Uses of Interface
org.orekit.utils.FieldPVCoordinatesProvider

Packages that use FieldPVCoordinatesProvider

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.gnss.attitude	This package provides classes related to navigation satellites attitude modeling.
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.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.utils	This package provides useful objects.

Uses of FieldPVCoordinatesProvider in org.orekit.attitudes

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

Modifier and Type	Method	Description
<T extends RealFieldElement<T>> FieldAttitude<T>	AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	AttitudesSequence.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	InertialProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends RealFieldElement<T>> FieldAttitude<T>	YawCompensation.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the base system state at given date, without compensation.
<T extends RealFieldElement<T>> FieldAttitude<T>	YawSteering.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the base system state at given date, without compensation.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	BodyCenterPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
abstract <T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	GroundPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	LofOffsetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	NadirPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	TargetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	YawCompensation.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> TimeStampedFieldPVCoordinates<T>	YawSteering.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends RealFieldElement<T>> T	YawCompensation.getYawAngle(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the yaw compensation angle at date.

Uses of FieldPVCoordinatesProvider in org.orekit.gnss.attitude

Methods in org.orekit.gnss.attitude with parameters of type FieldPVCoordinatesProvider

Modifier and Type	Method	Description
<T extends RealFieldElement<T>> FieldAttitude<T>	AbstractGNSSAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.

Uses of FieldPVCoordinatesProvider in org.orekit.orbits

Classes in org.orekit.orbits that implement FieldPVCoordinatesProvider

Modifier and Type	Class	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.
class	FieldOrbit<T extends RealFieldElement<T>>	This class handles orbital parameters.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation

Subinterfaces of FieldPVCoordinatesProvider in org.orekit.propagation

Modifier and Type	Interface	Description
interface	FieldBoundedPropagator<T extends RealFieldElement<T>>	This interface is intended for ephemerides valid only during a time range.
interface	FieldPropagator<T extends RealFieldElement<T>>	This interface provides a way to propagate an orbit at any time.

Classes in org.orekit.propagation that implement FieldPVCoordinatesProvider

Modifier and Type	Class	Description
class	FieldAbstractPropagator<T extends RealFieldElement<T>>	Common handling of Propagator methods for analytical propagators.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical

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

Modifier and Type	Class	Description
class	FieldAbstractAnalyticalPropagator<T extends RealFieldElement<T>>	Common handling of FieldPropagator methods for analytical propagators.
class	FieldEcksteinHechlerPropagator<T extends RealFieldElement<T>>	This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
class	FieldKeplerianPropagator<T extends RealFieldElement<T>>	Simple Keplerian orbit propagator.

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

Modifier and Type	Method	Description
FieldPVCoordinatesProvider<T>	FieldAbstractAnalyticalPropagator.getPvProvider()	Get PV coordinates provider.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.integration

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

Modifier and Type	Class	Description
class	FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
class	FieldIntegratedEphemeris<T extends RealFieldElement<T>>	This class stores sequentially generated orbital parameters for later retrieval.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.numerical

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

Modifier and Type	Class	Description
class	FieldNumericalPropagator<T extends RealFieldElement<T>>	This class propagates orbits using numerical integration.

Uses of FieldPVCoordinatesProvider in org.orekit.utils

Methods in org.orekit.utils that return FieldPVCoordinatesProvider

Modifier and Type	Method	Description
default <T extends RealFieldElement<T>> FieldPVCoordinatesProvider<T>	ExtendedPVCoordinatesProvider.toFieldPVCoordinatesProvider(Field<T> field)	Convert to a FieldPVCoordinatesProvider with a specific type.