeris - package org.orekit.gnss.metric.messages.rtcm.ephemeris

This package provides all supported RTCM ephemeris messages.

org.orekit.gnss.metric.messages.ssr - package org.orekit.gnss.metric.messages.ssr

This package provides all supported IGS SSR messages.

org.orekit.gnss.metric.messages.ssr.igm - package org.orekit.gnss.metric.messages.ssr.igm

This package provides all supported IGS Generic SSR Message types.

org.orekit.gnss.metric.messages.ssr.subtype - package org.orekit.gnss.metric.messages.ssr.subtype

This package provides all supported IGS SSR Sub-Type Message.

org.orekit.gnss.metric.ntrip - package org.orekit.gnss.metric.ntrip

This package provides streams reading from ntrip casters.

org.orekit.gnss.metric.parser - package org.orekit.gnss.metric.parser

This package provides the top level MessagesParser class that can extract messages from binary containers like ByteArrayEncodedMessages or {link org.orekit.metric.gnss.ssr.parser.InputStreamEncodedMessages InputStreamEncodedMessages}.

org.orekit.gnss.rflink - package org.orekit.gnss.rflink

This package provides classes related to RF-links binary formats.

org.orekit.gnss.rflink.gps - package org.orekit.gnss.rflink.gps

This package provides classes related to GPS RF-links binary formats.

org.orekit.models - package org.orekit.models

Top level package for physical models.

org.orekit.models.earth - package org.orekit.models.earth

This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.

org.orekit.models.earth.atmosphere - package org.orekit.models.earth.atmosphere

This package provides the atmosphere model interface and several implementations.

org.orekit.models.earth.atmosphere.data - package org.orekit.models.earth.atmosphere.data

This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.

org.orekit.models.earth.displacement - package org.orekit.models.earth.displacement

This package provides models computing reference points displacements on Earth surface.

org.orekit.models.earth.ionosphere - package org.orekit.models.earth.ionosphere

This package provides models that simulate the impact of the ionosphere.

org.orekit.models.earth.tessellation - package org.orekit.models.earth.tessellation

This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.

org.orekit.models.earth.troposphere - package org.orekit.models.earth.troposphere

This package provides models that simulate the impact of the troposphere.

org.orekit.models.earth.weather - package org.orekit.models.earth.weather

This package provides models that simulate global weather conditions on Earth.

org.orekit.orbits - package org.orekit.orbits

This package provides classes to represent orbits.

org.orekit.propagation - package org.orekit.propagation

Propagation

org.orekit.propagation.analytical - package org.orekit.propagation.analytical

Top level package for analytical propagators.

org.orekit.propagation.analytical.gnss - package org.orekit.propagation.analytical.gnss

This package provides classes to propagate GNSS orbits.

org.orekit.propagation.analytical.gnss.data - package org.orekit.propagation.analytical.gnss.data

This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.

org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle

This package provides classes to read and extrapolate tle's.

org.orekit.propagation.analytical.tle.generation - package org.orekit.propagation.analytical.tle.generation

This package provides classes related to TLE generation.

org.orekit.propagation.conversion - package org.orekit.propagation.conversion

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.

org.orekit.propagation.events - package org.orekit.propagation.events

This package provides interfaces and classes dealing with events occurring during propagation.

org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers

This package provides an interface and classes dealing with events occurrence only.

org.orekit.propagation.integration - package org.orekit.propagation.integration

Utilities for integration-based propagators (both numerical and semi-analytical).

org.orekit.propagation.numerical - package org.orekit.propagation.numerical

Top level package for numerical propagators.

org.orekit.propagation.numerical.cr3bp - package org.orekit.propagation.numerical.cr3bp

Top level package for CR3BP Models used with a numerical propagator.

org.orekit.propagation.sampling - package org.orekit.propagation.sampling

This package provides interfaces and classes dealing with step handling during propagation.

org.orekit.propagation.semianalytical - package org.orekit.propagation.semianalytical

Top level package for semi-analytical propagators.

org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst

This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces

This package provides force models for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities

This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen

This package provides Hansen coefficient related utilities for Draper Semi-analytical Satellite Theory (DSST).

org.orekit.ssa - package org.orekit.ssa

Top level package for various space situational awareness fields as well as associated evaluation metrics.

org.orekit.ssa.collision.shorttermencounter.probability.twod - package org.orekit.ssa.collision.shorttermencounter.probability.twod

Package specific to calculus assuming a 2D short-term encounter model.

org.orekit.ssa.metrics - package org.orekit.ssa.metrics

This package stores space situational awareness evaluation metrics.

org.orekit.time - package org.orekit.time

This independent package provides classes to handle epochs, time scales, and to compare instants together.

org.orekit.utils - package org.orekit.utils

This package provides useful objects.

org.orekit.utils.units - package org.orekit.utils.units

This package provides very basic handling of units.

OrphanFrame - Class in org.orekit.frames

Prototype frame that can be built from leaf to roots and later attached to a tree.

OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame

Simple constructor.

osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating derivative.

osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating second derivative.

OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion

This class converts osculating orbital elements into mean elements.

OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator, double) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Constructor.

osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating value.

OutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.

OutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OutlierFilter

Simple constructor.

outputField(TimeConverter, OrbitManeuver) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Output one maneuver field.

P

P1 - Static variable in class org.orekit.models.earth.displacement.Tide

P₁ tide.

PA - Static variable in enum org.orekit.orbits.OrbitType

Name for perigee argument.

Panel - Class in org.orekit.forces

Base class representing one panel of a satellite.

Panel(double, boolean, double, double, double, double) - Constructor for class org.orekit.forces.Panel

Simple constructor.

ParameterDrivenDateIntervalDetector - Class in org.orekit.propagation.events

Detector for date intervals that may be offset thanks to parameter drivers.

ParameterDrivenDateIntervalDetector(String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Build a new instance.

ParameterDrivenDateIntervalDetector(String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Build a new instance.

ParameterDrivenDateIntervalDetector(AdaptableInterval, double, int, EventHandler, DateDriver, DateDriver, DateDriver, ParameterDriver) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Protected constructor with full parameters.

ParameterDriver - Class in org.orekit.utils

Class allowing to drive the value of a parameter.

ParameterDriver(String, TimeSpanMap<String>, TimeSpanMap<Double>, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver

Create a new instance from another parameterDriver informations for example (useful for ParameterDriversList.DelegatingDriver)) At construction, the parameter new is configured as not selected, the reference date is set to null.

ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver

Simple constructor.

ParameterDriversList - Class in org.orekit.utils

Class managing several parameter drivers, taking care of duplicated names.

ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList

Creates an empty list.

ParameterDriversList.DelegatingDriver - Class in org.orekit.utils

Specialized driver delegating to several other managing the same parameter name.

ParameterDriversProvider - Interface in org.orekit.utils

Provider for parameters drivers.

ParameterFunction - Interface in org.orekit.utils

Interface representing a scalar function depending on a ParameterDriver.

ParameterObserver - Interface in org.orekit.utils

Interface for observing parameters changes.

ParametricAcceleration - Class in org.orekit.forces.empirical

This class implements a parametric acceleration.

ParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration

Simple constructor.

ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration

Simple constructor.

PARITY_SIZE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame

Size of parity field.

parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser

Parse a stream.

parse(String) - Method in class org.orekit.data.PolynomialParser

Parse a polynomial expression.

parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser

Parse a stream.

parse(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Parse a CCSDS frame.

parse(String, IERSConventions, boolean, DataContext, boolean, boolean, boolean) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade

Simple constructor.

parse(String) - Static method in class org.orekit.files.ccsds.definitions.OdMethodFacade

Parse a string from OCM.

parse(String) - Static method in class org.orekit.files.ccsds.definitions.PocMethodFacade

Parse a string from CDM.

parse(String) - Static method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame

Build an instance from a normalized descriptor.

parse(String) - Method in class org.orekit.files.ccsds.definitions.TimeConverter

Parse a relative or absolute date.

parse(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem

Parse a value from a key=value entry.

parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Parse an attitude ephemeris file from a data source.

parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Parse an attitude ephemeris file from a data source.

parse(boolean, boolean, RotationOrder, boolean, ContextBinding, String[]) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Get the angular coordinates corresponding to the attitude data.

parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Parse an ephemeris file from a data source.

parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Parse an ephemeris file from a data source.

parse(DataSource) - Method in interface org.orekit.files.general.AttitudeEphemerisFileParser

Parse an attitude ephemeris file from a data source.

parse(DataSource) - Method in interface org.orekit.files.general.EphemerisFileParser

Parse an ephemeris file from a data source.

parse(DataSource) - Method in class org.orekit.files.ilrs.CPFParser

Parse an ephemeris file from a data source.

parse(DataSource) - Method in class org.orekit.files.ilrs.CRDParser

Parse a CRD file.

parse(InputStream) - Method in class org.orekit.files.rinex.clock.RinexClockParser

Parse an IGS clock file from an input stream using the UTF-8 charset.

parse(String) - Method in class org.orekit.files.rinex.clock.RinexClockParser

Parse an IGS clock file from a file on the local file system.

parse(BufferedReader, String) - Method in class org.orekit.files.rinex.clock.RinexClockParser

Parse an IGS clock file from a stream.

parse(DataSource) - Method in class org.orekit.files.rinex.navigation.RinexNavigationParser

Parse RINEX navigation messages.

parse(DataSource) - Method in class org.orekit.files.rinex.observation.RinexObservationParser

Parse RINEX observations messages.

parse(String, String, char) - Static method in enum org.orekit.files.sp3.DataUsed

Parse the string to get the data used.

parse(String) - Static method in enum org.orekit.files.sp3.SP3FileType

Parse the string to get the data used.

parse(DataSource) - Method in class org.orekit.files.sp3.SP3Parser

parse(String) - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem

Parses a coordinate system from a string.

parse(DataSource) - Method in class org.orekit.files.stk.STKEphemerisFileParser

parse(InputStream, String) - Method in interface org.orekit.frames.EopHistoryLoader.Parser

Parse EOP from the given input stream.

parse(EncodedMessage, boolean) - Method in class org.orekit.gnss.metric.parser.MessagesParser

Parse one message.

parse(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.MessageType

Parse an encoded message.

parse(EncodedMessage) - Static method in class org.orekit.gnss.rflink.gps.SubFrame

Builder for sub-frames.

parse(InputStream, String) - Method in class org.orekit.time.AGILeapSecondFilesLoader.Parser

Load UTC-TAI offsets entries read from some file.

parse(InputStream, String) - Method in class org.orekit.time.TAIUTCDatFilesLoader.Parser

Load UTC-TAI offsets entries read from some file.

parse(InputStream, String) - Method in class org.orekit.time.UTCTAIHistoryFilesLoader.Parser

Load UTC-TAI offsets entries read from some file.

parse(InputStream, String) - Method in interface org.orekit.time.UTCTAIOffsetsLoader.Parser

Parse leap seconds from the input stream.

parse(String) - Static method in class org.orekit.utils.units.Unit

Parse a unit.

parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseClockDataType(String) - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType

Parse a string to get the time system.

parseCoefficient(String, Flattener, double[], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a coefficient.

parseComment(int, String, RinexFile<?>) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse a comment.

parseDate(String) - Static method in class org.orekit.time.DateComponents

Parse a string in ISO-8601 format to build a date.

parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents

Parse a string in ISO-8601 format to build a date/time.

ParsedMessage - Class in org.orekit.gnss.metric.messages

Abstract base class for decoded IGS messages.

ParsedMessage(int) - Constructor for class org.orekit.gnss.metric.messages.ParsedMessage

Simple constructor.

parseDouble(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse a double value.

parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a double from a string.

ParsedUnitsBehavior - Enum in org.orekit.files.ccsds.ndm

Behavior adopted for units that have been parsed from a CCSDS message.

parseInt(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse an integer value.

parseMessage(DataSource) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Parse a data source.

parseMessage(DataSource) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Parse a data source.

parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser

Parse the message number.

parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.MessagesParser

Parse the message number.

parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser

Parse the message number.

parseMonth(String) - Static method in enum org.orekit.time.Month

Parse the string to get the month.

parseOneLetterCode(String) - Static method in enum org.orekit.gnss.TimeSystem

Parse a string to get the time system.

parseProgramRunByDate(String, int, String, TimeScales, RinexBaseHeader) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse program, run/by and date.

Parser() - Constructor for class org.orekit.time.AGILeapSecondFilesLoader.Parser

Simple constructor.

Parser() - Constructor for class org.orekit.time.TAIUTCDatFilesLoader.Parser

Simple constructor.

Parser() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader.Parser

Simple constructor.

Parser - Class in org.orekit.utils.units

Parser for units.

ParserBuilder - Class in org.orekit.files.ccsds.ndm

Builder for all CCSDS Message files parsers.

ParserBuilder() - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder

Simple constructor.

ParserBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder

Simple constructor.

parseRinexFileType(String) - Static method in enum org.orekit.files.rinex.utils.RinexFileType

Parse the string to get the type.

parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem

Parse a string to get the satellite system.

parseSatelliteSystemWithGPSDefault(String) - Static method in enum org.orekit.gnss.SatelliteSystem

Parse a string to get the satellite system.

parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType

Parse a string to get the satellite type.

parseString(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse a string value.

parseTime(String) - Static method in class org.orekit.time.TimeComponents

Parse a string in ISO-8601 format to build a time.

parseTimeSystem(String) - Static method in enum org.orekit.gnss.TimeSystem

Parse a string to get the time system.

ParseToken - Class in org.orekit.files.ccsds.utils.lexical

Token occurring during CCSDS file parsing.

ParseToken(TokenType, String, String, Unit, int, String) - Constructor for class org.orekit.files.ccsds.utils.lexical.ParseToken

Simple constructor.

ParseToken.BooleanConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume boolean values.

ParseToken.CenterConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume center values.

ParseToken.CenterListConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume center lists.

ParseToken.CharConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume character values.

ParseToken.DateConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume date values.

ParseToken.DoubleArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume double array.

ParseToken.DoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume double values.

ParseToken.DoublyIndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume doubly-indexed double values.

ParseToken.EnumConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume enum values.

ParseToken.EnumListConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume lists of enum values.

ParseToken.FrameConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume frame values.

ParseToken.IndexedDoubleArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume indexed double array values.

ParseToken.IndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume indexed double values.

ParseToken.IndexedIntConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume indexed integer values.

ParseToken.IndexedStringConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume indexed string values.

ParseToken.IntConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume integer values.

ParseToken.IntegerArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume integer array.

ParseToken.LabeledDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume labeled double values.

ParseToken.ManeuvrableConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume Maneuvrable values.

ParseToken.RotationOrderConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume otation order values.

ParseToken.StringConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume string values.

ParseToken.StringListConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume lists of strings values.

ParseToken.TimeSystemConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume time systems values.

ParseToken.UnitListConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume units lists values.

ParseToken.VectorConsumer - Interface in org.orekit.files.ccsds.utils.lexical

Interface representing instance methods that consume vector values.

parseTwoLettersCode(String) - Static method in enum org.orekit.gnss.TimeSystem

Parse a string to get the time system.

parseType(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Parse an attitude type.

parseType(String) - Static method in enum org.orekit.files.sp3.SP3OrbitType

Parse a string to get the type.

parseUtcId(String) - Static method in enum org.orekit.files.rinex.navigation.UtcId

Parse a string to get the UTC id.

parseVersionFileTypeSatelliteSystem(String, String, RinexBaseHeader, double...) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils

Parse version, file type and satellite system.

PASCAL - Static variable in class org.orekit.utils.units.Unit

Pascal unit.

PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the past direction.

Patera2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Compute the probability of collision using the method described in :"PATERA, Russell P.

Patera2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005

Default constructor built with the following trapezoid integrator: Minimal iteration count of 5 Maximum iteration count of 50000 .

Patera2005(UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005

Customizable constructor.

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(AbsoluteDate, GeodeticPoint, double, double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, T, T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel

pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel

Calculates the ionospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

PATTERN_DATETIME_DELIMITER_REGEX - Static variable in class org.orekit.files.ilrs.CRDHeader

Pattern of delimiter of datetime.

PATTERN_NAN - Static variable in class org.orekit.files.ilrs.CRD

Pattern of "NaN".

PERCENT - Static variable in class org.orekit.utils.units.Unit

Percentage unit.

PERCENTS_TO_UNIT - Static variable in class org.orekit.utils.units.UnitsConverter

Percents to units converter.

perige - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

perigee, expressed in KM and ALTITUDE.

perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

perigee, expressed in KM and ALTITUDE.

permutation(int, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Perform one symmetric permutation involving rows/columns k0 and k0+1.

Perturbations - Class in org.orekit.files.ccsds.ndm.odm.ocm

Perturbation parameters.

Perturbations(CelestialBodies) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Simple constructor.

PerturbationsKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for perturbations data entries.

Phase - Class in org.orekit.estimation.measurements.gnss

Class modeling a phase measurement from a ground station.

Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.Phase

Simple constructor.

PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with ambiguity.

PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier

Constructor.

PhaseBias - Class in org.orekit.gnss.metric.messages.common

Container for phase bias data.

PhaseBias(int, boolean, int, int, double) - Constructor for class org.orekit.gnss.metric.messages.common.PhaseBias

Constructor.

PhaseBuilder - Class in org.orekit.estimation.measurements.gnss

Builder for Phase measurements.

PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder

Simple constructor.

PhaseCentersGroundReceiverBaseModifier<T extends GroundReceiverMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers

Ground and on-board antennas offsets effect on range measurements.

PhaseCentersGroundReceiverBaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier

Simple constructor.

PhaseCentersOffsetComputer - Class in org.orekit.estimation.measurements.modifiers

Compute phase centers offset on an emitter-receiver link.

PhaseCentersOffsetComputer(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersOffsetComputer

Simple constructor.

PhaseCentersPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Ground and on-board antennas offsets effect on phase measurements.

PhaseCentersPhaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier

Simple constructor.

PhaseCentersRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Ground and on-board antennas offsets effect on range measurements.

PhaseCentersRangeModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier

Simple constructor.

PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna

Model for antennas phase center variations.

PhaseIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with ionospheric delay.

PhaseIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier

Constructor.

PhaseMinusCodeCombination - Class in org.orekit.estimation.measurements.gnss

Phase minus Code combination.

PhaseMinusCodeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss

Phase minus code cycle slip detectors.

PhaseMinusCodeCycleSlipDetector(double, double, int, int) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector

Polynomial single frequency cycle-slip detector Constructor.

PhaseShiftCorrection - Class in org.orekit.files.rinex.observation

Phase Shift corrections.

PhaseShiftCorrection(SatelliteSystem, ObservationType, double, List<SatInSystem>) - Constructor for class org.orekit.files.rinex.observation.PhaseShiftCorrection

Simple constructor.

PhaseTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with tropospheric delay.

PhaseTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier

Constructor.

PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Pluto.

PocMethodFacade - Class in org.orekit.files.ccsds.definitions

Facade in front of several probability of collision methods in CCSDS messages.

PocMethodFacade(String, PocMethodType) - Constructor for class org.orekit.files.ccsds.definitions.PocMethodFacade

Simple constructor.

PocMethodType - Enum in org.orekit.files.ccsds.definitions

Type of probability of collision method used in CCSDS Conjunction Data Messages.

pointAt(double) - Method in class org.orekit.bodies.Ellipse

Get a point of the 2D ellipse.

pointAt(T) - Method in class org.orekit.bodies.FieldEllipse

Get a point of the 2D ellipse.

pointAtDistance(double) - Method in class org.orekit.bodies.Loxodrome

Calculate the point at the specified distance from the origin point along the loxodrome.

pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the point observed from the station at some specified distance.

PointingPanel - Class in org.orekit.forces

Class representing one panel of a satellite, roughly pointing towards some target.

PointingPanel(Vector3D, ExtendedPVCoordinatesProvider, double, double, double, double, double) - Constructor for class org.orekit.forces.PointingPanel

Simple constructor.

pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid

Find a point on ellipsoid limb, as seen by an external observer.

pointOnLimb(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid

Find a point on ellipsoid limb, as seen by an external observer.

PoissonSeries - Class in org.orekit.data

Class representing a Poisson series for nutation or ephemeris computations.

PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries

Build a Poisson series from an IERS table file.

PoissonSeries.CompiledSeries - Interface in org.orekit.data

This interface represents a fast evaluator for Poisson series.

PoissonSeriesParser - Class in org.orekit.data

Parser for Poisson series files.

PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser

Build a parser for a Poisson series from an IERS table file.

PoleCorrection - Class in org.orekit.frames

Simple container class for pole correction parameters.

PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection

Simple constructor.

PolygonalFieldOfView - Class in org.orekit.geometry.fov

Class representing a spacecraft sensor Field Of View with polygonal shape.

PolygonalFieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView

Build a new instance.

PolygonalFieldOfView(Vector3D, PolygonalFieldOfView.DefiningConeType, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView

Build Field Of View with a regular polygon shape.

PolygonalFieldOfView.DefiningConeType - Enum in org.orekit.geometry.fov

Enumerate for cone/polygon relative position.

PolynomialAccelerationModel - Class in org.orekit.forces.empirical

Polynomial acceleration model.

PolynomialAccelerationModel(String, AbsoluteDate, int) - Constructor for class org.orekit.forces.empirical.PolynomialAccelerationModel

Simple constructor.

PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

A quadratic matrix of PolynomialFunction.

PolynomialNutation - Class in org.orekit.data

Polynomial nutation function.

PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation

Build a polynomial from its coefficients.

PolynomialParser - Class in org.orekit.data

Parser for polynomials in IERS tables.

PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser

Simple constructor.

PolynomialParser.Unit - Enum in org.orekit.data

Unit for the coefficients.

PolynomialThrustSegment - Class in org.orekit.forces.maneuvers.propulsion

One polynomial segment of a thrust profile.

PolynomialThrustSegment(AbsoluteDate, PolynomialFunction, PolynomialFunction, PolynomialFunction) - Constructor for class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment

Simple constructor.

POS_VEL_BASE_ACCURACY - Static variable in class org.orekit.files.sp3.SP3Utils

Base for general position/velocity accuracy.

POS_X - Static variable in enum org.orekit.orbits.OrbitType

Name for position along X.

POS_Y - Static variable in enum org.orekit.orbits.OrbitType

Name for position along Y.

POS_Z - Static variable in enum org.orekit.orbits.OrbitType

Name for position along Z.

Position - Class in org.orekit.estimation.measurements

Class modeling a position only measurement.

Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with one double for the standard deviation.

Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with one vector for the standard deviation.

Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position

Constructor with full covariance matrix and all inputs.

POSITION_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Position accuracy unit.

POSITION_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Position unit.

PositionAngleBased - Interface in org.orekit.orbits

This interface represent orbit-like trajectory whose definition is based on a so-called position angle.

PositionAngleDetector - Class in org.orekit.propagation.events

Detector for in-orbit position angle.

PositionAngleDetector(OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector

Build a new detector.

PositionAngleDetector(double, double, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector

Build a detector.

PositionAngleDetector(AdaptableInterval, double, int, EventHandler, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector

Protected constructor with full parameters.

PositionAngleType - Enum in org.orekit.orbits

Enumerate for true, eccentric and mean position angles.

PositionBuilder - Class in org.orekit.estimation.measurements.generation

Builder for Position measurements.

PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder

Simple constructor.

positionShiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted position.

positionShiftedBy(double) - Method in class org.orekit.utils.PVCoordinates

Get a time-shifted position.

PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential

This abstract class represents a Gravitational Potential Coefficients file reader.

PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Simple constructor.

PotentialCoefficientsReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Simple constructor.

power(String, Fraction) - Method in class org.orekit.utils.units.Unit

Create power of unit.

PowerTerm - Class in org.orekit.utils.units

A container for a term with associated power.

PREAMBLE_VALUE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame

TLM preamble.

Predefined - Enum in org.orekit.frames

Predefined frames provided by Frames.

PredictedEOPHistory - Class in org.orekit.frames

This class extends an EOPHistory for some weeks using fitting.

PredictedEOPHistory(EOPHistory, double, EOPFitter) - Constructor for class org.orekit.frames.PredictedEOPHistory

Simple constructor.

PREFIX - Static variable in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay

Prefix for state name.

prepareComments(List<RinexComment>) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Prepare comments to be emitted at specified lines.

prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Prepare data for parsing.

prepareData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Prepare data for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Prepare header for parsing.

prepareHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Prepare header for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Prepare metadata for parsing.

prepareMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser

Prepare metadata for parsing.

previous() - Method in class org.orekit.utils.TimeSpanMap.Span

Get the previous time span.

previous() - Method in class org.orekit.utils.TimeSpanMap.Transition

Get the previous transition.

ProbabilityOfCollision - Class in org.orekit.ssa.metrics

Container for values relative to the probability of collision : Value of the probability of collision. Name of the method with which it was computed. Upper and lower limit of the value if the method provides them (such as Laas2015 for example). Flag defining if the probability was maximized in any way (such as Alfriend1999Max for example).

ProbabilityOfCollision(double, String) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision

Constructor with default values of 0 for the upper/lower limits and default false flag for maximum probability.

ProbabilityOfCollision(double, String, boolean) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision

Constructor with default values of 0 for the upper and lower limits.

ProbabilityOfCollision(double, double, double, String, boolean) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision

Constructor.

process(ParseToken, AcmParser) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey

Process one token.

process(ParseToken, ContextBinding, AcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey

Process an token.

process(ParseToken, ContextBinding, AttitudeCovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey

Process an token.

process(ParseToken, AcmParser, ContextBinding, AttitudeDetermination) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey

Process an token.

process(ParseToken, ContextBinding, AttitudeDeterminationSensor) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey

Process an token.

process(ParseToken, ContextBinding, AttitudeManeuver) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey

Process an token.

process(ParseToken, ContextBinding, AttitudePhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey

Process an token.

process(ParseToken, ContextBinding, AttitudeStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey

Process an token.

process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey

Process one token.

process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey

Process one token.

process(ParseToken, ContextBinding, AemMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey

Process an token.

process(ParseToken, ContextBinding, AttitudeEntry) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey

Process an token.

process(ParseToken, ContextBinding, AngularVelocity) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey

Process one token.

process(ParseToken, ContextBinding, ApmQuaternion, ParseToken.DateConsumer) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey

Process one token.

process(ParseToken, ContextBinding, Euler) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey

Process one token.

process(ParseToken, ContextBinding, Inertia) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey

Process an token.

process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey

Process one token.

process(ParseToken, ContextBinding, SpinStabilized) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey

Process one token.

process(ParseToken, ContextBinding, AdditionalCovarianceMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey

Process one token.

process(ParseToken, ContextBinding, AdditionalParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey

Process one token.

process(ParseToken, ContextBinding, CdmHeader) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey

Process an token.

process(ParseToken, ContextBinding, CdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey

Process an token.

process(ParseToken, ContextBinding, CdmRelativeMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey

Process one token.

process(ParseToken, ContextBinding, ODParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey

Process one token.

process(ParseToken, ContextBinding, RTNCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey

Process one token.

process(ParseToken, ContextBinding, SigmaEigenvectorsCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey

Process one token.

process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey

Process one token.

process(ParseToken, CdmParser) - Method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey

Process one token.

process(ParseToken, ContextBinding, XYZCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey

Process one token.

process(ParseToken, ContextBinding, CartesianCovariance) - Method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey

Process one token.

process(ParseToken, ContextBinding, OdmCommonMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey

Process one token.

process(ParseToken, ContextBinding, KeplerianElements) - Method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey

Process one token.

process(String, ContextBinding, OrbitManeuver, int, String) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Process one field.

process(ParseToken, OcmParser) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey

Process one token.

process(ParseToken, ContextBinding, OcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey

Process an token.

process(ParseToken, ContextBinding, OrbitCovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey

Process an token.

process(ParseToken, ContextBinding, OrbitDetermination) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey

Process an token.

process(ParseToken, ContextBinding, OrbitManeuverHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey

Process an token.

process(ParseToken, ContextBinding, OrbitPhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey

Process an token.

process(ParseToken, ContextBinding, Perturbations) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey

Process an token.

process(ParseToken, ContextBinding, TrajectoryStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey

Process an token.

process(ParseToken, ContextBinding, OdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey

Process one token.

process(ParseToken, ContextBinding, OemMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey

Process an token.

process(ParseToken, ContextBinding, OmmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey

Process one token.

process(ParseToken, ContextBinding, OmmTle) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey

Process one token.

process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey

Process one token.

process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey

Process one token.

process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey

Process one token.

process(ParseToken, ContextBinding, RangeUnitsConverter, TdmMetadata, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType

Process an observation line.

process(ParseToken, ContextBinding, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey

Process one token.

process(ParseToken, ContextBinding, TdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey

Process an token.

process(ParseToken, ContextBinding, Header) - Method in enum org.orekit.files.ccsds.section.HeaderKey

Process an token.

process(ParseToken, AbstractConstituentParser<?, ?, ?>) - Method in enum org.orekit.files.ccsds.section.KvnStructureKey

Process an token.

process(ParseToken, ContextBinding, Metadata) - Method in enum org.orekit.files.ccsds.section.MetadataKey

Process an token.

process(ParseToken, AbstractConstituentParser<?, ?, ?>) - Method in enum org.orekit.files.ccsds.section.XmlStructureKey

Process an token.

process(ParseToken) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Process a parse token.

process(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Process a parse token.

processAsBoolean(ParseToken.BooleanConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a boolean.

processAsCenter(ParseToken.CenterConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a body center.

processAsCenterList(ParseToken.CenterListConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a body center list.

processAsDate(ParseToken.DateConsumer, ContextBinding) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a date.

processAsDouble(Unit, ParsedUnitsBehavior, ParseToken.DoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a double.

processAsDoubleArray(Unit, ParsedUnitsBehavior, ParseToken.DoubleArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an array of doubles.

processAsDoublyIndexedDouble(int, int, Unit, ParsedUnitsBehavior, ParseToken.DoublyIndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a doubly-indexed double.

processAsEnum(Class<T>, ParseToken.EnumConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an enum.

processAsEnumsList(Class<T>, ParseToken.EnumListConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a list of enums.

processAsFrame(ParseToken.FrameConsumer, ContextBinding, boolean, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a frame.

processAsFreeTextList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a list of free-text strings.

processAsFreeTextString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as free text string.

processAsIndexedDouble(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an indexed double.

processAsIndexedDoubleArray(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an indexed double array.

processAsIndexedInteger(int, ParseToken.IndexedIntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an indexed integer.

processAsIndexedNormalizedString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an indexed normalized string.

processAsIndexedUppercaseString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an indexed normalized uppercase string.

processAsInteger(ParseToken.IntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an integer.

processAsIntegerArray(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an array of integers.

processAsIntegerArrayNoSpace(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as an array of integers.

processAsLabeledDouble(char, Unit, ParsedUnitsBehavior, ParseToken.LabeledDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a labeled double.

processAsManeuvrableEnum(ParseToken.ManeuvrableConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content of the Maneuvrable enum.

processAsNormalizedCharacter(ParseToken.CharConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a normalized character.

processAsNormalizedList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a list of normalized strings.

processAsNormalizedString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a normalized string.

processAsRotationOrder(ParseToken.RotationOrderConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a rotation sequence.

processAsTimeSystem(ParseToken.TimeSystemConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a time system.

processAsUnitList(ParseToken.UnitListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a list of units.

processAsUppercaseList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a list of normalized uppercase strings.

processAsUppercaseString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a normalized uppercase string.

processAsVector(Unit, ParsedUnitsBehavior, ParseToken.VectorConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken

Process the content as a vector.

ProcessingState - Interface in org.orekit.files.ccsds.utils.parsing

Interface for processing parsing tokens for CCSDS NDM files.

processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Process several measurements.

processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator

Process a single measurement.

processMeasurements(List<ObservedMeasurement<?>>, ExtendedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Process a single measurement.

processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator

Process a single measurement.

processMeasurements(List<ObservedMeasurement<?>>, UnscentedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Process measurements.

processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator

Process several measurements.

processToken(ParseToken) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState

Process one token.

processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.HeaderProcessingState

Process one token.

processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.KvnStructureProcessingState

Process one token.

processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.XmlStructureProcessingState

Process one token.

processToken(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.ErrorState

Process one token.

processToken(ParseToken) - Method in interface org.orekit.files.ccsds.utils.parsing.ProcessingState

Process one token.

ProfileThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion

Thrust propulsion model based on segmented profile.

ProfileThrustPropulsionModel(TimeSpanMap<PolynomialThrustSegment>, double, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel

Generic constructor.

projectOntoCollisionPlane(RealMatrix) - Method in interface org.orekit.frames.encounter.EncounterLOF

Project given matrix expressed in this encounter local orbital frame onto the collision plane.

projectOntoCollisionPlane(FieldMatrix<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Project given matrix expressed in this encounter local orbital frame onto the collision plane defined by this same encounter local orbital frame.

projectOntoCollisionPlane(Vector3D) - Method in interface org.orekit.frames.encounter.EncounterLOF

Project given vector expressed in this encounter local orbital frame onto the collision plane.

projectOntoCollisionPlane(FieldVector3D<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Project given vector expressed in this encounter local orbital frame onto the collision plane.

projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.CircularFieldOfView

Find the direction on Field Of View Boundary closest to a line of sight.

projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView

Find the direction on Field Of View Boundary closest to a line of sight.

projectToBoundary(Vector3D) - Method in interface org.orekit.geometry.fov.FieldOfView

Find the direction on Field Of View Boundary closest to a line of sight.

projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView

Find the direction on Field Of View Boundary closest to a line of sight.

projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse

Find the closest ellipse point.

projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse

Project position-velocity-acceleration on an ellipse.

projectToEllipse(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse

Find the closest ellipse point.

projectToEllipse(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.bodies.FieldEllipse

Project position-velocity-acceleration on an ellipse.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a moving point to the ground.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a moving point to the ground.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid

projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid

propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate from a start date towards a target date.

propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Propagate towards a target date.

propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator

Propagate towards a target date.

propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer

Propagate from a start date towards a target date.

propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Gets the PVCoordinates of the GLONASS SV in ECEF frame.

propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Gets the PVCoordinates of the GNSS SV in ECEF frame.

propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Gets the PVCoordinates of the GNSS SV in ECEF frame.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Extrapolate an orbit up to a specific target date.

PropagationType - Enum in org.orekit.propagation

Enumerate to define the propagation type used by the propagator.

Propagator - Interface in org.orekit.propagation

This interface provides a way to propagate an orbit at any time.

PropagatorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build propagators for conversion.

PropagatorConverter - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction for propagators conversions.

PropagatorsParallelizer - Class in org.orekit.propagation

This class provides a way to propagate simultaneously several orbits.

PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer

Simple constructor.

PropagatorsParallelizer(List<Propagator>, double, MultiSatFixedStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer

Simple constructor.

properToNatural(double[], GroundStation, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Proper to natural correction for aberration of light.

properToNatural(double[], GroundStation, AbsoluteDate, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier

Proper to natural correction for aberration of light.

PropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion

Generic interface for a propulsion model used in a Maneuver.

put(String, double[]) - Method in class org.orekit.utils.DoubleArrayDictionary

Add an entry.

put(String, T[]) - Method in class org.orekit.utils.FieldArrayDictionary

Add an entry.

put(String, double[]) - Method in class org.orekit.utils.FieldArrayDictionary

Add an entry.

putAll(Map<String, double[]>) - Method in class org.orekit.utils.DoubleArrayDictionary

Put all the entries from the map in the dictionary.

putAll(DoubleArrayDictionary) - Method in class org.orekit.utils.DoubleArrayDictionary

Put all the entries from another dictionary.

putAll(Map<String, T[]>) - Method in class org.orekit.utils.FieldArrayDictionary

Put all the entries from the map in the dictionary.

putAll(FieldArrayDictionary<T>) - Method in class org.orekit.utils.FieldArrayDictionary

Put all the entries from another dictionary.

PV - Class in org.orekit.estimation.measurements

Class modeling a position-velocity measurement.

PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with two double for the standard deviations.

PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with two vectors for the standard deviations.

PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with one vector for the standard deviations.

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with 2 smaller covariance matrices.

PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV

Constructor with full covariance matrix and all inputs.

PVBuilder - Class in org.orekit.estimation.measurements.generation

Builder for PV measurements.

PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder

Simple constructor.

PVCoordinates - Class in org.orekit.utils

Simple container for Position/Velocity/Acceleration triplets.

PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates

Simple constructor.

PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet with zero acceleration.

PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet.

PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Multiplicative constructor.

PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Subtractive constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet from a FieldVector3D<Derivative>.

PVCoordinates(Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds PV coordinates with the givne position, zero velocity, and zero acceleration.

PVCoordinatesProvider - Interface in org.orekit.utils

Interface for PV coordinates providers.

Q

Q1 - Static variable in class org.orekit.models.earth.displacement.Tide

Q₁ tide.

Q22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Q22.

Q31 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Q31.

Q33 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Q33.

QOMS2T - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

QOMS2T.

QZSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Value of the earth's rotation rate in rad/s for QZSS user.

QZSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.

QZSS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for QZSS weeks: 1980-01-06.

QZSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

WGS 84 value of the Earth's universal gravitational parameter for QZSS user in m³/s².

QZSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

Number of weeks in the QZSS cycle.

QZSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data

This class holds a QZSS almanac as read from YUMA files.

QZSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Constructor.

QZSSCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a QZSS navigation message.

QZSSCivilianNavigationMessage(boolean) - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSCivilianNavigationMessage

Constructor.

QZSSLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a QZSS navigation message.

QZSSLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSLegacyNavigationMessage

Constructor.

QZSSScale - Class in org.orekit.time

QZSS time scale.

R

RAAN - Static variable in enum org.orekit.orbits.OrbitType

Name for right ascension of ascending node.

RADIAN - Static variable in class org.orekit.utils.units.Unit

Radian unit.

radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure.

RadiationSensitive - Interface in org.orekit.forces.radiation

Interface for spacecraft that are sensitive to radiation pressure forces.

radiusCorrection(double) - Method in enum org.orekit.propagation.events.VisibilityTrigger

Apply radius correction.

Range - Class in org.orekit.estimation.measurements

Class modeling a range measurement from a ground station.

Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range

Simple constructor.

RangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for Range measurements.

RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder

Simple constructor.

rangeErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier

Compute the measurement error due to Troposphere.

rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier

Compute the measurement error due to Troposphere.

RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with ionospheric delay.

RangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier

Constructor.

RangeMeasurement(AbsoluteDate, double, int) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement

Constructor.

RangeMeasurement(AbsoluteDate, double, int, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement

Constructor.

RangeMeasurement(AbsoluteDate, double, int, double, String) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement

Constructor.

RangeMode - Enum in org.orekit.files.ccsds.ndm.tdm

Type of range tones.

RangeModifierUtil - Class in org.orekit.estimation.measurements.modifiers

Utility class modifying theoretical range measurement.

RangeRate - Class in org.orekit.estimation.measurements

Class modeling one-way or two-way range rate measurement between two vehicles.

RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate

Simple constructor.

RangeRateBuilder - Class in org.orekit.estimation.measurements.generation

Builder for RangeRate measurements.

RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder

Simple constructor.

rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Compute the measurement error due to Ionosphere.

rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Compute the measurement error due to Troposphere.

RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range-rate measurement with ionospheric delay.

RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier

Constructor.

RangeRateModifierUtil - Class in org.orekit.estimation.measurements.modifiers

Utility class modifying theoretical range-rate measurement.

RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range-rate measurements with tropospheric delay.

RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier

Constructor.

RangeSupplement(AbsoluteDate, String, double, double, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeSupplement

Constructor.

RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with tropospheric delay.

RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier

Constructor.

RangeUnits - Enum in org.orekit.files.ccsds.ndm.tdm

Units of the range observable.

RangeUnitsConverter - Interface in org.orekit.files.ccsds.ndm.tdm

Interface for converting Range Units to meters.

RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).

RAPID_DATA_PREDICTION_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).

RateElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm

Attitude rate element set type used in CCSDS Attitude Comprehensive Messages.

rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Check if rates are specified in frame A.

rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Check if rates are specified in frame A.

rawDataIsBinary() - Method in interface org.orekit.data.DataSource.Opener

Check if the raw data is binary.

RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide raw spherical harmonics coefficients.

RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The raw spherical harmonics at a particular instant.

rawToSI(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType

Convert a measurement to SI units.

readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Read a gravity field coefficients provider from the first supported file.

readGravityField(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields

Read a gravity field coefficients provider from the first supported file.

Receiver(String, String, double, double, double) - Constructor for class org.orekit.files.rinex.clock.RinexClock.Receiver

Constructor.

ReceiverAntenna - Class in org.orekit.gnss.antenna

GNSS receiver antenna model.

ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna

Simple constructor.

receiverToInert(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp

Compute rotation from receiver to inertial frame.

receiverToInert(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUp

Compute rotation from receiver to inertial frame.

receiverToInert(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp

Compute rotation from receiver to inertial frame.

Record - Class in org.orekit.gnss.metric.ntrip

Record in source table.

Record(String) - Constructor for class org.orekit.gnss.metric.ntrip.Record

Build a record by parsing a source table line.

RecordAndContinue - Class in org.orekit.propagation.events.handlers

Handler that will record every time an event occurs and always return Action.CONTINUE.

RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue

Create a new handler using an ArrayList to store events.

RecordAndContinue(List<RecordAndContinue.Event>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue

Create a handler using the given collection to store events.

RecordAndContinue.Event - Class in org.orekit.propagation.events.handlers

A single event detected during propagation.

RecordType - Enum in org.orekit.gnss.metric.ntrip

Enumerate for record types in sourcetable.

recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Recover ambiguities prior to the Z-transformation.

recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping

Recover ambiguities prior to the Z-transformation.

reduction() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Perform LAMBDA reduction.

reduction() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod

Perform LAMBDA reduction.

reduction() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Perform MLAMBDA reduction.

ReferenceClock(String, String, double, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.files.rinex.clock.RinexClock.ReferenceClock

Constructor.

referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter reference date has been changed.

ReferenceEllipsoid - Class in org.orekit.models.earth

A Reference Ellipsoid for use in geodesy.

ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid

Creates a new geodetic Reference Ellipsoid from four defining parameters.

referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter reference value has been changed.

REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for reflection coefficient.

refuseFurtherComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer

Set flag to refuse further comments.

RegionCode - Enum in org.orekit.files.rinex.navigation

Enumerate for region code.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Register an attitude provider.

registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence

Register all wrapped switch events to the propagator.

registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence

Register all wrapped switch events to the propagator.

RegularXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical

Regular builder using XML elements names and content for tokens.

RegularXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder

Simple constructor.

reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Reinitialize the beginning of the step.

reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Reinitialize the beginning of the step.

RelativisticClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites phase measurement with relativistic clock correction.

RelativisticClockInterSatellitesPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier

Simple constructor.

RelativisticClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites range measurement with relativistic clock correction.

RelativisticClockInterSatellitesRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier

Simple constructor.

RelativisticClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical one-way GNSS phase measurement with relativistic clock correction.

RelativisticClockOneWayGNSSPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier

Simple constructor.

RelativisticClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical one-way GNSS range measurement with relativistic clock correction.

RelativisticClockOneWayGNSSRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier

Simple constructor.

RelativisticClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with relativistic clock correction.

RelativisticClockPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier

Simple constructor.

RelativisticClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with relativistic clock correction.

RelativisticClockRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier

Simple constructor.

RelativisticClockRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range-rate measurement with relativistic frequency deviation.

RelativisticClockRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier

Simple constructor.

relativisticCorrection(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier

Computes the relativistic clock correction.

RelativisticJ2ClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites phase measurements with relativistic J2 clock correction.

RelativisticJ2ClockInterSatellitesPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier

Modifier constructor.

RelativisticJ2ClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.

RelativisticJ2ClockInterSatellitesRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier

Modifier constructor.

RelativisticJ2ClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical one-way phase measurements with relativistic J2 clock correction.

RelativisticJ2ClockOneWayGNSSPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier

Modifier constructor.

RelativisticJ2ClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying one-way GNSS range theoretical measurements with relativistic J2 clock correction.

RelativisticJ2ClockOneWayGNSSRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier

Modifier constructor.

RelativisticJ2ClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurements with relativistic J2 clock correction.

RelativisticJ2ClockPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier

Modifier constructor.

RelativisticJ2ClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurements with relativistic J2 clock correction.

RelativisticJ2ClockRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier

Modifier constructor.

relativisticJ2Correction(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier

Computes the relativistic J2 clock time delay correction.

Relativity - Class in org.orekit.forces.gravity

Post-Newtonian correction force due to general relativity.

Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity

Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.

remove(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Remove a handler.

remove(FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer

Remove a handler.

remove(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Remove a handler.

remove(OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer

Remove a handler.

remove(String) - Method in class org.orekit.utils.DoubleArrayDictionary

Remove an entry.

remove(String) - Method in class org.orekit.utils.FieldArrayDictionary

remove an entry.

removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Remove all perturbing force models from the global perturbation model.

removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Remove all force models (except central attraction).

removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Remove all perturbing force models from the global perturbation model (except central attraction).

removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Remove all perturbing force models from the global perturbation model (except central attraction).

removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver

Remove an observer.

removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Remove one provider.

removeRates() - Method in class org.orekit.orbits.CircularOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in class org.orekit.orbits.EquinoctialOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in class org.orekit.orbits.FieldCircularOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in class org.orekit.orbits.KeplerianOrbit

Create a new instance such that PositionAngleBased.hasRates() is false.

removeRates() - Method in interface org.orekit.orbits.PositionAngleBased

Create a new instance such that PositionAngleBased.hasRates() is false.

removeSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Remove spurious solution.

replaceObserver(ParameterObserver, ParameterObserver) - Method in class org.orekit.utils.ParameterDriver

Replace an observer.

requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer

Determines whether this handler needs dense output.

rescale(double, boolean, Flattener, Flattener, double[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Rescale coefficients arrays.

rescale(boolean, Flattener, Flattener, TimeDependentHarmonic[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Rescale coefficients arrays.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.NdmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser

Reset parser to initial state before parsing.

reset(FileFormat) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser

Reset parser to initial state before parsing.

reset(FileFormat, ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Reset parser to initial state before parsing.

resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence

Reset the active provider.

resetFiltersToDefault() - Method in class org.orekit.data.DataProvidersManager

Reset all filters to default.

resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic

Reset fitting.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris

Try (and fail) to reset the initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Reset the propagator initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Reset the initial state.

resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Reset the initial state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Reset an intermediate state.

resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Reset an intermediate state.

resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Reset an intermediate state.

resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Reset the orbit in the propagator builder.

resetOrbit(Orbit, PropagationType) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Reset the orbit in the propagator builder.

resetOrbit(Orbit) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Reset the orbit in the propagator builder.

resetState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Reset state as a maneuver triggers.

resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter

Reset state as a maneuver triggers.

resetState(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter

Reset state as a maneuver triggers.

resetState(EventDetector, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Reset the state prior to continue propagation.

resetState(EventDetector, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Reset the state prior to continue propagation.

resetState(FieldEventDetector<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler

Reset the state prior to continue propagation.

ResidualFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering

Residual pre-processing filter.

ResidualFilter(double) - Constructor for class org.orekit.estimation.measurements.filtering.ResidualFilter

Constructor.

restrictStep(FieldSpacecraftState<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator

Create a new restricted version of the instance.

restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Create a new restricted version of the instance.

REV_PER_DAY - Static variable in class org.orekit.files.ccsds.definitions.Units

Revolutions per day unit.

REV_PER_DAY2_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units

Scaled revolutions per square day unit.

REV_PER_DAY3_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units

Scaled revolutions per cubic day divieded by 6 unit.

revert() - Method in class org.orekit.utils.AngularCoordinates

Revert a rotation/rotation rate/ rotation acceleration triplet.

revert() - Method in class org.orekit.utils.FieldAngularCoordinates

Revert a rotation / rotation rate / rotation acceleration triplet.

revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Revert a rotation/rotation rate pair.

revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Revert a rotation/rotation rate pair.

REVOLUTION - Static variable in class org.orekit.utils.units.Unit

Revolution unit.

RichardsonExpansion - Class in org.orekit.orbits

Class implementing the Third-Order Richardson Expansion.

RichardsonExpansion(CR3BPSystem, LagrangianPoints) - Constructor for class org.orekit.orbits.RichardsonExpansion

Simple Constructor.

RinexBaseHeader - Class in org.orekit.files.rinex.section

Base container for Rinex headers.

RinexBaseHeader(RinexFileType) - Constructor for class org.orekit.files.rinex.section.RinexBaseHeader

Simple constructor.

RinexClock - Class in org.orekit.files.rinex.clock

Represents a parsed clock file from the IGS.

RinexClock(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.rinex.clock.RinexClock

Constructor.

RinexClock.ClockDataLine - Class in org.orekit.files.rinex.clock

Clock data for a single station.

RinexClock.ClockDataType - Enum in org.orekit.files.rinex.clock

Clock data type.

RinexClock.Receiver - Class in org.orekit.files.rinex.clock

Represents a receiver or a satellite with its position in the considered frame.

RinexClock.ReferenceClock - Class in org.orekit.files.rinex.clock

Represents a reference clock with its validity time span.

RinexClockParser - Class in org.orekit.files.rinex.clock

A parser for the clock file from the IGS.

RinexClockParser() - Constructor for class org.orekit.files.rinex.clock.RinexClockParser

Create an clock file parser using default values.

RinexClockParser(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.rinex.clock.RinexClockParser

Create a clock file parser and specify the frame builder.

RinexClockParser(Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.rinex.clock.RinexClockParser

Constructor, build the IGS clock file parser.

RinexComment - Class in org.orekit.files.rinex.section

Container for comment in RINEX file.

RinexComment(int, String) - Constructor for class org.orekit.files.rinex.section.RinexComment

Simple constructor.

RinexFile<T extends RinexBaseHeader> - Class in org.orekit.files.rinex

Container for Rinex file.

RinexFile(T) - Constructor for class org.orekit.files.rinex.RinexFile

Simple constructor.

RinexFileType - Enum in org.orekit.files.rinex.utils

Enumerate for RINEX files types.

RinexLabels - Enum in org.orekit.files.rinex.section

Labels for Rinex files.

RinexNavigation - Class in org.orekit.files.rinex.navigation

Represents a parsed RINEX navigation messages files.

RinexNavigation() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigation

Constructor.

RinexNavigationHeader - Class in org.orekit.files.rinex.navigation

Header for Rinex Navigation.

RinexNavigationHeader() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationHeader

Simple constructor.

RinexNavigationParser - Class in org.orekit.files.rinex.navigation

Parser for RINEX navigation messages files.

RinexNavigationParser() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationParser

Constructor.

RinexNavigationParser(TimeScales) - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationParser

Constructor.

RinexObservation - Class in org.orekit.files.rinex.observation

Container for Rinex observation file.

RinexObservation() - Constructor for class org.orekit.files.rinex.observation.RinexObservation

Simple constructor.

RinexObservationHeader - Class in org.orekit.files.rinex.observation

Container for Rinex observation file header.

RinexObservationHeader() - Constructor for class org.orekit.files.rinex.observation.RinexObservationHeader

Simple constructor.

RinexObservationParser - Class in org.orekit.files.rinex.observation

Parser for Rinex measurements files.

RinexObservationParser() - Constructor for class org.orekit.files.rinex.observation.RinexObservationParser

Simple constructor.

RinexObservationParser(TimeScales) - Constructor for class org.orekit.files.rinex.observation.RinexObservationParser

Create a RINEX loader/parser with the given source of RINEX auxiliary data files.

RinexObservationWriter - Class in org.orekit.files.rinex.observation

Writer for Rinex observation file.

RinexObservationWriter(Appendable, String) - Constructor for class org.orekit.files.rinex.observation.RinexObservationWriter

Simple constructor.

RinexUtils - Class in org.orekit.files.rinex.utils.parsing

Utilities for RINEX various messages files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Root element for XML messages.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Root element for XML messages.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm

Root element for XML files.

ROOT - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm

Root element for XML files.

ROOT22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ROOT22.

ROOT32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ROOT32.

ROOT44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ROOT44.

ROOT52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ROOT52.

ROOT54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ROOT54.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(PVCoordinates) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(PVCoordinates, PVCoordinates) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(PVCoordinates, PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(PVCoordinates, PVCoordinates) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame

Get the rotation from inertial to this encounter local orbital frame.

rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.LocalMagneticFieldFrame

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in class org.orekit.frames.LocalMagneticFieldFrame

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

rotationFromLOF(Field<T>, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF

Get the rotation from input local orbital frame to the instance.

rotationFromLOF(LOF, AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF

Get the rotation from input local orbital frame to the instance.

rotationFromLOF(LOFType, PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the rotation from input local orbital frame to the instance.

rotationFromLOF(Field<T>, LOFType, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType

Get the rotation from input local orbital frame to the instance.

rotationFromLOFInToLOFOut(Field<T>, LOF, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Static method in interface org.orekit.frames.LOF

Get the rotation from input to output local orbital frame.

rotationFromLOFInToLOFOut(LOF, LOF, AbsoluteDate, PVCoordinates) - Static method in interface org.orekit.frames.LOF

Get the rotation from input to output local orbital frame.

rotationShiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates

Get a time-shifted rotation.

rotationShiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted rotation.

RotationXmlTokenBuilder - Class in org.orekit.files.ccsds.ndm.adm

Builder for rotation angles and rates.

RotationXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder

Simple constructor.

roundIfNeeded(int, int) - Method in class org.orekit.time.DateTimeComponents

Round this date-time to the given precision if needed to prevent rounding up to an invalid seconds number.

ROW_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator

Default row dimension for position-velocity state covariance.

Rtcm1019 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

RTCM 1019 message: GPS Satellite Ephemeris Data.

Rtcm1019(int, Rtcm1019Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019

Constructor.

Rtcm1019Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for RTCM 1019 data.

Rtcm1019Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Constructor.

Rtcm1020 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

RTCM 1020 message: Glonass Satellite Ephemeris Data.

Rtcm1020(int, Rtcm1020Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020

Constructor.

Rtcm1020Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for RTCM 1020 data.

Rtcm1020Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Constructor.

Rtcm1042 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

RTCM 1042 message: Beidou Satellite Ephemeris Data.

Rtcm1042(int, Rtcm1042Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042

Constructor.

Rtcm1042Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for RTCM 1042 data.

Rtcm1042Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Constructor.

Rtcm1044 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

RTCM 1044 message: QZSS Satellite Ephemeris Data.

Rtcm1044(int, Rtcm1044Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044

Constructor.

Rtcm1044Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for RTCM 1044 data.

Rtcm1044Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Constructor.

Rtcm1045 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

RTCM 1045 message: Galileo F/NAV Satellite Ephemeris Data.

Rtcm1045(int, Rtcm1045Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045

Constructor.

Rtcm1045Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for RTCM 1045 data.

Rtcm1045Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Constructor.

Rtcm1057 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1057 message: GPS Orbit Correction Message.

Rtcm1057(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1057

Constructor.

Rtcm1058 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1057 message: GPS Clock Correction Message.

Rtcm1058(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1058

Constructor.

Rtcm1060 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1060 message: GPS Combined Orbit and Clock Correction Message.

Rtcm1060(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1060

Constructor.

Rtcm1063 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1063 message: GLONASS Orbit Correction Message.

Rtcm1063(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1063

Constructor.

Rtcm1064 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1064 message: GLONASS Clock Correction Message.

Rtcm1064(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1064

Constructor.

Rtcm1066 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1066 message: GLONASS Combined Orbit and Clock Correction Message.

Rtcm1066(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1066

Constructor.

Rtcm1240 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1240 message: Galileo Orbit Correction Message.

Rtcm1240(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1240

Constructor.

Rtcm1241 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1241 message: Galileo Clock Correction Message.

Rtcm1241(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1241

Constructor.

Rtcm1243 - Class in org.orekit.gnss.metric.messages.rtcm.correction

RTCM 1242 message: Combined Galileo Clock Correction Message.

Rtcm1243(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1243

Constructor.

RtcmClockCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM clock correction message type.

RtcmClockCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData

Constructor.

RtcmCombinedCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM combined corrections message type.

RtcmCombinedCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Constructor.

RtcmCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM corrections message type.

RtcmCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData

Constructor.

RtcmCorrectionHeader - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM Correction Message type header.

RtcmCorrectionHeader() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Constructor.

RtcmCorrectionMessage<H extends RtcmCorrectionHeader,D extends RtcmCorrectionData> - Class in org.orekit.gnss.metric.messages.rtcm.correction

The RTCM Correction Message types provide elements to calculate GNSS satellite corrections.

RtcmCorrectionMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage

Constructor.

RtcmData - Class in org.orekit.gnss.metric.messages.rtcm

Container for common data in RTCM message.

RtcmData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmData

Empty constructor.

RtcmDataField - Enum in org.orekit.gnss.metric.parser

Enum containing all intermediate level data fields that can be parsed to build a RTCM message.

RtcmEphemerisData - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Container for common data in RTCM ephemeris message type.

RtcmEphemerisData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData

Constructor.

RtcmEphemerisMessage<D extends RtcmEphemerisData> - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris

Base class for RTCM ephemeris messages.

RtcmEphemerisMessage(int, D) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage

Constructor.

RtcmMessage<D extends RtcmData> - Class in org.orekit.gnss.metric.messages.rtcm

Base class for RTCM messages.

RtcmMessage(int, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmMessage

Constructor.

RtcmMessagesParser - Class in org.orekit.gnss.metric.parser

Parser for RTCM encoded messages.

RtcmMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.RtcmMessagesParser

Constructor.

RtcmMessageType - Enum in org.orekit.gnss.metric.parser

Enum containing the supported RTCM messages types.

RtcmOrbitCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM orbit correction message type.

RtcmOrbitCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData

Constructor.

RtcmOrbitCorrectionHeader - Class in org.orekit.gnss.metric.messages.rtcm.correction

Container for common data in RTCM Orbit Correction Message type header.

RtcmOrbitCorrectionHeader() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader

Constructor.

RTNCovariance - Class in org.orekit.files.ccsds.ndm.cdm

Container for RTN covariance matrix data.

RTNCovariance() - Constructor for class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Simple constructor.

RTNCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM covariance matrix entries.

RTNCovarianceWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for RTN covariance matrix data block for CCSDS Conjunction Data Messages.

run() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor

ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter

Convert a range expressed in Range Units.

ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter

Convert a range expressed in Range Units.

S

S - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S.

S2 - Static variable in class org.orekit.models.earth.displacement.Tide

S₂ tide.

s4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

s* new value for the contant s.

s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

s* new value for the contant s.

S_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_2FASX4.

S_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_3FASX6.

S_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_FASX2.

S_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_G22.

S_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_G32.

S_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_G44.

S_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_G52.

S_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

S_G54.

S_PER_SC_N - Static variable in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Converters for Klobuchar parameters.

SaastamoinenModel - Class in org.orekit.models.earth.troposphere

The modified Saastamoinen model.

SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel

Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.

SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel

Create a new Saastamoinen model for the troposphere using the given environmental conditions.

SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel

Create a new Saastamoinen model for the troposphere using the given environmental conditions.

sameDimension(Unit) - Method in class org.orekit.utils.units.Unit

Check if a unit has the same dimension as another unit.

sameDimensionSI() - Method in class org.orekit.utils.units.Unit

Create the SI unit with same dimension.

sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Sample a zone of interest into a grid sample of geodetic points.

SatelliteAntenna - Class in org.orekit.gnss.antenna

GNSS satellite antenna model.

SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna

Simple constructor.

SatelliteClockScale - Class in org.orekit.time

Scale for on-board clock.

SatelliteClockScale(String, AbsoluteDate, TimeScale, double, double) - Constructor for class org.orekit.time.SatelliteClockScale

Create a linear model for satellite clock.

SatelliteSystem - Enum in org.orekit.gnss

Enumerate for satellite system.

SatelliteType - Enum in org.orekit.gnss.antenna

Enumerate for satellite types.

SatInSystem - Class in org.orekit.gnss

Container for satellite system and PRN.

SatInSystem(SatelliteSystem, int) - Constructor for class org.orekit.gnss.SatInSystem

Simple constructor.

SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Saturn.

SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants

WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².

SbasId - Enum in org.orekit.files.rinex.navigation

Enumerate for the SBAS ids.

SBASNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data

Container for data contained in a SBAS navigation message.

SBASNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Constructor.

SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data

This interface provides the minimal set of orbital elements needed by the SBASPropagator.

SBASPropagator - Class in org.orekit.propagation.analytical.gnss

This class aims at propagating a SBAS orbit from SBASOrbitalElements.

SBASPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss

This nested class aims at building a SBASPropagator.

SBASPropagatorBuilder(SBASOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Initializes the builder.

SBASPropagatorBuilder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder

Initializes the builder.

scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType

Compute scaling factor for parameters drivers.

scale(String, double) - Method in class org.orekit.utils.units.Unit

Scale a unit.

SCALE_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm

Default value for scale.

scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter scale has been changed.

ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion

Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.

ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Constructor with min/max deviation for the scale factors.

scaledIncrement(double, DoubleArrayDictionary.Entry) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Increment the value with another scaled entry.

scaledIncrement(T, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Increment the value with another scaled entry.

scaledIncrement(double, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Increment the value with another scaled entry.

ScaleFactorCorrection - Class in org.orekit.files.rinex.observation

Scale Factor to be applied.

ScaleFactorCorrection(double, List<ObservationType>) - Constructor for class org.orekit.files.rinex.observation.ScaleFactorCorrection

Simple constructor.

Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation

Interface for generating measurements sequences.

ScreenType - Enum in org.orekit.files.ccsds.ndm.cdm

Screening type options allowed in CCSDS Conjunction Data Messages.

ScreenVolumeFrame - Enum in org.orekit.files.ccsds.ndm.cdm

Screening volume frame possibilities used in CCSDS Conjunction Data Messages.

ScreenVolumeShape - Enum in org.orekit.files.ccsds.ndm.cdm

Screening volume shape possibilities used in CCSDS Conjunction Data Messages.

SDP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for SDP4 type of ephemeris.

SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP4 type of ephemeris.

SDP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for SDP8 type of ephemeris.

SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP8 type of ephemeris.

SECOND - Static variable in class org.orekit.utils.units.Unit

Second unit.

Section - Interface in org.orekit.files.ccsds.section

Top level interface for all CCSDS message sections.

SecularAndHarmonic - Class in org.orekit.utils

Class for fitting evolution of osculating orbital parameters.

SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic

Simple constructor.

Segment<M extends Metadata,D extends Data> - Class in org.orekit.files.ccsds.section

NDM segments are (Metadata, Data) pairs.

Segment(M, D) - Constructor for class org.orekit.files.ccsds.section.Segment

Constructor.

SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter

Empty constructor.

SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter

Empty constructor.

select(Unit, Unit) - Method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior

Select the unit to use for interpreting parsed value.

select(DataSource) - Static method in class org.orekit.files.ccsds.utils.lexical.LexicalAnalyzerSelector

Select a LexicalAnalyzer for a DataSource based on content.

selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector

Select dates within an interval.

selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector

Select dates within an interval.

selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector

Select dates within an interval.

selectExtrapolator(FieldTLE<T>, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(FieldTLE<T>, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter selection status has been changed.

selectPredefined(int, int) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Select a predefined transform between two years.

selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType

Get next function transformer in the specified direction.

SEMI_CIRCLE - Static variable in class org.orekit.gnss.metric.parser.Units

Semi-circles units.

SemiAnalyticalKalmanEstimator - Class in org.orekit.estimation.sequential

Implementation of an Extended Semi-analytical Kalman Filter (ESKF) to perform orbit determination.

SemiAnalyticalKalmanEstimator(MatrixDecomposer, DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator

Kalman filter estimator constructor (package private).

SemiAnalyticalKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential

Builder for a Semi-analytical Kalman Filter.

SemiAnalyticalKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder

Default constructor.

SemiAnalyticalKalmanModel - Class in org.orekit.estimation.sequential

Process model to use with a SemiAnalyticalKalmanEstimator.

SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Kalman process model constructor (package private).

SemiAnalyticalMeasurementHandler - Class in org.orekit.estimation.sequential

Step handler picking up measurements for both SemiAnalyticalUnscentedKalmanEstimator and SemiAnalyticalKalmanEstimator.

SemiAnalyticalMeasurementHandler(SemiAnalyticalProcess, KalmanFilter<MeasurementDecorator>, List<ObservedMeasurement<?>>, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler

Simple constructor.

SemiAnalyticalMeasurementHandler(SemiAnalyticalProcess, KalmanFilter<MeasurementDecorator>, List<ObservedMeasurement<?>>, AbsoluteDate, boolean) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler

Simple constructor.

SemiAnalyticalProcess - Interface in org.orekit.estimation.sequential

Interface for both SemiAnalyticalUnscentedKalmanModel and SemiAnalyticalKalmanModel.

SemiAnalyticalUnscentedKalmanEstimator - Class in org.orekit.estimation.sequential

Implementation of an Unscented Semi-analytical Kalman filter (USKF) to perform orbit determination.

SemiAnalyticalUnscentedKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential

Builder for an Unscented Semi-analytical Kalman filter estimator.

SemiAnalyticalUnscentedKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Default constructor.

SemiAnalyticalUnscentedKalmanModel - Class in org.orekit.estimation.sequential

Class defining the process model dynamics to use with a SemiAnalyticalUnscentedKalmanEstimator.

SemiAnalyticalUnscentedKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Unscented Kalman process model constructor (package private).

SEMParser - Class in org.orekit.gnss

This class reads SEM almanac files and provides GPS almanacs.

SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser

Simple constructor.

SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser

Create a SEM loader/parser with the given source of SEM auxiliary data files.

SequentialBatchLSEstimator - Class in org.orekit.estimation.leastsquares

Sequential least squares estimator for orbit determination.

SequentialBatchLSEstimator(SequentialGaussNewtonOptimizer, PropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.SequentialBatchLSEstimator

Simple constructor.

SessionStatistics(String, double, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.SessionStatistics

Constructor.

setA(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit semi-major axis.

setA(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Set acceleration component.

setA0(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the constant term of the offset.

setA1(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

set the linear term of the offset.

setA2(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the quadratic term of the offset.

setA2b(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Set rotation direction.

setAcceleration(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set acceleration component.

setAccelerationDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ angular off-nominal acceleration direction.

setAccelerationInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set interpolation mode between current and next acceleration line.

setAccelerationMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ percent error on acceleration magnitude.

setAccuracy(int, double) - Method in class org.orekit.files.sp3.SP3Header

Set the accuracy.

setAccuracyProvider(AccuracyProvider) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData

Set the accuracy provider of the ephemeris message.

setAcmDataElements(List<AcmElements>) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the list of elements of information data blocks included in this message.

setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.

setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set actual time span used for the OD of the object.

setActuatorUsed(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set actuator used.

setAdditionalParametersBlock(AdditionalParameters) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Set the additional parameters logical block.

setAdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Unique identifier of Attitude Data Message linked to this Orbit Data Message.

setAdmMsgLink(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.

setADot(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for the change rate in semi-major axis.

setADot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for the change rate in semi-major axis.

setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body reference radius.

setAf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the SV Clock Bias Correction Coefficient (s).

setAf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the SV Clock Drift Correction Coefficient (s/s).

setAf2(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Drift Rate Correction Coefficient (s/s²).

setAgency(String) - Method in class org.orekit.files.sp3.SP3Header

Set the agency string for this SP3 file.

setAgencyName(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the agency name.

setAgencyName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Setter for the agency name.

setAGf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Setter for the SV clock bias.

setAGf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Setter for the SV relative frequency.

setAGoM(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the SGP4-XP solar radiation pressure-like coefficient Aγ/m.

setAi0(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Set aᵢ₀.

setAi1(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Set aᵢ₁.

setAi2(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Set aᵢ₂.

setAlbedoGridSize(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set albedo grid size.

setAlbedoModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set albedo model.

setAlphaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage

Set one α coefficient.

setAlphaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Set one α coefficient.

setAltCovRefFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the name of the reference frame in which the alternate covariance data are given.

setAltCovType(AltCovarianceType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the flag indicating the type of alternate covariance information provided.

setAlternateNames(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the alternate names for this space object.

setAmplifierBandwidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the amplifier bandwidth.

setAmplifierGain(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the amplifier gain.

setAmplifierInUse(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the amplifier in use.

setAnalysisCenterID(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the analysis center ID.

setAnalysisCenterName(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the analysis center name.

setAngleType(AngleType) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the angleType.

setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid

Set the angular convergence threshold.

setAngvelFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set frame in which angular velocities are specified.

setAngVelX(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Set the angular velocity around X axis (rad/s).

setAngVelY(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Set the angular velocity around Y axis (rad/s).

setAngVelZ(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Set the angular velocity around Z axis (rad/s).

setAnomaly(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit anomaly.

setAnomalyType(PositionAngleType) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the type of anomaly.

setAntennaAzimuth(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the azimuth of the zero direction of a fixed antenna.

setAntennaBSight(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the antenna B.Sight.

setAntennaHeight(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the antenna height.

setAntennaNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the number of the antenna.

setAntennaPhaseCenter(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the antenna phasecenter.

setAntennaReferencePoint(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the position of antenna reference point for antenna on vehicle.

setAntennaType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the type of the antenna.

setAntennaZeroDirection(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the zero direction of antenna.

setAODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Setter for the age of data clock.

setAODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Setter for the age of data ephemeris.

setApoapsisAltitude(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the distance of the furthest point in the objects orbit above the equatorial radius of the central body.

setApplicableWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the applicable wavelength.

setAppliedVoltage(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the applied voltage.

setApproachAngle(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.

setApproxPos(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the Approximate Marker Position.

setAreAdditionalDataAvailable(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the flag indicating if additional parameters are in the message.

setAreaDRG(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the effective area of the object exposed to atmospheric drag.

setAreaPC(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the actual area of the object.

setAreaPCMax(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the maximum area for the object to be used to compute the collision probability.

setAreaPCMin(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Get the minimum area of the object to be used to compute the collision probability.

setAreaSRP(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the effective area of the object exposed to solar radiation pressure.

setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set name of atmospheric model.

setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set name of atmospheric model.

setAttBasis(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set basis of this attitude state time history data.

setAttBasisID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set identification number of the orbit determination or simulation upon which this attitude is based.

setAttID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set attitude identification number.

setAttitudeActuatorType(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the type of actuator for attitude control.

setAttitudeControlAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the accuracy of attitude control.

setAttitudeControlMode(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the attitude control mode.

setAttitudeKnowledgeAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the accuracy of attitude knowledge.

setAttitudePointingAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the overall accuracy of spacecraft to maintain attitude.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Set the attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.StateMapper

Set the attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set attitude provider.

setAttitudeStates(AttitudeElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set attitude states.

setAttitudeType(AttitudeElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set attitude element set type.

setAttitudeType(AttitudeType) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the format of the data lines in the message.

setAttPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set identification number of previous attitude.

setBeamDivergence(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the beam divergence.

setBeginTime(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set start time of actual maneuver, relative to t₀.

setBeidouNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Set the Beidou navigation message.

setBeidouToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Set the Beidou time of clock.

setBetaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Set one β coefficient.

setBGDE1E5a(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the E1/E5a broadcast group delay (s).

setBGDE5bE1(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the E5b/E1 broadcast group delay (s).

setBiasMode(String) - Method in class org.orekit.files.sinex.DcbDescription

Set the bias mode.

setBN(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS B_n Word.

setBolDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the total ΔV capability at beginning of life.

setBStar(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the SGP/SGP4 drag-like coefficient.

setBTerm(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the SGP4-XP drag-like coefficient.

setBusModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the bus model name.

setC1cCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the code phase bias correction for GLONASS ObservationType.C1C signal.

setC1pCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the code phase bias correction for GLONASS ObservationType.C1P signal.

setC2cCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the code phase bias correction for GLONASS ObservationType.C2C signal.

setC2pCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the code phase bias correction for GLONASS ObservationType.C2P signal.

setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration

Set the number of slots to use in caches.

setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the specification of satellite catalog source.

setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the satellite catalog name used for object.

setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the specification of satellite catalog source.

setCDAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the object’s Cd x A/m used to propagate the state vector and covariance to TCA.

setCdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.

setCdrgdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,7] in covariance matrix (with index starting at 1).

setCdrgdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,7] in covariance matrix (with index starting at 1).

setCdrgn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,3] in covariance matrix (with index starting at 1).

setCdrgndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,6] in covariance matrix (with index starting at 1).

setCdrgr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,1] in covariance matrix (with index starting at 1).

setCdrgrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,4] in covariance matrix (with index starting at 1).

setCdrgt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,2] in covariance matrix (with index starting at 1).

setCdrgtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [7,5] in covariance matrix (with index starting at 1).

setCdrgx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,1] in covariance matrix (with index starting at 1).

setCdrgxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,4] in covariance matrix (with index starting at 1).

setCdrgy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,2] in covariance matrix (with index starting at 1).

setCdrgydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,5] in covariance matrix (with index starting at 1).

setCdrgz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,3] in covariance matrix (with index starting at 1).

setCdrgzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [7,6] in covariance matrix (with index starting at 1).

setCelestialSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the source and version of celestial body (e.g.

setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Set the body at origin of reference frame.

setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the origin of reference frame.

setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Set the origin of reference frame.

setCenterMass(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the current center of mass of vehicle in body fixed coordinate system.

setCenterOfMassOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the approximate center of mass to reflector offset.

setCenterOfPressure(Vector3D) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set the location of center of pressure.

setCenterOfPressureReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set reference frame for center of pressure.

setCentralBodyRotation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set central body angular rotation rate.

setCic(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for te Cic parameter.

setCis(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Cis parameter.

setClassification(String) - Method in class org.orekit.files.ccsds.section.Header

Set the classification/caveats.

setClassificationType(char) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the classification type.

setClkOffset(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the realtime-derived receiver clock offset.

setClockBase(double) - Method in class org.orekit.files.sp3.SP3Header

Set the base for clock/clock-rate accuracy.

setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData

Set the clock correction data.

setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Set the clock correction data.

setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data

Set the clock correction data.

setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Set the clock correction data.

setClosedOrbitConstraint(boolean) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Set the constraint of a closed orbit or not.

setCndotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,3] in covariance matrix (with index starting at 1).

setCndotndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,6] in covariance matrix (with index starting at 1).

setCndotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,1] in covariance matrix (with index starting at 1).

setCndotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,4] in covariance matrix (with index starting at 1).

setCndott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,2] in covariance matrix (with index starting at 1).

setCndottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [6,5] in covariance matrix (with index starting at 1).

setCnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Set the cosine parameters of spherical harmonics expansion of degree N and order M.

setCnn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [3,3] in covariance matrix (with index starting at 1).

setCnr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [3,1] in covariance matrix (with index starting at 1).

setCnt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [3,2] in covariance matrix (with index starting at 1).

setCollisionPercentile(int[]) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.

setCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.

setCollisionProbaMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the method that was used to calculate the collision probability.

setComparator(Comparator<IntegerLeastSquareSolution>) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Set a custom comparator for integer least square solutions comparison.

setComponents(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Set the components (config ids) for system configuration.

setConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set confidence metric.

setConfigurationId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

Set the configuration ID.

setConfigurationRecords(CRDConfiguration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Set the configuration records for the current data block.

setConjunctionId(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Originator’s ID that uniquely identifies the conjunction to which the message refers.

setConsiderN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of consider parameters.

setConsiderParameters(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set description of consider parameters.

setConstellation(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the name of the constellation this space object belongs to.

setContext(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Reset context binding.

setContext(ContextBinding) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Reset context binding.

setContinuousEstimation(boolean) - Method in class org.orekit.utils.ParameterDriver

Set parameter estimation to continuous, by default step estimation.

setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set a custom convergence checker.

setConvergenceRMS(double) - Method in class org.orekit.utils.SecularAndHarmonic

Set RMS for convergence.

setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3Header

Set the coordinate system used for the orbit entries.

setCorrectionAberrationDiurnal(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the diurnal aberration correction.

setCorrectionAberrationYearly(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the yearly aberration correction.

setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionAngle1.

setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionAngle2.

setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionDoppler.

setCorrectionMagnitude(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the magnitude correction.

setCorrectionRcs(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the radar cross section correction.

setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionReceive.

setCorrectionsApplied(CorrectionApplied) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionApplied.

setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the correctionTransmit.

setCountry(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the name of the country where the space object owner is based.

setCovarianceMatrixBlock(RTNCovariance) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Set the additional covariance metadata logical block.

setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set an entry in the RTN covariance matrix.

setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set an entry in the XYZ covariance matrix.

setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Set an entry in the Position/Velocity covariance matrix.

setCovarianceMethod(CovarianceMethod) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the method name used to calculate covariance during OD.

setCovarianceSource(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the source of the covariance data.

setCovarianceType(AttitudeCovarianceType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set type of attitude error state.

setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set basis of this covariance time history data.

setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set basis of this covariance time history data.

setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set identification number of the orbit determination or simulation upon which this covariance is based.

setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set identification number of the orbit determination or simulation upon which this covariance is based.

setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the measure of the confidence in the covariance errors matching reality.

setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set the measure of confidence in covariance error matching reality.

setCovConfidenceMethod(String) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the method used for the calculation of COV_CONFIDENCE.

setCovFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set epoch of the covariance reference frame.

setCovID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set covariance identification number.

setCovID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set covariance identification number.

setCovNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set identification number of next covariance.

setCovOrdering(Ordering) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set covariance ordering.

setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set identification number of previous covariance.

setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set identification number of previous covariance.

setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set reference frame of the covariance.

setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set reference frame of the covariance.

setCovScaleMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set the maximum scale factor to apply to achieve realism.

setCovScaleMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set the minimum scale factor to apply to achieve realism.

setCovType(AttitudeCovarianceType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Set covariance element set type.

setCovType(OrbitElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set covariance element set type.

setCovUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Set covariance element set units.

setCRAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the object’s Cr x A/m used to propagate the state vector and covariance to TCA.

setCrc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Crc parameter.

setCrdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [4, 3] in covariance matrix (with index starting at 1).

setCrdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [4,1] in covariance matrix (with index starting at 1).

setCrdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [4, 4] in covariance matrix (with index starting at 1).

setCrdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [4, 2] in covariance matrix (with index starting at 1).

setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.section.Header

Set the message creation date and time in UTC.

setCreationDate(AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the creation date.

setCreationDate(AbsoluteDate) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the creation date.

setCreationDateComponents(DateTimeComponents) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the creation date as a string.

setCreationDateString(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the creation date as a string.

setCreationTimeString(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the creation time as a string.

setCreationTimeZone(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the creation time zone.

setCreationTimeZoneString(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the creation time zone.

setCrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [1,1] in covariance matrix (with index starting at 1).

setCrs(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Crs parameter.

setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header

Set the Global/Regional CRS Indicator.

setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header

Set the Global/Regional CRS Indicator.

setcScaleFactor(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the (median) suggested covariance scale factor.

setcScaleFactorMax(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

set the maximum suggested covariance scale factor.

setcScaleFactorMin(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the minimum suggested covariance scale factor.

setCsig3eigvec3(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance

Set the Sigma/Eigenvectors Covariance data.

setCsrpdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,7] in covariance matrix (with index starting at 1).

setCsrpdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,7] in covariance matrix (with index starting at 1).

setCsrpn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,3] in covariance matrix (with index starting at 1).

setCsrpndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,6] in covariance matrix (with index starting at 1).

setCsrpr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,1] in covariance matrix (with index starting at 1).

setCsrprdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,4] in covariance matrix (with index starting at 1).

setCsrpsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,8] in covariance matrix (with index starting at 1).

setCsrpsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,8] in covariance matrix (with index starting at 1).

setCsrpt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,2] in covariance matrix (with index starting at 1).

setCsrptdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [8,5] in covariance matrix (with index starting at 1).

setCsrpx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,1] in covariance matrix (with index starting at 1).

setCsrpxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,4] in covariance matrix (with index starting at 1).

setCsrpy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,2] in covariance matrix (with index starting at 1).

setCsrpydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,5] in covariance matrix (with index starting at 1).

setCsrpz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,3] in covariance matrix (with index starting at 1).

setCsrpzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [8,6] in covariance matrix (with index starting at 1).

setCtdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [5,3] in covariance matrix (with index starting at 1).

setCtdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [5,1] in covariance matrix (with index starting at 1).

setCtdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [5,4] in covariance matrix (with index starting at 1).

setCtdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [5,2] in covariance matrix (with index starting at 1).

setCtdottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [5,5] in covariance matrix (with index starting at 1).

setCthrdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,7] in covariance matrix (with index starting at 1).

setCthrdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,7] in covariance matrix (with index starting at 1).

setCthrn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,3] in covariance matrix (with index starting at 1).

setCthrndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,6] in covariance matrix (with index starting at 1).

setCthrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,1] in covariance matrix (with index starting at 1).

setCthrrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,4] in covariance matrix (with index starting at 1).

setCthrsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,8] in covariance matrix (with index starting at 1).

setCthrsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,8] in covariance matrix (with index starting at 1).

setCthrt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,2] in covariance matrix (with index starting at 1).

setCthrtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,5] in covariance matrix (with index starting at 1).

setCthrthr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [9,9] in covariance matrix (with index starting at 1).

setCthrthr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,9] in covariance matrix (with index starting at 1).

setCthrx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,1] in covariance matrix (with index starting at 1).

setCthrxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,4] in covariance matrix (with index starting at 1).

setCthry(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,2] in covariance matrix (with index starting at 1).

setCthrydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,5] in covariance matrix (with index starting at 1).

setCthrz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,3] in covariance matrix (with index starting at 1).

setCthrzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [9,6] in covariance matrix (with index starting at 1).

setCtr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [2,1] in covariance matrix (with index starting at 1).

setCtt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Set the object [2,2] in covariance matrix (with index starting at 1).

setCuc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Cuc parameter.

setCus(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Cus parameter.

setCxdotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [4,1] in covariance matrix (with index starting at 1).

setCxdotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [4, 4] in covariance matrix (with index starting at 1).

setCxdoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [4, 2] in covariance matrix (with index starting at 1).

setCxdotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [4, 3] in covariance matrix (with index starting at 1).

setCxx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [1,1] in covariance matrix (with index starting at 1).

setCydotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [5,1] in covariance matrix (with index starting at 1).

setCydotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [5,4] in covariance matrix (with index starting at 1).

setCydoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [5,2] in covariance matrix (with index starting at 1).

setCydotydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [5,5] in covariance matrix (with index starting at 1).

setCydotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [5,3] in covariance matrix (with index starting at 1).

setCyx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [2,1] in covariance matrix (with index starting at 1).

setCyy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [2,2] in covariance matrix (with index starting at 1).

setCzdotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,1] in covariance matrix (with index starting at 1).

setCzdotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,4] in covariance matrix (with index starting at 1).

setCzdoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,2] in covariance matrix (with index starting at 1).

setCzdotydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,5] in covariance matrix (with index starting at 1).

setCzdotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,3] in covariance matrix (with index starting at 1).

setCzdotzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [6,6] in covariance matrix (with index starting at 1).

setCzx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [3,1] in covariance matrix (with index starting at 1).

setCzy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [3,2] in covariance matrix (with index starting at 1).

setCzz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Set the object [3,3] in covariance matrix (with index starting at 1).

setDarkCount(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the dark count.

setDataQuality(DataQuality) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the dataQuality.

setDataReleaseFlag(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the flag indicating the data release.

setDataSource(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the data source.

setDataType(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the data type.

setDataTypes(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set observation data types used.

setDataTypes(List<ObservationType>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the data types in the data section.

setDataUsed(List<DataUsed>) - Method in class org.orekit.files.sp3.SP3Header

Set the data used indicator for this SP3 file.

setDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set date.

setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the reference date of the ephemeris.

setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the reference epoch.

setDateAndTime(String) - Method in class org.orekit.files.ilrs.CRDHeader

Set the string value of date and time.

setDayFraction(double) - Method in class org.orekit.files.sp3.SP3Header

Set the day fraction for this SP3 file.

setDcBodyFrame(SpacecraftBodyFrame) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set spacecraft body frame in which OrbitManeuverHistoryMetadata.getDcBodyTrigger() is specified.

setDcBodyTrigger(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set direction in body frame for triggering duty cycle.

setDcExecStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the start time of initial duty cycle-based maneuver execution.

setDcExecStop(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the end time of final duty cycle-based maneuver execution.

setDcMaxCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the maximum number of "ON" duty cycles.

setDcMinCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the minimum number of "ON" duty cycles.

setDcPhaseStartAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set phase angle of pulse start.

setDcPhaseStopAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set phase angle of pulse stop.

setDcpSensitivityVectorPosition(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the DCP sensitivity vector (position errors at TCA).

setDcpSensitivityVectorVelocity(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the DCP sensitivity vector (velocity errors at TCA).

setDcRefDir(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set reference direction for triggering duty cycle.

setDcRefTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set duty cycle thrust reference time.

setDcTimePulseDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set duty cycle pulse "ON" duration.

setDcTimePulsePeriod(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set duty cycle elapsed time between start of a pulse and start of next pulse.

setDcType(DutyCycleType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set type of duty cycle.

setDcWindowClose(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the end time of duty cycle-based maneuver window.

setDcWindowOpen(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the start time of duty cycle-based maneuver window.

setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext

Set the default data context that is used to implement Orekit's static factories.

setDefinedTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the time system defined by this message.

setDeltaInc(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the the correction of orbit reference inclination at reference time.

setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Set mass change during maneuver.

setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set mass change.

setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Set mass change during maneuver (value is < 0).

setDeltaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the delta of satellite mean motion.

setDeltaN0Dot(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for change rate in Δn₀.

setDeltaN0Dot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for change rate in Δn₀.

setDeltaSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the difference between the square root of the semi-major axis and the square root of the nominal semi-major axis.

setDeltaTN(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the deltaTauN value.

setDensityForecastUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the atmospheric density forecast error.

setDeployDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ angular off-nominal deployment vector direction.

setDeployDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set velocity increment component of deployed "child" object.

setDeployDvCda(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.

setDeployDvRatio(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set ratio of child-to-host ΔV vectors.

setDeployDvSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ percent error on deployment ΔV magnitude.

setDeployId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set identifier of resulting "child" object deployed from this host.

setDeployMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set decrement in host mass as a result of deployment.

setDescription(DcbDescription) - Method in class org.orekit.files.sinex.DcbSatellite

Set the data contained in "DCB/DESCRIPTION" block of the Sinex file.

setDescription(DcbDescription) - Method in class org.orekit.files.sinex.DcbStation

Set the data contained in "DCB/DESCRIPTION" block of the Sinex file.

setDetectorId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the detector configuration ID.

setDetectorType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the detector type.

setDeterminationMethod(String) - Method in class org.orekit.files.sinex.DcbDescription

Set the determination mode used to generate the bias results.

setDockedWith(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the other space objects this object is docked to.

setDoi(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the Digital Object Information.

setDomes(String) - Method in class org.orekit.files.sinex.Station

Set the DOMES number.

setDopplerCountBias(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the Doppler count bias.

setDopplerCountRollover(boolean) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the indicator for Doppler count rollover.

setDopplerCountScale(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the Doppler count Scale.

setDragArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Set the drag area.

setDragCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Set the drag coefficient.

setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set the the drag coefficient.

setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the the nominal drag coefficient.

setDragConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.

setDragUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the drag coefficient 1σ uncertainty.

setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set the mass without propellant.

setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the mass without propellant.

setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set duration.

setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Set duration (value is 0 for impulsive maneuver).

setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set duration.

setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Set duration (value is 0 for impulsive maneuver).

setDut1(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the ΔUT₁.

setDut1Dot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the ΔUT₁ first derivative.

setDut1DotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the ΔUT₁ second derivative.

setDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set velocity increment component.

setDV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Set velocity increment component.

setDvDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ angular off-nominal ΔV direction.

setDvMagSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ percent error on ΔV magnitude.

setE(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit eccentricity.

setE(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter the eccentricity.

setEarthTides(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set Enum YesNoUnknown that indicates if Earth and ocean tides are taken into account or not.

setEccentricities(Vector2D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the eccentricities of antenna center.

setEccRefSystem(Station.ReferenceSystem) - Method in class org.orekit.files.sinex.Station

Set the reference system used to define the eccentricity vector (local or cartesian).

setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set an element of the matrix.

setElementSetNo(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the element set number for this satellite.

setEn(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Get the GLONASS E_n Word.

setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Enable or disable a measurement.

setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement

Enable or disable a measurement.

setEndEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the ending epoch (UTC).

setEndTagSeen(boolean) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Set the flag for XML end tag.

setEndTime(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set end time of actual maneuver, relative to t₀.

setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory

Set the threshold to check EOP continuity.

setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop

Set the threshold to check EOP continuity.

setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames

Set the threshold to check EOP continuity.

setEopSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the source and version of Earth Orientation Parameters.

setEphemerisNames(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the external ephemeris names for participants.

setEphemerisType(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the ephemeris type.

setEphemName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the name of external ephemeris used for OD.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Set matrix epoch.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set epoch of state vector, Keplerian elements and covariance matrix data.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set time tag for orbit determination solved-for state.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Set epoch of state vector, Keplerian elements and covariance matrix data.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Set the coordinates reference epoch.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3Header

Set the epoch of the SP3 file.

setEpochDelayCorrection(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the epoch delay correction.

setEpochEigenInt(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.

setEpochEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set positional error ellipsoid 1σ major eigenvalue at the epoch of OD.

setEpochEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.

setEpochFreedom(int, boolean) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Set the epoch of a patch point to free or not.

setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting

Set the epoch of a patch point to free or not.

setEpochIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the epoch identifier.

setEpochIgnition(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Set epoch ignition.

setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3Header

Set the epoch interval for this SP3 file.

setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Set epoch start.

setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the epoch to which all relative times are referenced in data blocks.

setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the epoch to which all relative times are referenced in data blocks.

setEpochTime1s(double) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the Epoch Time 1s.

setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the time of clock epoch.

setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the time of clock epoch.

setEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set oblate spheroid equatorial radius of central body.

setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Set the estimated value.

setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set the rotation order for Euler angles.

setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set the rotation order for Euler angles.

setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the rotation order for Euler angles.

setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the rotation order for Euler angles.

setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Set the counter for evaluations.

setExternalClockReference(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the external clock reference.

setExternalSignalProcessing(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the external signal processing.

setFallback(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Set fallback processing state.

setField(int, int, int, int, int[]) - Method in class org.orekit.gnss.rflink.gps.SubFrame

Set a field.

setField(int, int, int, int, int, int, int, int[]) - Method in class org.orekit.gnss.rflink.gps.SubFrame

Set a field.

setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.ilrs.CPF

Set the derivatives filter.

setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.sp3.SP3Header

Set the derivatives filter.

setFitInterval(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the fit interval.

setFix(int, int, double, double, double, double, double) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Set GPS fix data to send as NMEA sentence to Ntrip caster if required.

setFixedF10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.

setFixedF10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.

setFixedGeomagneticAp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.

setFixedGeomagneticDst(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.

setFixedGeomagneticKp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.

setFixedM10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux daily proxy M10.7.

setFixedM10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.

setFixedS10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux daily proxy S10.7.

setFixedS10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.

setFixedY10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux daily proxy Y10.7.

setFixedY10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.

setFlags(int) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Set the disturbance flags.

setFormat(String) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the file format.

setFormatVersion(double) - Method in class org.orekit.files.ccsds.section.Header

Set the CCSDS NDM (ADM, ODM or TDM) format version.

setFormatVersion(double) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the format version.

setFormatVersion(double) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the format version.

setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Set frame in which angular velocities are specified.

setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Set frame in which inertia is specified.

setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Set Coordinate system for the torque vector.

setFrameA(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Set frame A.

setFrameB(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

Set frame B.

setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Set epoch of reference frame, if not intrinsic to the definition of the reference frame.

setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Set epoch of reference frame, if not intrinsic to the definition of the reference frame.

setFrameName(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the frame name.

setFreqOffset(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the freqOffset.

setFrequencyNumber(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Setter for the frequency number.

setFrequencySource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the frequency source.

setFT(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS F_T Word.

setGalileoDataValidityStatus(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Set the Galileo data validity status.

setGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Set the Galileo navigation message.

setGalileoToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data

Set the Galileo time of clock.

setGammaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Setter for the SV relative frequency bias.

setGdop(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set generalize Dilution Of Precision.

setGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the Glonass navigation message.

setGm(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set gravitational coefficient of attracting body.

setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Set the GNSS IOD.

setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData

Set the GNSS IOD.

setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data

Set the GNSS IOD.

setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Set the GNSS IOD.

setGpsCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Set the GPS code on L2.

setGpsFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Set the GPS fit interval.

setGpsL2PDataFlag(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Set the GPS L2 P-code data flag.

setGpsNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Set the GPS navigation message.

setGpsToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data

Set the GPS time of clock.

setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3Header

Set the GPS week of the SP3 file.

setGravitationalAssist(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the origin of gravitational assist.

setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set gravity model.

setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set gravity model.

setGroupDelayDifference(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Set group delay difference.

setHandlers(List<EventHandler>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler

Change handlers list with user input.

setHbr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the object hard body radius.

setHeader(H) - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Set the header.

setHeader(CRDHeader) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock

Set the header for the current data block.

setHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the health status.

setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac

Sets the health status.

setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for health.

setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Sets the health status.

setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Sets the health status.

setHealthAvailabilityIndicator(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the flag indicating if GLONASS almanac health is available.

setHealthE1(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the E1-B/C signal health status.

setHealthE5a(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the E5a signal health status.

setHealthE5b(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the E5b signal health status.

setHealthFlags(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Set health flag.

setHeightIonosphericLayer(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Set the height of the ionospheric layer.

setHighRateClockCorrection(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data

Set the high rate clock correction to be added to the polynomial clock correction.

setHumiSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the humidity sensor manufacturer.

setHumiSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the humidity sensor model.

setHumiSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the humidity sensor serial number.

setI(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit inclination.

setI0(double, double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac

Sets the Inclination Angle at Reference Time (rad).

setI0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the Inclination Angle at Reference Time (rad).

setId(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set identification number.

setID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set maneuver identification number.

setId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set identification number.

setIDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Rate of Inclination Angle (rad/s).

setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set the flag to ignore or not the creation of a NewtonianAttraction.

setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the flag to ignore or not the creation of a NewtonianAttraction.

setIlrsSatelliteId(String) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the IRLS satellite ID (based on COSPAR ID).

setInclination(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the angle between the objects orbit plane and the orbit centers equatorial plane.

setIndexedRotationAngle(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the Euler angle about axis.

setIndexedRotationRate(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the rate of Euler angle about axis.

setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set an entry in the inertia matrix.

setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Set an entry in the inertia matrix.

setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set an entry in the inertia matrix.

setInertiaReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set reference frame for inertia.

setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations

Set the Jacobian with respect to state into a one-dimensional additional state array.

setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations

Method adding the standard initial values of the additional state to the initial spacecraft state.

setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set the initial state.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the initial state.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state with osculating orbital elements.

setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state.

setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the initial state with osculating orbital elements.

setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the initial state.

setInitialWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the total mass at beginning of life.

setInRotationAngles(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set flag for rotation angle parsing.

setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the integrationInterval.

setIntegrationRef(IntegrationReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the integrationRef.

setIntegrityFlags(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for B1C integrity flags.

setInternationalDes(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the international designator used for object.

setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the international designator for the object.

setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the international designator for the object.

setInterpMethodEOP(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the interpolation method for Earth Orientation Parameters.

setInterpMethodSW(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set the interpolation method for Space Weather data.

setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the interpolation degree.

setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the interpolation degree.

setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set the interpolation degree.

setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the interpolation degree.

setInterpolationDegree(int) - Method in class org.orekit.frames.LazyLoadedEop

Set the degree for interpolation degree.

setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the interpolation grid generator.

setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the interpolation grid generator.

setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the interpolation grid generator.

setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the interpolation grid generator.

setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the interpolation method to be used.

setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the interpolation method to be used.

setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set the interpolation method to be used.

setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the interpolation method to be used.

setInterpolationSample(int) - Method in class org.orekit.files.ilrs.CPF

Set the interpolation sample.

setInterval(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the observation interval in seconds.

setIntrackThrust(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set boolean that indicates if intrack thrust modeling was into account or not.

setIOD(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac

Sets the Issue of Data (IOD).

setIODC(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for the Issue of Data Clock.

setIODC(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the Issue of Data Clock.

setIODE(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for the Issue of Data Ephemeris.

setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the Issue of Data Ephemeris.

setIODEC(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Setter for the Issue of Data, Ephemeris and Clock.

setIODN(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Setter for the issue of data navigation.

setIODNav(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the Issue of Data of the navigation batch.

setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the IOD SSR.

setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the IOD SSR.

setIonosphericCorrectionType(IonosphericCorrectionType) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Setter for the ionospheric correction type.

setIscB1CD(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for inter Signal Delay for B1 CD.

setIscB1CP(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for inter Signal Delay for B1 CP.

setIscB2AD(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for inter Signal Delay for B2 AD.

setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CPFHeader

Set the flag telling if the center of mass correction is applied.

setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader

Set the center of mass correction applied indicator.

setIscL1CA(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L1 C/A.

setIscL1CD(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L1 CD.

setIscL1CP(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L1 CP.

setIscL2C(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L2 C.

setIscL5I5(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L5I.

setIscL5Q5(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for inter Signal Delay for L5Q.

setIsCompatibleWithTIVs(boolean) - Method in class org.orekit.files.ilrs.CPFHeader

Set the flag for compatibility with TIVs.

setIsConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header

Set the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.

setIsFirst(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the flag for the placement of the quaternion QC in the attitude data.

setIsMelbourneWubbenaConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header

Set the flag indicating if consistency between code and phase biases is maintained for the MW combinations.

setIsReceiveAmplitudeCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader

Set the receive amplitude correction applied indicator.

setIsSpacecraftTimeSimplified(boolean) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the spacecraft time simplified flag.

setIsStationSystemDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader

Set the station system delay applied indicator.

setIsTransponderDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader

Set the spacecraft system delay applied (transponders) indicator.

setIsTroposphericRefractionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader

Set the tropospheric refraction correction applied indicator.

setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

Set the counter for iterations.

setITRFVersion(int) - Method in class org.orekit.files.sinex.SinexLoader

Set the ITRF version used in EOP entries processing.

setKlobucharAlpha(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Set the "alpha" ionspheric parameters.

setKlobucharBeta(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Set the "beta" ionospheric parameters.

setLabeledRotationAngle(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the Euler angle about axis.

setLabeledRotationRate(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the rate of Euler angle about axis.

setLaserId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the laser configuration ID.

setLaserType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the laser type.

setLeapSeconds(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the Number of leap seconds since 6-Jan-1980.

setLeapSecondsDayNum(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the respective leap second day number.

setLeapSecondsFuture(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the future or past leap seconds.

setLeapSecondsWeekNum(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the respective leap second week number.

setLicense(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the license of use.

setLNFifthString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS l_n Word extracted from fifth string of the subframe.

setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS l_n Word extracted from third string of the subframe.

setLocalTimingId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the local timing system configuration ID.

setLod(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the length of day.

setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel

Set the low elevation threshold value for path delay computation.

setM(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS M Word.

setM0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the Mean Anomaly at Reference Time (rad).

setMahalanobisDistance(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Mahalanobis Distance.

setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given main field coefficients.

setManBasis(ManBasis) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set basis of this maneuver history data.

setManBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set identification number of the orbit determination or simulation upon which this maneuver is based.

setManComposition(List<ManeuverFieldType>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set maneuver element of information.

setManDeviceID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set identifier of the device used for this maneuver.

setManeuverable(Maneuvrable) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the object maneuver ability.

setManeuversFrequency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).

setManFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set epoch of the maneuver reference frame.

setManID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set maneuver identification number.

setManNextEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set start time of next maneuver.

setManNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set identification number of next maneuver.

setManPredSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set prediction source on which this maneuver is based.

setManPrevEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set completion time of previous maneuver.

setManPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set identification number of previous maneuver.

setManPurpose(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set purpose of maneuver.

setManPurpose(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set the purposes of the maneuver.

setManReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set reference frame of the maneuver.

setManufacturer(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set manufacturer name.

setManUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Set maneuver element of information units.

setMarkerName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set name of the antenna marker.

setMarkerNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set number of the antenna marker.

setMarkerType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set type of the antenna marker.

setMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the mass of the object.

setMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Set the spacecraft mass.

setMass(double) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder

Set the initial mass.

setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the initial mass.

setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set values for all elements.

setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set the value of a line of the matrix.

setMaxAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the maximum cross-sectional area for collision probability estimation purposes.

setMaxCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set max collision probability.

setMaxCollisionProbabilityMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set max collision probability method.

setMaxDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Set the available data range maximum date.

setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set the maximum number of model evaluations.

setMaximumObsGap(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set maximum time between observations in the OD of the object.

setMaxIter(int) - Method in class org.orekit.utils.SecularAndHarmonic

Set maximum number of iterations.

setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set the maximum number of iterations.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the degree limit for the next file parsing.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the degree limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the order limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the order limit for the next file parsing.

setMaxPredictedEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.

setMaxRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the maximum radar cross-section.

setMaxThrust(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the maximum composite thrust the spacecraft can accomplish.

setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver

Set maximum parameter value.

setMeanElementTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Set the description of the Mean Element Theory.

setMeanMotion(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit mean motion.

setMeanMotionDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the first time derivative of the mean motion.

setMeanMotionDotDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the second time derivative of the mean motion.

setMergedFiles(int) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Setter for the number of merged files.

setMessageFor(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader

Set the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.

setMessageId(String) - Method in class org.orekit.files.ccsds.section.Header

Set the ID that uniquely identifies a message from a given originator.

setMetadata(M) - Method in class org.orekit.files.ccsds.section.Segment

Set the segment metadata.

setMeteorologicalId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the meteorological configuration ID.

setMethod(AdMethodType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set attitude determination method.

setMethod(OdMethodFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set orbit determination method.

setMinAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the minimum cross-sectional area for collision probability estimation purposes.

setMinDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Set the available data range minimum date.

setMinPredictedEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.

setMinRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the minimum radar cross-section.

setMinValue(double) - Method in class org.orekit.utils.ParameterDriver

Set minimum parameter value.

setMissDistance(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the norm of relative position vector at TCA.

setMode(TrackingMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the mode.

setModifiedJulianDay(int) - Method in class org.orekit.files.sp3.SP3Header

Set the modified julian day for this SP3 file.

setMomentumAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the right ascension of angular momentum vector (rad).

setMomentumDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the declination of the angular momentum vector (rad).

setMu(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the gravitational coefficient.

setMu(double) - Method in class org.orekit.files.ilrs.CPF

Set the gravitational coefficient.

setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body attraction coefficient.

setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the central attraction coefficient μ.

setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set the central attraction coefficient μ.

setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the central attraction coefficient μ.

setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the central attraction coefficient μ.

setMuCreated(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser

Set the gravitational coefficient created from the knowledge of the central body.

setMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the Multiple Message Indicator.

setMuParsed(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser

Set the gravitational coefficient parsed in the ODM File.

setN4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the four-year interval number starting from 1996.

setNA(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS N^A Word.

setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector

Create the name of a satellite from its PRN number and satellite System it belongs to.

setName(String) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the satellite target name.

setName(String) - Method in class org.orekit.utils.ParameterDriver

Change the general name of this parameter driver.

setNbObsPerSatellite(SatInSystem, ObservationType, int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set number of observations for a satellite.

setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set n-body perturbation bodies.

setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set n-body perturbation bodies.

setNbSat(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set number of satellites.

setNbSensorNoiseCovariance(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Set number of noise elements for sensor.

setNbStates(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set number of states for AdMethodType.EKF, AdMethodType.BATCH or AdMethodType.FILTER_SMOOTHER.

setNbStates(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set the number of data states included (attitude components plus rates components).

setNeQuickAlpha(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation

Set the "alpha" ionospheric parameters.

setNextLeapEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the epoch of next leap second.

setNextLeapEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the epoch of next leap second.

setNextLeapTaimutc(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the difference (TAI – UTC) in seconds incorporated at epoch AcmMetadata.getNextLeapEpoch().

setNextLeapTaimutc(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().

setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.

setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the creation date of next message from a given originator.

setNextMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the unique ID identifying next message from a given originator.

setNominalFireRate(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the nominal fire rate.

setNoradID(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the NORAD Catalog Number ("Satellite Number").

setNoradId(String) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the satellite NORAD ID.

setNormalizedValue(double, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Set normalized value at specific date.

setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver

Set normalized value at specific date.

setNt(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the current date.

setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Set the number of biases processed for the current satellite.

setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Set the number of biases processed for the current satellite.

setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3Header

Set the number of epochs as contained in the SP3 file.

setNumberOfIonosphericLayers(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header

Set the number of ionospheric layers.

setNumberOfLeapSeconds(int) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the number of leap seconds.

setNumberOfLeapSeconds(int) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader

Setter for the current number of leap seconds.

setNumberOfLeapSecondsGNSS(int) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the number of leap seconds for GNSS time scales.

setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the number of satellites for the current IGM message.

setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader

Set the number of satellites for the current IGM message.

setNutation(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the nutation angle of spin axis (rad).

setNutationPeriod(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the body nutation period of the spin axis (s).

setNutationPhase(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the inertial nutation phase (rad).

setNutationVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the angular velocity of spin vector around angular momentum vector.

setNutLn(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the nutation correction in longitude.

setNutOb(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the nutation correction in obliquity.

setNutX(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the nutation correction X.

setNutY(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the nutation correction Y.

setObject(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the object name for which metadata are given.

setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the unique satellite identification designator for the object.

setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the satellite designator for the object for which metadata are given.

setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the unique satellite identification designator for the object.

setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Set the spacecraft ID for which the attitude data are provided.

setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Set the spacecraft ID for which the orbit state is provided.

setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Set the spacecraft name for which the attitude data are provided.

setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the spacecraft name used for object.

setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata

Set the spacecraft name for which the orbit state is provided.

setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the type of object.

setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the type of object.

setOblateFlattening(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set central body oblate spheroid oblateness.

setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the number of observations available for the OD of the object.

setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of observations available within the actual OD span.

setObsBeforeNextMessage(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.

setObservationCode(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the observation code of the average phasecenter position w/r to antenna reference point.

setObservations(List<Observation>) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock

Set the list of Observations Data Lines.

setObservationSampling(int) - Method in class org.orekit.files.sinex.DcbDescription

Set the observation sampling interval used for data analysis.

setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set an observer for iterations.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator

Set the observer.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator

Set the observer.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Set the observer.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator

Set the observer.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Set the observer.

setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator

Set the observer.

setObserverName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set name of the observer.

setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the number of observations accepted for the OD of the object.

setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of observations accepted within the actual OD span.

setOceanTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set ocean tides model.

setOcmDataElements(List<OcmElements>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the list of elements of information data blocks included in this message.

setOdEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the epoch of the orbit determination used for this message.

setOdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the Unique identifier of Orbit Data Message linked to this Attitude Data Message.

setOdmMsgLink(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.

setODParametersBlock(ODParameters) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Set the OD parameters logical block.

setOebAreaAlongIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.

setOebAreaAlongMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.

setOebAreaAlongMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.

setOebIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the intermediate physical dimension of the OEB.

setOebMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the maximum physical dimension of the OEB.

setOebMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the minimum physical dimension of the OEB.

setOebParentFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the Optimally Enclosing Box parent reference frame.

setOebParentFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the Optimally Enclosing Box parent reference frame epoch.

setOebQ(int, double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

set the component of quaternion defining Optimally Enclosing Box.

setOmega0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).

setOmegaDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the rate of Rate of Right Ascension (rad/s).

setOperator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the operator of the space object.

setOperatorContactPosition(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the contact position for the object owner / operator.

setOperatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the object operator email.

setOperatorOrganization(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the contact organisation of the object.

setOperatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the operator phone of the object.

setOpsStatus(OpsStatus) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the operational status.

setOrbAveraging(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set type of averaging (Osculating, mean Brouwer, other.

setOrbitCategory(OrbitCategory) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the orbit category.

setOrbitCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the central body name for object 1 and 2.

setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData

Set the orbit correction data.

setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData

Set the orbit correction data.

setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data

Set the orbit correction data.

setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Set the orbit correction data.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set propagation orbit type.

setOrbitTypeKey(String) - Method in class org.orekit.files.sp3.SP3Header

Set the orbit type key for this SP3 file.

setOrbRevNum(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the integer orbit revolution number.

setOrbRevNumBasis(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the basis for orbit revolution number.

setOriginator(String) - Method in class org.orekit.files.ccsds.section.Header

Set the message originator.

setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the address of Programmatic Point Of Contact at originator.

setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the address of Programmatic Point Of Contact at originator.

setOriginatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the email address of Programmatic Point Of Contact at originator.

setOriginatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the email address of Programmatic Point Of Contact at originator.

setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the phone number of Programmatic Point Of Contact at originator.

setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the phone number of Programmatic Point Of Contact at originator.

setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the programmatic Point Of Contact at originator.

setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the programmatic Point Of Contact at originator.

setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the position of Programmatic Point Of Contact at originator.

setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the position of Programmatic Point Of Contact at originator.

setOutputPulseType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the output pulse type.

setOutputPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the output pulse width.

setOwner(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the owner of the space object.

setP(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Set position component.

setP(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS P Word.

setP1(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS P1 Word.

setP2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS P2 Word.

setP3(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the the GLONASS P3 Word.

setP4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS P4 Word.

setPa(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit argument of pericenter.

setPa(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter fir the Argument of Perigee (rad).

setParameterDerivatives(ParameterDriver, AbsoluteDate, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the partial derivatives of the simulated measurement with respect to parameter.

setParameterDerivatives(ParameterDriver, TimeSpanMap<double[]>) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the partial derivatives of the simulated measurement with respect to parameter.

setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder

Set the selected parameters.

setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator

Set convergence threshold.

setParameterSpacing(int) - Method in class org.orekit.files.sinex.DcbDescription

Set the parameter spacing interval between the bias value.

setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the participants.

setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting

Set a component of a patch point to free or not.

setPath(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the path.

setPath1(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the path1.

setPath2(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the path2.

setPeriapsisAltitude(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the distance of the closest point in the objects orbit above the equatorial radius of the central body.

setPhaseCenterSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set satellite system for average phase center.

setPosition(Vector3D) - Method in class org.orekit.files.sinex.Station

Set the station position.

setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set position angle type.

setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set position angle type.

setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper

Set position angle type.

setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Set position angle type.

setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set position angle type.

setPosVelBase(double) - Method in class org.orekit.files.sp3.SP3Header

Set the base for position/velocity accuracy.

setPredictionProvider(String) - Method in class org.orekit.files.ilrs.CRDHeader

Set the prediction provider.

setPredictionType(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the prediction type.

setPressSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the pressure sensor manufacturer.

setPressSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the pressure sensor model.

setPressSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the pressure sensor serial number.

setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local pressure at the evaluation location

setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set identification of previous orbit determination.

setPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set identification number of previous maneuver.

setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set identification of previous orbit determination.

setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.

setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the creation date of previous message from a given originator.

setPreviousMessageId(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the ID of previous CDM issued for event identified by CONJUNCTION_ID.

setPreviousMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the unique ID identifying previous message from a given originator.

setPrf(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the Pulse Repetition Frequency (PRF).

setPrimaryWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the primary wavelength.

setPrmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Unique identifier of Pointing Request Message linked to this Orbit Data Message.

setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the PRN number of the satellite.

setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the PRN number of the satellite.

setProcessingSoftwareName(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the processing software name.

setProcessingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Set the processing softwares.

setProcessingSoftwareVersion(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the processing software version.

setProcessingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Set the processing software versions.

setProductionEpoch(DateComponents) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the date component of the ephemeris production.

setProductionHour(int) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the hour of ephemeris production.

setProgramName(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the program name.

setProgramName(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the program name.

setPropagator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set the orbit propagator used to generate this trajectory.

setProxy(Proxy.Type, String, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Set proxy parameters.

setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the pulse energy.

setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the pulse energy.

setPulseInOutgoingSemiTrain(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the number of pulses in outgoing semi-train.

setPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Set the pulse width.

setQ(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Set quaternion component.

setQDot(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Set quaternion derivative component.

setQualityIndicator(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the data quality indicator.

setQuantumEfficiency(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the quantum efficiency at applicable wavelength.

setQzssCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Set the QZSS code on L2.

setQzssFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Set the QZSS fit interval.

setQzssNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Set the QZSS navigation message.

setQzssToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data

Set the QZSS time of clock.

setRaan(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Set the orbit right ascension of ascending node.

setRangeMode(RangeMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the rangeMode.

setRangeType(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the range type indicator.

setRangeUnits(RangeUnits) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the rangeUnits.

setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set the frame in which rates are specified.

setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Set the frame in which rates are specified.

setRateProcessNoiseStdDev(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set process noise standard deviation if AttitudeDetermination.rateStates is RateElementsType.ANGVEL.

setRateStates(RateElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set attitude rate states.

setRateType(RateElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Set attitude rate element set type.

setRawCoefficients(boolean, Flattener, double[], double[], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the tesseral-sectorial coefficients matrix.

setRawCorrectionRange(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the raw correction for range.

setRawRangeModulus(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the raw range modulus.

setRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the typical (50th percentile) radar cross-section.

setRdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Unique identifier of Reentry Data Message linked to this Orbit Data Message.

setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the indicator for completed read.

setReceiveBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the receiveBand.

setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the receiveDelays.

setReceiverNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the number of the receiver.

setReceiverType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the type of the receiver.

setReceiverVersion(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the version of the receiver.

setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the recommended OD time span calculated for the object.

setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set time span of observation recommended for the OD of the object.

setReconnectParameters(double, double, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Set Reconnect parameters.

setReductionTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set reduction theory used for precession and nutation modeling.

setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Set reference date.

setReferenceEpoch(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the reference epoch.

setReferenceEpoch(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the reference epoch.

setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Set the reference frame in which data are given.

setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Set the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).

setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Set Coordinate system for velocity increment vector.

setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Set the reference frame in which data are given: used for RADEC tracking data.

setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester

Set up reference state.

setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester

Set up reference state.

setReferenceState(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester

Set up reference state.

setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Set up reference state.

setReferenceTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the time system used as a reference to define a time system.

setReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.KalmanModel

Setter for the reference trajectories.

setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver

Set reference parameter value.

setRefFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the name of the reference frame in which the state vector data are given.

setRefFrame(Frame) - Method in class org.orekit.files.ilrs.CPFHeader

Set the reference frame.

setRefFrameId(int) - Method in class org.orekit.files.ilrs.CPFHeader

Set the reference frame identifier.

setReflectance(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the typical (50th percentile) coefficient of reflectance.

setRegionCode(RegionCode) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage

Set the region code.

setRelativeMetadata(CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set the relative metadata following header, they are the common metadata for the CDM.

setRelativePositionN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the N component of Object2’s position relative to Object1’s in RTN frame.

setRelativePositionR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the R component of Object2’s position relative to Object1’s in RTN frame.

setRelativePositionT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the T component of Object2’s position relative to Object1’s in RTN frame.

setRelativeSpeed(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the norm of relative velocity vector at TCA.

setRelativeVelocityN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the N component of Object2’s velocity relative to Object1’s in RTN frame.

setRelativeVelocityR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the R component of Object2’s velocity relative to Object1’s in RTN frame.

setRelativeVelocityT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the T component of Object2’s velocity relative to Object1’s in RTN frame.

setRemainingDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the total ΔV remaining for spacecraft.

setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Allow/disallow resetting the initial state at end of propagation.

setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Allow/disallow resetting the initial state at end of propagation.

setResidualsAccepted(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the percentage of residuals accepted in the OD of the object (from 0 to 100).

setRevAtEpoch(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Set the revolution rumber.

setRolloverReference(DateComponents) - Static method in class org.orekit.time.GNSSDate

Set a reference date for ensuring continuity across GNSS week rollover.

setRotationalAngleType(int) - Method in class org.orekit.files.ilrs.CPFHeader

Set the rotation angle type.

setRunByName(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the run/by name.

setSatConfiguration(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Sets the satellite configuration.

setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData

Set the satellite ID.

setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData

Set the satellite ID.

setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData

Set the satellite ID.

setSatelliteReferenceDatum(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader

Set the satellite reference datum.

setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Override the default value of the parameter.

setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Override the default value of the parameter.

setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the satellite system.

setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the satellite system.

setSatelliteType(BeidouSatelliteType) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for satellite type.

setSbasId(SbasId) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the SBAS Id.

setScale(double) - Method in class org.orekit.utils.ParameterDriver

Set scale.

setScaleLength(double) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Set the scale length.

setScaleLength(double) - Method in class org.orekit.utils.AbstractMultipleShooting

Set the scale length.

setScaleTime(double) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter

Set the scale time.

setScaleTime(double) - Method in class org.orekit.utils.AbstractMultipleShooting

Set the scale time.

setSclkOffsetAtEpoch(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the spacecraft clock count at OcmMetadata.getEpochT0().

setSclkSecPerSISec(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the number of spacecraft clock seconds occurring during one SI second.

setScreenEntryTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the time in UTC when Object2 enters the screening volume.

setScreenExitTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the time in UTC when Object2 exits the screening volume.

setScreeningDataSource(String) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Set the source (or origin) of the specific orbital data for this object.

setScreenPcThreshold(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the collision probability screening threshold used to identify this conjunction.

setScreenType(ScreenType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the type of screening to be used.

setScreenVolumeFrame(ScreenVolumeFrame) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the name of the Object1 centered reference frame in which the screening volume data are given.

setScreenVolumeRadius(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

set the screen volume radius.

setScreenVolumeShape(ScreenVolumeShape) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the shape of the screening volume.

setScreenVolumeX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.

setScreenVolumeY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.

setScreenVolumeZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the N component size of the screening volume in the corresponding frame.

setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3Header

Set the seconds of the GPS week for this SP3 file.

setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given secular variation coefficients.

setSedr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the amount of energy being removed from the object’s orbit by atmospheric drag.

setSedr(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set Specific Energy Dissipation Rate.

setSefiCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Space Environment Fragmentation Impact probability.

setSefiCollisionProbabilityMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Space Environment Fragmentation Impact probability method.

setSefiFragmentationModel(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Space Environment Fragmentation Impact fragmentation model.

setSegments(List<S>) - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Set the segments.

setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver

Configure a parameter selection status.

setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the selected short periodic coefficients that must be stored as additional states.

setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Set the selected short periodic coefficients that must be stored as additional states.

setSensorFrequency(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Set frequency of sensor data for sensor.

setSensorNoiseCovariance(double[]) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Set standard deviation of sensor noise for sensor.

setSensorNumber(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Set number of the sensor.

setSensors(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set description of sensors used.

setSensorsN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of sensors used.

setSensorUsed(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Set sensor used.

setSequenceNumber(int) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the ephemeris sequence number.

setShadowBodies(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set celestial bodies casting shadows.

setShadowModel(ShadowModel) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set shadow model used for solar radiation pressure.

setShortPeriodTerms(List<ShortPeriodTerms>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Override the default value short periodic terms.

setSic(String) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the SIC ID.

setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter

Set the current value of sigma.

setSigmaU(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set rate random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.

setSigmaV(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set angle random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.

setSignalStrengthUnit(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the unit of the carrier to noise ratio observables.

setSisa(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the signal in space accuracy.

setSisaiOc1(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for Signal In Space Accuracy Index (clock drift accuracy).

setSisaiOc2(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for Signal In Space Accuracy Index (clock drift rate accuracy).

setSisaiOcb(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for Signal In Space Accuracy Index (radial and clock).

setSisaiOe(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for Signal In Space Accuracy Index (along track and across track).

setSismai(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for Signal In Space Monitoring Accuracy Index.

setSiteCode(String) - Method in class org.orekit.files.sinex.Station

Set the site code (station identifier).

setSma(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the semi-major axis.

setSnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Set the sine parameters of spherical harmonics expansion of degree N and order M.

setSoftwareId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Set the software configuration ID.

setSolarRadArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Set the solar radiation pressure area.

setSolarRadCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Get the solar radiation pressure coefficient.

setSolarRadiationPressure(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Set Enum that indicates if Solar Radiation Pressure is taken into account or not.

setSolidTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set solid tides model.

setSolveN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of solved-for states.

setSolveStates(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set description of state elements solved-for.

setSource(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Set source of attitude estimate.

setSource(String) - Method in class org.orekit.files.ilrs.CPFHeader

Set the ephemeris source.

setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Sets the source of this GPS almanac.

setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Sets the source of this GPS almanac.

setSpacecraftClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the spacecraft clock offset and drift applied indicator.

setSpacecraftEpochTimeScale(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the spacecraft epoch time scale.

setSpaceWeatherEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set epoch of the Space Weather data.

setSpaceWeatherSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set Space Weather data source.

setSpatialFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the spatial filter.

setSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the spectral filter.

setSphericalHarmonicsDegree(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Set the degree of spherical harmonic expansion.

setSphericalHarmonicsOrder(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Set the order of spherical harmonic expansion.

setSpinAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the right ascension of spin axis vector (rad).

setSpinAngle(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the phase of the satellite about the spin axis (rad).

setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the angular velocity of satellite around spin axis (rad/s).

setSpinDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Set the declination of the spin axis vector (rad).

setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for the Square Root of Semi-Major Axis (√m).

setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac

Sets the Square Root of Semi-Major Axis (m^1/2).

setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Setter for the Square Root of Semi-Major Axis (m^1/2).

setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac

Setter for the Square Root of Semi-Major Axis (m^1/2).

setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac

Setter for the Square Root of Semi-Major Axis (m^1/2).

setSrpCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the nominal SRP coefficient.

setSrpConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.

setSrpModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations

Set Solar Radiation Pressure model.

setSrpUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the SRP coefficient 1σ uncertainty.

setSsrEpoch1s(double) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the SSR Epoch Time 1s.

setSsrMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the SSR Multiple Message Indicator.

setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the SSR Provider ID.

setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the SSR Provider ID.

setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the SSR Solution ID.

setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the SSR Solution ID.

setSsrUpdateInterval(SsrUpdateInterval) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader

Set the SSR Update Interval.

setSsrUpdateInterval(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader

Set the SSR Update Interval.

setSsrUra(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data

Set the SSR User Range Accuracy (URA).

setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Set a start date.

setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Set a start date.

setStartEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the staring epoch (UTC).

setStartScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the start time in UTC of the screening period for the conjunction assessment.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the time of the earliest data contained in the OCM.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set start of total time span covered by attitude data.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the time of the earliest data contained in the OCM.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set start of total time span covered by ephemerides data and covariance data.

setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the startTime.

setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement

Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.

setStationClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the station clock offset and drift applied indicator.

setStationIdentifier(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the station identifier.

setStationInformation(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader

Setter for the station information.

setStationName(String) - Method in class org.orekit.files.ilrs.CRDHeader

Set the station name from official list.

setStationName(String) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the station name.

setStationNetword(String) - Method in class org.orekit.files.ilrs.CRDHeader

Set the station network.

setStationOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the estimated station oscillator drift in parts in 10¹⁵.

setStationUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the estimated station UTC offset.

setStatus(EstimatedMeasurementBase.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase

Set the status.

setStatusFlags(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Set status flag.

setStep(int) - Method in class org.orekit.files.ilrs.CPFHeader

Set the time between table entries.

setStepHandler(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator

Set a single handler for fixed stepsizes.

setStepHandler(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator

Set a single handler for variable stepsizes.

setStepHandler(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator

Set a single handler for fixed stepsizes.

setStepHandler(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator

Set a single handler for variable stepsizes.

setStopScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the stop time in UTC of the screening period for the conjunction assessment.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the time of the latest data contained in the OCM.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set end of total time span covered by attitude data.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the time of the latest data contained in the OCM.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set end of total time span covered by ephemerides data and covariance data.

setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the stopTime.

setSubDailySequenceNumber(int) - Method in class org.orekit.files.ilrs.CPFHeader

Set the sub-daily ephemeris sequence number.

setSumOfAllConstantDelays(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the sum of all constant delays (electronic, geometric, optical) that are not included in the time of flight measurements or time- variant or point angle-variant delays in the “42” record below (m, one way).

setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader

Set the supported names regular expression.

setSurveyedTargetDistance(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the surveyed target distance.

setSurveyError(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the survey error.

setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Setter for the user SV accuracy.

setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for the user SV accuracy.

setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the user SV accuracy.

setSvHealth(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data

Set the satellite health status.

setSvHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for the satellite health status.

setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage

Setter for the SV health status.

setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Setter for the satellite health status.

setSvHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the satellite health status.

setSVN(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Sets the "SVN" reference number.

setSystemId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Set the system configuration ID.

setSystemIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the system identifier.

setSystemNumber(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the system number.

setSystemOccupancy(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the system occupancy.

setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Set the difference (TAI – UTC) in seconds at epoch AcmMetadata.getEpochT0().

setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().

setTargetAttitude(Rotation) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set target attitude (if purpose is attitude adjustment).

setTargetClass(int) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the target class.

setTargetLocation(int) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the target location.

setTargetMomentum(Vector3D) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set target momentum (if purpose is momentum desaturation).

setTargetMomFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set reference frame for AttitudeManeuver.getTargetMomentum().

setTargetName(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Set the target name or ID.

setTargetSpinRate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Set target spin rate (if purpose is spin rate adjustment).

setTauC(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the GLONASS time scale correction to UTC time.

setTauGps(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the correction to GPS time relative to GLONASS time.

setTauN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Setter for the SV clock bias.

setTca(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the date and time in UTC of the closest approach.

setTdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Unique identifier of Tracking Data Message linked to this Orbit Data Message.

setTechAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the address of Technical Point Of Contact at originator.

setTechEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the email address of Technical Point Of Contact at originator.

setTechOrg(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the creating agency or operator.

setTechPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the phone number of Technical Point Of Contact at originator.

setTechPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the Technical Point Of Contact at originator.

setTechPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the position of Technical Point Of Contact at originator.

setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local temperature at the evaluation location

setTempSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the temperature sensor manufacturer.

setTempSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the temperature sensor model.

setTempSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Set the temperature sensor serial number.

setTFirstObs(AbsoluteDate) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the time of First observation record.

setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for the Group Delay Differential (s).

setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Setter for the Group Delay Differential (s).

setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage

Setter for the Group Delay Differential (s).

setTGD1(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Setter for the B1/B3 Group Delay Differential (s).

setTGD2(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage

Setter for the B2/B3 Group Delay Differential (s).

setTgdB1Cp(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for B1/B3 Group Delay Differential (s).

setTgdB2ap(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for B2 AP Group Delay Differential (s).

setTgdB2bI(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage

Setter for B2B_i / B3I Group Delay Differential (s).

setThrust(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set thrust component.

setThrustAcceleration(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Set the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.

setThrustDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ angular off-nominal thrust direction.

setThrustEfficiency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set thrust efficiency η.

setThrustInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set interpolation mode between current and next thrust line.

setThrustIsp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set thrust specific impulse.

setThrustMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver

Set one σ percent error on thrust magnitude.

setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the TideSystem used in the gravity field.

setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the reference time of the orbit as a duration from week start.

setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Setter for the message frame time.

setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Setter for the reference time of the SBAS orbit in GPS seconds of the week.

setTimeLastObsEnd(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the start of a time interval (UTC) that contains the time of the last accepted observation.

setTimeLastObsStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the start of a time interval (UTC) that contains the time of the last accepted observation.

setTimeout(int) - Method in class org.orekit.data.NetworkCrawler

Set the timeout for connection.

setTimeout(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Set timeout for connections and reads.

setTimer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the timer name.

setTimerSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the timer serial number.

setTimeScale(TimeScale) - Method in class org.orekit.files.ilrs.CPF

Set the time scale.

setTimeScale(TimeScale) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the data time scale.

setTimeSinceFirstObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set time elapsed between first accepted observation on epoch.

setTimeSinceLastObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set time elapsed between last accepted observation on epoch.

setTimeSource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Set the time source.

setTimeSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the span of time in seconds that the OCM covers.

setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Set the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.

setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.section.Metadata

Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.

setTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.clock.RinexClock

Setter for the file time system.

setTimeSystem(TimeSystem) - Method in class org.orekit.files.sinex.DcbDescription

Set the time system used for DCB data.

setTimeSystem(TimeSystem) - Method in class org.orekit.files.sp3.SP3Header

Set the time system used in this SP3 file.

setTimetagRef(TimetagReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the timetagRef.

setTk(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data

Set the time referenced to the beginning of the frame within the current day.

setTLastObs(AbsoluteDate) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set the time of last observation record.

setTorque(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Set the torque vector (N.m).

setTrackId(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the tracking data identifier.

setTrackingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Set the tracking softwares.

setTrackingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Set the tracking software versions.

setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the number of sensor tracks available for the OD of the object.

setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of sensors tracks available for the OD within the actual OD span.

setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the number of sensor tracks used for the OD of the object.

setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set number of sensors tracks accepted for the OD within the actual OD span.

setTrajBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set basis of this trajectory state time history data.

setTrajBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set identification number of the orbit determination or simulation upon which this trajectory is based.

setTrajFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set epoch of the trajectory reference frame.

setTrajID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set trajectory identification number.

setTrajNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set identification number of next trajectory.

setTrajPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set identification number of previous trajectory.

setTrajReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set reference frame of the trajectory.

setTrajType(OrbitElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set trajectory element set type.

setTrajUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set trajectory element set units.

setTransmissionOfSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Set the percentage of transmission of spectral filter.

setTransmissionTime(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the message transmission time.

setTransmissionTime(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the message transmission time.

setTransmissionTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage

Setter for transmission time.

setTransmitBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the transmitBand.

setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the transmitDelays.

setTransmitTime(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.IonosphereBaseMessage

Set the transmit time.

setTranspClkRef(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the transponder Clock Reference Time.

setTranspClkRefTime(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the transponder clock reference time.

setTransponderId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the transponder configuration ID.

setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the transponder Oscillator Drift in parts.

setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the estimated transponder oscillator drift in parts in 10¹⁵.

setTranspTransmitDelay(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the transponder transmit delay.

setTranspUtcOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader

Set the transponder UTC offset.

setTranspUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Set the estimated transponder UTC offset.

setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the turnaroundDenominator.

setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Setter for the turnaroundNumerator.

setTypAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.

setType(SP3FileType) - Method in class org.orekit.files.sp3.SP3Header

Set the file type for this SP3 file.

setTypeObs(SatelliteSystem, List<ObservationType>) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader

Set number of observations for a satellite.

setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Wrap an Orekit event detector and register it to the integrator.

setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Wrap an Orekit event detector and register it to the integrator.

setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator

Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.

setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in interface org.orekit.propagation.Propagator

Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.

setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set up State Transition Matrix and Jacobian matrix handling.

setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set up State Transition Matrix and Jacobian matrix handling.

setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set up State Transition Matrix and Jacobian matrix handling.

setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set up all user defined event detectors.

setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator

Set up all user defined event detectors.

setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage

Setter for the user range accuracy.

setURA(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac

Sets the average URA number.

setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage

Setter for the user range accuracy.

setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage

Setter for the user range accuracy.

setUraiEd(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for Elevation-Dependent User Range Accuracy.

setUraiNed0(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for term 0 of Non-Elevation-Dependent User Range Accuracy.

setUraiNed1(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for term 1 of Non-Elevation-Dependent User Range Accuracy.

setUraiNed2(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage

Setter for term 2 of Non-Elevation-Dependent User Range Accuracy.

setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set start of useable time span covered by attitude data.

setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Set end of useable time span covered by ephemerides data.

setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.

setUserDefinedBlock(UserDefined) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Set the user defined logical block.

setUt1MinusUtc(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the UT1-UTC offset.

setUt1mutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Set the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().

setUtcId(UtcId) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Set the UTC Id.

setV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Set velocity component.

setValidFrom(AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Set the start of validity.

setValidUntil(AbsoluteDate) - Method in class org.orekit.files.sinex.Station

Set the end of validity.

setValue(double, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver

Set parameter value at specific date.

setValue(double) - Method in class org.orekit.utils.ParameterDriver

Set parameter value.

setValueSpanMap(ParameterDriver) - Method in class org.orekit.utils.ParameterDriver

Set current parameter value span map to match another driver.

setVelocity(Vector3D) - Method in class org.orekit.files.sinex.Station

Set the station velocity.

setVersion(int) - Method in class org.orekit.files.ilrs.ILRSHeader

Set the format version.

setVersion(char) - Method in class org.orekit.files.sp3.SP3Header

Set the file version.

setVmAbsolute(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the typical (50th percentile) visual magnitude.

setVmApparent(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the typical (50th percentile) apparent visual magnitude.

setVmApparentMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the maximum apparent visual magnitude.

setVmApparentMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Set the minimum apparent visual magnitude.

setVtecQualityIndicator(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header

Set the VTEC quality indicator.

setWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Set the transmit wavelength.

setWeek(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData

Setter for the reference week of the orbit.

setWeightedRMS(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Set the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.

setWeightedRms(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Set weighted RMS residual ratio.

setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Set the total mass at T₀.

setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties

Set the total mass at T₀.

setX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Position Vector X component.

setX(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite X position.

setXdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Velocity Vector X component.

setXDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite X velocity.

setXDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite X acceleration.

setXp(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the X component of the pole.

setXpDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the X component of the pole first derivative.

setXpDotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the X component of the pole second derivative.

setxPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the X polar motion.

setY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Position Vector Y component.

setY(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Y position.

setYawAngle(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Set the yaw angle used for computation of phase wind-up correction.

setYawRate(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Set the yaw rate.

setYdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Velocity Vector Y component.

setYDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Y velocity.

setYDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Y acceleration.

setYearOfCentury(int) - Method in class org.orekit.files.ilrs.CRDHeader

Set the year of century from CPF or TLE.

setYp(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the Y component of the pole.

setYpDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the Y component of the pole first derivative.

setYpDotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

Set the Y component of the pole second derivative.

setyPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry

Set the Y polar motion.

setZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Position Vector Z component.

setZ(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Z position.

setZdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Set object Velocity Vector Z component.

setZDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Z velocity.

setZDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Setter for the satellite Z acceleration.

SFU - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Converter for Nequick-G aᵢ₀ parameter.

SFU_PER_DEG - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Converter for Nequick-G aᵢ₁ parameter.

SFU_PER_DEG2 - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage

Converter for Nequick-G aᵢ₂ parameter.

SGP - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for SGP type of ephemeris.

SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP type of ephemeris.

SGP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for SGP4 type of ephemeris.

SGP4 - Class in org.orekit.propagation.analytical.tle

This class contains methods to compute propagated coordinates with the SGP4 model.

SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4

Constructor for a unique initial TLE.

SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4

Constructor for a unique initial TLE.

SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP4 type of ephemeris.

SGP4_XP_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Constant for SGP4-XP mean elements theory.

SGP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE

Identifier for SGP8 type of ephemeris.

SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP8 type of ephemeris.

SGP_SGP4_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Constant for SGP/SGP4 mean elements theory.

ShadowModel - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Shadow model for solar radiation pressure.

shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier

Compute Shapiro path dilation between two points in a gravity field.

ShapiroInterSatellitePhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.

ShapiroInterSatellitePhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier

Simple constructor.

ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with Shapiro time delay.

ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier

Simple constructor.

ShapiroOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.

ShapiroOneWayGNSSPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier

Simple constructor.

ShapiroOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with Shapiro time delay.

ShapiroOneWayGNSSRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier

Simple constructor.

ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical phase measurement with Shapiro time delay.

ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier

Simple constructor.

ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical range measurement with Shapiro time delay.

ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier

Simple constructor.

shiftedBy(double) - Method in class org.orekit.attitudes.Attitude

Get a time-shifted attitude.

shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude

Get a time-shifted attitude.

shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude

Get a time-shifted attitude.

shiftedBy(double) - Method in class org.orekit.frames.FieldTransform

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.frames.FieldTransform

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.frames.Transform

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get a time-shifted instance.

shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit

Get a time-shifted orbit.

shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.Orbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState

Get a time-shifted state.

shiftedBy(Field<T>, FieldOrbit<T>, T) - Method in class org.orekit.propagation.FieldStateCovariance

Get a time-shifted covariance matrix.

shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState

Get a time-shifted state.

shiftedBy(Orbit, double) - Method in class org.orekit.propagation.StateCovariance

Get a time-shifted covariance matrix.

shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate

Get a time-shifted date.

shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate

Get a time-shifted date.

shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate

Get a time-shifted date.

shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable

Get a time-shifted instance.

shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get a time-shifted state.

shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Get a time-shifted state.

ShiftingTransformProvider - Class in org.orekit.frames

Transform provider using thread-safe shifts on transforms sample.

ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider

Simple constructor.

SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for SHM files.

SHMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the SHM gravity field format.

SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader

Simple constructor.

SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader

Simple constructor.

SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Name of the prefix for short period coefficients keys.

SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Name of the prefix for short period coefficients keys.

SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Name of the prefix for short period coefficients keys.

ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolated short periodics coefficients.

ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Simple constructor.

ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces

Additive short period terms contributing to the mean to osculating orbit mapping.

ShortTermEncounter2DDefinition - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod

Defines the encounter between two collision object at time of closest approach assuming a short-term encounter model .

ShortTermEncounter2DDefinition(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Constructor.

ShortTermEncounter2DDefinition(Orbit, StateCovariance, Orbit, StateCovariance, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Constructor.

ShortTermEncounter2DDefinition(Orbit, StateCovariance, double, Orbit, StateCovariance, double, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Constructor.

ShortTermEncounter2DDefinition(Orbit, StateCovariance, Orbit, StateCovariance, double, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition

Constructor.

ShortTermEncounter2DPOCMethod - Interface in org.orekit.ssa.collision.shorttermencounter.probability.twod

Interface common to all short-term encounter probability of collision computing methods.

ShortTermEncounter2DPOCMethodType - Enum in org.orekit.ssa.collision.shorttermencounter.probability.twod

This enum stores every probability of collision computing method using the short-term encounter model available in Orekit.

siAccuracy(Unit, double, int) - Static method in class org.orekit.files.sp3.SP3Utils

Convert an accuracy to SI units.

SigmaEigenvectorsCovariance - Class in org.orekit.files.ccsds.ndm.cdm

Container for Sigma/Eigenvectors Covariance data.

SigmaEigenvectorsCovariance(boolean) - Constructor for class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance

Simple constructor.

SigmaEigenvectorsCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for covariance format entries.

sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod

Return the symbol of parameter a.

SignalCode - Enum in org.orekit.gnss

Enumerate for satellite signal code.

SignalInSpaceAccuracy - Class in org.orekit.gnss.metric.messages.common

Signal-In-Space Accuracy (SISA).

SignalInSpaceAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.SignalInSpaceAccuracy

Simple constructor.

signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Compute propagation delay on a link leg (typically downlink or uplink).

signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement

Compute propagation delay on a link leg (typically downlink or uplink).

signedAmplitude(SpacecraftState, double[]) - Method in interface org.orekit.forces.empirical.AccelerationModel

Compute the signed amplitude of the acceleration.

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.empirical.AccelerationModel

Compute the signed amplitude of the acceleration.

signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel

Compute the signed amplitude of the acceleration.

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel

Compute the signed amplitude of the acceleration.

signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel

Compute the signed amplitude of the acceleration.

signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel

Compute the signed amplitude of the acceleration.

SignSemantic - Enum in org.orekit.estimation.measurements.generation

Enumerate for the semantic of the g function sign during measurements generation.

SimpleExponentialAtmosphere - Class in org.orekit.models.earth.atmosphere

Simple exponential atmospheric model.

SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere

Create an exponential atmosphere.

SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss

Ambiguity acceptance test based on a ratio of the two best candidates.

SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance

Simple constructor.

SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data

Parser for simple tables containing time stamped data.

SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser

Simple constructor.

SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data

Interface for converting a table row into time-stamped data.

SinexEopEntry - Class in org.orekit.files.sinex

Container for EOP entry read in a Sinex file.

SinexEopEntry(AbsoluteDate) - Constructor for class org.orekit.files.sinex.SinexEopEntry

Constructor.

SinexLoader - Class in org.orekit.files.sinex

Loader for Solution INdependent EXchange (SINEX) files.

SinexLoader(String) - Constructor for class org.orekit.files.sinex.SinexLoader

Simple constructor.

SinexLoader(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.files.sinex.SinexLoader

Construct a loader by specifying the source of SINEX auxiliary data files.

SinexLoader(DataSource) - Constructor for class org.orekit.files.sinex.SinexLoader

Simple constructor.

SinexLoader(DataSource, TimeScales) - Constructor for class org.orekit.files.sinex.SinexLoader

Loads SINEX from the given input stream using the specified auxiliary data.

SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity

Body attraction force model computed as absolute acceleration towards a body.

SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction

Simple constructor.

SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity

Body attraction force model computed as relative acceleration towards frame center.

SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction

Simple constructor.

SingleFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering

Single frequency Hatch filter.

SingleFrequencyHatchFilter(ObservationData, ObservationData, MeasurementType, double, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter

Constructor for the Single Frequency Hatch Filter.

SingleFrequencySmoother - Class in org.orekit.estimation.measurements.filtering

Handler to perform pseudo-range smoothing using single frequency measurements.

SingleFrequencySmoother(MeasurementType, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother

Simple constructor.

SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere

Single Layer Model (SLM) ionospheric mapping function.

SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction

Constructor with default value.

SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction

Constructor.

SingleParameterFitter - Class in org.orekit.frames

Fitter for one Earth Orientation Parameter.

SingleParameterFitter(double, double, double, int, double...) - Constructor for class org.orekit.frames.SingleParameterFitter

Deprecated.

replaced by SingleParameterFitter.SingleParameterFitter(double, double, int, double...)

SingleParameterFitter(double, double, int, double...) - Constructor for class org.orekit.frames.SingleParameterFitter

Simple constructor.

sini0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

sinus original inclination.

sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sinus original inclination.

siToCcsdsName(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a SI unit name to a CCSDS name.

siToCcsdsName(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a SI unit name to a CCSDS name.

siToRaw(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType

Convert a measurement from SI units.

size() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Get the size of the value array.

size() - Method in class org.orekit.utils.DoubleArrayDictionary

Get the number of dictionary entries.

size() - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Get the size of the value array.

size() - Method in class org.orekit.utils.FieldArrayDictionary

Get the number of dictionary entries.

SlewingPanel - Class in org.orekit.forces

Class representing one panel of a satellite, slewing about an axis at constant rate.

SlewingPanel(Vector3D, double, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.SlewingPanel

Simple constructor.

SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Identifier for sMm coefficients.

SMALL_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Truncation tolerance for small orbits.

SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers

Analytical model for small maneuvers.

SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in spacecraft frame.

SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in user-specified frame.

SmoothedObservationDataSet - Class in org.orekit.estimation.measurements.filtering

Container used to store smoothed observation data along with the original data set it originates from.

SmoothedObservationDataSet(ObservationData, ObservationDataSet) - Constructor for class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet

Simple constructor.

SmoothFieldOfView - Class in org.orekit.geometry.fov

Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.

SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView

Build a new instance.

SoftwareConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Empty constructor.

SOLAR_FLUX_UNIT - Static variable in class org.orekit.utils.units.Unit

Solar Flux Unit.

SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for solar system barycenter.

SolarActivityGenerator(Collection<L>) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator

Constructor.

SolarRadiationPressure - Class in org.orekit.forces.radiation

Solar radiation pressure force model.

SolarRadiationPressure(ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Simple constructor with default reference values.

SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Complete constructor.

SOLFSMYDataLoader - Class in org.orekit.models.earth.atmosphere.data

This class reads solar activity data from SOLFSMY files for the class JB2008SpaceEnvironmentData.

SOLFSMYDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Constructor.

SOLFSMYDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data

Container class for Solar activity indexes.

SolidTides - Class in org.orekit.forces.gravity

Solid tides force model.

SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Find the best solutions to an Integer Least Square problem.

solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver

Find the best solutions to an Integer Least Square problem.

sort() - Method in class org.orekit.utils.ParameterDriversList

Sort the parameters lexicographically.

SourceTable - Class in org.orekit.gnss.metric.ntrip

Source table for ntrip streams retrieval.

SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint

South pole.

SP3 - Class in org.orekit.files.sp3

Represents a parsed SP3 orbit file.

SP3(double, int, Frame) - Constructor for class org.orekit.files.sp3.SP3

Create a new SP3 file object.

SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3Header

String representation of the center of ephemeris coordinate system.

SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3Parser

String representation of the center of ephemeris coordinate system.

SP3Coordinate - Class in org.orekit.files.sp3

A single record of position clock and possibly derivatives in an SP3 file.

SP3Coordinate(AbsoluteDate, Vector3D, Vector3D, Vector3D, Vector3D, double, double, double, double, boolean, boolean, boolean, boolean) - Constructor for class org.orekit.files.sp3.SP3Coordinate

Create a coordinate with position and velocity.

SP3CoordinateHermiteInterpolator - Class in org.orekit.files.sp3

Interpolator for SP3 coordinates.

SP3CoordinateHermiteInterpolator(int, double, boolean) - Constructor for class org.orekit.files.sp3.SP3CoordinateHermiteInterpolator

Constructor.

SP3Ephemeris - Class in org.orekit.files.sp3

Single satellite ephemeris from an SP3 file.

SP3Ephemeris(String, double, Frame, int, CartesianDerivativesFilter) - Constructor for class org.orekit.files.sp3.SP3Ephemeris

Create an ephemeris for a single satellite.

SP3FileType - Enum in org.orekit.files.sp3

File type indicator.

SP3Header - Class in org.orekit.files.sp3

Header for SP3 files.

SP3Header() - Constructor for class org.orekit.files.sp3.SP3Header

Create a new SP3 header.

SP3OrbitType - Enum in org.orekit.files.sp3

Orbit type indicator.

SP3Parser - Class in org.orekit.files.sp3

A parser for the SP3 orbit file format.

SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser

Create an SP3 parser using default values.

SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser

Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.

SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser

Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.

SP3Segment - Class in org.orekit.files.sp3

One segment of an SP3Ephemeris.

SP3Segment(double, Frame, int, CartesianDerivativesFilter) - Constructor for class org.orekit.files.sp3.SP3Segment

Simple constructor.

SP3Utils - Class in org.orekit.files.sp3

Constants for SP3 files.

SP3Writer - Class in org.orekit.files.sp3

Writer for SP3 file.

SP3Writer(Appendable, String, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Writer

Simple constructor.

SpacecraftBodyFrame - Class in org.orekit.files.ccsds.definitions

Frames used in CCSDS Attitude Data Messages for the spacecraft body.

SpacecraftBodyFrame(SpacecraftBodyFrame.BaseEquipment, String) - Constructor for class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame

Simple constructor.

SpacecraftBodyFrame.BaseEquipment - Enum in org.orekit.files.ccsds.definitions

Equipment on which the frame is located.

SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.odm

Container for spacecraft parameters.

SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Create an empty state data set.

SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for ODM spacecraft parameters entries.

SpacecraftParametersWriter - Class in org.orekit.files.ccsds.ndm.odm

Writer for spacecraft parameters data.

SpacecraftParametersWriter(String, String, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter

Create a writer.

SpacecraftState - Class in org.orekit.propagation

This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.

SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit only.

SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and attitude.

SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit and mass.

SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude and mass.

SpacecraftState(Orbit, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and additional states.

SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude and additional states.

SpacecraftState(Orbit, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit, mass and additional states.

SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude, mass and additional states.

SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.

SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration only.

SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration and attitude.

SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from position-velocity-acceleration and mass.

SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration, attitude and mass.

SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration and additional states.

SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration, attitude and additional states.

SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from position-velocity-acceleration, mass and additional states.

SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.

SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.

SpacecraftStateInterpolator - Class in org.orekit.propagation

Generic class for spacecraft state interpolator.

SpacecraftStateInterpolator(Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Simplest constructor to create a default Hermite interpolator for every spacecraft state field.

SpacecraftStateInterpolator(int, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

SpacecraftStateInterpolator(int, Frame, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

SpacecraftStateInterpolator(int, double, Frame, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

SpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor to create a customizable Hermite interpolator for every spacecraft state field.

SpacecraftStateInterpolator(Frame, TimeInterpolator<Orbit>, TimeInterpolator<AbsolutePVCoordinates>, TimeInterpolator<TimeStampedDouble>, TimeInterpolator<Attitude>, TimeInterpolator<TimeStampedDouble>) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s

SpacecraftStateInterpolator(int, double, Frame, TimeInterpolator<Orbit>, TimeInterpolator<AbsolutePVCoordinates>, TimeInterpolator<TimeStampedDouble>, TimeInterpolator<Attitude>, TimeInterpolator<TimeStampedDouble>) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator

Constructor.

SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants

Speed of light: 299792458.0 m/s.

SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide spherical harmonics coefficients.

SpinStabilized - Class in org.orekit.attitudes

This class handles a spin stabilized attitude provider.

SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized

Creates a new instance.

SpinStabilized - Class in org.orekit.files.ccsds.ndm.adm.apm

Container for Attitude Parameter Message data lines.

SpinStabilized() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Simple constructor.

SpinStabilizedKey - Enum in org.orekit.files.ccsds.ndm.adm.apm

Keys for APM spin-stabilized entries.

splice(Collection<SP3>) - Static method in class org.orekit.files.sp3.SP3

Splice several SP3 files together.

sqrt(String) - Method in class org.orekit.utils.units.Unit

Create root of unit.

SSA - Static variable in class org.orekit.models.earth.displacement.Tide

Ssa tide.

SsrData - Class in org.orekit.gnss.metric.messages.ssr

Container for common data in SSR message data.

SsrData() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrData

Empty constructor.

SsrHeader - Class in org.orekit.gnss.metric.messages.ssr

Container for common data in SSR messages header.

SsrHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrHeader

Empty constructor.

SsrIgm01 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR Orbit Correction Message.

SsrIgm01(int, SatelliteSystem, SsrIgm01Header, List<SsrIgm01Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01

Constructor.

SsrIgm01Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM01 data.

SsrIgm01Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data

Constructor.

SsrIgm01Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM01 header.

SsrIgm01Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header

Constructor.

SsrIgm02 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR Clock Correction Message.

SsrIgm02(int, SatelliteSystem, SsrIgm02Header, List<SsrIgm02Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02

Constructor.

SsrIgm02Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM02 data.

SsrIgm02Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data

Constructor.

SsrIgm02Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM02 header.

SsrIgm02Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Header

Constructor.

SsrIgm03 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR Combined Orbit and Clock Correction Message.

SsrIgm03(int, SatelliteSystem, SsrIgm03Header, List<SsrIgm03Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03

Constructor.

SsrIgm03Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM03 data.

SsrIgm03Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data

Constructor.

SsrIgm03Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM03 header.

SsrIgm03Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header

Constructor.

SsrIgm04 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR High Rate Clock Correction Message.

SsrIgm04(int, SatelliteSystem, SsrIgm04Header, List<SsrIgm04Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04

Constructor.

SsrIgm04Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM04 data.

SsrIgm04Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data

Constructor.

SsrIgm04Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM04 header.

SsrIgm04Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Header

Constructor.

SsrIgm05 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR Code Bias Message.

SsrIgm05(int, SatelliteSystem, SsrIgm05Header, List<SsrIgm05Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05

Constructor.

SsrIgm05Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM05 data.

SsrIgm05Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data

Constructor.

SsrIgm05Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM05 header.

SsrIgm05Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Header

Constructor.

SsrIgm06 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR Phase Bias Message.

SsrIgm06(int, SatelliteSystem, SsrIgm06Header, List<SsrIgm06Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06

Constructor.

SsrIgm06Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM06 data.

SsrIgm06Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data

Constructor.

SsrIgm06Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM06 header.

SsrIgm06Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header

Constructor.

SsrIgm07 - Class in org.orekit.gnss.metric.messages.ssr.igm

GNSS SSR SSR URA Message.

SsrIgm07(int, SatelliteSystem, SsrIgm07Header, List<SsrIgm07Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07

Constructor.

SsrIgm07Data - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM07 data.

SsrIgm07Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data

Constructor.

SsrIgm07Header - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for SSR IGM07 header.

SsrIgm07Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Header

Constructor.

SsrIgmData - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for common data in IGS Generic SSR Message type.

SsrIgmData() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData

Constructor.

SsrIgmHeader - Class in org.orekit.gnss.metric.messages.ssr.igm

Container for common data in IGS Generic SSR Message type header.

SsrIgmHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader

Constructor.

SsrIgmMessage<H extends SsrIgmHeader,D extends SsrIgmData> - Class in org.orekit.gnss.metric.messages.ssr.igm

The IGS Generic SSR Message types provide elements to calculate GNSS satellite corrections.

SsrIgmMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage

Constructor.

SsrIm201 - Class in org.orekit.gnss.metric.messages.ssr.subtype

SSR Ionosphere VTEC Spherical Harmonics Message.

SsrIm201(int, SsrIm201Header, List<SsrIm201Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201

Constructor.

SsrIm201Data - Class in org.orekit.gnss.metric.messages.ssr.subtype

Container for SSR IM201 data.

SsrIm201Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data

Constructor.

SsrIm201Header - Class in org.orekit.gnss.metric.messages.ssr.subtype

Container for SSR IM201 header.

SsrIm201Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header

Constructor.

SsrMessage<H extends SsrHeader,D extends SsrData> - Class in org.orekit.gnss.metric.messages.ssr

Base class for SSR messages.

SsrMessage(int, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrMessage

Constructor.

SsrUpdateInterval - Class in org.orekit.gnss.metric.messages.common

SSR Update interval.

SsrUpdateInterval(int) - Constructor for class org.orekit.gnss.metric.messages.common.SsrUpdateInterval

Constructor.

SsrVtecIonosphericModel - Class in org.orekit.models.earth.ionosphere

Ionospheric model based on SSR IM201 message.

SsrVtecIonosphericModel(SsrIm201) - Constructor for class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel

Constructor.

STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric pressure (Pa).

STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric temperature (K).

STANDARDIZED_LOCALE - Static variable in class org.orekit.utils.AccurateFormatter

Standardized locale to use, to ensure files can be exchanged without internationalization issues.

start() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage

Start message extraction.

start() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage

Start message extraction.

start() - Method in interface org.orekit.gnss.metric.parser.EncodedMessage

Start message extraction.

start() - Method in class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage

Start message extraction.

START_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Default suffix for start driver.

START_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Default suffix for start driver.

started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin

startMessage(String, String, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Start CCSDS message.

startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Start CCSDS message.

startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Start CCSDS message.

startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Start parsing.

StartStopEventsTrigger<A extends AbstractDetector<A>,O extends AbstractDetector<O>> - Class in org.orekit.forces.maneuvers.trigger

Maneuver triggers based on a pair of event detectors that defines firing start and stop.

StartStopEventsTrigger(A, O) - Constructor for class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger

Simple constructor.

startStreaming(String, Type, boolean, boolean) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Connect to a mount point and start streaming data from it.

STATE_DIMENSION - Static variable in class org.orekit.propagation.AbstractMatricesHarvester

State dimension, fixed to 6.

STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.EpochDerivativesEquations

State dimension, fixed to 6.

STATE_DIMENSION - Static variable in class org.orekit.propagation.StateCovariance

State dimension.

stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Notify about a state change.

stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Notify about a state change.

StateCovariance - Class in org.orekit.propagation

This class is the representation of a covariance matrix at a given date.

StateCovariance(RealMatrix, AbsoluteDate, LOF) - Constructor for class org.orekit.propagation.StateCovariance

Constructor.

StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovariance

Constructor.

StateCovarianceBlender - Class in org.orekit.propagation

State covariance blender.

StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceBlender

Constructor.

StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceBlender

Constructor.

StateCovarianceKeplerianHermiteInterpolator - Class in org.orekit.propagation

State covariance Keplerian quintic interpolator.

StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output local orbital frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output local orbital frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, CartesianDerivativesFilter, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output local orbital frame and : Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, double, TimeInterpolator<Orbit>, CartesianDerivativesFilter, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output local orbital frame.

StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, CartesianDerivativesFilter, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

StateCovarianceKeplerianHermiteInterpolator(int, double, TimeInterpolator<Orbit>, CartesianDerivativesFilter, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator

Constructor using an output frame.

StateCovarianceMatrixProvider - Class in org.orekit.propagation

Additional state provider for state covariance matrix.

StateCovarianceMatrixProvider(String, String, MatricesHarvester, StateCovariance) - Constructor for class org.orekit.propagation.StateCovarianceMatrixProvider

Constructor.

StateFunction - Interface in org.orekit.utils

Interface representing a vector function depending on SpacecraftState.

StateJacobian - Interface in org.orekit.utils

Interface representing the Jacobian of a vector function depending on SpacecraftState.

StateMapper - Class in org.orekit.propagation.integration

This class maps between raw double elements and SpacecraftState instances.

StateMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper

Simple constructor.

stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TleGenerationAlgorithm) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE

Convert Spacecraft State into TLE.

stateToTLE(SpacecraftState, TLE, TleGenerationAlgorithm) - Static method in class org.orekit.propagation.analytical.tle.TLE

Convert Spacecraft State into TLE.

StateVector - Class in org.orekit.files.ccsds.ndm.cdm

Container for state vector data.

StateVector() - Constructor for class org.orekit.files.ccsds.ndm.cdm.StateVector

Simple constructor.

StateVector - Class in org.orekit.files.ccsds.ndm.odm

Container for state vector data.

StateVector() - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVector

Create an empty data set.

StateVectorKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM state vector entries.

StateVectorKey - Enum in org.orekit.files.ccsds.ndm.odm

Keys for ODM state vector container entries.

StateVectorWriter - Class in org.orekit.files.ccsds.ndm.cdm

Writer for state vector data for CCSDS Conjunction Data Messages.

StateVectorWriter - Class in org.orekit.files.ccsds.ndm.odm

Writer for state vector data.

StateVectorWriter(String, String, StateVector, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVectorWriter

Create a writer.

staticShiftedBy(T) - Method in class org.orekit.frames.FieldTransform

Shift the transform in time considering all rates, then return only the translation and rotation portion of the transform.

staticShiftedBy(double) - Method in class org.orekit.frames.Transform

Shift the transform in time considering all rates, then return only the translation and rotation portion of the transform.

StaticTransform - Interface in org.orekit.frames

A transform that only includes translation and rotation.

Station - Class in org.orekit.files.sinex

Station model.

Station() - Constructor for class org.orekit.files.sinex.Station

Constructor.

Station.ReferenceSystem - Enum in org.orekit.files.sinex

Eccentricity reference system.

StationDisplacement - Interface in org.orekit.models.earth.displacement

Interface for computing reference points displacement.

stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel

This method allows the computation of the Stant Total Electron Content (STEC).

stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel

This method allows the computation of the Stant Total Electron Content (STEC).

StepHandlerMultiplexer - Class in org.orekit.propagation.sampling

This class gathers several OrekitStepHandler instances into one.

StepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.StepHandlerMultiplexer

Simple constructor.

stillAcceptsData() - Method in interface org.orekit.data.DataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.gnss.SEMParser

stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser

stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader

Check if the loader still accepts new data.

STKEphemeris(String, double, List<STKEphemerisFile.STKEphemerisSegment>) - Constructor for class org.orekit.files.stk.STKEphemerisFile.STKEphemeris

Constructs a STKEphemerisFile.STKEphemeris instance.

STKEphemerisFile - Class in org.orekit.files.stk

STK ephemeris file.

STKEphemerisFile(String, String, STKEphemerisFile.STKEphemeris) - Constructor for class org.orekit.files.stk.STKEphemerisFile

Constructs a STKEphemerisFile instance.

STKEphemerisFile.STKCoordinateSystem - Enum in org.orekit.files.stk

STK coordinate system.

STKEphemerisFile.STKEphemeris - Class in org.orekit.files.stk

Ephemeris from an STK ephemeris file.

STKEphemerisFile.STKEphemerisSegment - Class in org.orekit.files.stk

Ephemeris segment from an STK ephemeris file.

STKEphemerisFileParser - Class in org.orekit.files.stk

Parser of STKEphemerisFiles.

STKEphemerisFileParser(String, double, UTCScale, Map<STKEphemerisFile.STKCoordinateSystem, Frame>) - Constructor for class org.orekit.files.stk.STKEphemerisFileParser

Constructs a STKEphemerisFileParser instance.

STKEphemerisSegment(double, Frame, int, CartesianDerivativesFilter, List<TimeStampedPVCoordinates>) - Constructor for class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment

Constructs a STKEphemerisFile.STKEphemerisSegment instance.

STMEquations - Class in org.orekit.propagation.numerical.cr3bp

Class calculating the state transition matrix coefficient for CR3BP Computation.

STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations

Simple constructor.

STOP_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector

Default suffix for stop driver.

STOP_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector

Default suffix for stop driver.

stopMonitoring() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor

Stop monitoring.

StopOnDecreasing - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing

Empty constructor.

StopOnEvent - Class in org.orekit.propagation.events.handlers

Event handler which will always return stop as a state.

StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent

Empty constructor.

StopOnIncreasing - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing

Empty constructor.

stopStreaming(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient

Stop streaming data from all connected mount points.

STR_NAN - Static variable in class org.orekit.files.ilrs.CRD

String of "NaN".

STR_VALUE_NOT_AVAILABLE - Static variable in class org.orekit.files.ilrs.CRD

Value of 'not available' or 'not applicable' or 'no information'.

StreamedMessage - Class in org.orekit.gnss.metric.ntrip

Container for streamed messages meta-data.

StreamingAemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem

A writer for AEM files.

StreamingAemWriter(Generator, AemWriter, AdmHeader, AemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter

Simple constructor.

StreamingAemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.adm.aem

A writer for a segment of an AEM.

StreamingCpfWriter - Class in org.orekit.files.ilrs

A writer for CPF files.

StreamingCpfWriter(Appendable, TimeScale, CPFHeader) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter

Create a CPF writer than streams data to the given output stream.

StreamingCpfWriter(Appendable, TimeScale, CPFHeader, boolean) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter

Create a CPF writer than streams data to the given output stream.

StreamingCpfWriter.HeaderLineWriter - Enum in org.orekit.files.ilrs

Writer for specific header lines.

StreamingCpfWriter.Segment - Class in org.orekit.files.ilrs

A writer for a segment of a CPF.

StreamingOcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm

A writer for OCM files.

StreamingOcmWriter(Generator, OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter

Construct a writer that for each segment uses the reference frame of the first state's attitude.

StreamingOcmWriter(Generator, OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter

Simple constructor.

StreamingOcmWriter.BlockWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm

A writer for a trajectory state history block of an OCM.

StreamingOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem

A writer for OEM files.

StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter

Construct a writer that for each segment uses the reference frame of the first state's attitude.

StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter

Construct a writer that writes position, velocity, and acceleration at each time step.

StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata, boolean, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter

Simple constructor.

StreamingOemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.odm.oem

A writer for a segment of an OEM.

StreamMonitor - Class in org.orekit.gnss.metric.ntrip

Monitor for retrieving streamed data from one mount point.

StreamMonitor(NtripClient, String, Type, boolean, boolean, double, double, int) - Constructor for class org.orekit.gnss.metric.ntrip.StreamMonitor

Build a monitor for streaming data from a mount point.

stringValue(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.DataField

Get the value of the field as a String.

SubFrame - Class in org.orekit.gnss.rflink.gps

Container for sub-frames in a GPS navigation message.

SubFrame(int[], int) - Constructor for class org.orekit.gnss.rflink.gps.SubFrame

Simple constructor.

SubFrame1 - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 1.

SubFrame2 - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 2.

SubFrame3 - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 3.

SubFrame45 - Class in org.orekit.gnss.rflink.gps

Base container for sub-frames 4 and 5.

SubFrame4A - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, pages 1, 6, 11, 16 and 21, but also for sub-frames 4, pages 2, 3, 4, 5, 7, 8, and 9 which have a similar structure.

SubFrame4A0 - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, pages 1, 6, 11, 16 and 21.

SubFrame4A1 - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, pages 2, 3, 4, 5, 7, 8, and 9.

SubFrame4B - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, pages 10, 14, 15, 17.

SubFrame4C - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, page 13.

SubFrame4D - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, page 18.

SubFrame4E - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 4, page 25.

SubFrame5B - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 5, page 25.

SubFrameAlmanac - Class in org.orekit.gnss.rflink.gps

Container for sub-frames 5, page 1-24.

SubFrameDummyAlmanac - Class in org.orekit.gnss.rflink.gps

Almanac for dummy SV.

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Subtract an offset from the instance.

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Subtract an offset from the instance.

SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Sun.

SUN_PULSATION - Static variable in class org.orekit.frames.SingleParameterFitter

Sun pulsation, one year period.

SUN_RADIUS - Static variable in interface org.orekit.utils.Constants

Sun radius: 695700000 m (source: resolution B3 from IAU 2015).

SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader

Regular expression for supported files names.

supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField

Indicates whether this model supports time transformation or not.

swap12() - Method in class org.orekit.attitudes.FieldInertia

Swap axes 1 and 2.

swap12() - Method in class org.orekit.attitudes.Inertia

Swap axes 1 and 2.

swap13() - Method in class org.orekit.attitudes.FieldInertia

Swap axes 1 and 3.

swap13() - Method in class org.orekit.attitudes.Inertia

Swap axes 1 and 3.

swap23() - Method in class org.orekit.attitudes.FieldInertia

Swap axes 2 and 3.

swap23() - Method in class org.orekit.attitudes.Inertia

Swap axes 2 and 3.

switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler

Method called when attitude is switched from one law to another law.

sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4

Initialization proper to each propagator (SGP or SDP).

sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Initialization proper to each propagator (SGP or SDP).

sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4

Initialization proper to each propagator (SGP or SDP).

sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Initialization proper to each propagator (SGP or SDP).

sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4

Propagation proper to each propagator (SGP or SDP).

sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Propagation proper to each propagator (SGP or SDP).

sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4

Propagation proper to each propagator (SGP or SDP).

sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Propagation proper to each propagator (SGP or SDP).

SystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Constructor.

SystemTimeOffsetMessage - Class in org.orekit.files.rinex.navigation

Container for data contained in a System Time Offset navigation message.

SystemTimeOffsetMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage

Simple constructor.

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

3/2 * C1.

t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

3/2 * C1.

TabulatedLofOffset - Class in org.orekit.attitudes

This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.

TabulatedLofOffset(Frame, LOF, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset

Creates new instance.

TabulatedLofOffset(Frame, LOF, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.attitudes.TabulatedLofOffset

Creates new instance.

TabulatedProvider - Class in org.orekit.attitudes

This class handles an attitude provider interpolating from a predefined table.

TabulatedProvider(Frame, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider

Creates new instance.

TabulatedProvider(List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, AttitudeBuilder) - Constructor for class org.orekit.attitudes.TabulatedProvider

Creates new instance.

TAIScale - Class in org.orekit.time

International Atomic Time.

TAIUTCDatFilesLoader - Class in org.orekit.time

Loader for UTC-TAI extracted from tai-utc.dat file from USNO.

TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader

Build a loader for tai-utc.dat file from USNO.

TAIUTCDatFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader

Build a loader for tai-utc.dat file from USNO.

TAIUTCDatFilesLoader.Parser - Class in org.orekit.time

Internal class performing the parsing.

TargetPointing - Class in org.orekit.attitudes

This class handles target pointing attitude provider.

TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body frame and target expressed in Cartesian coordinates.

TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body shape and target expressed in geodetic coordinates.

TCBScale - Class in org.orekit.time

Barycentric Coordinate Time.

TCGScale - Class in org.orekit.time

Geocentric Coordinate Time.

TDBScale - Class in org.orekit.time

Barycentric Dynamic Time.

Tdm - Class in org.orekit.files.ccsds.ndm.tdm

This class stores all the information of the CCSDS Tracking Data Message parsed by TDMParser or TDMXMLParser.

Tdm(TdmHeader, List<Segment<TdmMetadata, ObservationsBlock>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Tdm

Simple constructor.

TdmDataKey - Enum in org.orekit.files.ccsds.ndm.tdm

Keys for TDM observations entries, except the measurements themselves.

TdmHeader - Class in org.orekit.files.ccsds.ndm.tdm

Header of a CCSDS Tracking Data Message.

TdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmHeader

Constructor.

TdmMetadata - Class in org.orekit.files.ccsds.ndm.tdm

The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).

TdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Create a new TDM meta-data.

TdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.tdm

Keys for TDM container entries.

TdmParser - Class in org.orekit.files.ccsds.ndm.tdm

Class for CCSDS Tracking Data Message parsers.

TdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, RangeUnitsConverter, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmParser

Complete constructor.

TdmWriter - Class in org.orekit.files.ccsds.ndm.tdm

Writer for CCSDS Tracking Data Message.

TdmWriter(IERSConventions, DataContext, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmWriter

Complete constructor.

TDOA - Class in org.orekit.estimation.measurements

Class modeling a Time Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.

TDOA(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TDOA

Simple constructor.

TDOABuilder - Class in org.orekit.estimation.measurements.generation

Builder for TDOA measurements.

TDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TDOABuilder

Simple constructor.

TDOAIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical TDOA measurements with ionospheric delay.

TDOAIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier

Constructor.

TDOATroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical TDOA measurements with tropospheric delay.

TDOATroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier

Constructor.

TectonicsDisplacement - Class in org.orekit.models.earth.displacement

Modeling of displacement of reference points due to plate tectonics.

TectonicsDisplacement(AbsoluteDate, Vector3D) - Constructor for class org.orekit.models.earth.displacement.TectonicsDisplacement

Simple constructor.

TESLA - Static variable in class org.orekit.utils.units.Unit

tesla unit.

tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Tessellate a zone of interest into tiles.

THDT - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

THDT.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRange

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRangeRate

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.FDOA

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TDOA

Estimate the theoretical value.

theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange

Estimate the theoretical value.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRange

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRangeRate

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.FDOA

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TDOA

Estimate the theoretical value without derivatives.

theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange

Estimate the theoretical value without derivatives.

theoryIsSgpSdp() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata

Check if mean element theory in SGP or SDP.

theta2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

cos io squared.

theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cos io squared.

ThirdBodyAttraction - Class in org.orekit.forces.gravity

Third body attraction force model.

ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction

Simple constructor.

ThirdBodyAttractionEpoch - Class in org.orekit.forces.gravity

Third body attraction force model.

ThirdBodyAttractionEpoch(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttractionEpoch

Simple constructor.

ThreeEighthesFieldIntegratorBuilder<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion

Builder for ThreeEighthesFieldIntegrator.

ThreeEighthesFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder

Constructor.

ThreeEighthesFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder

Constructor using a "fielded" step.

ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ThreeEighthesIntegrator.

ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a new instance.

THRUST - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Parameter name for thrust.

THRUST_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel

Thrust scaling factor.

ThrustDirectionAndAttitudeProvider - Class in org.orekit.forces.maneuvers.propulsion

This class is used in to both manage the attitude of the satellite and the direction of thrust.

ThrustDirectionProvider - Interface in org.orekit.forces.maneuvers.propulsion

Interface to compute the thrust direction of a maneuver.

ThrustPropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion

Interface for a thrust-based propulsion model.

THRUSTX_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Parameter name for the scale factor on the X component of the thrust in S/C frame.

THRUSTY_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Parameter name for the scale factor on the Y component of the thrust in S/C frame.

THRUSTZ_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel

Parameter name for the scale factor on the Z component of the thrust in S/C frame.

TidalDisplacement - Class in org.orekit.models.earth.displacement

Modeling of displacement of reference points due to tidal effects.

TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement

Simple constructor.

Tide - Class in org.orekit.models.earth.displacement

Class representing a tide.

Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide

Simple constructor.

Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide

Simple constructor.

TideSystem - Enum in org.orekit.forces.gravity.potential

Enumerate for tie systems.

TideSystemProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide tide systems.

Tile - Class in org.orekit.models.earth.tessellation

Simple data structure for a quadrilateral tile shape on a body surface.

Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile

Create a tile.

TileAiming - Interface in org.orekit.models.earth.tessellation

Interface defining the aiming direction of tiles.

TimeComponents - Class in org.orekit.time

Class representing a time within the day broken up as hour, minute and second components.

TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from its clock elements.

TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents

Build a time from its clock elements.

TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeConverter - Class in org.orekit.files.ccsds.definitions

Dates reader/writer.

TimeConverter(TimeScale, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.definitions.TimeConverter

Build a time system.

TimeDerivativesEquations - Interface in org.orekit.propagation.numerical

Interface summing up the contribution of several forces into orbit and mass derivatives.

TimeInterpolator<T extends TimeStamped> - Interface in org.orekit.time

This interface represents objects that can interpolate a time stamped value with respect to time.

TimeScalarFunction - Interface in org.orekit.time

This interface represents a scalar function of time.

TimeScale - Interface in org.orekit.time

Interface for time scales.

TimeScales - Interface in org.orekit.time

A collection of TimeScales.

TimeScalesFactory - Class in org.orekit.time

Factory for predefined time scales.

timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the offset between two time scales at the current instant.

timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Compute the offset between two time scales at the current instant.

TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time

This interface represents objects that can be shifted in time.

TimeSpanDragForce - Class in org.orekit.forces.drag

Time span atmospheric drag force model.

TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce

Constructor with default UTC time scale for the default names of the drag parameter drivers.

TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce

Constructor.

TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere

Time span estimated tropospheric model.

TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Constructor with default UTC time scale.

TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel

Constructor with default UTC time scale.

TimeSpanMap<T> - Class in org.orekit.utils

Container for objects that apply to spans of time.

TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap

Create a map containing a single object, initially valid throughout the timeline.

TimeSpanMap.Span<S> - Class in org.orekit.utils

Holder for one time span.

TimeSpanMap.Transition<S> - Class in org.orekit.utils

Class holding transition times.

TimeSpanParametricAcceleration - Class in org.orekit.forces.empirical

Time span parametric acceleration model.

TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Simple constructor.

TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration

Simple constructor.

TimeStamped - Interface in org.orekit.time

This interface represents objects that have a AbsoluteDate date attached to them.

TimeStampedAngularCoordinates - Class in org.orekit.utils

time-stamped version of AngularCoordinates.

TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a TimeStampedAngularCoordinates from a FieldRotation<Derivative>.

TimeStampedAngularCoordinatesHermiteInterpolator - Class in org.orekit.utils

Class using Hermite interpolator to interpolate time stamped angular coordinates.

TimeStampedAngularCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedAngularCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

/** Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedAngularCoordinatesHermiteInterpolator(int, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedAngularCoordinatesHermiteInterpolator(int, double, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator

Constructor.

TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils

Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.

TimeStampedCacheException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.

TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedDouble - Class in org.orekit.time

Class that associates a double with a date.

TimeStampedDouble(double, AbsoluteDate) - Constructor for class org.orekit.time.TimeStampedDouble

Constructor.

TimeStampedDoubleHermiteInterpolator - Class in org.orekit.time

Hermite interpolator of time stamped double value.

TimeStampedDoubleHermiteInterpolator() - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedDoubleHermiteInterpolator(int) - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator

Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).

TimeStampedDoubleHermiteInterpolator(int, double) - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator

Constructor.

TimeStampedField<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.time

Class that associates a field with a date.

TimeStampedField(KK, AbsoluteDate) - Constructor for class org.orekit.time.TimeStampedField

Constructor with normal date.

TimeStampedField(KK, FieldAbsoluteDate<KK>) - Constructor for class org.orekit.time.TimeStampedField

Constructor.

TimeStampedFieldAngularCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldAngularCoordinates.

TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds an instance for a regular TimeStampedAngularCoordinates.

TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.

TimeStampedFieldAngularCoordinatesHermiteInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.utils

Class using Hermite interpolator to interpolate time stamped angular coordinates.

TimeStampedFieldAngularCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldAngularCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

/** Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldAngularCoordinatesHermiteInterpolator(int, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldAngularCoordinatesHermiteInterpolator(int, double, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator

Constructor.

TimeStampedFieldHermiteInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.time

Hermite interpolator of time stamped field value.

TimeStampedFieldHermiteInterpolator() - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldHermiteInterpolator(int) - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldHermiteInterpolator(int, double) - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator

Constructor.

TimeStampedFieldPVCoordinates<T extends org.hipparchus.CalculusFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldPVCoordinates.

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a PVCoordinates pair.

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a PVCoordinates pair.

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Basic constructor.

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Basic constructor.

TimeStampedFieldPVCoordinates(Field<T>, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Constructor from Field and TimeStampedPVCoordinates.

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Subtractive constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Subtractive constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.

TimeStampedFieldPVCoordinatesHermiteInterpolator<KK extends org.hipparchus.CalculusFieldElement<KK>> - Class in org.orekit.utils

Class using a Hermite interpolator to interpolate time stamped position-velocity-acceleration coordinates.

TimeStampedFieldPVCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldPVCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldPVCoordinatesHermiteInterpolator(int, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedFieldPVCoordinatesHermiteInterpolator(int, double, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator

Constructor.

TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils

Generator to use for creating entries in time stamped caches.

TimeStampedPair<K extends TimeStamped,V extends TimeStamped> - Class in org.orekit.time

Pair of time stamped values being defined at the same date.

TimeStampedPair(K, V) - Constructor for class org.orekit.time.TimeStampedPair

Constructor.

TimeStampedPair(K, V, double) - Constructor for class org.orekit.time.TimeStampedPair

Constructor.

TimeStampedPVCoordinates - Class in org.orekit.utils

time-stamped version of PVCoordinates.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates pair.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position and velocity.

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position velocity acceleration coordinates.

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Multiplicative constructor

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Subtractive constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<Derivative>.

TimeStampedPVCoordinatesHermiteInterpolator - Class in org.orekit.utils

Class using a Hermite interpolator to interpolate time stamped position-velocity-acceleration coordinates.

TimeStampedPVCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedPVCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedPVCoordinatesHermiteInterpolator(int, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).

TimeStampedPVCoordinatesHermiteInterpolator(int, double, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator

Constructor.

TimeSystem - Enum in org.orekit.files.ccsds.definitions

The set of time systems defined in CCSDS standards (ADM, ODM, NDM).

TimeSystem - Enum in org.orekit.gnss

Enumerate for the time systems used in navigation files.

TimeSystemCorrection - Class in org.orekit.files.rinex.navigation

Container for time system corrections.

TimeSystemCorrection(String, AbsoluteDate, double, double) - Constructor for class org.orekit.files.rinex.navigation.TimeSystemCorrection

Constructor.

TimetagReference - Enum in org.orekit.files.ccsds.ndm.tdm

Reference for time tag.

TimeVectorFunction - Interface in org.orekit.time

This interface represents a multi-valued function of time.

TimingSystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Empty constructor.

tle - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

Initial state.

TLE - Class in org.orekit.propagation.analytical.tle

This class is a container for a single set of TLE data.

TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from unparsed two lines.

TLE(String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from unparsed two lines using the given time scale as UTC.

TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from already parsed elements.

TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from already parsed elements using the given time scale as UTC.

tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

Initial state.

TLEConstants - Class in org.orekit.propagation.analytical.tle

Constants necessary to TLE propagation.

TleGenerationAlgorithm - Interface in org.orekit.propagation.analytical.tle.generation

This interface provides a way to generate a TLE from a spacecraft state.

TleGenerationUtil - Class in org.orekit.propagation.analytical.tle.generation

Utility class for TLE generation algorithm.

TLEPropagator - Class in org.orekit.propagation.analytical.tle

This class provides elements to propagate TLE's.

TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator

Protected constructor for derived classes.

TLEPropagator(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator

Protected constructor for derived classes.

TLEPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for TLEPropagator.

TLEPropagatorBuilder(TLE, PositionAngleType, double, TleGenerationAlgorithm) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a new instance.

TLEPropagatorBuilder(TLE, PositionAngleType, double, DataContext, TleGenerationAlgorithm) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a new instance.

toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate

Transform the FieldAbsoluteDate in an AbsoluteDate.

toAbsolutePVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Converts to an AbsolutePVCoordinates instance.

toAngular(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState

Convert to angular coordinates.

toAngular(AbsoluteDate, RotationOrder, Rotation, int, double[]) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType

Convert to angyla coordinates.

toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates

Convert to a regular angular coordinates.

toAttitude() - Method in class org.orekit.attitudes.FieldAttitude

Converts to an Attitude instance.

toAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Transforms the FieldAuxiliaryElements instance into an AuxiliaryElements instance.

toCartesian(AbsoluteDate, double[], OneAxisEllipsoid, double) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

Convert to Cartesian coordinates.

toCartesian(OneAxisEllipsoid, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Convert to Cartesian coordinates.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.Calibration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.CalibrationDetail

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

Get a string representation of the instance in the CRD format.

toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Get a string representation of the instance in the CRD format.

toDate(DateComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Create a date from components.

toDate(DateComponents, TimeComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Create a date from components.

toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Convert the instance to a Java Date.

toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Convert the instance to a Java Date.

toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.

toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldPVCoordinates<DerivativeStructure>.

toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates

Transform the instance to a FieldRotation<DerivativeStructure>.

toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates

Transform the instance to a FieldRotation<FieldDerivativeStructure>.

toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldVector3D<FieldDerivativeStructure>.

toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldVector3D<DerivativeStructure>.

toEncounter() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition

Get new encounter instance.

toEopEntry(IERSConventions.NutationCorrectionConverter, ITRFVersion, TimeScale) - Method in class org.orekit.files.sinex.SinexEopEntry

Converts to an EOPEntry.

toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider

Convert to a FieldPVCoordinatesProvider with a specific type.

toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator

Convert a point on the unit 2-sphere to geodetic coordinates.

TokenType - Enum in org.orekit.files.ccsds.utils.lexical

Enumerate for tokens occurring during CCSDS file parsing.

tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Estimate tolerance vectors for integrators.

tolerances(T, T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator

Estimate tolerance vectors for integrators when propagating in orbits.

tolerances(double, AbsolutePVCoordinates) - Static method in class org.orekit.propagation.numerical.NumericalPropagator

Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.

tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator

Estimate tolerance vectors for integrators when propagating in orbits.

tolerances(double, double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator

Estimate tolerance vectors for integrators when propagating in orbits.

tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

tolerances(double, double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

tolerances(T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

tolerances(T, T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

toMap() - Method in class org.orekit.utils.DoubleArrayDictionary

Create a map from the instance.

toMap() - Method in class org.orekit.utils.FieldArrayDictionary

Create a map from the instance.

ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext

2 / (n² * a) .

ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext

2 / (n² * a) .

toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit

toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit

Transforms the FieldOrbit instance into an Orbit instance.

toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Transforms the FieldOrbit instance into an Orbit instance.

toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Transforms the FieldOrbit instance into an Orbit instance.

toOrbit() - Method in class org.orekit.orbits.FieldOrbit

Transforms the FieldOrbit instance into an Orbit instance.

toOrbitRelativeFrame() - Method in enum org.orekit.frames.LOFType

Convert current local orbital frame to CCSDS equivalent orbit relative frame when possible, null otherwise.

toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse

Project a point to the ellipse plane.

toPlane(FieldVector3D<T>) - Method in class org.orekit.bodies.FieldEllipse

Project a point to the ellipse plane.

TopocentricFrame - Class in org.orekit.frames

Topocentric frame.

TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame

Simple constructor.

toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates

Convert to a constant position-velocity.

toRawElements(TimeStampedPVCoordinates, Frame, OneAxisEllipsoid, double) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

Convert to raw elements array.

toRotation(RotationOrder, double[]) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType

Convert to rotation.

TorqueFree - Class in org.orekit.attitudes

This class handles torque-free motion of a general (non-symmetrical) body.

TorqueFree(Attitude, Inertia) - Constructor for class org.orekit.attitudes.TorqueFree

Simple constructor.

toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit

Convert value from instance unit to corresponding SI unit.

toSI(double) - Method in class org.orekit.utils.units.Unit

Convert a value to SI units.

toSI(Double) - Method in class org.orekit.utils.units.Unit

Convert a value to SI units.

toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse

Create a point from its ellipse-relative coordinates.

toSpace(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse

Create a point from its ellipse-relative coordinates.

toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState

To convert a FieldSpacecraftState instance into a SpacecraftState instance.

toStateCovariance() - Method in class org.orekit.propagation.FieldStateCovariance

Get new state covariance instance.

toStaticTransform() - Method in class org.orekit.frames.FieldTransform

Create a so-called static transform from the instance.

toStaticTransform() - Method in class org.orekit.frames.Transform

Create a so-called static transform from the instance.

toStaticTransform() - Method in class org.orekit.propagation.FieldSpacecraftState

Compute the static transform from state defining frame to spacecraft frame.

toStaticTransform() - Method in class org.orekit.propagation.SpacecraftState

Compute the static transform from state defining frame to spacecraft frame.

toString() - Method in class org.orekit.bodies.FieldGeodeticPoint

toString() - Method in class org.orekit.bodies.GeodeticPoint

toString() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame

toString() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType

toString() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType

toString() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints

toString() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

toString() - Method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable

.

toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus

toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory

toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

toString() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement

toString() - Method in class org.orekit.files.ilrs.CRD.Calibration

toString() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement

toString() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement

toString() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement

toString() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement

toString() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration

toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

toString() - Method in class org.orekit.frames.Frame

New definition of the java.util toString() method.

toString() - Method in class org.orekit.frames.OrphanFrame

toString() - Method in class org.orekit.gnss.metric.ntrip.GnssData

toString() - Method in enum org.orekit.gnss.metric.ntrip.NavigationSystem

toString() - Method in class org.orekit.models.earth.GeoMagneticElements

toString() - Method in class org.orekit.orbits.CartesianOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.CircularOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.EquinoctialOrbit

Returns a string representation of this equinoctial parameters object.

toString() - Method in class org.orekit.orbits.FieldCartesianOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.FieldCircularOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit

Returns a string representation of this equinoctial parameters object.

toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit

Returns a string representation of this Keplerian parameters object.

toString() - Method in class org.orekit.orbits.KeplerianOrbit

Returns a string representation of this Keplerian parameters object.

toString() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Get a string representation of this TLE set.

toString() - Method in class org.orekit.propagation.analytical.tle.TLE

Get a string representation of this TLE set.

toString() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event

toString() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event

toString() - Method in class org.orekit.propagation.FieldSpacecraftState

toString() - Method in class org.orekit.propagation.SpacecraftState

toString() - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location with up to 16 digits of precision for the seconds value.

toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.

toString(int) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a local time.

toString(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a local time.

toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a time zone.

toString(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location for a time zone.

toString() - Method in class org.orekit.time.BDTScale

toString() - Method in class org.orekit.time.DateComponents

Get a string representation (ISO-8601) of the date.

toString() - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this pair.

toString(int) - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this date-time, rounded to millisecond precision.

toString(int, int) - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this date-time, rounded to the given precision.

toString() - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location with up to 16 digits of precision for the seconds value.

toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.

toString(int) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a local time.

toString(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a local time.

toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a time zone.

toString(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate

Get a String representation of the instant location for a time zone.

toString() - Method in class org.orekit.time.GalileoScale

toString() - Method in class org.orekit.time.GLONASSScale

toString() - Method in class org.orekit.time.GMSTScale

toString() - Method in class org.orekit.time.GPSScale

toString() - Method in class org.orekit.time.IRNSSScale

toString() - Method in class org.orekit.time.QZSSScale

toString() - Method in class org.orekit.time.SatelliteClockScale

toString() - Method in class org.orekit.time.TAIScale

toString() - Method in class org.orekit.time.TCBScale

toString() - Method in class org.orekit.time.TCGScale

toString() - Method in class org.orekit.time.TDBScale

toString() - Method in class org.orekit.time.TimeComponents

Get a string representation of the time including the offset from UTC.

toString() - Method in class org.orekit.time.TTScale

toString() - Method in class org.orekit.time.UT1Scale

toString() - Method in class org.orekit.time.UTCScale

toString() - Method in class org.orekit.utils.DoubleArrayDictionary

Get a string representation of the dictionary.

toString() - Method in class org.orekit.utils.FieldArrayDictionary

Get a string representation of the dictionary.

toString() - Method in class org.orekit.utils.FieldPVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache

toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache

toString() - Method in class org.orekit.utils.ParameterDriver

Get a text representation of the parameter.

toString() - Method in class org.orekit.utils.PVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Return a string representation of this date, position, velocity, and acceleration.

toString(TimeScale) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Return a string representation of this date, position, velocity, and acceleration.

toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates

Return a string representation of this date, position, velocity, and acceleration.

toString(TimeScale) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Return a string representation of this date, position, velocity, and acceleration.

toString() - Method in class org.orekit.utils.units.Unit

toString() - Method in class org.orekit.utils.units.UnitsConverter

toStringRfc3339(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Represent the given date as a string according to the format in RFC 3339.

toStringRfc3339() - Method in class org.orekit.time.DateTimeComponents

Represent the given date and time as a string according to the format in RFC 3339.

toStringWithoutUtcOffset(TimeScale, int) - Method in class org.orekit.time.AbsoluteDate

Return a string representation of this date-time, rounded to the given precision.

toStringWithoutUtcOffset() - Method in class org.orekit.time.DateTimeComponents

Get a string representation of the date-time without the offset from UTC.

toStringWithoutUtcOffset(int, int) - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this date-time, rounded to the given precision.

toStringWithoutUtcOffset() - Method in class org.orekit.time.TimeComponents

Get a string representation of the time without the offset from UTC.

TOTAL_ELECTRON_CONTENT_UNIT - Static variable in class org.orekit.utils.units.Unit

Total Electron Content Unit.

TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel

Name of the parameter of this model: the total zenith delay.

toTaylorProvider() - Method in class org.orekit.utils.AbsolutePVCoordinates

Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).

toTaylorProvider() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates

Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).

toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).

toTimeStampedPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Convert to TimeStampedPVCoordinates.

toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Convert to a constant position-velocity.

toTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE

Convert FieldTLE into TLE.

toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState

Compute the transform from state defining frame to spacecraft frame.

toTransform() - Method in class org.orekit.propagation.SpacecraftState

Compute the transform from state defining frame to spacecraft frame.

toUnivariateDerivative1PV() - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative1>.

toUnivariateDerivative1PV() - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldPVCoordinates<UnivariateDerivative1>.

toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.AngularCoordinates

Transform the instance to a FieldRotation<UnivariateDerivative1>.

toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates

Transform the instance to a FieldRotation<UnivariateDerivative1>.

toUnivariateDerivative1Vector() - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldVector3D<FieldUnivariateDerivative1>.

toUnivariateDerivative1Vector() - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldVector3D<UnivariateDerivative1>.

toUnivariateDerivative2PV() - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative2>.

toUnivariateDerivative2PV() - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldPVCoordinates<UnivariateDerivative2>.

toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.AngularCoordinates

Transform the instance to a FieldRotation<UnivariateDerivative2>.

toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates

Transform the instance to a FieldRotation<UnivariateDerivative2>.

toUnivariateDerivative2Vector() - Method in class org.orekit.utils.FieldPVCoordinates

Transform the instance to a FieldVector3D<FieldUnivariateDerivative2>.

toUnivariateDerivative2Vector() - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldVector3D<UnivariateDerivative2>.

TrackingCoordinates - Class in org.orekit.utils

Container for azimut/elevation/range coordinates as seen from a ground point.

TrackingCoordinates(double, double, double) - Constructor for class org.orekit.utils.TrackingCoordinates

Simple constructor.

TrackingMode - Enum in org.orekit.files.ccsds.ndm.tdm

Tracking mode.

TRAJ_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Trajectory line element for XML messages.

TrajectoryState - Class in org.orekit.files.ccsds.ndm.odm.ocm

Trajectory state entry.

TrajectoryState(OrbitElementsType, AbsoluteDate, String[], int, List<Unit>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Simple constructor.

TrajectoryState(OrbitElementsType, AbsoluteDate, double[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState

Simple constructor.

TrajectoryStateHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm

Trajectory state history.

TrajectoryStateHistory(TrajectoryStateHistoryMetadata, List<TrajectoryState>, OneAxisEllipsoid, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Simple constructor.

TrajectoryStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm

Metadata for trajectory state history.

TrajectoryStateHistoryMetadata(AbsoluteDate, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Simple constructor.

TrajectoryStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm

Keys for rajectory state history container entries.

transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape

Transform a Cartesian point to a surface-relative point.

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape

Transform a Cartesian point to a surface-relative point.

transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape

Transform a surface-relative point to a Cartesian point.

transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape

Transform a surface-relative point to a Cartesian point.

transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a surface-relative point to a Cartesian point.

transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a surface-relative point to a Cartesian point.

transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a Cartesian point to a surface-relative point.

Transform - Class in org.orekit.frames

Transformation class in three dimensional space.

Transform(AbsoluteDate, PVCoordinates, AngularCoordinates) - Constructor for class org.orekit.frames.Transform

Build a transform from its primitive operations.

Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform.

Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first and second time derivatives.

Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform

Build a transform by combining two existing ones.

transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid

Transform a Cartesian point to a surface-relative point.

transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid

Transform a Cartesian point to a surface-relative point.

transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid

Transform a surface-relative point to a Cartesian point.

transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid

Transform a surface-relative point to a Cartesian point.

transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF

Get the transform from an inertial frame defining position-velocity and the local orbital frame.

transformFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF

Get the transform from an inertial frame defining position-velocity and the local orbital frame.

transformFromLOF(LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF

Get the rotation from input commonly used local orbital frame to the instance.

transformFromLOF(LOF, AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF

Get the rotation from input local orbital frame to the instance.

transformFromLOFInToLOFOut(LOF, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Static method in interface org.orekit.frames.LOF

Get the transform from input to output local orbital frame.

transformFromLOFInToLOFOut(LOF, LOF, AbsoluteDate, PVCoordinates) - Static method in interface org.orekit.frames.LOF

Get the transform from input to output local orbital frame.

TransformGenerator - Class in org.orekit.frames

Generator to use transforms in GenericTimeStampedCache.

TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator

simple constructor.

transformLine(Line) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a line.

transformLine(FieldLine<T>) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a line.

transformLine(Line) - Method in interface org.orekit.frames.StaticTransform

Transform a line.

transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using secular variation coefficients.

transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.

transformPosition(Vector3D) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a position vector (including translation effects).

transformPosition(FieldVector3D<T>) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a position vector (including translation effects).

transformPosition(Vector3D) - Method in interface org.orekit.frames.StaticTransform

Transform a position vector (including translation effects).

transformPosition(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform

Transform a position vector (including translation effects).

TransformProvider - Interface in org.orekit.frames

Interface for Transform providers.

TransformProviderUtils - Class in org.orekit.frames

Utility for Transform providers.

transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform

Transform PVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform FieldPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformVector(Vector3D) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a vector (ignoring translation effects).

transformVector(FieldVector3D<T>) - Method in interface org.orekit.frames.FieldStaticTransform

Transform a vector (ignoring translation effects).

transformVector(Vector3D) - Method in interface org.orekit.frames.StaticTransform

Transform a vector (ignoring translation effects).

transformVector(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform

Transform a vector (ignoring translation effects).

TransponderConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration

Empty constructor.

TriggerDate - Class in org.orekit.forces.maneuvers.jacobians

Generator for one column of a Jacobian matrix for special case of trigger dates.

TriggerDate(String, String, boolean, Maneuver, double) - Constructor for class org.orekit.forces.maneuvers.jacobians.TriggerDate

Simple constructor.

TroposphericModelUtils - Class in org.orekit.models.earth.troposphere

Utility class for tropospheric models.

TRUE_ANOM - Static variable in enum org.orekit.orbits.OrbitType

Name for mean anomaly.

TRUE_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for mean argument of latitude.

TRUE_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType

Name for mean argument of longitude.

trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit

Computes the eccentric latitude argument from the true latitude argument.

trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit

Computes the eccentric longitude argument from the true longitude argument.

trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit

Computes the eccentric latitude argument from the true latitude argument.

trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit

Computes the eccentric longitude argument from the true longitude argument.

TruncatingFilter - Class in org.orekit.data

Filter for truncating line-oriented files.

TruncatingFilter(int) - Constructor for class org.orekit.data.TruncatingFilter

Simple constructor.

tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Try to accept the current history up to the given time.

tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState

Try to accept the current history up to the given time.

tsi - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

tsi from SPTRCK #3.

tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

tsi from SPTRCK #3.

TTScale - Class in org.orekit.time

Terrestrial Time as defined by IAU(1991) recommendation IV.

TurnAroundRange - Class in org.orekit.estimation.measurements

Class modeling a turn-around range measurement using a primary ground station and a secondary ground station.

TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange

Simple constructor.

TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation

Builder for TurnAroundRange measurements.

TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder

Simple constructor.

TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical TurnAroundRange measurement with ionospheric delay.

TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier

Constructor.

TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers

Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.

TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier

Constructor.

TWO_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

Constant 2.0 / 3.0.

TwoBodiesBaryFrame - Class in org.orekit.frames

Class creating the inertial barycenter frame from two bodies.

TwoBodiesBaryFrame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.TwoBodiesBaryFrame

Simple constructor.

TwoDVariation - Class in org.orekit.gnss.antenna

Interpolator for 2D phase center variation data.

TwoDVariation(double, double, double, double[][]) - Constructor for class org.orekit.gnss.antenna.TwoDVariation

Simple constructor.

twoWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier

Apply a modifier to a two-way range measurement.

Type - Enum in org.orekit.gnss.metric.ntrip

Enumerate for messages type.

TypeSvMessage - Class in org.orekit.files.rinex.navigation

Container for data shared by several navigation messages.

TypeSvMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.TypeSvMessage

Simple constructor.

U

unFixAmbiguity(ParameterDriver) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver

Un-fix an integer ambiguity (typically after a phase cycle slip).

Unit - Class in org.orekit.utils.units

Basic handling of multiplicative units.

Unit(String, double, Fraction, Fraction, Fraction, Fraction, Fraction) - Constructor for class org.orekit.utils.units.Unit

Simple constructor.

Units - Class in org.orekit.files.ccsds.definitions

Units used in CCSDS messages.

UNITS - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Name of the units attribute.

Units - Class in org.orekit.gnss.metric.parser

Units used in RTCM and IGS SSR messages.

UnitsCache - Class in org.orekit.utils.units

Cache for parsed units.

UnitsCache() - Constructor for class org.orekit.utils.units.UnitsCache

Simple constructor.

UnitsConverter - Class in org.orekit.utils.units

Converter between units.

UnitsConverter(Unit, Unit) - Constructor for class org.orekit.utils.units.UnitsConverter

Simple constructor.

unitsListToString(List<Unit>) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Convert a list of units to a bracketed string.

unitsListToString(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Convert a list of units to a bracketed string.

UnivariateProcessNoise - Class in org.orekit.estimation.sequential

Provider for a temporal evolution of the process noise matrix.

UnivariateProcessNoise(RealMatrix, LOFType, PositionAngleType, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise

Simple constructor.

UnivariateProcessNoise(RealMatrix, LOFType, PositionAngleType, UnivariateFunction[], UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise

Simple constructor.

UnixCompressFilter - Class in org.orekit.data

Filter for Unix compressed data.

UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter

Empty constructor.

UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm

Default name for unknown object.

UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm

Default name for unknown object.

unmodifiableView() - Method in class org.orekit.utils.DoubleArrayDictionary

Get an unmodifiable view of the dictionary.

unmodifiableView() - Method in class org.orekit.utils.FieldArrayDictionary

Get an unmodifiable view of the dictionary.

unnormalizeCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Un-nomalized the covariance matrix.

UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide un-normalized spherical harmonics coefficients.

UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

Un-normalized spherical harmonics coefficients evaluated at a specific instant.

unnormalizeInnovationCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Un-normalize the innovation covariance matrix.

unnormalizeKalmanGainMatrix(RealMatrix, double[], double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Un-normalize the Kalman gain matrix.

unnormalizeMeasurementJacobian(RealMatrix, double[], double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Un-normalize the measurement matrix.

unnormalizeStateTransitionMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil

Un-nomalized the state transition matrix.

UnscentedKalmanEstimator - Class in org.orekit.estimation.sequential

Implementation of an Unscented Kalman filter to perform orbit determination.

UnscentedKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential

Builder for an Unscented Kalman filter estimator.

UnscentedKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Default constructor.

UnscentedKalmanModel - Class in org.orekit.estimation.sequential

Class defining the process model dynamics to use with a UnscentedKalmanEstimator.

UnscentedKalmanModel(List<PropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.UnscentedKalmanModel

Unscented Kalman process model constructor (package private).

unscentedTransformProvider(UnscentedTransformProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder

Configure the unscented transform provider.

unscentedTransformProvider(UnscentedTransformProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder

Configure the unscented transform provider.

UnsupportedParameterException - Exception in org.orekit.errors

Exception for unsupported ParameterDriver in a model implementing ParameterDriversProvider.

UnsupportedParameterException(String, List<ParameterDriver>) - Constructor for exception org.orekit.errors.UnsupportedParameterException

Constructor.

unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException

Recover a OrekitException, possibly embedded in a MathRuntimeException.

unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a TimeStampedCacheException, possibly embedded in a OrekitException.

unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.

UpdatableFrame - Class in org.orekit.frames

Frame whose transform from its parent can be updated.

UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame

Build a non-inertial frame from its transform with respect to its parent.

UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame

Build a frame from its transform with respect to its parent.

updateAdditionalConstraints(int, double[]) - Method in class org.orekit.utils.AbstractMultipleShooting

Update the array of additional constraints.

updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Update state by adding all additional states.

updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Update state by adding all additional states.

updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris

Update state by adding all additional states.

updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Update state by adding all additional states.

updateFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester

Update the short periodic terms for the "field" elements.

updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Update a spacecraft mass due to maneuver.

updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Update the nominal spacecraft state.

updateNominalSpacecraftState(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Update the nominal spacecraft state.

updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Update the nominal spacecraft state.

updateReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.KalmanModel

Update the reference trajectories using the propagators as input.

updateReferenceTrajectory(DSSTPropagator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Update the reference trajectories using the propagator as input.

updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel

Update the DSST short periodic terms.

updateShortPeriods(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess

Update the DSST short periodic terms.

updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel

Update the DSST short periodic terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Update the short period terms.

updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Update the short period terms.

updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal

Update the short period terms.

updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame

Update the transform from parent frame implicitly according to two other frames.

updateUnmanagedStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Update state by adding unmanaged states.

updateUnmanagedStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator

Update state by adding unmanaged states.

UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities

Utility class to compute upper bounds for truncation algorithms.

URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Uranus.

USER_DEFINED_PREFIX - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined

Prefix for user defined parameters keys.

USER_DEFINED_XML_ATTRIBUTE - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined

Attribute name for user defined parameters keys.

USER_DEFINED_XML_TAG - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined

Tag name for user defined parameters keys.

UserDefined - Class in org.orekit.files.ccsds.ndm.odm

Container for user defined data.

UserDefined() - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefined

Create an empty data set.

UserDefinedWriter - Class in org.orekit.files.ccsds.ndm.odm

Writer for user defined parameters data.

UserDefinedWriter(String, String, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter

Create a writer.

UserDefinedXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical

Builder for user-defined parameters.

UserDefinedXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder

Empty constructor.

UserRangeAccuracy - Class in org.orekit.gnss.metric.messages.common

User Range Accuracy.

UserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.UserRangeAccuracy

Simple constructor.

UT1Scale - Class in org.orekit.time

Universal Time 1.

UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale

Simple constructor.

utc - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

UTC time scale.

utc - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

UTC time scale.

UtcId - Enum in org.orekit.files.rinex.navigation

Enumerate for the UTC ids.

UTCScale - Class in org.orekit.time

Coordinated Universal Time.

UTCTAIBulletinAFilesLoader - Class in org.orekit.time

Loader for UTC-TAI extracted from bulletin A files.

UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader

Build a loader for IERS bulletins A files.

UTCTAIBulletinAFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader

Build a loader for IERS bulletins A files.

UTCTAIHistoryFilesLoader - Class in org.orekit.time

Loader for UTC versus TAI history files.

UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader

Build a loader for UTC-TAI history file.

UTCTAIHistoryFilesLoader(DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader

Build a loader for UTC-TAI history file.

UTCTAIHistoryFilesLoader.Parser - Class in org.orekit.time

Internal class performing the parsing.

UTCTAIOffset - Class in org.orekit.time

Offset between UTC and TAI time scales.

UTCTAIOffsetsLoader - Interface in org.orekit.time

Interface for loading UTC-TAI offsets data files.

UTCTAIOffsetsLoader.Parser - Interface in org.orekit.time

Interface for parsing UTC-TAI offsets from a stream.

UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control

Empty constructor.

V

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata

Check is all mandatory entries have been initialized.

validate() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties

Check is all mandatory entries have been initialized.

validate() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent

Validate the file message for required and forbidden entries.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.section.CommentsContainer

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.section.Header

Check is all mandatory entries have been initialized.

validate(double) - Method in class org.orekit.files.ccsds.section.Metadata

Check is all mandatory entries have been initialized.

validate(double) - Method in interface org.orekit.files.ccsds.section.Section

Check is all mandatory entries have been initialized.

validate(boolean, String) - Method in class org.orekit.files.sp3.SP3

Check file is valid.

validFrom() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the start of the validity period for this model.

validityEnd() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider

Get end of validity for this provider.

validityStart() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider

Get start of validity for this provider.

validTo() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the end of the validity period for this model.

ValsecchiEncounterFrame - Class in org.orekit.frames.encounter

Valsecchi encounter local orbital frame based on Valsecchi formulation from : "Valsecchi, G.

ValsecchiEncounterFrame(PVCoordinates) - Constructor for class org.orekit.frames.encounter.ValsecchiEncounterFrame

Constructor.

ValsecchiEncounterFrame(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.ValsecchiEncounterFrame

Constructor.

value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(BodiesElements) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(double) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

value(T) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

value(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel

value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the value of the gravity field.

value(double, double) - Method in class org.orekit.gnss.antenna.OneDVariation

Evaluate phase center variation in one signal direction.

value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction

Evaluate phase center variation in one signal direction.

value(double, double) - Method in class org.orekit.gnss.antenna.TwoDVariation

Evaluate phase center variation in one signal direction.

value(FieldOrbit<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients

Evaluate the contributions of the short period terms.

value(T) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction

value(Orbit) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients

Evaluate the contributions of the short period terms.

value(double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.IntegrableFunction

value(FieldOrbit<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms

Evaluate the contributions of the short period terms.

value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms

Evaluate the contributions of the short period terms.

value(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient

Compute the value of the coefficient.

value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Compute the value of the coefficient.

value(AbsoluteDate) - Method in interface org.orekit.time.TimeScalarFunction

Compute a function of time.

value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScalarFunction

Compute a function of time.

value(AbsoluteDate) - Method in interface org.orekit.time.TimeVectorFunction

Compute a function of time.

value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeVectorFunction

Compute a function of time.

value(ParameterDriver, AbsoluteDate) - Method in interface org.orekit.utils.ParameterFunction

Evaluate the function.

value(SpacecraftState) - Method in interface org.orekit.utils.StateFunction

Evaluate the function.

value(SpacecraftState) - Method in interface org.orekit.utils.StateJacobian

Evaluate the Jacobian of the function.

valueChanged(double, ParameterDriver, AbsoluteDate) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter value has been changed.

valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurementBase.Status

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.AdMethodType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CenterName

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OnOff

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.YesNoUnknown

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmElements

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AltCovarianceType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmElements

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.section.HeaderKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.section.MetadataKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.FileFormat

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.IonosphericCorrectionType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.RegionCode

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.SbasId

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.UtcId

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.section.RinexLabels

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.rinex.utils.RinexFileType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.DataUsed

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3FileType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.maneuvers.Control3DVectorCostType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.encounter.EncounterLOFType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.ITRFVersion

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.LOFType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.Frequency

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.MeasurementType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.RecordType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Type

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.DataType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.ObservationTimeScale

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.ObservationType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.SatelliteSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.SignalCode

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.gnss.TimeSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitFamily

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.PositionAngleType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.VisibilityTrigger

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.PropagationType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.time.Month

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.IERSConventions

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.LagrangianPoints

Returns the enum constant of this type with the specified name.

values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.errors.OrekitMessages

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurementBase.Status

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.AdMethodType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.CenterName

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.OnOff

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.definitions.YesNoUnknown

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmElements

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AltCovarianceType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmElements

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.section.HeaderKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.section.MetadataKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.utils.FileFormat

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.navigation.IonosphericCorrectionType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.navigation.RegionCode

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.navigation.SbasId

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.navigation.UtcId

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.section.RinexLabels

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.rinex.utils.RinexFileType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.DataUsed

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3FileType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.maneuvers.Control3DVectorCostType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.encounter.EncounterLOFType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.ITRFVersion

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.LOFType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.antenna.SatelliteType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.Frequency

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.MeasurementType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.Authentication

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.RecordType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.ntrip.Type

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.parser.DataType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.ObservationTimeScale

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.ObservationType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.SatelliteSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.SignalCode

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.gnss.TimeSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.LibrationOrbitFamily

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.LibrationOrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.PositionAngleType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.FilterType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.VisibilityTrigger

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.PropagationType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.time.Month

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.IERSConventions

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.LagrangianPoints

Returns an array containing the constants of this enum type, in the order they are declared.

valueSpanMapChanged(TimeSpanMap<Double>, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver

Notify that a parameter value span map has been changed.

VEL_X - Static variable in enum org.orekit.orbits.OrbitType

Name for velocity along X.

VEL_Y - Static variable in enum org.orekit.orbits.OrbitType

Name for velocity along Y.

VEL_Z - Static variable in enum org.orekit.orbits.OrbitType

Name for velocity along Z.

VELOCITY_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Velocity accuracy unit.

VELOCITY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils

Velocity unit.

VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Venus.

VersionedITRF - Class in org.orekit.frames

Specific version of International Terrestrial Reference Frame.

VERTICAL_TOTAL_ELECTRON_CONTENT - Static variable in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel

Name of the parameter of this model: the Vertical Total Electron Content.

verticesRadius(double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType

Compute radius of cone going through vertices.

ViennaModelCoefficientsLoader - Class in org.orekit.models.earth.troposphere

Loads Vienna tropospheric coefficients a given input stream.

ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Constructor with supported names given by user.

ViennaModelCoefficientsLoader(String, double, double, ViennaModelType, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Constructor with supported names and source of mapping function files given by the user.

ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader

Constructor with default supported names.

ViennaModelType - Enum in org.orekit.models.earth.troposphere

Enumerate for Vienna tropospheric model 1 and 3.

ViennaOneModel - Class in org.orekit.models.earth.troposphere

The Vienna1 tropospheric delay model for radio techniques.

ViennaOneModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel

Build a new instance.

ViennaOneModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel

Build a new instance.

ViennaThreeModel - Class in org.orekit.models.earth.troposphere

The Vienna3 tropospheric delay model for radio techniques.

ViennaThreeModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel

Build a new instance.

ViennaThreeModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel

Build a new instance.

VisibilityTrigger - Enum in org.orekit.propagation.events

Enumerate for triggering visibility of spherical bodies.

VOLT - Static variable in class org.orekit.utils.units.Unit

Volt unit.

W

W_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units

Watt per kilograms units.

wasEndTagSeen() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser

Check if XML end tag has been seen.

WATT - Static variable in class org.orekit.utils.units.Unit

Watt unit.

WaypointPVBuilder - Class in org.orekit.utils

Builder class, enabling incremental building of an PVCoordinatesProvider instance using waypoints defined on an ellipsoid.

WaypointPVBuilder(WaypointPVBuilder.InterpolationFactory, OneAxisEllipsoid) - Constructor for class org.orekit.utils.WaypointPVBuilder

Create a new instance.

WaypointPVBuilder.InterpolationFactory - Interface in org.orekit.utils

Factory interface, creating the PVCoordinatesProvider instances between the provided waypoints.

WeatherModel - Interface in org.orekit.models.earth.weather

Defines a surface meteorology model that can be used to compute the different weather parameters (pressure, temperature, ...).

weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model

weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel

weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.WeatherModel

Calculates the weather parameters of the model.

WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.

WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from WGS84 model: .

WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from WGS84 model: 6378137.0 m.

WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from WGS84 model: 1.0 / 298.257223563.

WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².

WideLaneCombination - Class in org.orekit.estimation.measurements.gnss

Wide-Lane combination.

WindUp - Class in org.orekit.estimation.measurements.gnss

Modifier for wind-up effect in GNSS phase measurements.

WindUpFactory - Class in org.orekit.estimation.measurements.gnss

Factory for wind-up modifiers.

WindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.WindUpFactory

Simple constructor.

withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the minimum elevation for detection.

withConstantElevation(double) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the minimum elevation for detection.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up IERS conventions.

withDataContext(DataContext) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up data context used to retrieve frames, time scales, etc..

withDefaultInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Set up the default interpolation degree.

withDefaultMass(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Set up the default mass.

withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns for Doodson multipliers and Doodson number.

withElevationMask(ElevationMask) - Method in class org.orekit.gnss.DOPComputer

Set the elevation mask.

withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation mask for detection using the passed in mask object.

withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the elevation mask for detection using the passed in mask object.

withEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up the central body equatorial radius.

withFilter(Function<ParseToken, List<ParseToken>>) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Add a filter for parsed tokens.

withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of Delaunay multiplier.

withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of planetary multiplier.

withFlattening(double) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up the central body flattening.

withFunction(Function<FieldSpacecraftState<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector

Create a new event detector with a new g function, keeping all other attributes the same.

withFunction(ToDoubleFunction<SpacecraftState>) - Method in class org.orekit.propagation.events.FunctionalDetector

Create a new event detector with a new g function, keeping all other attributes the same.

withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up column of GMST tide multiplier.

withHandler(EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the event handler to call at event occurrences.

withHandler(FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the event handler to call at event occurrences.

withMargin(double) - Method in class org.orekit.propagation.events.EclipseDetector

Setup a margin to angle detection.

withMargin(T) - Method in class org.orekit.propagation.events.FieldEclipseDetector

Setup a margin to angle detection.

withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Setup the detector margin.

withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum checking interval.

withMaxCheck(AdaptableInterval) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum checking interval.

withMaxCheck(double) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the maximum checking interval.

withMaxCheck(FieldAdaptableInterval<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the maximum checking interval.

withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum number of iterations in the event time search.

withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the maximum number of iterations in the event time search.

withMinElevation(double) - Method in class org.orekit.gnss.DOPComputer

Set the minimum elevation.

withMinGap(double) - Method in class org.orekit.propagation.events.DateDetector

Setup minimum gap between added dates.

withMinGap(double) - Method in class org.orekit.propagation.events.FieldDateDetector

Setup minimum gap between added dates.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up mission reference date or Mission Elapsed Time or Mission Relative Time time systems.

withMu(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Set up the gravitational coefficient.

withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up optional column.

withParsedUnitsBehavior(ParsedUnitsBehavior) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Set up the behavior to adopt for handling parsed units.

withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to penumbra detection.

withPenumbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Setup the detector to penumbra detection.

withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser

Set up polynomial part parsing.

withRangeUnitsConverter(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder

Set up the converter for Range Units.

withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude

Get a similar attitude with a specific reference frame.

withReferenceFrame(Frame) - Method in class org.orekit.attitudes.FieldAttitude

Get a similar attitude with a specific reference frame.

withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation detector to use an atmospheric refraction model in its calculations.

withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.FieldElevationDetector

Setup the elevation detector to use an atmospheric refraction model in its calculations.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder

Set up flag for ignoring tidal effects when interpolating EOP.

withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns of the sine and cosine coefficients.

withSkimmingAltitude(double) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector

Setup the skimming altitude.

withSwitch(int, int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00

Change a switch.

withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the convergence threshold.

withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector

Setup the convergence threshold.

withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to full umbra detection.

withUmbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector

Setup the detector to full umbra detection.

WORD_SIZE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame

Words size.

write(Appendable, AttitudeEphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter

Write the passed in AttitudeEphemerisFile using the passed in Appendable.

write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter

Write the section, including surrounding tags.

write(Appendable, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter

Write the passed in AttitudeEphemerisFile using the passed in Appendable.

write(String, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter

Write the passed in AttitudeEphemerisFile to a file at the output path specified.

write(Appendable, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(String, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter

Write the passed in EphemerisFile to a file at the output path specified.

write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ilrs.CPFWriter

Write the passed in EphemerisFile using the passed in Appendable.

write(CPFHeader, Appendable, TimeScale) - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter

Write a line.

write(SP3) - Method in class org.orekit.files.sp3.SP3Writer

Write a SP3 file.

writeComment(Generator, String) - Method in class org.orekit.files.ccsds.ndm.NdmWriter

Write a comment line.

writeComments(List<String>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write comment lines.

writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Write comment lines.

writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Write comment lines.

writeCompleteFile(RinexObservation) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Write a complete observation file.

writeConstituent(Generator, F) - Method in class org.orekit.files.ccsds.ndm.NdmWriter

Write a constituent.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParametersWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParametersWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovarianceWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVectorWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.StateVectorWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter

Write the content of the section, excluding surrounding tags.

writeContent(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter

Write the content of the section, excluding surrounding tags.

writeEndOfFile() - Method in class org.orekit.files.ilrs.StreamingCpfWriter

Write end of file.

writeEntry(String, List<String>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, Enum<?>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, TimeConverter, AbsoluteDate, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, Double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, char, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, int, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write a single key/value entry.

writeEntry(String, String, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, List<String>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, Enum<?>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, TimeConverter, AbsoluteDate, boolean, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, char, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, int, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, Double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write a single key/value entry.

writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator

Write a single key/value entry.

writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Write a single key/value entry.

writeEphemerisLine(TimeStampedPVCoordinates) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment

Write ephemeris lines.

writeFooter(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Write footer for the file.

writeFooter(Generator) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Write footer for the file.

writeFooter(Generator) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Write footer for the file.

writeHeader(Generator, CdmHeader) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Write header for the file.

writeHeader(Generator, H) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Write header for the file.

writeHeader(Generator, H) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Write header for the file.

writeHeader() - Method in class org.orekit.files.ilrs.StreamingCpfWriter

Writes the CPF header for the file.

writeHeader(RinexObservationHeader) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Write header.

writeMessage(Generator, Ndm) - Method in class org.orekit.files.ccsds.ndm.NdmWriter

Write one complete message.

writeMessage(Generator, F) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Write one complete message.

writeObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Write one observation data set.

writeOneAttributeElement(String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Write an element with one attribute.

writePendingRinex2Observations() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Write one observation data set in RINEX 2 format.

writePendingRinex34Observations() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter

Write one observation data set in RINEX 3/4 format.

writeRawData(char) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write raw data.

writeRawData(CharSequence) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Write raw data.

writeRawData(char) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write raw data.

writeRawData(CharSequence) - Method in interface org.orekit.files.ccsds.utils.generation.Generator

Write raw data.

WriterBuilder - Class in org.orekit.files.ccsds.ndm

Builder for all CCSDS Message files writers.

WriterBuilder() - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder

Simple constructor.

WriterBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder

Simple constructor.

writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Write RelativeMetadata part only once after header.

writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter

writeSegment(Generator, CdmSegment) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Write one segment.

writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter

Write one segment.

writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Write one segment.

writeSegment(Generator, S) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter

Write one segment.

writeSegmentContent(Generator, double, Segment<AcmMetadata, AcmData>) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, AemSegment) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<AdmMetadata, ApmData>) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<OcmMetadata, OcmData>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, OemSegment) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<OmmMetadata, OmmData>) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<OdmCommonMetadata, OpmData>) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, Segment<TdmMetadata, ObservationsBlock>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmWriter

Write one segment content (without XML wrapping).

writeSegmentContent(Generator, double, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter

Write one segment content (without XML wrapping).

writeTwoAttributesElement(String, String, String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator

Write an element with two attributes.

writeUnits(Unit) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator

Check if unit must be written.

X

XJ2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

XJ2.

XJ3 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

XJ3.

XJ4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

XJ4.

XKE - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

XKE.

xl - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

L from SPTRCK #3.

xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

L from SPTRCK #3.

xmdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

common parameter for mean anomaly (M) computation.

xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for mean anomaly (M) computation.

XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOP XML files (IAU1980 compatibles).

XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOP XML files (IAU2000 compatibles).

XmlGenerator - Class in org.orekit.files.ccsds.utils.generation

Generator for eXtended Markup Language CCSDS messages.

XmlGenerator(Appendable, int, String, double, boolean, String) - Constructor for class org.orekit.files.ccsds.utils.generation.XmlGenerator

Simple constructor.

XmlLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical

Lexical analyzer for XML CCSDS messages.

XmlLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer

Simple constructor.

XmlStructureKey - Enum in org.orekit.files.ccsds.section

Keys for FileFormat.XML format structure.

XmlStructureProcessingState - Class in org.orekit.files.ccsds.section

ProcessingState for structure of FileFormat.XML CCSDS Messages.

XmlStructureProcessingState(String, AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.XmlStructureProcessingState

Simple constructor.

XmlSubStructureKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keywords for CDM data sub-structure in XML files.

XmlTokenBuilder - Interface in org.orekit.files.ccsds.utils.lexical

Builder for building ParseToken from XML elements.

xn0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

original recovered mean motion.

xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered mean motion.

xnodcf - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

common parameter for raan (OMEGA) computation.

xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

xnode - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

final RAAN.

xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final RAAN.

xnodot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator

common parameter for raan (OMEGA) computation.

xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

XYZCovariance - Class in org.orekit.files.ccsds.ndm.cdm

Container for XYZ covariance matrix data.

XYZCovariance(boolean) - Constructor for class org.orekit.files.ccsds.ndm.cdm.XYZCovariance

Simple constructor.

XYZCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm

Keys for CDM covariance matrix entries.

Y

YawCompensation - Class in org.orekit.attitudes

This class handles yaw compensation attitude provider.

YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation

Creates a new instance.

YawSteering - Class in org.orekit.attitudes

This class handles yaw steering law.

YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering

Creates a new instance.

YEAR - Static variable in class org.orekit.utils.units.Unit

Julian year unit.

YesNoUnknown - Enum in org.orekit.files.ccsds.definitions

Yes, No, Unknown values for various elements.

yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider

Check if this provider should yield so another provider has an opportunity to add missing parts.

yields(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider

Check if this provider should yield so another provider has an opportunity to add missing parts.

YUMAParser - Class in org.orekit.gnss

This class reads Yuma almanac files and provides GPS almanacs.

YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser

Simple constructor.

YUMAParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.YUMAParser

Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Z

ZeisModel - Class in org.orekit.propagation.semianalytical.dsst.forces

Zeis model for J2-squared second-order terms.

ZeisModel() - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel

Constructor.

ZEL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ZEL.

ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

0 represented as a polynomial.

zero() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry

Reset the value to zero.

zero() - Method in class org.orekit.utils.FieldArrayDictionary.Entry

Reset the value to zero.

ZERO - Static variable in class org.orekit.utils.PVCoordinates

Fixed position/velocity at origin (both p, v and a are zero vectors).

ZERO_CORRECTION - Static variable in class org.orekit.gnss.antenna.FrequencyPattern

Pattern with zero correction (i.e.

ZES - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ZES.

zIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod

Get the index of an entry in the Z transformation matrix.

ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider

Pattern for name of zip/jar archives.

ZipJarCrawler - Class in org.orekit.data

Helper class for loading data files from a zip/jar archive.

ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on filesystem.

ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on network.

ZNL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ZNL.

ZNS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants

ZNS.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z