Uses of Interface
org.orekit.propagation.Propagator

Packages that use Propagator

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
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.generation	This package provides Orbit Determination measurements generation.
org.orekit.estimation.sequential	The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
org.orekit.gnss	This package provides classes related to GNSS applications.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Uses of Propagator in org.orekit.attitudes

Methods in org.orekit.attitudes with parameters of type Propagator

Modifier and Type	Method and Description
void	AttitudesSequence.registerSwitchEvents(Propagator propagator) Register all wrapped switch events to the propagator.

Uses of Propagator in org.orekit.estimation.leastsquares

Methods in org.orekit.estimation.leastsquares that return Propagator

Modifier and Type	Method and Description
Propagator[]	AbstractBatchLSModel.createPropagators(org.hipparchus.linear.RealVector point) Create the propagators and parameters corresponding to an evaluation point.
Propagator[]	BatchLSEstimator.estimate() Estimate the orbital, propagation and measurements parameters.

Methods in org.orekit.estimation.leastsquares with parameters of type Propagator

Modifier and Type	Method and Description
protected abstract MatricesHarvester	AbstractBatchLSModel.configureHarvester(Propagator propagator) Configure the propagator to compute derivatives.
protected MatricesHarvester	BatchLSModel.configureHarvester(Propagator propagator) Configure the propagator to compute derivatives.
protected MatricesHarvester	DSSTBatchLSModel.configureHarvester(Propagator propagator) Configure the propagator to compute derivatives.
protected abstract Orbit	AbstractBatchLSModel.configureOrbits(MatricesHarvester harvester, Propagator propagator) Configure the current estimated orbits.
protected Orbit	BatchLSModel.configureOrbits(MatricesHarvester harvester, Propagator propagator) Configure the current estimated orbits.
protected Orbit	DSSTBatchLSModel.configureOrbits(MatricesHarvester harvester, Propagator propagator) Configure the current estimated orbits.

Uses of Propagator in org.orekit.estimation.measurements.generation

Methods in org.orekit.estimation.measurements.generation that return Propagator

Modifier and Type	Method and Description
Propagator	Generator.getPropagator(ObservableSatellite satellite) Get a registered propagator.

Methods in org.orekit.estimation.measurements.generation with parameters of type Propagator

Modifier and Type	Method and Description
ObservableSatellite	Generator.addPropagator(Propagator propagator) Add a propagator.

Constructors in org.orekit.estimation.measurements.generation with parameters of type Propagator

Constructor and Description
EventBasedScheduler(MeasurementBuilder<T> builder, DatesSelector selector, Propagator propagator, EventDetector detector, SignSemantic signSemantic) Simple constructor.

Uses of Propagator in org.orekit.estimation.sequential

Methods in org.orekit.estimation.sequential that return Propagator

Modifier and Type	Method and Description
Propagator[]	KalmanEstimator.estimationStep(ObservedMeasurement<?> observedMeasurement) Process a single measurement.
Propagator[]	UnscentedKalmanEstimator.estimationStep(ObservedMeasurement<?> observedMeasurement) Process a single measurement.
Propagator[]	UnscentedKalmanModel.getEstimatedPropagators() Get the propagators estimated with the values set in the propagators builders.
Propagator[]	KalmanModel.getEstimatedPropagators() Get the propagators estimated with the values set in the propagators builders.
Propagator[]	KalmanModel.getReferenceTrajectories() Getter for the reference trajectories.
Propagator[]	KalmanEstimator.processMeasurements(Iterable<ObservedMeasurement<?>> observedMeasurements) Process several measurements.
Propagator[]	UnscentedKalmanEstimator.processMeasurements(Iterable<ObservedMeasurement<?>> observedMeasurements) Process several measurements.

Methods in org.orekit.estimation.sequential with parameters of type Propagator

Modifier and Type	Method and Description
void	KalmanModel.setReferenceTrajectories(Propagator[] referenceTrajectories) Setter for the reference trajectories.
protected void	KalmanModel.updateReferenceTrajectories(Propagator[] propagators) Update the reference trajectories using the propagators as input.

Uses of Propagator in org.orekit.gnss

Method parameters in org.orekit.gnss with type arguments of type Propagator

Modifier and Type	Method and Description
DOP	DOPComputer.compute(AbsoluteDate date, List<Propagator> gnss) Compute the DOP at a given date for a set of GNSS spacecrafts.

Uses of Propagator in org.orekit.orbits

Constructors in org.orekit.orbits with parameters of type Propagator

Constructor and Description
OrbitBlender(org.hipparchus.analysis.polynomials.SmoothStepFactory.SmoothStepFunction blendingFunction, Propagator blendingPropagator, Frame outputInertialFrame) Default constructor.

Uses of Propagator in org.orekit.propagation

Subinterfaces of Propagator in org.orekit.propagation

Modifier and Type	Interface and Description
interface	BoundedPropagator This interface is intended for ephemerides valid only during a time range.

Classes in org.orekit.propagation that implement Propagator

Modifier and Type	Class and Description
class	AbstractPropagator Common handling of Propagator methods for analytical propagators.

Methods in org.orekit.propagation that return types with arguments of type Propagator

Modifier and Type	Method and Description
List<Propagator>	PropagatorsParallelizer.getPropagators() Get an unmodifiable list of the underlying mono-satellite propagators.

Constructor parameters in org.orekit.propagation with type arguments of type Propagator

Constructor and Description
PropagatorsParallelizer(List<Propagator> propagators, double h, MultiSatFixedStepHandler globalHandler) Simple constructor.
PropagatorsParallelizer(List<Propagator> propagators, MultiSatStepHandler globalHandler) Simple constructor.

Uses of Propagator in org.orekit.propagation.analytical

Classes in org.orekit.propagation.analytical that implement Propagator

Modifier and Type	Class and Description
class	AbstractAnalyticalPropagator Common handling of Propagator methods for analytical propagators.
class	AdapterPropagator Orbit propagator that adapts an underlying propagator, adding differential effects.
class	AggregateBoundedPropagator A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
class	BrouwerLyddanePropagator This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
class	EcksteinHechlerPropagator This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
class	Ephemeris This class is designed to accept and handle tabulated orbital entries.
class	KeplerianPropagator Simple Keplerian orbit propagator.

Methods in org.orekit.propagation.analytical that return Propagator

Modifier and Type	Method and Description
Propagator	AdapterPropagator.getPropagator() Get the reference propagator.

Constructors in org.orekit.propagation.analytical with parameters of type Propagator

Constructor and Description
AdapterPropagator(Propagator reference) Build a propagator from an underlying reference propagator.

Uses of Propagator in org.orekit.propagation.analytical.gnss

Classes in org.orekit.propagation.analytical.gnss that implement Propagator

Modifier and Type	Class and Description
class	GLONASSAnalyticalPropagator This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
class	GNSSPropagator Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
class	SBASPropagator This class aims at propagating a SBAS orbit from SBASOrbitalElements.

Uses of Propagator in org.orekit.propagation.analytical.tle

Classes in org.orekit.propagation.analytical.tle that implement Propagator

Modifier and Type	Class and Description
class	DeepSDP4 This class contains the methods that compute deep space perturbation terms.
class	SGP4 This class contains methods to compute propagated coordinates with the SGP4 model.
class	TLEPropagator This class provides elements to propagate TLE's.

Uses of Propagator in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return Propagator

Modifier and Type	Method and Description
Propagator	KeplerianPropagatorBuilder.buildPropagator(double[] normalizedParameters) Build a propagator.
Propagator	EcksteinHechlerPropagatorBuilder.buildPropagator(double[] normalizedParameters) Build a propagator.
Propagator	EphemerisPropagatorBuilder.buildPropagator(double[] normalizedParameters) Build a propagator.
Propagator	PropagatorBuilder.buildPropagator(double[] normalizedParameters) Build a propagator.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, List<String> freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, List<String> freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	AbstractPropagatorConverter.convert(List<SpacecraftState> states, boolean positionOnly, String... freeParameters) Find the propagator that minimize the mean square error for a sample of states.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator to another.
Propagator	AbstractPropagatorConverter.getAdaptedPropagator() Get the adapted propagator.

Methods in org.orekit.propagation.conversion with parameters of type Propagator

Modifier and Type	Method and Description
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, List<String> freeParameters) Convert a propagator to another.
Propagator	PropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator into another one.
Propagator	AbstractPropagatorConverter.convert(Propagator source, double timeSpan, int nbPoints, String... freeParameters) Convert a propagator to another.

Constructors in org.orekit.propagation.conversion with parameters of type Propagator

Constructor and Description
OsculatingToMeanElementsConverter(SpacecraftState state, int satelliteRevolution, Propagator propagator, double positionScale) Constructor.

Uses of Propagator in org.orekit.propagation.integration

Classes in org.orekit.propagation.integration that implement Propagator

Modifier and Type	Class and Description
class	AbstractIntegratedPropagator Common handling of Propagator methods for both numerical and semi-analytical propagators.
class	IntegratedEphemeris This class stores sequentially generated orbital parameters for later retrieval.

Uses of Propagator in org.orekit.propagation.numerical

Classes in org.orekit.propagation.numerical that implement Propagator

Modifier and Type	Class and Description
class	GLONASSNumericalPropagator This class propagates GLONASS orbits using numerical integration.
class	NumericalPropagator This class propagates orbits using numerical integration.

Uses of Propagator in org.orekit.propagation.semianalytical.dsst

Classes in org.orekit.propagation.semianalytical.dsst that implement Propagator

Modifier and Type	Class and Description
class	DSSTPropagator This class propagates orbits using the DSST theory.