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.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.gnss	This package provides methods to handle GNSS measurements.
org.orekit.files.ccsds.ndm.adm	This package contains class managing CCSDS Attitude Data Message.
org.orekit.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
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.intelsat	This package provides classes to propagate Intelsat's 11 elements.
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.sampling	This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
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 CalculusFieldElement<T>> FieldAttitude<T>	AttitudeBuilder.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude)	Build a filtered attitude.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	FixedFrameBuilder.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude)	Build a filtered attitude.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AggregateBoundedAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AlignedAndConstrained.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AttitudesSequence.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	FrameAlignedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	TorqueFree.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	AggregateBoundedAttitudeProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	AlignedAndConstrained.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
default <T extends CalculusFieldElement<T>> FieldRotation<T>	AttitudeProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	AttitudesSequence.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
<T extends CalculusFieldElement<T>> FieldRotation<T>	CelestialBodyPointed.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	FixedRate.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	FrameAlignedProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	GroundPointing.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	LofOffset.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	LofOffsetPointing.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldRotation<T>	SpinStabilized.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
<T extends CalculusFieldElement<T>> FieldAttitude<T>	GroundPointingAttitudeModifier.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the base system state at given date, without modifications.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	BodyCenterPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	GroundPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	GroundPointingAttitudeModifier.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	LofOffsetPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	NadirPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
protected <T extends CalculusFieldElement<T>> FieldVector3D<T>	TargetPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	BodyCenterPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
protected abstract <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	GroundPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	GroundPointingAttitudeModifier.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	LofOffsetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	NadirPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	TargetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute the target point position/velocity in specified frame.
<T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T>	NadirPointing.getTargetPVViaInterpolation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)	Compute target position-velocity-acceleration vector via interpolation (Field version).
<T extends CalculusFieldElement<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.estimation.measurements

Methods in org.orekit.estimation.measurements with parameters of type FieldPVCoordinatesProvider

Modifier and Type	Method	Description
static <T extends CalculusFieldElement<T>> T	AbstractMeasurement.signalTimeOfFlightAdjustableEmitter(FieldPVCoordinatesProvider<T> adjustableEmitter, FieldAbsoluteDate<T> approxEmissionDate, FieldVector3D<T> receiverPosition, FieldAbsoluteDate<T> signalArrivalDate, Frame frame)	Compute propagation delay on a link leg (typically downlink or uplink).
static <T extends CalculusFieldElement<T>> T	AbstractMeasurement.signalTimeOfFlightAdjustableReceiver(FieldVector3D<T> emitterPosition, FieldAbsoluteDate<T> emissionDate, FieldPVCoordinatesProvider<T> adjustableReceiver, FieldAbsoluteDate<T> approxReceptionDate, Frame frame)	Compute propagation delay on a link leg (typically downlink or uplink).

Uses of FieldPVCoordinatesProvider in org.orekit.estimation.measurements.gnss

Methods in org.orekit.estimation.measurements.gnss that return FieldPVCoordinatesProvider

Modifier and Type	Method	Description
protected FieldPVCoordinatesProvider<Gradient>	AbstractInterSatellitesMeasurement.getRemotePV(SpacecraftState[] states, int freeParameters)	Get emitting satellite position/velocity provider.
protected abstract FieldPVCoordinatesProvider<Gradient>	AbstractOnBoardMeasurement.getRemotePV(SpacecraftState[] states, int freeParameters)	Get emitting satellite position/velocity provider.
protected FieldPVCoordinatesProvider<Gradient>	AbstractOneWayGNSSMeasurement.getRemotePV(SpacecraftState[] states, int freeParameters)	Get emitting satellite position/velocity provider.

Uses of FieldPVCoordinatesProvider in org.orekit.files.ccsds.ndm.adm

Methods in org.orekit.files.ccsds.ndm.adm with parameters of type FieldPVCoordinatesProvider

Modifier and Type	Method	Description
<T extends CalculusFieldElement<T>> FieldAttitude<T>	AttitudeEndpoints.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude)	Build a filtered attitude.

Uses of FieldPVCoordinatesProvider in org.orekit.forces.maneuvers.propulsion

Methods in org.orekit.forces.maneuvers.propulsion with parameters of type FieldPVCoordinatesProvider

Modifier and Type	Method	Description
<T extends CalculusFieldElement<T>> FieldAttitude<T>	ThrustDirectionAndAttitudeProvider.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 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.
class	FieldOrbit<T extends CalculusFieldElement<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 CalculusFieldElement<T>>	This interface is intended for ephemerides valid only during a time range.
interface	FieldPropagator<T extends CalculusFieldElement<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 CalculusFieldElement<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 CalculusFieldElement<T>>	Common handling of FieldPropagator methods for analytical propagators.
class	FieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>>	This class propagates a FieldSpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
class	FieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>>	This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
class	FieldKeplerianPropagator<T extends CalculusFieldElement<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.analytical.intelsat

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

Modifier and Type	Class	Description
class	FieldIntelsatElevenElementsPropagator<T extends CalculusFieldElement<T>>	This class provides elements to propagate Intelsat's 11 elements.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical.tle

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

Modifier and Type	Class	Description
class	FieldDeepSDP4<T extends CalculusFieldElement<T>>	This class contains the methods that compute deep space perturbation terms.
class	FieldSGP4<T extends CalculusFieldElement<T>>	This class contains methods to compute propagated coordinates with the SGP4 model.
class	FieldTLEPropagator<T extends CalculusFieldElement<T>>	This class provides elements to propagate TLE's.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.events

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

Modifier and Type	Method	Description
FieldPVCoordinatesProvider<T>	FieldBetaAngleDetector.getCelestialBodyProvider()	Coordinate provider for the celestial body.
FieldPVCoordinatesProvider<T>	FieldExtremumApproachDetector.getSecondaryPVProvider()	Get the secondary position-velocity provider stored in this instance.
FieldPVCoordinatesProvider<T>	FieldRelativeDistanceDetector.getSecondaryPVProvider()	Get the secondary position-velocity provider stored in this instance.

Methods in org.orekit.propagation.events with parameters of type FieldPVCoordinatesProvider

Modifier and Type	Method	Description
static <T extends CalculusFieldElement<T>> T	FieldBetaAngleDetector.calculateBetaAngle(FieldSpacecraftState<T> state, FieldPVCoordinatesProvider<T> celestialBodyProvider)	Calculate the beta angle between the orbit plane and the celestial body.
static <T extends CalculusFieldElement<T>> T	FieldBetaAngleDetector.calculateBetaAngle(FieldSpacecraftState<T> state, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame frame)	Calculate the beta angle between the orbit plane and the celestial body.
FieldBetaAngleDetector<T>	FieldBetaAngleDetector.withCelestialProvider(FieldPVCoordinatesProvider<T> newProvider)	Create a new instance with the provided coordinate provider.

Constructors in org.orekit.propagation.events with parameters of type FieldPVCoordinatesProvider

Constructor	Description
FieldBetaAngleDetector(Field<T> field, T betaAngleThreshold, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame inertialFrame)	Class constructor.
FieldBetaAngleDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, T betaAngleThreshold, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame inertialFrame)	Protected constructor with full parameters.
FieldExtremumApproachDetector(Field<T> field, FieldPVCoordinatesProvider<T> secondaryPVProvider)	Constructor with default values.
FieldExtremumApproachDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, FieldPVCoordinatesProvider<T> secondaryPVProvider)	Constructor.
FieldRelativeDistanceDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, FieldPVCoordinatesProvider<T> secondaryPVProvider, T distanceThreshold)	Constructor.
FieldRelativeDistanceDetector(FieldPVCoordinatesProvider<T> secondaryPVProvider, T distanceThreshold)	Constructor with default values.

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 CalculusFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
class	FieldIntegratedEphemeris<T extends CalculusFieldElement<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 CalculusFieldElement<T>>	This class propagates orbits using numerical integration.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.sampling

Subinterfaces of FieldPVCoordinatesProvider in org.orekit.propagation.sampling

Modifier and Type	Interface	Description
interface	FieldOrekitStepInterpolator<T extends CalculusFieldElement<T>>	This interface is a space-dynamics aware step interpolator.

Uses of FieldPVCoordinatesProvider in org.orekit.propagation.semianalytical.dsst

Classes in org.orekit.propagation.semianalytical.dsst that implement FieldPVCoordinatesProvider

Modifier and Type	Class	Description
class	FieldDSSTPropagator<T extends CalculusFieldElement<T>>	This class propagates orbits using the DSST theory.

Uses of FieldPVCoordinatesProvider in org.orekit.utils

Classes in org.orekit.utils that implement FieldPVCoordinatesProvider

Modifier and Type	Class	Description
class	FieldAbsolutePVCoordinates<T extends CalculusFieldElement<T>>	Field implementation of AbsolutePVCoordinates.
class	FieldShiftingPVCoordinatesProvider<T extends CalculusFieldElement<T>>	Provider using simple FieldPVCoordinates.shiftedBy(CalculusFieldElement) shiftedBy} and frame transforms for evolution.

Methods in org.orekit.utils that return FieldPVCoordinatesProvider

Modifier and Type	Method	Description
default <T extends CalculusFieldElement<T>> FieldPVCoordinatesProvider<T>	ExtendedPositionProvider.toFieldPVCoordinatesProvider(Field<T> field)	Convert to a FieldPVCoordinatesProvider with a specific type.
FieldPVCoordinatesProvider<T>	FieldAbsolutePVCoordinates.toTaylorProvider()	Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).