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.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.

Uses of FieldPVCoordinatesProvider in org.orekit.attitudes

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

Modifier and Type	Method and Description
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	InertialProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	AttitudesSequence.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.RealFieldElement<T>> FieldAttitude<T>	TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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.orbits

Classes in org.orekit.orbits that implement FieldPVCoordinatesProvider

Modifier and Type	Class and 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.
class	FieldOrbit<T extends org.hipparchus.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 and Description
interface	FieldBoundedPropagator<T extends org.hipparchus.RealFieldElement<T>> This interface is intended for ephemerides valid only during a time range.
interface	FieldPropagator<T extends org.hipparchus.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 and Description
class	FieldAbstractPropagator<T extends org.hipparchus.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 and Description
class	FieldAbstractAnalyticalPropagator<T extends org.hipparchus.RealFieldElement<T>> Common handling of FieldPropagator methods for analytical propagators.
class	FieldEcksteinHechlerPropagator<T extends org.hipparchus.RealFieldElement<T>> This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
class	FieldKeplerianPropagator<T extends org.hipparchus.RealFieldElement<T>> Simple Keplerian orbit propagator.

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

Modifier and Type	Method and 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 and Description
class	FieldAbstractIntegratedPropagator<T extends org.hipparchus.RealFieldElement<T>> Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
class	FieldIntegratedEphemeris<T extends org.hipparchus.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 and Description
class	FieldNumericalPropagator<T extends org.hipparchus.RealFieldElement<T>> This class propagates orbits using numerical integration.