Uses of Class org.orekit.orbits.FieldOrbit (ORbit Extrapolation KIT 9.3 API)

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.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.

Uses of FieldOrbit in org.orekit.orbits

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

Methods in org.orekit.orbits that return FieldOrbit
Modifier and Type	Method	Description
`abstract <T extends org.hipparchus.RealFieldElement<T>> FieldOrbit<T>`	OrbitType.`convertType(FieldOrbit<T> orbit)`	Convert an orbit to the instance type.
`abstract <T extends org.hipparchus.RealFieldElement<T>> FieldOrbit<T>`	OrbitType.`mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngle type, FieldAbsoluteDate<T> date, double mu, Frame frame)`	Convert state array to orbital parameters.
`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	Description
`abstract <T extends org.hipparchus.RealFieldElement<T>> FieldOrbit<T>`	OrbitType.`convertType(FieldOrbit<T> orbit)`	Convert an orbit to the instance type.
`abstract <T extends org.hipparchus.RealFieldElement<T>> void`	OrbitType.`mapOrbitToArray(FieldOrbit<T> orbit, PositionAngle type, T[] stateVector, T[] stateVectorDot)`	Convert orbit to state array.

Method parameters in org.orekit.orbits with type arguments of type FieldOrbit
Modifier and Type	Method	Description
`FieldCartesianOrbit<T>`	FieldCartesianOrbit.`interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample)`	Get an interpolated instance.
`FieldCircularOrbit<T>`	FieldCircularOrbit.`interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample)`	Get an interpolated instance.
`FieldEquinoctialOrbit<T>`	FieldEquinoctialOrbit.`interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample)`	Get an interpolated instance.
`FieldKeplerianOrbit<T>`	FieldKeplerianOrbit.`interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample)`	Get an interpolated instance.

Constructors in org.orekit.orbits with parameters of type FieldOrbit
Constructor	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	Description
`FieldOrbit<T>`	FieldSpacecraftState.`getOrbit()`	Gets the current orbit.

Constructors in org.orekit.propagation with parameters of type FieldOrbit
Constructor	Description
`FieldSpacecraftState(FieldOrbit<T> orbit)`	Build a spacecraft state from orbit only.
`FieldSpacecraftState(FieldOrbit<T> orbit, Map<String,T[]> additional)`	Build a spacecraft state from orbit only.
`FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude)`	Build a spacecraft state from orbit and attitude provider.
`FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, Map<String,T[]> additional)`	Build a spacecraft state from orbit and attitude provider.
`FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass)`	Build a spacecraft state from orbit, attitude provider and mass.
`FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass, Map<String,T[]> additional)`	Build a spacecraft state from orbit, attitude provider and mass.
`FieldSpacecraftState(FieldOrbit<T> orbit, T mass)`	Create a new instance from orbit and mass.
`FieldSpacecraftState(FieldOrbit<T> orbit, T mass, Map<String,T[]> additional)`	Create a new instance from orbit and mass.

Uses of FieldOrbit in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical that return FieldOrbit
Modifier and Type	Method	Description
`protected abstract FieldOrbit<T>`	FieldAbstractAnalyticalPropagator.`propagateOrbit(FieldAbsoluteDate<T> date)`	Extrapolate an orbit up to a specific target date.
`protected FieldOrbit<T>`	FieldKeplerianPropagator.`propagateOrbit(FieldAbsoluteDate<T> date)`	Extrapolate an orbit up to a specific target date.

Constructors in org.orekit.propagation.analytical with parameters of type FieldOrbit
Constructor	Description
`FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60)`	Build a propagator from FieldOrbit and potential.
`FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double 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, UnnormalizedSphericalHarmonicsProvider provider)`	Build a propagator from FieldOrbit, attitude provider and potential provider.
`FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, double 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, UnnormalizedSphericalHarmonicsProvider provider)`	Build a propagator from FieldOrbit, 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, UnnormalizedSphericalHarmonicsProvider provider)`	Build a propagator from FieldOrbit and potential provider.
`FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, T mass, double referenceRadius, double 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.
`FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit)`	Build a propagator from orbit only.
`FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, double mu)`	Build a propagator from orbit and central attraction coefficient μ.
`FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv)`	Build a propagator from orbit and attitude provider.
`FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv, double mu)`	Build a propagator from orbit, attitude provider and central attraction coefficient μ.
`FieldKeplerianPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double mu, T mass)`	Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

Uses of FieldOrbit in org.orekit.propagation.events

Constructors in org.orekit.propagation.events with parameters of type FieldOrbit
Constructor	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	Description
`protected FieldOrbit<T>`	FieldIntegratedEphemeris.`propagateOrbit(FieldAbsoluteDate<T> date)`	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	Description
`static <T extends org.hipparchus.RealFieldElement<T>> double[][]`	FieldNumericalPropagator.`tolerances(T dP, FieldOrbit<T> orbit, OrbitType type)`	Estimate tolerance vectors for integrators.