Uses of Interface
org.orekit.utils.PVCoordinatesProvider

Packages that use PVCoordinatesProvider

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
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.estimation.measurements.model	This package contains physical models for measurement prediction.
org.orekit.files.ccsds.definitions	This package contains definitions for CCSDS objects (frames, time systems...).
org.orekit.files.ccsds.ndm.adm	This package contains class managing CCSDS Attitude Data Message.
org.orekit.files.ccsds.ndm.adm.apm	This package contains class managing CCSDS Attitude Parameter Message.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.models.earth.displacement	This package provides models computing reference points displacements on Earth surface.
org.orekit.models.earth.ionosphere	This package provides models that simulate the impact of the ionosphere.
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.gnss	This package provides classes to propagate GNSS orbits.
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.events.handlers	This package provides an interface and classes dealing with events occurrence only.
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.signal	This package contains methods and architecture for signal travel time.
org.orekit.utils	This package provides useful objects.

Uses of PVCoordinatesProvider in org.orekit.attitudes

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

Modifier and Type	Method	Description
Attitude	AttitudeBuilder.build(Frame frame, PVCoordinatesProvider pvProv, TimeStampedAngularCoordinates rawAttitude)	Build a filtered attitude.
Attitude	FixedFrameBuilder.build(Frame frame, PVCoordinatesProvider pvProv, TimeStampedAngularCoordinates rawAttitude)	Build a filtered attitude.
Attitude	AggregateBoundedAttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	AlignedAndConstrained.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
default Attitude	AttitudeProviderModifier.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	CelestialBodyPointed.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	FixedRate.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	FrameAlignedProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	GroundPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	LofOffset.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	LofOffsetPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	SpinStabilized.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	TabulatedLofOffset.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	TabulatedProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	TorqueFree.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	YawCompensation.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	YawSteering.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Rotation	AggregateBoundedAttitudeProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	AlignedAndConstrained.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
default Rotation	AttitudeProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	CelestialBodyPointed.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	FixedRate.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	FrameAlignedProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	GroundPointing.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	LofOffset.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	LofOffsetPointing.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	SpinStabilized.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Attitude	GroundPointingAttitudeModifier.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the base system state at given date, without modifications.
protected Vector3D	BodyCenterPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
protected Vector3D	GroundPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
protected Vector3D	GroundPointingAttitudeModifier.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
protected Vector3D	LofOffsetPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
protected Vector3D	NadirPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
protected Vector3D	TargetPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position in specified frame.
TimeStampedPVCoordinates	BodyCenterPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
protected abstract TimeStampedPVCoordinates	GroundPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	GroundPointingAttitudeModifier.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	LofOffsetPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	NadirPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	TargetPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	NadirPointing.getTargetPVViaInterpolation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute target position-velocity-acceleration vector via interpolation.
double	YawCompensation.getYawAngle(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the yaw compensation angle at date.

Uses of PVCoordinatesProvider in org.orekit.bodies

Subinterfaces of PVCoordinatesProvider in org.orekit.bodies

Modifier and Type	Interface	Description
interface	CelestialBody	Interface for celestial bodies like Sun, Moon or solar system planets.

Classes in org.orekit.bodies that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	AnalyticalLunarPositionProvider	Class computing low-fidelity positions for the Moon.
class	AnalyticalSolarPositionProvider	Class computing low-fidelity positions for the Sun.

Uses of PVCoordinatesProvider in org.orekit.estimation.measurements

Methods in org.orekit.estimation.measurements that return PVCoordinatesProvider

Modifier and Type	Method	Description
static PVCoordinatesProvider	AbstractParticipant.extractPVCoordinatesProvider(SpacecraftState templateState, TimeStampedPVCoordinates pvCoordinates)	Create PV provider from position-velocity-acceleration vector and template state.
final PVCoordinatesProvider	GroundStation.getPVCoordinatesProvider()	Return the PVCoordinatesProvider.
PVCoordinatesProvider	Observer.getPVCoordinatesProvider()	Return the PVCoordinatesProvider.
final PVCoordinatesProvider	ObserverSatellite.getPVCoordinatesProvider()	Return the PVCoordinatesProvider.

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

Modifier and Type	Method	Description
protected AbsoluteDate	AngularMeasurement.computeEmissionDate(SignalReceptionCondition receptionCondition, PVCoordinatesProvider emitter)	Compute the signal emission date.

Constructors in org.orekit.estimation.measurements with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	ObserverSatellite(String name, PVCoordinatesProvider pvCoordsProvider)	Simple constructor.
	ObserverSatellite(String name, PVCoordinatesProvider pvCoordsProvider, QuadraticClockModel quadraticClock)	Simple constructor.

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

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

Modifier and Type	Method	Description
protected PVCoordinatesProvider	AbstractInterSatellitesMeasurement.getRemotePV(SpacecraftState state)	Return the FieldPVCoordinatesProvider.

Uses of PVCoordinatesProvider in org.orekit.estimation.measurements.model

Methods in org.orekit.estimation.measurements.model with parameters of type PVCoordinatesProvider

Modifier and Type	Method	Description
protected Vector3D	AbstractAngularMeasurementModel.getEmitterToReceiverVector(SignalReceptionCondition receptionCondition, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute emitter-to-receiver vector.
double	OneLeggedRangeRateModel.value(SignalReceptionCondition receptionCondition, Vector3D receiverVelocity, PVCoordinatesProvider emitter)	Compute measurement without guess.
double	OneLeggedRangeRateModel.value(SignalReceptionCondition receptionCondition, Vector3D receiverVelocity, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute measurement.
double[]	RaDecModel.value(SignalReceptionCondition receptionCondition, PVCoordinatesProvider emitter)	Compute theoretical measurement.
double[]	RaDecModel.value(SignalReceptionCondition receptionCondition, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute theoretical measurement with guess for the emission date.
double[]	TopocentricAzElModel.value(GeodeticPoint receiver, AbsoluteDate receptionDate, PVCoordinatesProvider emitter)	Compute theoretical measurement.
double[]	TopocentricAzElModel.value(GeodeticPoint receiver, AbsoluteDate receptionDate, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute theoretical measurement with guess for emission date.
double	TwoLeggedRangeRateModel.value(Frame frame, PVCoordinates receiverPV, AbsoluteDate receptionDate, PVCoordinatesProvider relay, AbsoluteDate approxRelayDate, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute measurement.
double	TwoLeggedRangeRateModel.value(Frame frame, PVCoordinates receiverPV, AbsoluteDate receptionDate, PVCoordinatesProvider relay, PVCoordinatesProvider emitter)	Compute measurement without guess.

Uses of PVCoordinatesProvider in org.orekit.files.ccsds.definitions

Methods in org.orekit.files.ccsds.definitions with parameters of type PVCoordinatesProvider

Modifier and Type	Method	Description
static Transform	FrameFacade.getTransform(FrameFacade frameIn, FrameFacade frameOut, Frame inertialPivotFrame, AbsoluteDate date, PVCoordinatesProvider pv)	Get the transform between CCSDS frames.

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

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

Modifier and Type	Method	Description
Attitude	AttitudeEndpoints.build(Frame frame, PVCoordinatesProvider pvProv, TimeStampedAngularCoordinates rawAttitude)	Build a filtered attitude.

Uses of PVCoordinatesProvider in org.orekit.files.ccsds.ndm.adm.apm

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

Modifier and Type	Method	Description
Attitude	Apm.getAttitude(Frame frame, PVCoordinatesProvider pvProvider)	Get the attitude.
Attitude	ApmData.getAttitude(Frame frame, PVCoordinatesProvider pvProvider)	Get the attitude.

Uses of PVCoordinatesProvider in org.orekit.files.general

Classes in org.orekit.files.general that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	EphemerisSegmentPropagator<C extends TimeStampedPVCoordinates>	A Propagator based on a EphemerisFile.EphemerisSegment.

Uses of PVCoordinatesProvider in org.orekit.frames

Classes in org.orekit.frames that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	TopocentricFrame	Topocentric frame.

Constructors in org.orekit.frames with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	LocalOrbitalFrame(Frame parent, LOF lof, PVCoordinatesProvider provider, String name)	Build a new instance.

Uses of PVCoordinatesProvider in org.orekit.models.earth.displacement

Constructors in org.orekit.models.earth.displacement with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	TidalDisplacement(double rEarth, double sunEarthSystemMassRatio, double earthMoonMassRatio, PVCoordinatesProvider sun, PVCoordinatesProvider moon, IERSConventions conventions, boolean removePermanentDeformation)	Simple constructor.

Uses of PVCoordinatesProvider in org.orekit.models.earth.ionosphere

Methods in org.orekit.models.earth.ionosphere with parameters of type PVCoordinatesProvider

Modifier and Type	Method	Description
default <T extends CalculusFieldElement<T>> T	IonosphericModel.pathDelay(FieldSpacecraftState<T> state, PVCoordinatesProvider coordsProvider, double frequency, T[] parameters)	Calculates the ionospheric path delay for the signal path from an observation object to the satellite being measured.
default double	IonosphericModel.pathDelay(SpacecraftState state, PVCoordinatesProvider coordsProvider, double frequency, double[] parameters)	Calculates the ionospheric path delay for the signal path from an observation object to the satellite being measured.

Uses of PVCoordinatesProvider in org.orekit.orbits

Classes in org.orekit.orbits that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	CartesianOrbit	This class holds Cartesian orbital parameters.
class	CircularOrbit	This class handles circular orbital parameters.
class	EquinoctialOrbit	This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
class	KeplerianExtendedPositionProvider	Position provider assuming pure Keplerian motion.
class	KeplerianOrbit	This class handles traditional Keplerian orbital parameters.
class	Orbit	This class handles orbital parameters.

Uses of PVCoordinatesProvider in org.orekit.propagation

Subinterfaces of PVCoordinatesProvider in org.orekit.propagation

Modifier and Type	Interface	Description
interface	BoundedPropagator	This interface is intended for ephemerides valid only during a time range.
interface	Propagator	This interface provides a way to propagate an orbit at any time.

Classes in org.orekit.propagation that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	AbstractPropagator	Common handling of Propagator methods for propagators.

Uses of PVCoordinatesProvider in org.orekit.propagation.analytical

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

Modifier and Type	Class	Description
class	AbstractAnalyticalPropagator	Common handling of Propagator methods for analytical propagators.
class	AdapterPropagator	Orbit propagator that adapts an underlying propagator, adding differential effects.
class	AggregateBoundedPropagator	A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
class	BrouwerLyddanePropagator	This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
class	EcksteinHechlerPropagator	This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
class	Ephemeris	This class is designed to accept and handle tabulated orbital entries.
class	EphemerisExtendedPositionProvider	Class providing position, including Field, based on ephemeris (tabulated states).
class	KeplerianPropagator	Simple Keplerian orbit propagator.

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

Modifier and Type	Method	Description
PVCoordinatesProvider	AbstractAnalyticalPropagator.getPvProvider()	Get PV coordinates provider.

Uses of PVCoordinatesProvider in org.orekit.propagation.analytical.gnss

Classes in org.orekit.propagation.analytical.gnss that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	GLONASSAnalyticalPropagator	This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
class	GNSSExtendedPositionProvider	Class for GNSS extended position provider.
class	GNSSPropagator	Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
class	SBASPropagator	This class aims at propagating a SBAS orbit from SBASOrbitalElements.

Uses of PVCoordinatesProvider in org.orekit.propagation.analytical.intelsat

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

Modifier and Type	Class	Description
class	IntelsatElevenElementsPropagator	This class provides elements to propagate Intelsat's 11 elements.

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

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

Modifier and Type	Class	Description
class	DeepSDP4	This class contains the methods that compute deep space perturbation terms.
class	SGP4	This class contains methods to compute propagated coordinates with the SGP4 model.
class	TleExtendedPositionProvider	Position provider from a TLE.
class	TLEPropagator	This class provides elements to propagate TLE's.

Uses of PVCoordinatesProvider in org.orekit.propagation.events

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

Modifier and Type	Method	Description
PVCoordinatesProvider	AngularSeparationDetector.getBeacon()	Get the beacon at the center of the proximity zone.
PVCoordinatesProvider	BetaAngleDetector.getCelestialBodyProvider()	Coordinate provider for the celestial body.
PVCoordinatesProvider	AngularSeparationDetector.getObserver()	Get the observer for the spacecraft.
PVCoordinatesProvider	AngularSeparationFromSatelliteDetector.getPrimaryObject()	Get the primaryObject, at the center of the proximity zone.
PVCoordinatesProvider	AlignmentDetector.getPVCoordinatesProvider()	Get the body to align.
PVCoordinatesProvider	FieldOfViewDetector.getPVTarget()	Get the position/velocity provider of the target .
PVCoordinatesProvider	InterSatDirectViewDetector.getSecondary()	Get the provider for the secondary satellite.
PVCoordinatesProvider	AngularSeparationFromSatelliteDetector.getSecondaryObject()	Get the secondaryObject.
PVCoordinatesProvider	ExtremumApproachDetector.getSecondaryPVProvider()	Get the secondary position-velocity provider stored in this instance.
PVCoordinatesProvider	RelativeDistanceDetector.getSecondaryPVProvider()	Get the secondary position-velocity provider stored in this instance.

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

Modifier and Type	Method	Description
static double	BetaAngleDetector.calculateBetaAngle(SpacecraftState state, PVCoordinatesProvider celestialBodyProvider)	Calculate the beta angle between the orbit plane and the celestial body.
static double	BetaAngleDetector.calculateBetaAngle(SpacecraftState state, PVCoordinatesProvider celestialBodyProvider, Frame frame)	Calculate the beta angle between the orbit plane and the celestial body.
BetaAngleDetector	BetaAngleDetector.withCelestialProvider(PVCoordinatesProvider newProvider)	Create a new instance with the provided coordinate provider.

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

Modifier	Constructor	Description
	AlignmentDetector(double maxCheck, double threshold, PVCoordinatesProvider body, double alignAngle)	Build a new alignment detector.
	AlignmentDetector(double threshold, Orbit orbit, PVCoordinatesProvider body, double alignAngle)	Build a new alignment detector.
	AlignmentDetector(Orbit orbit, PVCoordinatesProvider body, double alignAngle)	Build a new alignment detector.
protected	AlignmentDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider body, double alignAngle)	Protected constructor with full parameters.
	AlignmentDetector(EventDetectionSettings detectionSettings, PVCoordinatesProvider body, double alignAngle)	Build a new alignment detector.
protected	AngularSeparationDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider beacon, PVCoordinatesProvider observer, double proximityAngle)	Protected constructor with full parameters.
	AngularSeparationDetector(PVCoordinatesProvider beacon, PVCoordinatesProvider observer, double proximityAngle)	Build a new angular separation detector.
protected	AngularSeparationFromSatelliteDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider primaryObject, PVCoordinatesProvider secondaryObject, double proximityAngle)	Protected constructor with full parameters.
	AngularSeparationFromSatelliteDetector(PVCoordinatesProvider primaryObject, PVCoordinatesProvider secondaryObject, double proximityAngle)	Build a new angular detachment detector.
	BetaAngleDetector(double betaAngleThreshold, PVCoordinatesProvider celestialBodyProvider, Frame inertialFrame)	Class constructor.
protected	BetaAngleDetector(EventDetectionSettings detectionSettings, EventHandler handler, double betaAngleThreshold, PVCoordinatesProvider celestialBodyProvider, Frame inertialFrame)	Protected constructor with full parameters.
	CylindricalShadowEclipseDetector(PVCoordinatesProvider sun, double occultingBodyRadius, EventDetectionSettings eventDetectionSettings, EventHandler handler)	Constructor.
	CylindricalShadowEclipseDetector(PVCoordinatesProvider sun, double occultingBodyRadius, EventHandler handler)	Constructor with default detection settings.
protected	ExtremumApproachDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider secondaryPVProvider)	Constructor.
	ExtremumApproachDetector(PVCoordinatesProvider secondaryPVProvider)	Constructor with default values.
	FieldExtremumApproachDetector(Field<T> field, PVCoordinatesProvider secondaryPVProvider)	Constructor with default values.
protected	FieldOfViewDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider pvTarget, double radiusTarget, VisibilityTrigger trigger, FieldOfView fov)	Protected constructor with full parameters.
	FieldOfViewDetector(PVCoordinatesProvider pvTarget, double radiusTarget, VisibilityTrigger trigger, FieldOfView fov)	Build a new instance.
	FieldOfViewDetector(PVCoordinatesProvider pvTarget, FieldOfView fov)	Build a new instance.
	GroundAtNightDetector(TopocentricFrame groundLocation, PVCoordinatesProvider sun, double dawnDuskElevation, AtmosphericRefractionModel refractionModel)	Simple constructor.
protected	InterSatDirectViewDetector(OneAxisEllipsoid body, double skimmingAltitude, PVCoordinatesProvider secondary, EventDetectionSettings detectionSettings, EventHandler handler)	Protected constructor.
	InterSatDirectViewDetector(OneAxisEllipsoid body, PVCoordinatesProvider secondary)	simple constructor.
protected	RelativeDistanceDetector(EventDetectionSettings detectionSettings, EventHandler handler, PVCoordinatesProvider secondaryPVProvider, double distanceThreshold)	Constructor.
	RelativeDistanceDetector(PVCoordinatesProvider secondaryPVProvider, double distanceThreshold)	Constructor with default values.

Uses of PVCoordinatesProvider in org.orekit.propagation.events.handlers

Methods in org.orekit.propagation.events.handlers that return PVCoordinatesProvider

Modifier and Type	Method	Description
PVCoordinatesProvider	SecondaryEventLogger.getSecondaryPVCoordinatesProvider()	Getter for the secondary trajectory provider.

Constructors in org.orekit.propagation.events.handlers with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	SecondaryEventLogger(PVCoordinatesProvider secondaryPVCoordinatesProvider)	Constructor with default Action (CONTINUE).
	SecondaryEventLogger(PVCoordinatesProvider secondaryPVCoordinatesProvider, Action action)	Constructor.

Uses of PVCoordinatesProvider in org.orekit.propagation.integration

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

Modifier and Type	Class	Description
class	AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
class	IntegratedEphemeris	This class stores sequentially generated orbital parameters for later retrieval.

Uses of PVCoordinatesProvider in org.orekit.propagation.numerical

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

Modifier and Type	Class	Description
class	GLONASSNumericalPropagator	This class propagates GLONASS orbits using numerical integration.
class	NumericalPropagator	This class propagates orbits using numerical integration.

Uses of PVCoordinatesProvider in org.orekit.propagation.sampling

Subinterfaces of PVCoordinatesProvider in org.orekit.propagation.sampling

Modifier and Type	Interface	Description
interface	OrekitStepInterpolator	This interface is a space-dynamics aware step interpolator.

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

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

Modifier and Type	Class	Description
class	DSSTPropagator	This class propagates orbits using the DSST theory.

Uses of PVCoordinatesProvider in org.orekit.signal

Methods in org.orekit.signal with parameters of type PVCoordinatesProvider

Modifier and Type	Method	Description
double[]	DifferencesOfSignalArrival.computeDelays(SignalReceptionCondition primaryReceptionCondition, PVCoordinatesProvider secondaryReceiver, AbsoluteDate approxSecondaryReception, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute (positive) delays from emission.
double[]	DifferencesOfSignalArrival.computeDelays(SignalReceptionCondition primaryReceptionCondition, PVCoordinatesProvider secondaryReceiver, PVCoordinatesProvider emitter)	Compute (positive) delays from emission without guesses.
double[]	TwoLeggedSignalTimer.computeDelays(SignalReceptionCondition endReceptionCondition, PVCoordinatesProvider relay, AbsoluteDate approxRelayDate, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute first and second leg delays.
double[]	TwoLeggedSignalTimer.computeDelays(SignalReceptionCondition endReceptionCondition, PVCoordinatesProvider relay, PVCoordinatesProvider emitter)	Compute first and second leg delays without guess.
AdjustableEmitterSignalTimer	SignalTravelTimeModel.getAdjustableEmitterComputer(PVCoordinatesProvider emitter)	Method constructing a delay computer with input emitter.
AdjustableReceiverSignalTimer	SignalTravelTimeModel.getAdjustableReceiverComputer(PVCoordinatesProvider receiver)	Method constructing a delay computer with input receiver.

Constructors in org.orekit.signal with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	AdjustableEmitterSignalTimer(PVCoordinatesProvider adjustableEmitterPVProvider)	Constructor with default iteration settings.
	AdjustableEmitterSignalTimer(PVCoordinatesProvider adjustableEmitterPVProvider, ConvergenceChecker<Double> checker)	Constructor.
	AdjustableReceiverSignalTimer(PVCoordinatesProvider adjustableReceiverPVProvider)	Constructor.
	AdjustableReceiverSignalTimer(PVCoordinatesProvider adjustableReceiverPVProvider, ConvergenceChecker<Double> checker)	Constructor.

Uses of PVCoordinatesProvider in org.orekit.utils

Classes in org.orekit.utils with type parameters of type PVCoordinatesProvider

Modifier and Type	Class	Description
class	AbstractExtendedPositionProvider<T extends PVCoordinatesProvider>	Abstract class for position provider based on a given type of provider.
interface	ShiftablePVCoordinatesHolder<T extends PVCoordinatesProvider>	Interface for time-shiftable PV provider holding themselves PV coordinates.

Subinterfaces of PVCoordinatesProvider in org.orekit.utils

Modifier and Type	Interface	Description
interface	BoundedPVCoordinatesProvider	Interface for bounded PV coordinates providers.
interface	ExtendedPositionProvider	Interface for position providers (including for Field).
interface	ShiftablePVCoordinatesHolder<T extends PVCoordinatesProvider>	Interface for time-shiftable PV provider holding themselves PV coordinates.

Classes in org.orekit.utils that implement PVCoordinatesProvider

Modifier and Type	Class	Description
class	AbsolutePVCoordinates	Position - Velocity - Acceleration linked to a date and a frame.
class	AbstractExtendedPositionProvider<T extends PVCoordinatesProvider>	Abstract class for position provider based on a given type of provider.
class	AggregatedPVCoordinatesProvider	Aggregate multiple PVCoordinatesProvider instances together.
static class	AggregatedPVCoordinatesProvider.InvalidPVProvider	Implementation of PVCoordinatesProvider that throws an OrekitException exception.
class	ConstantPositionProvider	Fixed-position (in a given frame) provider.
class	FrameAdapter	Adapter from Frame to ExtendedPositionProvider.
class	GeodeticExtendedPositionProvider	Position provider from a given fixed point w.r.t. to a body.
class	TaylorExtendedPositionProvider	Class providing position, including Field, according to 2nd order Taylor expansion.

Methods in org.orekit.utils that return PVCoordinatesProvider

Modifier and Type	Method	Description
PVCoordinatesProvider	WaypointPVBuilder.build()	Build a PVCoordinatesProvider from the waypoints added to this builder.
PVCoordinatesProvider	WaypointPVBuilder.InterpolationFactory.create(AbsoluteDate date1, GeodeticPoint point1, AbsoluteDate date2, GeodeticPoint point2, OneAxisEllipsoid body)	Create a PVCoordinatesProvider which interpolates between the provided waypoints.
protected PVCoordinatesProvider	WaypointPVBuilder.createFinal(GeodeticPoint lastPoint)	Create the final provider.
protected PVCoordinatesProvider	WaypointPVBuilder.createInitial(GeodeticPoint firstPoint)	Create the initial provider.
PVCoordinatesProvider	AbsolutePVCoordinates.toTaylorProvider()	Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).
PVCoordinatesProvider	TimeStampedPVCoordinates.toTaylorProvider(Frame instanceFrame)	Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).

Methods in org.orekit.utils with parameters of type PVCoordinatesProvider

Modifier and Type	Method	Description
AggregatedPVCoordinatesProvider.Builder	AggregatedPVCoordinatesProvider.Builder.addPVProviderAfter(AbsoluteDate date, PVCoordinatesProvider pvProv, boolean erasesLater)	Add a PVCoordinatesProvider to the collection.
AggregatedPVCoordinatesProvider.Builder	AggregatedPVCoordinatesProvider.Builder.addPVProviderBefore(AbsoluteDate date, PVCoordinatesProvider pvProv, boolean erasesEarlier)	Add a PVCoordinatesProvider to the collection.
static BoundedPVCoordinatesProvider	BoundedPVCoordinatesProvider.of(PVCoordinatesProvider provider, TimeInterval interval)	Bound a given coordinates provider.

Constructors in org.orekit.utils with parameters of type PVCoordinatesProvider

Modifier	Constructor	Description
	Builder(PVCoordinatesProvider initialProvider)	Create a builder using the provided initial provider.

Constructor parameters in org.orekit.utils with type arguments of type PVCoordinatesProvider

Modifier	Constructor	Description
	AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider> map)	Class constructor.
	AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider> map, AbsoluteDate minDate, AbsoluteDate maxDate)	Class constructor.