Uses of Class
org.orekit.orbits.FieldOrbit

Packages that use FieldOrbit

Package	Description
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.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.events	This package provides interfaces and classes dealing with events occurring during propagation.
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).
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities	This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.ssa.collision.shorttermencounter.probability.twod	Package specific to calculus assuming a 2D short-term encounter model.
org.orekit.utils	This package provides useful objects.

Uses of FieldOrbit in org.orekit.orbits

Subclasses of FieldOrbit in org.orekit.orbits

Modifier and Type	Class and Description
class	FieldCartesianOrbit<T extends org.hipparchus.CalculusFieldElement<T>> This class holds Cartesian orbital parameters.
class	FieldCircularOrbit<T extends org.hipparchus.CalculusFieldElement<T>> This class handles circular orbital parameters.
class	FieldEquinoctialOrbit<T extends org.hipparchus.CalculusFieldElement<T>> This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
class	FieldKeplerianOrbit<T extends org.hipparchus.CalculusFieldElement<T>> This class handles traditional Keplerian orbital parameters.

Methods in org.orekit.orbits that return FieldOrbit

Modifier and Type	Method and Description
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.convertToFieldOrbit(org.hipparchus.Field<T> field, Orbit orbit) Convert an orbit to the "Fielded" instance type.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
protected FieldOrbit<KK>	FieldOrbitHermiteInterpolator.interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData) Interpolate instance from given interpolation data.
FieldOrbit<KK>	FieldOrbitBlender.interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData) Interpolate instance from given interpolation data.
FieldOrbit<KK>	AbstractFieldOrbitInterpolator.interpolate(FieldAbsoluteDate<KK> interpolationDate, Collection<FieldOrbit<KK>> sample) Get an interpolated instance.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngleType type, FieldAbsoluteDate<T> date, T mu, Frame frame) Convert state array to orbital parameters.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference) Normalize one orbit with respect to a reference one.
abstract FieldOrbit<T>	FieldOrbit.shiftedBy(T dt) Get a time-shifted orbit.

Methods in org.orekit.orbits with parameters of type FieldOrbit

Modifier and Type	Method and Description
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> void	OrbitType.mapOrbitToArray(FieldOrbit<T> orbit, PositionAngleType type, T[] stateVector, T[] stateVectorDot) Convert orbit to state array.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference) Normalize one orbit with respect to a reference one.
abstract <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference) Normalize one orbit with respect to a reference one.

Method parameters in org.orekit.orbits with type arguments of type FieldOrbit

Modifier and Type	Method and Description
FieldOrbit<KK>	AbstractFieldOrbitInterpolator.interpolate(FieldAbsoluteDate<KK> interpolationDate, Collection<FieldOrbit<KK>> sample) Get an interpolated instance.

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

Constructor and Description
FieldCartesianOrbit(FieldOrbit<T> op) Constructor from any kind of orbital parameters.
FieldCircularOrbit(FieldOrbit<T> op) Constructor from any kind of orbital parameters.
FieldEquinoctialOrbit(FieldOrbit<T> op) Constructor from any kind of orbital parameters.
FieldKeplerianOrbit(FieldOrbit<T> op) Constructor from any kind of orbital parameters.

Uses of FieldOrbit in org.orekit.propagation

Methods in org.orekit.propagation that return FieldOrbit

Modifier and Type	Method and Description
FieldOrbit<T>	FieldSpacecraftState.getOrbit() Get the current orbit.

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

Modifier and Type	Method and Description
Optional<FieldTimeInterpolator<FieldOrbit<KK>,KK>>	FieldSpacecraftStateInterpolator.getOrbitInterpolator() Get orbit interpolator.

Methods in org.orekit.propagation with parameters of type FieldOrbit

Modifier and Type	Method and Description
FieldStateCovariance<T>	FieldStateCovariance.changeCovarianceFrame(FieldOrbit<T> orbit, Frame frameOut) Get the covariance in the output frame.
FieldStateCovariance<T>	FieldStateCovariance.changeCovarianceFrame(FieldOrbit<T> orbit, LOF lofOut) Get the covariance in a given local orbital frame.
FieldStateCovariance<T>	FieldStateCovariance.changeCovarianceType(FieldOrbit<T> orbit, OrbitType outOrbitType, PositionAngleType outAngleType) Get the covariance matrix in another orbit type.
FieldStateCovariance<T>	FieldStateCovariance.shiftedBy(org.hipparchus.Field<T> field, FieldOrbit<T> orbit, T dt) Get a time-shifted covariance matrix.

Constructors in org.orekit.propagation with parameters of type FieldOrbit

Constructor and Description
FieldSpacecraftState(FieldOrbit<T> orbit) Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldArrayDictionary<T> additional) Build a spacecraft state from orbit and additional states.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude) Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, FieldArrayDictionary<T> additional) Build a spacecraft state from orbit attitude and additional states.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass) Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional) Build a spacecraft state from orbit, attitude, mass and additional states.
FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional, FieldArrayDictionary<T> additionalDot) Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
FieldSpacecraftState(FieldOrbit<T> orbit, T mass) Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T> orbit, T mass, FieldArrayDictionary<T> additional) Create a new instance from orbit, mass and additional states.

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

Constructor and Description

FieldSpacecraftStateInterpolator(Frame outputFrame, FieldTimeInterpolator<FieldOrbit<KK>,KK> orbitInterpolator, FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>,KK> absPVAInterpolator, FieldTimeInterpolator<TimeStampedField<KK>,KK> massInterpolator, FieldTimeInterpolator<FieldAttitude<KK>,KK> attitudeInterpolator, FieldTimeInterpolator<TimeStampedField<KK>,KK> additionalStateInterpolator) Constructor.

Uses of FieldOrbit in org.orekit.propagation.analytical

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

Modifier and Type	Method and Description
protected FieldOrbit<T>	FieldKeplerianPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.
protected abstract FieldOrbit<T>	FieldAbstractAnalyticalPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Methods in org.orekit.propagation.analytical with parameters of type FieldOrbit

Modifier and Type	Method and Description
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldCircularOrbit<T>	FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double M2Value, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldCircularOrbit<T>	FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Conversion from osculating to mean orbit.
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value) Conversion from osculating to mean orbit.
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldCircularOrbit<T>	FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double epsilon, int maxIterations) Conversion from osculating to mean orbit.

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

Constructor and Description
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2, double epsilon, int maxIterations) Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2) Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType, double M2) Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, attitude provider and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2) Build a propagator from orbit, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, T mass, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, double M2) Build a propagator from orbit and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2) Build a propagator from orbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations) Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType) Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType) Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60) Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, T mass, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider) Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType) Build a propagator from orbit and potential provider.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit) Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv) Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv, T mu) Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mu, T mass) Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, T mu) Build a propagator from orbit and central attraction coefficient μ.

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

Methods in org.orekit.propagation.analytical.tle that return FieldOrbit

Modifier and Type	Method and Description
FieldOrbit<T>	FieldTLEPropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Uses of FieldOrbit in org.orekit.propagation.conversion

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

Modifier and Type	Method and Description
org.hipparchus.ode.AbstractFieldIntegrator<T>	AbstractFieldIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType) Build a first order integrator.
org.hipparchus.ode.AbstractFieldIntegrator<T>	FieldODEIntegratorBuilder.buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType) Build a first order integrator.

Uses of FieldOrbit in org.orekit.propagation.events

Constructors in org.orekit.propagation.events with parameters of type FieldOrbit

Constructor and Description
FieldApsideDetector(FieldOrbit<T> orbit) Build a new instance.
FieldApsideDetector(T threshold, FieldOrbit<T> orbit) Build a new instance.
FieldNodeDetector(FieldOrbit<T> orbit, Frame frame) Build a new instance.
FieldNodeDetector(T threshold, FieldOrbit<T> orbit, Frame frame) Build a new instance.

Uses of FieldOrbit in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return FieldOrbit

Modifier and Type	Method and Description
protected FieldOrbit<T>	FieldIntegratedEphemeris.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.

Uses of FieldOrbit in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical with parameters of type FieldOrbit

Modifier and Type	Method and Description
static <T extends org.hipparchus.CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, FieldOrbit<T> orbit, OrbitType type) Estimate tolerance vectors for integrators.
static <T extends org.hipparchus.CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, T dV, FieldOrbit<T> orbit, OrbitType type) Estimate tolerance vectors for integrators when propagating in orbits.

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

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type FieldOrbit

Modifier and Type	Method and Description
static <T extends org.hipparchus.CalculusFieldElement<T>> double[][]	FieldDSSTPropagator.tolerances(T dP, FieldOrbit<T> orbit) Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
static <T extends org.hipparchus.CalculusFieldElement<T>> double[][]	FieldDSSTPropagator.tolerances(T dP, T dV, FieldOrbit<T> orbit) Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

Uses of FieldOrbit in org.orekit.propagation.semianalytical.dsst.forces

Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldOrbit

Modifier and Type	Method and Description
T[]	AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients.value(FieldOrbit<T> meanOrbit) Evaluate the contributions of the short period terms.
T[]	FieldShortPeriodTerms.value(FieldOrbit<T> meanOrbit) Evaluate the contributions of the short period terms.

Uses of FieldOrbit in org.orekit.propagation.semianalytical.dsst.utilities

Methods in org.orekit.propagation.semianalytical.dsst.utilities that return FieldOrbit

Modifier and Type	Method and Description
FieldOrbit<T>	FieldAuxiliaryElements.getOrbit() Get the orbit.

Constructors in org.orekit.propagation.semianalytical.dsst.utilities with parameters of type FieldOrbit

Constructor and Description
FieldAuxiliaryElements(FieldOrbit<T> orbit, int retrogradeFactor) Simple constructor.

Uses of FieldOrbit in org.orekit.ssa.collision.shorttermencounter.probability.twod

Methods in org.orekit.ssa.collision.shorttermencounter.probability.twod that return FieldOrbit

Modifier and Type	Method and Description
FieldOrbit<T>	FieldShortTermEncounter2DDefinition.getOtherAtTCA() Get other's orbit at time of closest approach.
FieldOrbit<T>	FieldShortTermEncounter2DDefinition.getReferenceAtTCA() Get reference's orbit at time of closest approach.

Methods in org.orekit.ssa.collision.shorttermencounter.probability.twod with parameters of type FieldOrbit

Modifier and Type	Method and Description
default <T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius) Compute the probability of collision using parameters necessary for creating a collision definition instance.
default <T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	AbstractShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	AbstractShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.
default <T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius) Compute the probability of collision using parameters necessary for creating a collision definition instance.
default <T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	ShortTermEncounter2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	AbstractShortTermEncounter1DNumerical2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius, org.hipparchus.analysis.integration.FieldUnivariateIntegrator<T> customIntegrator, int customMaxNbOfEval, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.
<T extends org.hipparchus.CalculusFieldElement<T>> FieldProbabilityOfCollision<T>	AbstractShortTermEncounter1DNumerical2DPOCMethod.compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius, org.hipparchus.analysis.integration.FieldUnivariateIntegrator<T> customIntegrator, int customMaxNbOfEval, double zeroThreshold) Compute the probability of collision using parameters necessary for creating a collision definition instance.

Constructors in org.orekit.ssa.collision.shorttermencounter.probability.twod with parameters of type FieldOrbit

Constructor and Description
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius, EncounterLOFType encounterFrameType, double tcaTolerance) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius, EncounterLOFType encounterFrameType, double tcaTolerance) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius, EncounterLOFType encounterFrameType, double tcaTolerance) Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius, EncounterLOFType encounterFrameType, double tcaTolerance) Constructor.

Uses of FieldOrbit in org.orekit.utils

Methods in org.orekit.utils that return FieldOrbit

Modifier and Type	Method and Description
static <T extends org.hipparchus.CalculusFieldElement<T>> FieldOrbit<T>	Fieldifier.fieldify(org.hipparchus.Field<T> field, Orbit orbit) Fieldify given orbit with given field.