Uses of Interface
org.orekit.utils.ExtendedPositionProvider

Packages that use ExtendedPositionProvider

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.control.indirect.adjoint	This package provides routines to model the adjoint dynamics as in the Pontryagin Maximum Principle, as used in indirect control.
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.gravity	This package provides all gravity-related forces.
org.orekit.forces.radiation	This package provides all radiation pressure related forces.
org.orekit.gnss.antenna	This package provides classes related to receiver and satellites antenna modeling.
org.orekit.gnss.attitude	This package provides classes related to navigation satellites attitude modeling.
org.orekit.models.earth.atmosphere	This package provides the atmosphere model interface and several implementations.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
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 ExtendedPositionProvider in org.orekit.attitudes

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

Modifier and Type	Method	Description
<T extends CalculusFieldElement<T>> FieldVector3D<FieldUnivariateDerivative2<T>>	GroundPointTarget.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame)	Get a target vector.
FieldVector3D<UnivariateDerivative2>	GroundPointTarget.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
default <T extends CalculusFieldElement<T>> FieldVector3D<FieldUnivariateDerivative2<T>>	TargetProvider.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame)	Get a target vector.
default FieldVector3D<UnivariateDerivative2>	TargetProvider.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	GroundPointTarget.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame)	Get a target vector.
Vector3D	GroundPointTarget.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
<T extends CalculusFieldElement<T>> FieldVector3D<T>	TargetProvider.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame)	Get a target vector.
default Vector3D	TargetProvider.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.

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

Constructor	Description
AlignedAndConstrained(Vector3D primarySat, TargetProvider primaryTarget, Vector3D secondarySat, TargetProvider secondaryTarget, Frame inertialFrame, ExtendedPositionProvider sun, OneAxisEllipsoid earth)	Simple constructor.
AlignedAndConstrained(Vector3D primarySat, TargetProvider primaryTarget, Vector3D secondarySat, TargetProvider secondaryTarget, ExtendedPositionProvider sun, OneAxisEllipsoid earth)	Constructor with default inertial frame.
CelestialBodyPointed(Frame celestialFrame, ExtendedPositionProvider pointedBody, Vector3D phasingCel, Vector3D pointingSat, Vector3D phasingSat)	Creates new instance.
YawSteering(Frame inertialFrame, GroundPointing groundPointingLaw, ExtendedPositionProvider sun, Vector3D phasingAxis)	Creates a new instance.

Uses of ExtendedPositionProvider in org.orekit.bodies

Subinterfaces of ExtendedPositionProvider in org.orekit.bodies

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

Classes in org.orekit.bodies that implement ExtendedPositionProvider

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

Uses of ExtendedPositionProvider in org.orekit.control.indirect.adjoint

Constructors in org.orekit.control.indirect.adjoint with parameters of type ExtendedPositionProvider

Constructor	Description
AbstractCartesianAdjointNonCentralBodyTerm(double mu, ExtendedPositionProvider bodyPositionProvider)	Constructor.
CartesianAdjointSingleBodyTerm(double mu, ExtendedPositionProvider bodyPositionProvider)	Constructor.
CartesianAdjointThirdBodyTerm(double mu, ExtendedPositionProvider bodyPositionProvider)	Constructor.

Uses of ExtendedPositionProvider in org.orekit.forces

Methods in org.orekit.forces with parameters of type ExtendedPositionProvider

Modifier and Type	Method	Description
static List<Panel>	BoxAndSolarArraySpacecraft.buildPanels(double xLength, double yLength, double zLength, ExtendedPositionProvider sun, double solarArrayArea, Vector3D solarArrayAxis, double drag, double liftRatio, double absorption, double reflection)	Build the panels of a simple parallelepiped box plus one solar array panel.

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

Constructor	Description
BoxAndSolarArraySpacecraft(double xLength, double yLength, double zLength, ExtendedPositionProvider sun, double solarArrayArea, Vector3D solarArrayAxis, double dragCoeff, double liftRatio, double absorptionCoeff, double reflectionCoeff)	Build a spacecraft model with best lighting of solar array.
PointingPanel(Vector3D rotationAxis, ExtendedPositionProvider target, double area, double drag, double liftRatio, double absorption, double reflection)	Simple constructor.

Uses of ExtendedPositionProvider in org.orekit.forces.gravity

Methods in org.orekit.forces.gravity that return ExtendedPositionProvider

Modifier and Type	Method	Description
ExtendedPositionProvider	DeSitterRelativity.getEarth()	Get the Earth model used to compute De Sitter effect.

Constructors in org.orekit.forces.gravity with parameters of type ExtendedPositionProvider

Constructor	Description
AbstractBodyAttraction(ExtendedPositionProvider positionProvider, String name, double mu)	Simple constructor.
SingleBodyAbsoluteAttraction(ExtendedPositionProvider positionProvider, String name, double mu)	Simple constructor.
SingleBodyRelativeAttraction(ExtendedPositionProvider positionProvider, String name, double mu)	Simple constructor.
ThirdBodyAttraction(ExtendedPositionProvider positionProvider, String name, double mu)	Simple constructor.

Uses of ExtendedPositionProvider in org.orekit.forces.radiation

Methods in org.orekit.forces.radiation that return ExtendedPositionProvider

Modifier and Type	Method	Description
ExtendedPositionProvider	AbstractLightFluxModel.getOccultedBody()	Getter for the occulted body's position provider.

Methods in org.orekit.forces.radiation with parameters of type ExtendedPositionProvider

Modifier and Type	Method	Description
void	AbstractRadiationForceModel.addOccultingBody(ExtendedPositionProvider provider, double radius)	Add a new occulting body.

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

Constructor	Description
AbstractLightFluxModel(ExtendedPositionProvider occultedBody)	Constructor.
AbstractRadiationForceModel(ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, EventDetectionSettings eclipseDetectionSettings)	Default constructor.
AbstractSolarLightFluxModel(double kRef, ExtendedPositionProvider occultedBody, double occultingBodyRadius, EventDetectionSettings eventDetectionSettings)	Constructor.
AbstractSolarLightFluxModel(ExtendedPositionProvider occultedBody, double occultingBodyRadius, EventDetectionSettings eventDetectionSettings)	Constructor with default value for reference flux.
ConicallyShadowedLightFluxModel(double kRef, double occultedBodyRadius, ExtendedPositionProvider occultedBody, double occultingBodyRadius)	Constructor with default event detection settings.
ConicallyShadowedLightFluxModel(double kRef, double occultedBodyRadius, ExtendedPositionProvider occultedBody, double occultingBodyRadius, EventDetectionSettings eventDetectionSettings)	Constructor.
ConicallyShadowedLightFluxModel(double occultedBodyRadius, ExtendedPositionProvider occultedBody, double occultingBodyRadius)	Constructor with default value for reference flux.
CylindricallyShadowedLightFluxModel(double kRef, ExtendedPositionProvider occultedBody, double occultingBodyRadius)	Constructor with default event detection settings.
CylindricallyShadowedLightFluxModel(double kRef, ExtendedPositionProvider occultedBody, double occultingBodyRadius, EventDetectionSettings eventDetectionSettings)	Constructor.
CylindricallyShadowedLightFluxModel(ExtendedPositionProvider occultedBody, double occultingBodyRadius)	Constructor with default value for reference flux.
ECOM2(int nD, int nB, double value, ExtendedPositionProvider sun, double equatorialRadius)	Constructor.
KnockeRediffusedForceModel(ExtendedPositionProvider sun, RadiationSensitive spacecraft, double equatorialRadius, double angularResolution)	Default Constructor.
KnockeRediffusedForceModel(ExtendedPositionProvider sun, RadiationSensitive spacecraft, double equatorialRadius, double angularResolution, TimeScale utc)	General constructor.
SolarRadiationPressure(double dRef, double pRef, ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, RadiationSensitive spacecraft)	Constructor with default eclipse detection settings.
SolarRadiationPressure(double dRef, double pRef, ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, RadiationSensitive spacecraft, EventDetectionSettings eclipseDetectionSettings)	Complete constructor.
SolarRadiationPressure(ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, RadiationSensitive spacecraft)	Simple constructor with default reference values.

Uses of ExtendedPositionProvider in org.orekit.gnss.antenna

Methods in org.orekit.gnss.antenna with parameters of type ExtendedPositionProvider

Modifier and Type	Method	Description
abstract GNSSAttitudeProvider	SatelliteType.buildAttitudeProvider(AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame, int prnNumber)	Build an attitude provider suitable for this satellite type.

Uses of ExtendedPositionProvider in org.orekit.gnss.attitude

Constructors in org.orekit.gnss.attitude with parameters of type ExtendedPositionProvider

Constructor	Description
BeidouGeo(AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
BeidouIGSO(AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
BeidouMeo(AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
Galileo(double yawRate, AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
GenericGNSS(AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
Glonass(double yawRate, AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
GPSBlockIIA(double yawRate, double yawBias, AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
GPSBlockIIF(double yawRate, double yawBias, AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.
GPSBlockIIR(double yawRate, AbsoluteDate validityStart, AbsoluteDate validityEnd, ExtendedPositionProvider sun, Frame inertialFrame)	Simple constructor.

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

Methods in org.orekit.models.earth.atmosphere that return ExtendedPositionProvider

Modifier and Type	Method	Description
protected ExtendedPositionProvider	AbstractSunInfluencedAtmosphere.getSun()	Getter for Sun's position provider.

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

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

Uses of ExtendedPositionProvider in org.orekit.propagation.events

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

Constructor	Description
EclipseDetector(ExtendedPositionProvider occulted, double occultedRadius, OneAxisEllipsoid occulting)	Build a new eclipse detector.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider sun, T occultingBodyRadius, FieldEventDetectionSettings<T> eventDetectionSettings, FieldEventHandler<T> handler)	Constructor.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider sun, T occultingBodyRadius, FieldEventHandler<T> handler)	Constructor with default detection settings.
FieldEclipseDetector(Field<T> field, ExtendedPositionProvider occulted, double occultedRadius, OneAxisEllipsoid occulting)	Build a new eclipse detector.

Uses of ExtendedPositionProvider in org.orekit.propagation.semianalytical.dsst.forces

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

Constructor	Description
DSSTSolarRadiationPressure(double dRef, double pRef, double cr, double area, ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, double mu)	Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double cr, double area, ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, double mu)	Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(double dRef, double pRef, ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, RadiationSensitive spacecraft, double mu)	Complete constructor.
DSSTSolarRadiationPressure(ExtendedPositionProvider sun, OneAxisEllipsoid centralBody, RadiationSensitive spacecraft, double mu)	Simple constructor with default reference values, but custom spacecraft.

Uses of ExtendedPositionProvider in org.orekit.utils

Subinterfaces of ExtendedPositionProvider in org.orekit.utils

Modifier and Type	Interface	Description
interface	ExtendedPVCoordinatesProvider	Deprecated. since 13.0.

Classes in org.orekit.utils that implement ExtendedPositionProvider

Modifier and Type	Class	Description
class	FrameAdapter	Adapter from Frame to ExtendedPositionProvider.

Methods in org.orekit.utils that return ExtendedPositionProvider

Modifier and Type	Method	Description
ExtendedPositionProvider	OccultationEngine.getOcculted()	Getter for the occulted body.

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

Constructor	Description
ExtendedPositionProviderAdapter(Frame parent, ExtendedPositionProvider provider, String name)	Simple constructor.
OccultationEngine(ExtendedPositionProvider occulted, double occultedRadius, OneAxisEllipsoid occulting)	Build a new occultation engine.