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.forces	This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag.atmosphere	This package provides the atmosphere model interface and several implementations.
org.orekit.forces.radiation	This package provides all radiation pressure related forces.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.gnss.attitude	This package provides classes related to navigation satellites attitude modeling.
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.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.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for 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	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	GroundPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.
Attitude	InertialProvider.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	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.
Attitude	YawCompensation.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the base system state at given date, without compensation.
Attitude	YawSteering.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the base system state at given date, without compensation.
TimeStampedPVCoordinates	BodyCenterPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
abstract TimeStampedPVCoordinates	GroundPointing.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	YawCompensation.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	YawSteering.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
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, org.hipparchus.geometry.euclidean.threed.Vector3D phasingCel, org.hipparchus.geometry.euclidean.threed.Vector3D pointingSat, org.hipparchus.geometry.euclidean.threed.Vector3D phasingSat)	Creates new instance.
YawSteering(Frame inertialFrame, GroundPointing groundPointingLaw, PVCoordinatesProvider sun, org.hipparchus.geometry.euclidean.threed.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.forces

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

Constructor	Description
BoxAndSolarArraySpacecraft(double xLength, double yLength, double zLength, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, double dragCoeff, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double xLength, double yLength, double zLength, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, double dragCoeff, double liftRatio, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double xLength, double yLength, double zLength, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, AbsoluteDate referenceDate, org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal, double rotationRate, double dragCoeff, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(double xLength, double yLength, double zLength, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, AbsoluteDate referenceDate, org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal, double rotationRate, double dragCoeff, double liftRatio, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, double dragCoeff, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, double dragCoeff, double liftRatio, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, AbsoluteDate referenceDate, org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal, double rotationRate, double dragCoeff, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets, PVCoordinatesProvider sun, double solarArrayArea, org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis, AbsoluteDate referenceDate, org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal, double rotationRate, double dragCoeff, double liftRatio, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with linear rotation of solar array.

Uses of PVCoordinatesProvider in org.orekit.forces.drag.atmosphere

Constructors in org.orekit.forces.drag.atmosphere with parameters of type PVCoordinatesProvider

Constructor	Description
DTM2000(DTM2000InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth)	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.
NRLMSISE00(NRLMSISE00InputParameters parameters, PVCoordinatesProvider sun, BodyShape earth)	Constructor.

Uses of PVCoordinatesProvider in org.orekit.forces.radiation

Constructors in org.orekit.forces.radiation with parameters of type PVCoordinatesProvider

Constructor	Description
SolarRadiationPressure(double dRef, double pRef, PVCoordinatesProvider sun, double equatorialRadius, RadiationSensitive spacecraft)	Deprecated. as of 9.2 replaced by SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)
SolarRadiationPressure(PVCoordinatesProvider sun, double equatorialRadius, RadiationSensitive spacecraft)	Deprecated. as of 9.2 replaced by SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)

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, LOFType type, PVCoordinatesProvider provider, String name)	Build a new instance.

Uses of PVCoordinatesProvider in org.orekit.gnss.attitude

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

Modifier and Type	Method	Description
Attitude	AbstractGNSSAttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the attitude corresponding to an orbital state.

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	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	GPSPropagator	This class aims at propagating a GPS orbit from GPSOrbitalElements.

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	AngularSeparationDetector.getObserver()	Get the observer for the spacecraft.
PVCoordinatesProvider	EclipseDetector.getOcculted()	Get the occulted body.
PVCoordinatesProvider	FieldEclipseDetector.getOcculted()	Get the occulted body.
PVCoordinatesProvider	EclipseDetector.getOcculting()	Get the occulting body.
PVCoordinatesProvider	FieldEclipseDetector.getOcculting()	Get the occulting body.
PVCoordinatesProvider	AlignmentDetector.getPVCoordinatesProvider()	Get the body to align.
PVCoordinatesProvider	CircularFieldOfViewDetector.getPVTarget()	Get the position/velocity provider of the target .
PVCoordinatesProvider	FieldOfViewDetector.getPVTarget()	Get the position/velocity provider of the target .
PVCoordinatesProvider	InterSatDirectViewDetector.getSlave()	Get the provider for the slave satellite.

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.
AngularSeparationDetector(PVCoordinatesProvider beacon, PVCoordinatesProvider observer, double proximityAngle)	Build a new angular separation detector.
CircularFieldOfViewDetector(double maxCheck, PVCoordinatesProvider pvTarget, org.hipparchus.geometry.euclidean.threed.Vector3D center, double halfAperture)	Build a new instance.
EclipseDetector(double maxCheck, double threshold, PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius)	Build a new eclipse detector.
EclipseDetector(double maxCheck, PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius)	Build a new eclipse detector.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius)	Build a new eclipse detector.
FieldEclipseDetector(PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius, org.hipparchus.Field<T> field)	Build a new eclipse detector.
FieldEclipseDetector(T maxCheck, PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius)	Build a new eclipse detector.
FieldEclipseDetector(T maxCheck, T threshold, PVCoordinatesProvider occulted, double occultedRadius, PVCoordinatesProvider occulting, double occultingRadius)	Build a new eclipse detector.
FieldOfViewDetector(PVCoordinatesProvider pvTarget, FieldOfView fov)	Build a new instance.
GroundAtNightDetector(TopocentricFrame groundLocation, PVCoordinatesProvider sun, double dawnDuskElevation, AtmosphericRefractionModel refractionModel)	Simple constructor.
InterSatDirectViewDetector(OneAxisEllipsoid body, PVCoordinatesProvider slave)	simple 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	NumericalPropagator	This class propagates orbits using numerical integration.

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.propagation.semianalytical.dsst.forces

Constructors in org.orekit.propagation.semianalytical.dsst.forces with parameters of type PVCoordinatesProvider

Constructor	Description
DSSTSolarRadiationPressure(double dRef, double pRef, double cr, double area, PVCoordinatesProvider sun, double equatorialRadius)	Deprecated. as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double)
DSSTSolarRadiationPressure(double cr, double area, PVCoordinatesProvider sun, double equatorialRadius)	Deprecated. as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double)
DSSTSolarRadiationPressure(double dRef, double pRef, PVCoordinatesProvider sun, double equatorialRadius, RadiationSensitive spacecraft)	Deprecated. as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)
DSSTSolarRadiationPressure(PVCoordinatesProvider sun, double equatorialRadius, RadiationSensitive spacecraft)	Deprecated. as of 9.2 replaced by {DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)

Uses of PVCoordinatesProvider in org.orekit.utils

Subinterfaces of PVCoordinatesProvider in org.orekit.utils

Modifier and Type	Interface	Description
interface	ExtendedPVCoordinatesProvider	Interface for PV coordinates providers that also support fields.

Methods in org.orekit.utils that return PVCoordinatesProvider

Modifier and Type	Method	Description
PVCoordinatesProvider	TimeStampedPVCoordinates.toTaylorProvider(Frame instanceFrame)	Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).