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.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 CalculusFieldElement<T>> This class holds Cartesian orbital parameters.
class	FieldCircularOrbit<T extends CalculusFieldElement<T>> This class handles circular orbital parameters.
class	FieldEquinoctialOrbit<T extends CalculusFieldElement<T>> This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
class	FieldKeplerianOrbit<T extends 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 CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
abstract <T extends CalculusFieldElement<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 <T extends 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 CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.convertType(FieldOrbit<T> orbit) Convert an orbit to the instance type.
abstract <T extends CalculusFieldElement<T>> void	OrbitType.mapOrbitToArray(FieldOrbit<T> orbit, PositionAngle type, T[] stateVector, T[] stateVectorDot) Convert orbit to state array.
abstract <T extends CalculusFieldElement<T>> FieldOrbit<T>	OrbitType.normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference) Normalize one orbit with respect to a reference one.
abstract <T extends 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
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.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.
FieldCartesianOrbit<T>	FieldCartesianOrbit.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, 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, Map<String,T[]> additional) Deprecated. as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldAttitude, FieldArrayDictionary)
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, FieldAttitude<T> attitude, T mass, Map<String,T[]> additional) Deprecated. as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary)
FieldSpacecraftState(FieldOrbit<T> orbit, Map<String,T[]> additional) Deprecated. as of 11.1, replacezd by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldArrayDictionary)
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.
FieldSpacecraftState(FieldOrbit<T> orbit, T mass, Map<String,T[]> additional) Deprecated. as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, CalculusFieldElement, FieldArrayDictionary)

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 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 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 CalculusFieldElement<T>> FieldCircularOrbit<T>	FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Conversion from osculating to mean orbit.
static <T extends 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 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 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.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 CalculusFieldElement<T>> double[][]	FieldNumericalPropagator.tolerances(T dP, FieldOrbit<T> orbit, OrbitType type) Estimate tolerance vectors for integrators.
static <T extends 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 CalculusFieldElement<T>> double[][]	FieldDSSTPropagator.tolerances(T dP, FieldOrbit<T> orbit) Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
static <T extends 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

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

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