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.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).

Uses of FieldOrbit in org.orekit.orbits

Subclasses of FieldOrbit in org.orekit.orbits

Modifier and Type	Class and Description
class	FieldCartesianOrbit<T extends RealFieldElement<T>> This class holds Cartesian orbital parameters.
class	FieldCircularOrbit<T extends RealFieldElement<T>> This class handles circular orbital parameters.
class	FieldEquinoctialOrbit<T extends RealFieldElement<T>> This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
class	FieldKeplerianOrbit<T extends RealFieldElement<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 RealFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
abstract <T extends RealFieldElement<T>> FieldOrbit<T>	OrbitType.mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngle type, FieldAbsoluteDate<T> date, T 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 and Description
abstract <T extends RealFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
abstract <T extends 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 and Description
FieldCircularOrbit<T>	FieldCircularOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
FieldCartesianOrbit<T>	FieldCartesianOrbit.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 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.

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, 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, Map<String,T[]> additional) Build a spacecraft state from orbit only.
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 and 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 and Description
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, 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, 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.
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.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) 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 RealFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, FieldOrbit<T> orbit, OrbitType type) Estimate tolerance vectors for integrators.

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 RealFieldElement<T>> double[][]	FieldDSSTPropagator.tolerances(T dP, 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[]	FieldShortPeriodTerms.value(FieldOrbit<T> meanOrbit) Evaluate the contributions of the short period terms.

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

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

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