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.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.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.models.earth.atmosphere	This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.displacement	This package provides models computing reference points displacements on Earth surface.
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.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 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	AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	AttitudesSequence.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.
default Rotation	AttitudeProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude-related rotation corresponding to an orbital state.
Rotation	AttitudesSequence.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	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.

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

Constructor	Description
CelestialBodyPointed(Frame celestialFrame, PVCoordinatesProvider pointedBody, Vector3D phasingCel, Vector3D pointingSat, Vector3D phasingSat)	Creates new instance.
YawSteering(Frame inertialFrame, GroundPointing groundPointingLaw, PVCoordinatesProvider sun, Vector3D phasingAxis)	Creates a new instance.

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.

Uses of PVCoordinatesProvider in org.orekit.estimation.measurements

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

Modifier and Type	Method	Description
static double	AbstractMeasurement.signalTimeOfFlight(PVCoordinatesProvider adjustableEmitter, AbsoluteDate approxEmissionDate, Vector3D receiverPosition, AbsoluteDate signalArrivalDate, Frame receiverFrame)	Compute propagation delay on a link leg (typically downlink or uplink).

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[] states)	Get emitting satellite position/velocity provider.
protected abstract PVCoordinatesProvider	AbstractOnBoardMeasurement.getRemotePV(SpacecraftState[] states)	Get emitting satellite position/velocity provider.
protected PVCoordinatesProvider	AbstractOneWayGNSSMeasurement.getRemotePV(SpacecraftState[] states)	Get emitting satellite position/velocity provider.

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

Constructor	Description
AbstractOneWayGNSSMeasurement(PVCoordinatesProvider remotePV, QuadraticClockModel remoteClock, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
OneWayGNSSPhase(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local)	Deprecated. as of 12.1, replaced by OneWayGNSSPhase(PVCoordinatesProvider, String, QuadraticClockModel, AbsoluteDate, double, double, double, double, ObservableSatellite, AmbiguityCache)
OneWayGNSSPhase(PVCoordinatesProvider remote, String remoteName, QuadraticClockModel remoteClock, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache)	Simple constructor.
OneWayGNSSRange(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
OneWayGNSSRange(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
OneWayGNSSRangeRate(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
OneWayGNSSRangeRate(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.

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.forces.maneuvers.propulsion

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

Modifier and Type	Method	Description
Vector3D	ConstantThrustDirectionProvider.computeThrustDirection(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Vector3D	ThrustDirectionProvider.computeThrustDirection(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the thrust direction corresponding to an orbital state.
Attitude	ThrustDirectionAndAttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
protected Attitude	ThrustDirectionAndAttitudeProvider.getAttitudeFromFrame(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.

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

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

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

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

Constructor	Description
DTM2000(DTM2000InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth)	Simple constructor for independent computation.
DTM2000(DTM2000InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth, TimeScale utc)	Simple constructor for independent computation.
HarrisPriester(PVCoordinatesProvider sun, OneAxisEllipsoid earth)	Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sun, OneAxisEllipsoid earth, double n)	Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sun, OneAxisEllipsoid earth, double[][] tabAltRho)	Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sun, OneAxisEllipsoid earth, double[][] tabAltRho, double n)	Constructor for Modified Harris-Priester atmosphere model.
JB2008(JB2008InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth)	Constructor with space environment information for internal computation.
JB2008(JB2008InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth, TimeScale utc)	Constructor with space environment information for internal computation.
NRLMSISE00(NRLMSISE00InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth)	Constructor.
NRLMSISE00(NRLMSISE00InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth, TimeScale ut)	Constructor.

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

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

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.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	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 analytical 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	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	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	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

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.
AlignmentDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, PVCoordinatesProvider body, double alignAngle)	Protected constructor with full parameters.
AngularSeparationDetector(AdaptableInterval maxCheck, double threshold, int maxIter, 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.
AngularSeparationFromSatelliteDetector(AdaptableInterval maxCheck, double threshold, int maxIter, 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.
BetaAngleDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, double betaAngleThreshold, PVCoordinatesProvider celestialBodyProvider, Frame inertialFrame)	Protected constructor with full parameters.
CylindricalShadowEclipseDetector(PVCoordinatesProvider sun, double occultingBodyRadius, AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler)	Constructor.
CylindricalShadowEclipseDetector(PVCoordinatesProvider sun, double occultingBodyRadius, EventHandler handler)	Constructor with default detection settings.
ExtremumApproachDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, PVCoordinatesProvider secondaryPVProvider)	Constructor.
ExtremumApproachDetector(PVCoordinatesProvider secondaryPVProvider)	Constructor with default values.
FieldExtremumApproachDetector(Field<T> field, PVCoordinatesProvider secondaryPVProvider)	Constructor with default values.
FieldOfViewDetector(AdaptableInterval maxCheck, double threshold, int maxIter, 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.
GroundAtNightDetector(TopocentricFrame groundLocation, PVCoordinatesProvider sun, double dawnDuskElevation, AtmosphericRefractionModel refractionModel, AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler)	Private constructor.
InterSatDirectViewDetector(OneAxisEllipsoid body, double skimmingAltitude, PVCoordinatesProvider secondary, AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler)	Private constructor.
InterSatDirectViewDetector(OneAxisEllipsoid body, PVCoordinatesProvider secondary)	simple constructor.
RelativeDistanceDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, PVCoordinatesProvider secondaryPVProvider, double distanceThreshold)	Constructor.
RelativeDistanceDetector(PVCoordinatesProvider secondaryPVProvider, double distanceThreshold)	Constructor with default values.

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.utils

Subinterfaces of PVCoordinatesProvider in org.orekit.utils

Modifier and Type	Interface	Description
interface	ExtendedPositionProvider	Interface for position providers (including for Field).
interface	ExtendedPVCoordinatesProvider	Interface for PV coordinates providers that also support fields.

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	AggregatedPVCoordinatesProvider	Aggreate multiple PVCoordinatesProvider instances together This can be used to describe an aircraft or surface vehicle.
static class	AggregatedPVCoordinatesProvider.InvalidPVProvider	Implementation of PVCoordinatesProvider that throws an illegal state exception.
class	ConstantPVCoordinatesProvider	Provider based on a single point.
class	FrameAdapter	Adapter from Frame to ExtendedPVCoordinatesProvider.
class	ShiftingPVCoordinatesProvider	Provider using simple PVCoordinates.shiftedBy(double) shiftedBy} and frame transforms for evolution.

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(AbsoluteDate lastDate, GeodeticPoint lastPoint)	Create the final provider.
protected PVCoordinatesProvider	WaypointPVBuilder.createInitial(AbsoluteDate firstDate, 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.

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

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

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