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.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.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.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 and 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	TorqueFree.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	CelestialBodyPointed.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	LofOffset.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	FixedRate.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	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	YawCompensation.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	GroundPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	LofOffset.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	FrameAlignedProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	AggregateBoundedAttitudeProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
default org.hipparchus.geometry.euclidean.threed.Rotation	AttitudeProvider.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	AttitudesSequence.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	LofOffsetPointing.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	GroundPointing.getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
Attitude	YawSteering.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the base system state at given date, without compensation.
Attitude	YawCompensation.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the base system state at given date, without compensation.
protected org.hipparchus.geometry.euclidean.threed.Vector3D	GroundPointing.getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point position in specified frame.
TimeStampedPVCoordinates	YawSteering.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	BodyCenterPointing.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	YawCompensation.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	LofOffsetPointing.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.
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 and 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 and Description
interface	CelestialBody Interface for celestial bodies like Sun, Moon or solar system planets.

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

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

Constructor and Description
OneWayGNSSPhase(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local) Simple constructor.
OneWayGNSSRange(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double range, 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 and 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 and 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 and 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.forces.maneuvers.propulsion

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

Modifier and Type	Method and Description
org.hipparchus.geometry.euclidean.threed.Vector3D	ConstantThrustDirectionProvider.computeThrustDirection(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
org.hipparchus.geometry.euclidean.threed.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 and Description
class	TopocentricFrame Topocentric frame.

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

Constructor and 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 and 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 and 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 and 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 and 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 and 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 and 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 and 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 and 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.tle

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

Modifier and Type	Class and 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 and Description
PVCoordinatesProvider	AngularSeparationDetector.getBeacon() Get the beacon at the center of the proximity zone.
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.

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

Constructor and Description
AlignmentDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, PVCoordinatesProvider body, double alignAngle) Protected constructor with full parameters.
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(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.
ExtremumApproachDetector(AdaptableInterval maxCheck, double threshold, int maxIter, EventHandler handler, PVCoordinatesProvider secondaryPVProvider) Constructor.
ExtremumApproachDetector(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.

Uses of PVCoordinatesProvider in org.orekit.propagation.integration

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

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

Classes in org.orekit.utils that implement PVCoordinatesProvider

Modifier and Type	Class and 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.

Methods in org.orekit.utils that return PVCoordinatesProvider

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