Uses of Interface
fr.cnes.sirius.patrius.orbits.pvcoordinates.PVCoordinatesProvider

Packages that use PVCoordinatesProvider

Package	Description
fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.attitudes
fr.cnes.sirius.patrius.attitudes.directions
fr.cnes.sirius.patrius.attitudes.multi
fr.cnes.sirius.patrius.attitudes.orientations
fr.cnes.sirius.patrius.attitudes.profiles
fr.cnes.sirius.patrius.attitudes.slew
fr.cnes.sirius.patrius.bodies
fr.cnes.sirius.patrius.events
fr.cnes.sirius.patrius.events.sensor
fr.cnes.sirius.patrius.forces.atmospheres
fr.cnes.sirius.patrius.forces.radiation
fr.cnes.sirius.patrius.forces.relativistic
fr.cnes.sirius.patrius.frames
fr.cnes.sirius.patrius.groundstation
fr.cnes.sirius.patrius.orbits
fr.cnes.sirius.patrius.orbits.pvcoordinates
fr.cnes.sirius.patrius.projections
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.analytical
fr.cnes.sirius.patrius.propagation.analytical.tle
fr.cnes.sirius.patrius.propagation.analytical.twod
fr.cnes.sirius.patrius.propagation.events
fr.cnes.sirius.patrius.propagation.numerical
fr.cnes.sirius.patrius.propagation.precomputed
fr.cnes.sirius.patrius.propagation.precomputed.multi
fr.cnes.sirius.patrius.signalpropagation
fr.cnes.sirius.patrius.stela.bodies
fr.cnes.sirius.patrius.stela.forces.radiation
fr.cnes.sirius.patrius.stela.orbits
fr.cnes.sirius.patrius.stela.propagation
fr.cnes.sirius.patrius.time
fr.cnes.sirius.patrius.wrenches

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.assembly.models

Classes in fr.cnes.sirius.patrius.assembly.models that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	SensorModel

Methods in fr.cnes.sirius.patrius.assembly.models that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	SensorModel.getInhibitionTarget(int inhibitionFieldNumber) Returns inhibition field number #i.
PVCoordinatesProvider	SensorModel.getMainTarget() Returns the main target.

Methods in fr.cnes.sirius.patrius.assembly.models with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
void	SensorModel.setMainTarget(PVCoordinatesProvider target, LocalRadiusProvider radius) Sets the main target of the sensor property.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.assembly.properties

Methods in fr.cnes.sirius.patrius.assembly.properties that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider[]	SensorProperty.getInhibitionTargets()
PVCoordinatesProvider	SensorProperty.getMainTarget()

Methods in fr.cnes.sirius.patrius.assembly.properties with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
void	SensorProperty.setInhibitionFieldsAndTargets(IFieldOfView[] fields, PVCoordinatesProvider[] targets, LocalRadiusProvider[] targetRadiuses) Sets the arrays of inhibition fields and the associated targets : the two array must have the same length.
void	SensorProperty.setMainTarget(PVCoordinatesProvider target, LocalRadiusProvider radius) Sets the main target of the sensor

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes

Fields in fr.cnes.sirius.patrius.attitudes declared as PVCoordinatesProvider

Modifier and Type	Field and Description
protected PVCoordinatesProvider	AbstractAttitudeEphemerisGenerator.provider PV coordinate provider.

Methods in fr.cnes.sirius.patrius.attitudes that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	YawSteering.getSun() Returns the Sun.

Methods in fr.cnes.sirius.patrius.attitudes with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
void	IsisNumericalSpinBiasSlew.compute(PVCoordinatesProvider pvProv) Deprecated. Compute the slew corresponding to an orbital state.
void	IsisAnalyticalSpinBiasSlew.compute(PVCoordinatesProvider pvProv) Deprecated. Compute the slew corresponding to an orbital state.
void	TwoSpinBiasSlew.compute(PVCoordinatesProvider pvProv) Deprecated. Compute the slew corresponding to an orbital state.
void	TabulatedSlew.compute(PVCoordinatesProvider pvProv) Compute the slew corresponding to an orbital state.
void	ConstantSpinSlew.compute(PVCoordinatesProvider pvProv) Deprecated. as of 4.5, ConstantSpinSlew object should be built either from constructor or from class ConstantSpinSlewComputer.
void	Slew.compute(PVCoordinatesProvider pvProv) Deprecated. as of 4.5. Use slew computers in order to retrieve built slews.
double	TwoSpinBiasSlew.computeDuration(PVCoordinatesProvider pvProv) Deprecated. Computes the actual slew duration.
double	AbstractIsisSpinBiasSlew.computeDuration(PVCoordinatesProvider pvProv) Deprecated. Computes the slew duration.
Attitude	AbstractSlew.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Deprecated. Warning: provided PVCoordinatesProvider is here not used.
Attitude	LofOffsetPointing.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	AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	RelativeTabulatedAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLegLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	ComposedAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TabulatedAttitude.getAttitude(PVCoordinatesProvider pvProvider, 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	LofOffset.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	AeroAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TwoDirectionsAttitude.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	ConstantAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLawLeg.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	BodyCenterPointing.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	YawCompensation.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TabulatedSlew.getAttitude(PVCoordinatesProvider pvProvider, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	IsisSunPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	ConstantSpinSlew.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Warning: provided PVCoordinatesProvider is here not used.
Attitude	AbstractGroundPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TargetPointing.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	RelativeTabulatedAttitudeLeg.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLegsSequence.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Gets the attitude from the sequence.
Attitude	AbstractGroundPointingWrapper.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the base system state at given date, without compensation.
TimeStampedAngularCoordinates	YawSteering.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame orbitFrame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
TimeStampedAngularCoordinates	YawCompensation.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame orbitFrame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
abstract TimeStampedAngularCoordinates	AbstractGroundPointingWrapper.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
Attitude	AttitudeLegsSequence.getPreviousAttitude(PVCoordinatesProvider provider, AbsoluteDate date, Frame frame) Returns attitude from previous leg (compared to leg matching provided date) from the sequence.
protected Vector3D	LofOffsetPointing.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
protected Vector3D	NadirPointing.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
protected Vector3D	TargetGroundPointing.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
protected Vector3D	BodyCenterGroundPointing.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
protected abstract Vector3D	AbstractGroundPointing.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
protected Vector3D	AbstractGroundPointingWrapper.getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point in specified frame.
TimeStampedPVCoordinates	NadirPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point position/velocity in specified frame.
protected TimeStampedPVCoordinates	AbstractGroundPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the target point position/velocity in specified frame.
protected TimeStampedPVCoordinates	AbstractGroundPointingWrapper.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 fr.cnes.sirius.patrius.attitudes with parameters of type PVCoordinatesProvider

Constructor and Description
AbstractAttitudeEphemerisGenerator(AttitudeLegsSequence legsSequence, int transitionPoints, PVCoordinatesProvider providerIn) Simple constructor.
AttitudeFrame(PVCoordinatesProvider pvProvider, AttitudeLaw attitudeLaw, Frame referenceFrame) Constructor of the dynamic spacecraft frame.
AttitudeTransformProvider(AttitudeLaw law, PVCoordinatesProvider pv, Frame frame) Protected constructor.
CelestialBodyPointed(Frame pCelestialFrame, PVCoordinatesProvider pPointedBody, Vector3D pPhasingCel, Vector3D pPointingSat, Vector3D pPhasingSat) Creates new instance.
FixedStepAttitudeEphemerisGenerator(AttitudeLegsSequence legsSequence, double fixedStep, int transitions, PVCoordinatesProvider providerIn) Builds an attitude ephemeris generator using a fixed time step and choosing the treatment to apply to the transition points of the sequence.
FixedStepAttitudeEphemerisGenerator(AttitudeLegsSequence legsSequence, double fixedStep, PVCoordinatesProvider providerIn) Builds an attitude ephemeris generator using a fixed time step and ignoring the attitude law transition points of the sequence.
VariableStepAttitudeEphemerisGenerator(AttitudeLegsSequence legsSequence, double stepMin, double stepMax, double angDistMax, int transitions, PVCoordinatesProvider providerIn) Builds an attitude ephemeris generator using a variable time step and choosing the treatment to apply to the transition points of the sequence.
VariableStepAttitudeEphemerisGenerator(AttitudeLegsSequence legsSequence, double stepMin, double stepMax, double angDistMax, PVCoordinatesProvider providerIn) Builds an attitude ephemeris generator using a variable time step and ignoring the attitude law transition points of the sequence.
YawSteering(AbstractGroundPointing groundPointingLaw, PVCoordinatesProvider sunIn, Vector3D phasingAxisIn) Creates a new instance.
YawSteering(AbstractGroundPointing groundPointingLaw, PVCoordinatesProvider sunIn, Vector3D phasingAxisIn, Vector3D losInSatFrameVec, Vector3D losNormalInSatFrameVec) Constructor.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes.directions

Methods in fr.cnes.sirius.patrius.attitudes.directions with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
Vector3D	GlintApproximatePointingDirection.getGlintVectorPosition(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Get the position vector of the glint point
Line	MomentumDirection.getLine(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	EarthCenterDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	VelocityDirection.getLine(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	ConstantVectorDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the given origin point and directed by the direction vector
Line	ToCelestialBodyCenterDirection.getLine(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	NadirDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	GlintApproximatePointingDirection.getLine(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	EarthToCelestialBodyCenterDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	IDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	GroundVelocityDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	GenericTargetDirection.getLine(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Line	CrossProductDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the cross product of directions.
Line	CelestialBodyPolesAxisDirection.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the line containing the origin (given PV coordinates) and directed by the direction vector.
Vector3D	MomentumDirection.getVector(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	EarthCenterDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	VelocityDirection.getVector(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	ConstantVectorDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	ToCelestialBodyCenterDirection.getVector(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	NadirDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	GlintApproximatePointingDirection.getVector(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	EarthToCelestialBodyCenterDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	IDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	GroundVelocityDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	GenericTargetDirection.getVector(PVCoordinatesProvider origin, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.
Vector3D	CrossProductDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the cross product of direction1 vector and dirction2 vector.
Vector3D	CelestialBodyPolesAxisDirection.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Provides the direction vector at a given date in a given frame.

Constructors in fr.cnes.sirius.patrius.attitudes.directions with parameters of type PVCoordinatesProvider

Constructor and Description
GenericTargetDirection(PVCoordinatesProvider inTarget) Build a direction from a target described by its PVCoordinatesProvider
GlintApproximatePointingDirection(EllipsoidBodyShape shape, PVCoordinatesProvider sunPV) Constructor with default solver ( BisectionSolver.BisectionSolver(double, double)).
GlintApproximatePointingDirection(EllipsoidBodyShape shape, PVCoordinatesProvider sunPV, UnivariateSolver univariateSolver) Constructor.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes.multi

Method parameters in fr.cnes.sirius.patrius.attitudes.multi with type arguments of type PVCoordinatesProvider

Modifier and Type	Method and Description
Attitude	MultiAttitudeProviderWrapper.getAttitude(Map<String,PVCoordinatesProvider> pvProvs, AbsoluteDate date, Frame frame) Computes the attitude corresponding to several orbital states.
Attitude	MultiAttitudeProvider.getAttitude(Map<String,PVCoordinatesProvider> pvProvs, AbsoluteDate date, Frame frame) Computes the attitude corresponding to several orbital states.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes.orientations

Methods in fr.cnes.sirius.patrius.attitudes.orientations with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
double	OrientationAngleProvider.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.
double	ConstantOrientationAngleLeg.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.
double	ConstantOrientationAngleLaw.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.
double	OrientationAngleProfileSequence.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.
double	OrientationAngleLawLeg.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.
double	OrientationAngleLegsSequence.getOrientationAngle(PVCoordinatesProvider pvProv, AbsoluteDate date) Compute the orientation angle corresponding to an orbital state.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes.profiles

Methods in fr.cnes.sirius.patrius.attitudes.profiles with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
void	AngularVelocitiesPolynomialSlew.compute(PVCoordinatesProvider pvProv) Compute the slew corresponding to an orbital state.
Attitude	QuaternionHarmonicProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AngularVelocitiesPolynomialProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeProfilesSequence.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Gets the attitude from the sequence.
Attitude	QuaternionPolynomialProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AbstractAngularVelocitiesAttitudeProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.attitudes.slew

Methods in fr.cnes.sirius.patrius.attitudes.slew with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
ConstantSpinSlew	ConstantSpinSlewComputer.compute(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDate, AttitudeProvider finalLaw, AbsoluteDate finalDate) Compute the slew.
TabulatedSlew	TwoSpinBiasSlewComputer.compute(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDate, AttitudeProvider finalLaw, AbsoluteDate finalDate) Compute the slew.
TabulatedSlew	IsisSpinBiasSlewComputer.computeAnalytical(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDateIn, AttitudeProvider finalLaw, AbsoluteDate finalDate) Compute the slew (analytical version).
double	IsisSpinBiasSlewComputer.computeDuration(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDateIn, AttitudeProvider finalLaw, AbsoluteDate finalDate) Computes the slew duration.
double	TwoSpinBiasSlewComputer.computeDuration(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDate, AttitudeProvider finalLaw, AbsoluteDate finalDate) Computes the actual slew duration.
TabulatedSlew	IsisSpinBiasSlewComputer.computeNumerical(PVCoordinatesProvider pvProv, AttitudeProvider initialLaw, AbsoluteDate initialDateIn, AttitudeProvider finalLaw, AbsoluteDate finalDate) Compute the slew (numerical version).

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.bodies

Subinterfaces of PVCoordinatesProvider in fr.cnes.sirius.patrius.bodies

Modifier and Type	Interface and Description
interface	CelestialBody Interface for celestial bodies like Sun, Moon or solar system planets.
interface	EllipsoidBodyShape Extended interface for spheroid model to represent celestial bodies shape : extends the GeometricBodyShape interface by adding getters to access the spheroid parameters.
interface	GeometricBodyShape Extended interface for celestial bodies shapes : extends the OREKIT's BodyShape interface by adding geometric methods.

Classes in fr.cnes.sirius.patrius.bodies that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	AbstractCelestialBody Abstract implementation of the CelestialBody interface.
class	ExtendedOneAxisEllipsoid Implementation of the EllipsoidBodyShape interface : this an extended spheroid model to represent celestial bodies shapes.
class	MeeusMoon This class implements the Moon ephemerides according to the algorithm of Meeus.
class	MeeusSun This class implements the Sun ephemerides according to the algorithm of Meeus, it only provides the position.
class	UserCelestialBody User-defined celestial body.

Methods in fr.cnes.sirius.patrius.bodies with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
double	ExtendedOneAxisEllipsoid.getApparentRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBody) Calculate the apparent radius.
double	EllipsoidBodyShape.getApparentRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBody) Calculate the apparent radius.
Line	BasicBoardSun.getLine(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Get the line from the position in pvCoord to the Sun.
double	GeometricBodyShape.getLocalRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBody) Calculate the apparent radius.
double	ExtendedOneAxisEllipsoid.getLocalRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBody) Calculate the apparent radius.
Vector3D	BasicBoardSun.getVector(PVCoordinatesProvider pvCoord, AbsoluteDate date, Frame frame) Get the direction of the sun.

Constructors in fr.cnes.sirius.patrius.bodies with parameters of type PVCoordinatesProvider

Constructor and Description
UserCelestialBody(String name, PVCoordinatesProvider aPVCoordinateProvider, double gm, IAUPole iauPole) Build an instance and the underlying frame.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.events

Constructors in fr.cnes.sirius.patrius.events with parameters of type PVCoordinatesProvider

Constructor and Description
CentralBodyMaskCircularFOVDetector(PVCoordinatesProvider occultedBody, double occultedBodyRadius, GeometricBodyShape occultingBody, boolean totalEclipseFlag, Vector3D center, double halfAperture) Constructor with default maxcheck and default threshold, creating a circularFOVDetector and an EllipsoidEclipseDetector
CentralBodyMaskCircularFOVDetector(PVCoordinatesProvider occultedBody, double occultedBodyRadius, GeometricBodyShape occultingBody, boolean totalEclipseFlag, Vector3D center, double halfAperture, double maxCheck, double threshold) Constructor with user maxcheck and threshold creating a circularFOVDetector and an EllipsoidEclipseDetector The default implementation behaviour is to stop propagation when the target is visible.
CentralBodyMaskCircularFOVDetector(PVCoordinatesProvider occultedBody, double occultedBodyRadius, GeometricBodyShape occultingBody, boolean totalEclipseFlag, Vector3D center, double halfAperture, double maxCheck, double threshold, EventDetector.Action action) Constructor with user maxcheck and threshold creating a circularFOVDetector and an EllipsoidEclipseDetector
CentralBodyMaskCircularFOVDetector(PVCoordinatesProvider occultedBody, double occultedBodyRadius, GeometricBodyShape occultingBody, boolean totalEclipseFlag, Vector3D center, double halfAperture, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor with user maxcheck and threshold creating a circularFOVDetector and an EllipsoidEclipseDetector

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.events.sensor

Methods in fr.cnes.sirius.patrius.events.sensor that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	ExtremaSightAxisDetector.getTargetPoint() Get the target point.

Constructors in fr.cnes.sirius.patrius.events.sensor with parameters of type PVCoordinatesProvider

Constructor and Description
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Assembly assembly, String partName) Constructor based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Assembly assembly, String partName, double maxCheck, double threshold) Constructor based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Assembly assembly, String partName, double maxCheck, double threshold, EventDetector.Action action) Constructor for both minimal and maximal angle based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Assembly assembly, String partName, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor for both minimal and maximal angle based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Vector3D sightAxisDirection) Constructor to use without assembly.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Vector3D sightAxisDirection, double maxCheck, double threshold) Constructor to use without assembly.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Vector3D sightAxisDirection, double maxCheck, double threshold, EventDetector.Action action) Constructor to use without assembly.
ExtremaSightAxisDetector(int extremumType, PVCoordinatesProvider target, Vector3D sightAxisDirection, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor to use without assembly.
ExtremaSightAxisDetector(PVCoordinatesProvider target, Assembly assembly, String partName, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax) Constructor for both minimal and maximal angle based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(PVCoordinatesProvider target, Assembly assembly, String partName, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax, boolean removeMin, boolean removeMax) Constructor for both minimal and maximal angle based on an Assembly containing at least one part with sensor property describing the vehicle.
ExtremaSightAxisDetector(PVCoordinatesProvider target, Vector3D sightAxisDirection, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax) Constructor to use without assembly for both minimal and maximal angle detection.
ExtremaSightAxisDetector(PVCoordinatesProvider target, Vector3D sightAxisDirection, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax, boolean removeMin, boolean removeMax) Constructor to use without assembly for both minimal and maximal angle detection.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.forces.atmospheres

Methods in fr.cnes.sirius.patrius.forces.atmospheres that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	DTM2000.getSun() Getter for the sun position.

Constructors in fr.cnes.sirius.patrius.forces.atmospheres with parameters of type PVCoordinatesProvider

Constructor and Description
DTM2000(DTM2000InputParameters parameters, PVCoordinatesProvider sunIn, BodyShape earthIn) Simple constructor for independent computation.
HarrisPriester(PVCoordinatesProvider sunIn, BodyShape earthIn) Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sunIn, BodyShape earthIn, double nIn) Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sunIn, BodyShape earthIn, double[][] tabAltRhoIn) Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider sunIn, BodyShape earthIn, double[][] tabAltRhoIn, double nIn) Constructor for Modified Harris-Priester atmosphere model.
JB2006(JB2006InputParameters parameters, PVCoordinatesProvider sunIn, BodyShape earthIn) Constructor with space environment information for internal computation.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.forces.radiation

Methods in fr.cnes.sirius.patrius.forces.radiation that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	SolarRadiationPressureCircular.getSun() Get sun model
PVCoordinatesProvider	SolarRadiationPressureEllipsoid.getSunBody() Getter for the Sun model used at construction.

Methods in fr.cnes.sirius.patrius.forces.radiation with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
static double	SolarRadiationPressureEllipsoid.getLightningRatio(PVCoordinatesProvider sun, Vector3D satSunVector, GeometricBodyShape earthModel, Vector3D position, Frame frame, AbsoluteDate date) Get the lightning ratio ([0-1]).

Constructors in fr.cnes.sirius.patrius.forces.radiation with parameters of type PVCoordinatesProvider

Constructor and Description
RediffusedFlux(int nCorona, int nMeridian, Frame bodyFrame, CelestialBody sunProvider, PVCoordinatesProvider satProvider, AbsoluteDate d, IEmissivityModel model) Default constructor of rediffused flux.
RediffusedFlux(int nCorona, int nMeridian, Frame bodyFrame, CelestialBody sun, PVCoordinatesProvider satProvider, AbsoluteDate dDate, IEmissivityModel model, boolean inIr, boolean inAlbedo) Generic constructor of rediffused flux.
SolarRadiationPressureCircular(double dRef, double pRef, PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn) Complete constructor.
SolarRadiationPressureCircular(double dRef, double pRef, PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn, boolean computePD) Complete constructor.
SolarRadiationPressureCircular(Parameter refFlux, PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn) Complete constructor.
SolarRadiationPressureCircular(Parameter refFlux, PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn, boolean computePD) Complete constructor.
SolarRadiationPressureCircular(PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn) Simple constructor with default reference values.
SolarRadiationPressureCircular(PVCoordinatesProvider sunIn, double equatorialRadiusIn, RadiationSensitive spacecraftIn, boolean computePD) Simple constructor with default reference values.
SolarRadiationPressureEllipsoid(double dRef, double pRef, PVCoordinatesProvider sunBody, GeometricBodyShape shape, Assembly assembly, double multiplicativeFactorIn) Creates a new instance.
SolarRadiationPressureEllipsoid(double dRef, double pRef, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel) Complete constructor.
SolarRadiationPressureEllipsoid(double dRef, double pRef, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel, boolean computePD) Complete constructor.
SolarRadiationPressureEllipsoid(Parameter referenceFlux, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel) Complete constructor using Parameter.
SolarRadiationPressureEllipsoid(Parameter referenceFlux, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel, boolean computePD) Complete constructor using Parameter.
SolarRadiationPressureEllipsoid(PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel) Simple constructor with default reference values.
SolarRadiationPressureEllipsoid(PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationSensitive spacecraftModel, boolean computePD) Simple constructor with default reference values.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.forces.relativistic

Constructors in fr.cnes.sirius.patrius.forces.relativistic with parameters of type PVCoordinatesProvider

Constructor and Description
CoriolisRelativisticEffect(double sunMu, PVCoordinatesProvider sunPV) Constructor with partial derivative computation by default.
CoriolisRelativisticEffect(double sunMu, PVCoordinatesProvider sunPV, boolean computePartialDerivativesVel) Constructor.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.frames

Classes in fr.cnes.sirius.patrius.frames that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	TopocentricFrame Topocentric frame.

Constructors in fr.cnes.sirius.patrius.frames with parameters of type PVCoordinatesProvider

Constructor and Description
LocalOrbitalFrame(Frame parent, LOFType type, PVCoordinatesProvider provider, String name) Build a new instance.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.groundstation

Classes in fr.cnes.sirius.patrius.groundstation that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	GeometricStationAntenna Class representing an a geometric model for a ground station antenna.
class	RFStationAntenna This class represents an RF antenna model for a ground station.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.orbits

Classes in fr.cnes.sirius.patrius.orbits that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	AlternateEquinoctialOrbit This class handles alternate equinoctial orbital parameters, which can support both circular and equatorial orbits.
class	ApsisOrbit This class handles periapsis/apoapsis parameters.
class	CartesianOrbit This class holds cartesian orbital parameters.
class	CircularOrbit This class handles circular orbital parameters.
class	EquatorialOrbit This class handles non circular equatorial 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 fr.cnes.sirius.patrius.orbits.pvcoordinates

Classes in fr.cnes.sirius.patrius.orbits.pvcoordinates that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	AbstractBoundedPVProvider This abstract class shall be extended to provides a PVCoordinates provider based on manipulation of PVCoordinates ephemeris.
class	AlmanacPVCoordinates This class implements the PVCoordinatesProvider to compute position velocity of a GPS or Galileo constellation satellite from its almanac parameters.
class	EphemerisPvHermite This class extends AbstractBoundedPVProvider which implements PVCoordinatesProvider and so provides a position velocity for a given date.
class	EphemerisPvLagrange This class extends AbstractBoundedPVProvider which implements PVCoordinatesProvider and so provides a position velocity for a given date.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.projections

Classes in fr.cnes.sirius.patrius.projections that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	ProjectionEllipsoid Deprecated. as of 4.3. This class is replaced by ProjectionEllipsoidUtils

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation

Subinterfaces of PVCoordinatesProvider in fr.cnes.sirius.patrius.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 fr.cnes.sirius.patrius.propagation that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	AbstractPropagator Common handling of Propagator methods for analytical propagators.
class	AnalyticalIntegratedEphemeris This class stores sequentially generated orbital parameters for later retrieval.
class	PVCoordinatesPropagator This class is an analytical propagator which propagates states from the input PV, Attitude, and additional state provider.

Methods in fr.cnes.sirius.patrius.propagation that return PVCoordinatesProvider

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

Constructors in fr.cnes.sirius.patrius.propagation with parameters of type PVCoordinatesProvider

Constructor and Description
PVCoordinatesPropagator(PVCoordinatesProvider pvCoordProvider, AbsoluteDate initDate, double mu, Frame frame) Creates an instance of PVCoordinatePropagator without attitude and additional state providers
PVCoordinatesPropagator(PVCoordinatesProvider pvCoordProvider, AbsoluteDate initDate, double mu, Frame frame, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, List<AdditionalStateProvider> additionalStateProviders) Creates an instance of PVCoordinatePropagator with PV, attitude for forces, attitude for events, and additional state providers given by the user.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.analytical

Classes in fr.cnes.sirius.patrius.propagation.analytical that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	AbstractLyddanePropagator Abstract Lyddane propagator.
class	AdapterPropagator Orbit propagator that adapts an underlying propagator, adding differential effects.
class	EcksteinHechlerPropagator This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
class	J2SecularPropagator J2 secular propagator.
class	KeplerianPropagator Simple keplerian orbit propagator.
class	LyddaneLongPeriodPropagator Lyddane long period propagator.
class	LyddaneSecularPropagator Lyddane secular propagator.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.analytical.tle

Classes in fr.cnes.sirius.patrius.propagation.analytical.tle that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	TLEPropagator This class provides elements to propagate TLE's.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.analytical.twod

Classes in fr.cnes.sirius.patrius.propagation.analytical.twod that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	Analytical2DPropagator This class propagates an analytical 2D orbit model and extends the AbstractPropagator class.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.events

Methods in fr.cnes.sirius.patrius.propagation.events that return PVCoordinatesProvider

Modifier and Type	Method and Description
PVCoordinatesProvider	ExtremaDistanceDetector.getBody()
PVCoordinatesProvider	DistanceDetector.getBody() Returns the body.
PVCoordinatesProvider	ExtremaThreeBodiesAngleDetector.getFirstBody() Get 1st body
PVCoordinatesProvider	ThreeBodiesAngleDetector.getFirstBody() Get 1st body.
PVCoordinatesProvider	EclipseDetector.getOcculted() Get the occulted body.
PVCoordinatesProvider	EclipseDetector.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	DihedralFieldOfViewDetector.getPVTarget() Get the position/velocity provider of the target .
PVCoordinatesProvider	ExtremaThreeBodiesAngleDetector.getSecondBody() Get 2nd body
PVCoordinatesProvider	ThreeBodiesAngleDetector.getSecondBody() Get 2nd body.
PVCoordinatesProvider	NadirSolarIncidenceDetector.getSun() Returns Sun.
PVCoordinatesProvider	ExtremaThreeBodiesAngleDetector.getThirdBody() Get 3rd body
PVCoordinatesProvider	ThreeBodiesAngleDetector.getThirdBody() Get 3rd body.

Methods in fr.cnes.sirius.patrius.propagation.events with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
double	LocalRadiusProvider.getLocalRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBodyIn) Calculate the apparent radius.
double	VariableRadiusProvider.getLocalRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBodyIn) Calculate the apparent radius.
double	ConstantRadiusProvider.getLocalRadius(Vector3D position, Frame frame, AbsoluteDate date, PVCoordinatesProvider occultedBodyIn) Calculate the apparent radius.
protected AbsoluteDate	AbstractDetector.getSignalEmissionDate(PVCoordinatesProvider emitter, SpacecraftState s, double epsilon, AbstractDetector.PropagationDelayType delayType) Compute signal emission date which is date at which currently seen signal by spacecraft has been emitted by emitter depending on AbstractDetector.PropagationDelayType.
protected AbsoluteDate	AbstractDetector.getSignalReceptionDate(PVCoordinatesProvider receiver, SpacecraftState s, double epsilon, AbstractDetector.PropagationDelayType delayType) Compute signal reception date which is date at which currently seen signal by receiver has been emitted by spacecraft (emitter) depending on AbstractDetector.PropagationDelayType.
void	NadirSolarIncidenceDetector.setSun(PVCoordinatesProvider sun) Sets the sun PVCoordinatesProvider

Constructors in fr.cnes.sirius.patrius.propagation.events with parameters of type PVCoordinatesProvider

Constructor and Description
AlignmentDetector(Orbit orbit, PVCoordinatesProvider bodyIn, double alignAngleIn) Build a new alignment detector.
AlignmentDetector(Orbit orbit, PVCoordinatesProvider bodyIn, double alignAngleIn, double thresholdIn) Build a new alignment detector.
AlignmentDetector(Orbit orbit, PVCoordinatesProvider bodyIn, double alignAngleIn, double threshold, EventDetector.Action actionStart, EventDetector.Action actionEnd) Build a new alignment detector.
AlignmentDetector(Orbit orbit, PVCoordinatesProvider bodyIn, double alignAngleIn, double threshold, EventDetector.Action actionStart, EventDetector.Action actionEnd, boolean removeStart, boolean removeEnd) Build a new alignment detector.
AlignmentDetector(PVCoordinatesProvider bodyIn, double alignAngleIn, double maxcheck, double threshold, EventDetector.Action actionStart, EventDetector.Action actionEnd, boolean removeStart, boolean removeEnd) Build a new alignment detector.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheckIn) Build a new instance.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold) Build a new instance.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit) Build a new instance with defined actions at fov entry and exit.
CircularFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, double halfApertureIn, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new instance with defined actions at fov entry and exit.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck) Build a new instance.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck, double epsilon) Build a new instance.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck, EventDetector.Action entry, EventDetector.Action exit) Build a new instance.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new instance.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit, double epsilon) Build a new instance.
DihedralFieldOfViewDetector(PVCoordinatesProvider pvTarget, Vector3D centerIn, Vector3D axis1, double halfAperture1In, Vector3D axis2, double halfAperture2In, double maxCheck, EventDetector.Action entry, EventDetector.Action exit, double epsilon) Build a new instance.
DistanceDetector(PVCoordinatesProvider dBody, double dist) Constructor for a DistanceDetector instance.
DistanceDetector(PVCoordinatesProvider dBody, double dist, double maxCheck, double threshold) Constructor for a DistanceDetector instance with complimentary parameters.
DistanceDetector(PVCoordinatesProvider dBody, double dist, double maxCheck, double threshold, EventDetector.Action action) Constructor for a DistanceDetector instance with complimentary parameters.
DistanceDetector(PVCoordinatesProvider dBody, double dist, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor for a DistanceDetector instance with complimentary parameters.
EclipseDetector(IDirection occulted, PVCoordinatesProvider occulting, double occultingRadius, double maxCheck, double threshold) Build a new eclipse detector.
EclipseDetector(IDirection occulted, PVCoordinatesProvider occulting, double occultingRadius, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit) Build a new eclipse detector with defined actions when entering and exiting the eclipse.
EclipseDetector(IDirection occulted, PVCoordinatesProvider occulting, double occultingRadius, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new eclipse detector with defined actions when entering and exiting the eclipse.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold, EventDetector.Action action, boolean remove, int slopeSelection) Build a new eclipse detector based on a lighting ratio and with slope selection.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit, int slopeSelection) Build a new eclipse detector based on a lighting ratio and with slope selection.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, GeometricBodyShape occultingBodyIn, double lightingRatio, double maxCheck, double threshold, int slopeSelection) Build a new eclipse detector based on a lighting ratio and with slope selection.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, PVCoordinatesProvider occulting, double occultingRadius, double lightingRatio, double maxCheck, double threshold) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, PVCoordinatesProvider occulting, double occultingRadius, double lightingRatio, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, PVCoordinatesProvider occulting, double occultingRadius, double lightingRatio, double maxCheck, double threshold, EventDetector.Action entry, EventDetector.Action exit, boolean removeEntry, boolean removeExit) Build a new eclipse detector based on a lighting ratio.
EclipseDetector(PVCoordinatesProvider occulted, double occultedRadiusIn, PVCoordinatesProvider occulting, double occultingRadius, double lightingRatio, int slopeSelection, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor with slope selection.
ExtremaDistanceDetector(PVCoordinatesProvider dBody, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax) Constructor for both minimum and maximum distance .
ExtremaDistanceDetector(PVCoordinatesProvider dBody, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax, boolean removeMin, boolean removeMax) Constructor for both minimum and maximum distance .
ExtremaDistanceDetector(PVCoordinatesProvider dBody, int extremumType) Constructor for a ExtremaDistanceDetector instance.
ExtremaDistanceDetector(PVCoordinatesProvider dBody, int extremumType, double maxCheck, double threshold) Constructor for a ExtremaDistanceDetector instance with complimentary parameters.
ExtremaDistanceDetector(PVCoordinatesProvider dBody, int extremumType, double maxCheck, double threshold, EventDetector.Action action) Constructor for a ExtremaDistanceDetector instance with specified action when extrema is detected.
ExtremaDistanceDetector(PVCoordinatesProvider dBody, int extremumType, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor for a ExtremaDistanceDetector instance with specified action when extrema is detected.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax) Constructor for the min and max three bodies angle detector with specified action for both minimum and maximum.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax, boolean removeMin, boolean removeMax) Constructor for the min and max three bodies angle detector with specified action for both minimum and maximum.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, int extremumType) Simple constructor for the min and max three bodies angle detector.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, int extremumType, double maxCheck, double threshold) Constructor for the min and max three bodies angle detector with defined maximum check and convergence threshold.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, int extremumType, double maxCheck, double threshold, EventDetector.Action action) Constructor for the min and max three bodies angle detector with specified action when extrema is detected.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ExtremaThreeBodiesAngleDetector.BodyOrder bodyC, int extremumType, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor for the min and max three bodies angle detector with specified action when extrema is detected.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax) Constructor for the min and max three bodies angle detector with specified action for both minimum and maximum.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, double maxCheck, double threshold, EventDetector.Action actionMin, EventDetector.Action actionMax, boolean removeMin, boolean removeMax) Constructor for the min and max three bodies angle detector with specified action for both minimum and maximum.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, int extremumType) Constructor for the min and max three bodies angle detector.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, int extremumType, double maxCheck, double threshold) Constructor for the min and max three bodies angle detector.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, int extremumType, double maxCheck, double threshold, EventDetector.Action action) Constructor for the min and max three bodies angle detector with specified action when extrema is detected.
ExtremaThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, int extremumType, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Constructor for the min and max three bodies angle detector with specified action when extrema is detected.
ThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, double angle) Build a new three bodies angle detector.
ThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, double angle, double maxCheck, double threshold) Build a new three bodies angle detector with complimentary parameters.
ThreeBodiesAngleDetector(PVCoordinatesProvider firstBody, PVCoordinatesProvider secondBody, PVCoordinatesProvider thirdBody, double angle, double maxCheck, double threshold, EventDetector.Action action) Build a new three bodies angle detector with complimentary parameters.
ThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ThreeBodiesAngleDetector.BodyOrder bodyC, double angle) Build a new three bodies angle detector with a position among the parameters.
ThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ThreeBodiesAngleDetector.BodyOrder bodyC, double angle, double maxCheck, double threshold) Build a new three bodies angle detector with complimentary parameters.
ThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ThreeBodiesAngleDetector.BodyOrder bodyC, double angle, double maxCheck, double threshold, EventDetector.Action action) Build a new three bodies angle detector with complimentary parameters.
ThreeBodiesAngleDetector(PVCoordinatesProvider bodyA, PVCoordinatesProvider bodyB, ThreeBodiesAngleDetector.BodyOrder bodyC, double angle, double maxCheck, double threshold, EventDetector.Action action, boolean remove) Build a new three bodies angle detector with complimentary parameters.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.numerical

Classes in fr.cnes.sirius.patrius.propagation.numerical that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	NumericalPropagator This class propagates SpacecraftState using numerical integration.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.precomputed

Classes in fr.cnes.sirius.patrius.propagation.precomputed that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	Ephemeris This class is designed to accept and handle tabulated orbital entries.
class	IntegratedEphemeris This class stores sequentially generated orbital parameters for later retrieval.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.propagation.precomputed.multi

Classes in fr.cnes.sirius.patrius.propagation.precomputed.multi that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	MultiIntegratedEphemeris This interface is copied from IntegratedEphemeris and adapted to multi propagation.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.signalpropagation

Methods in fr.cnes.sirius.patrius.signalpropagation with parameters of type PVCoordinatesProvider

Modifier and Type	Method and Description
SignalPropagation	SignalPropagationModel.computeSignalPropagation(PVCoordinatesProvider transmitter, PVCoordinatesProvider receiver, AbsoluteDate date, SignalPropagationModel.FixedDate fixedDateType) Computes the signal propagation object in the void at a particular date

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.stela.bodies

Classes in fr.cnes.sirius.patrius.stela.bodies that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	MeeusMoonStela This class implements the Moon ephemerides according to the algorithm of Meeus, it only provides the position.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.stela.forces.radiation

Constructors in fr.cnes.sirius.patrius.stela.forces.radiation with parameters of type PVCoordinatesProvider

Constructor and Description
SRPPotential(PVCoordinatesProvider sun, double m, double s, double c) create a SRP Potential model using the sun and spacecraft characteristics.
SRPSquaring(RadiationSensitive radiativeSpacecraft, int quadraturePoints, PVCoordinatesProvider sunBody, double earthRadius) Create an instance with an assembly and a number of points.
SRPSquaring(RadiationSensitive radiativeSpacecraft, int quadraturePoints, PVCoordinatesProvider sunBody, double earthRadius, double dRef, double pRef) Create an instance with an assembly and a number of points.
SRPSquaring(RadiationSensitive radiativeSpacecraft, PVCoordinatesProvider sunBody, double earthRadius) Create an instance with an assembly and a number of points.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.stela.orbits

Classes in fr.cnes.sirius.patrius.stela.orbits that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	StelaEquinoctialOrbit This class handles Stela equinoctial orbital parameters, which can support both circular and equatorial orbits.

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.stela.propagation

Classes in fr.cnes.sirius.patrius.stela.propagation that implement PVCoordinatesProvider

Modifier and Type	Class and Description
class	StelaAbstractPropagator Common handling of Propagator methods for analytical propagators.
class	StelaGTOPropagator STELA propagator for Geostationnary Transfert Orbits (GTO).

Methods in fr.cnes.sirius.patrius.stela.propagation that return PVCoordinatesProvider

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

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.time

Constructors in fr.cnes.sirius.patrius.time with parameters of type PVCoordinatesProvider

Constructor and Description
LocalTimeAngle(PVCoordinatesProvider sunEphemeris) Constructor

Uses of PVCoordinatesProvider in fr.cnes.sirius.patrius.wrenches

Constructors in fr.cnes.sirius.patrius.wrenches with parameters of type PVCoordinatesProvider

Constructor and Description
SolarRadiationWrench(double distance, double pressure, double sunRadius, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationWrenchSensitive spacecraftModel) Complete constructor.
SolarRadiationWrench(Parameter distance, Parameter pressure, Parameter sunRadius, PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationWrenchSensitive spacecraftModel) Complete constructor using Parameter.
SolarRadiationWrench(PVCoordinatesProvider sunBody, GeometricBodyShape shape, RadiationWrenchSensitive spacecraftModel) Simple constructor with default reference values.