Uses of Interface
org.orekit.attitudes.AttitudeProvider

Packages that use AttitudeProvider

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.control.indirect.shooting.propagation	This package provides classes relative to the propagation part of indirect shooting.
org.orekit.estimation.measurements.gnss	This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.ilrs	This package provides parsers for laser ranging data stored in CDR and CPF formats.
org.orekit.files.sp3	This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces.empirical	This package provides empirical forces.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.gnss.attitude	This package provides classes related to navigation satellites attitude modeling.
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.gnss.data	This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
org.orekit.propagation.analytical.intelsat	This package provides classes to propagate Intelsat's 11 elements.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.conversion.osc2mean	This package provides the ability to convert osculating orbits into mean orbits according to different theories (Brouwer-Lyddane, Eckstein-Hechler, SGP4/SDP4, DSST) with different conversion algorithms (fixed-point, least-squares).
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.utils	This package provides useful objects.

Uses of AttitudeProvider in org.orekit.attitudes

Subinterfaces of AttitudeProvider in org.orekit.attitudes

Modifier and Type	Interface	Description
interface	AttitudeProviderModifier	This interface represents an attitude provider that modifies/wraps another underlying provider.
interface	BoundedAttitudeProvider	This interface is intended for attitude ephemerides valid only during a time range.

Classes in org.orekit.attitudes that implement AttitudeProvider

Modifier and Type	Class	Description
class	AggregateBoundedAttitudeProvider	A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.
class	AlignedAndConstrained	Attitude provider with one satellite vector aligned and another one constrained to two targets.
class	AttitudesSequence	This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
class	AttitudesSwitcher	This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
class	BodyCenterPointing	This class handles body center pointing attitude provider.
class	CelestialBodyPointed	This class handles a celestial body pointed attitude provider.
class	FixedRate	This class handles a simple attitude provider at constant rate around a fixed axis.
class	FrameAlignedProvider	This class handles an attitude provider aligned with a frame or a fixed offset to it.
class	GroundPointing	Base class for ground pointing attitude providers.
class	GroundPointingAttitudeModifier	Abstract class for attitude provider modifiers using an underlying ground pointing law.
class	LofOffset	Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
class	LofOffsetPointing	This class provides a default attitude provider.
class	NadirPointing	This class handles nadir pointing attitude provider.
class	SpinStabilized	This class handles a spin stabilized attitude provider.
class	TabulatedLofOffset	This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
class	TabulatedProvider	This class handles an attitude provider interpolating from a predefined table.
class	TargetPointing	This class handles target pointing attitude provider.
class	TorqueFree	This class handles torque-free motion of a general (non-symmetrical) body.
class	YawCompensation	This class handles yaw compensation attitude provider.
class	YawSteering	This class handles yaw steering law.

Methods in org.orekit.attitudes that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	AttitudeProviderModifier.getUnderlyingAttitudeProvider()	Get the underlying attitude provider.
AttitudeProvider	SpinStabilized.getUnderlyingAttitudeProvider()	Get the underlying attitude provider.
static AttitudeProvider	FrameAlignedProvider.of(Frame satelliteFrame)	Creates an attitude provider aligned with the given frame.

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

Modifier and Type	Method	Description
<T extends EventDetector> void	AttitudesSequence.addSwitchingCondition(AttitudeProvider past, AttitudeProvider future, T switchEvent, boolean switchOnIncrease, boolean switchOnDecrease, double transitionTime, AngularDerivativesFilter transitionFilter, AttitudeSwitchHandler switchHandler)	Add a switching condition between two attitude providers.
<T extends EventDetector> void	AttitudesSwitcher.addSwitchingCondition(AttitudeProvider past, AttitudeProvider future, T switchEvent, boolean switchOnIncrease, boolean switchOnDecrease, AttitudeSwitchHandler switchHandler)	Add a switching condition between two attitude providers.
static AttitudeProviderModifier	AttitudeProviderModifier.getFrozenAttitudeProvider(AttitudeProvider attitudeProvider)	Wrap the input provider with a new one always returning attitudes with zero rotation rate and acceleration.
static BoundedAttitudeProvider	BoundedAttitudeProvider.of(AttitudeProvider attitudeProvider, TimeInterval interval)	Creates a bounded provider given a time interval and a standard attitude provider, with the same outputs.
void	AttitudeSwitchHandler.switchOccurred(AttitudeProvider preceding, AttitudeProvider following, SpacecraftState state)	Method called when attitude is switched from one law to another law.

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

Modifier	Constructor	Description
	LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector)	Creates new instance.
	SpinStabilized(AttitudeProvider nonRotatingLaw, AbsoluteDate start, Vector3D axis, double rate)	Creates a new instance.

Uses of AttitudeProvider in org.orekit.control.indirect.shooting.propagation

Methods in org.orekit.control.indirect.shooting.propagation that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	ShootingPropagationSettings.getAttitudeProvider()	Getter for the attitude provider.

Constructors in org.orekit.control.indirect.shooting.propagation with parameters of type AttitudeProvider

Modifier	Constructor	Description
	ShootingPropagationSettings(List<ForceModel> forceModels, AdjointDynamicsProvider adjointDynamicsProvider, Frame propagationFrame, ShootingIntegrationSettings integrationSettings, AttitudeProvider attitudeProvider)	Constructor.

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

Methods in org.orekit.estimation.measurements.gnss with parameters of type AttitudeProvider

Modifier and Type	Method	Description
OneWayGNSSWindUp	OneWayGNSSWindUpFactory.getWindUp(SatelliteSystem emitterSystem, int emitterPrnNumber, Dipole emitterDipole, String receiverName, Dipole receiverDipole, AttitudeProvider emitterAttitude)	Get a modifier for an emitter/receiver pair.

Uses of AttitudeProvider in org.orekit.estimation.measurements.modifiers

Constructors in org.orekit.estimation.measurements.modifiers with parameters of type AttitudeProvider

Modifier	Constructor	Description
	ModifierGradientConverter(SpacecraftState state, int freeStateParameters, AttitudeProvider provider)	Simple constructor.
	OnBoardAntennaOneWayGNSSPhaseModifier(Vector3D receiverPhaseCenter, Vector3D emitterPhaseCenter, AttitudeProvider attitudeProvider)	Simple constructor.
	OnBoardAntennaOneWayGNSSPhaseModifier(FrequencyPattern receiverPattern, FrequencyPattern emitterPattern, AttitudeProvider attitudeProvider)	Simple constructor.
	OnBoardAntennaOneWayGNSSRangeModifier(Vector3D receiverPhaseCenter, Vector3D emitterPhaseCenter, AttitudeProvider attitudeProvider)	Simple constructor.
	OnBoardAntennaOneWayGNSSRangeModifier(FrequencyPattern receiverPattern, FrequencyPattern emitterPattern, AttitudeProvider attitudeProvider)	Simple constructor.
	PhaseCentersOneWayGNSSBaseModifier(FrequencyPattern receiverPattern, FrequencyPattern emitterPattern, AttitudeProvider attitudeProvider)	Simple constructor.

Uses of AttitudeProvider in org.orekit.files.general

Methods in org.orekit.files.general with parameters of type AttitudeProvider

Modifier and Type	Method	Description
default BoundedPropagator	EphemerisFile.EphemerisSegment.getPropagator(AttitudeProvider attitudeProvider)	View this ephemeris segment as a propagator.
default BoundedPropagator	EphemerisFile.SatelliteEphemeris.getPropagator(AttitudeProvider attitudeProvider)	View this ephemeris as a propagator, combining data from all segments.

Constructors in org.orekit.files.general with parameters of type AttitudeProvider

Modifier	Constructor	Description
	EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment<C> ephemeris, AttitudeProvider attitudeProvider)	Create a Propagator from an ephemeris segment.

Uses of AttitudeProvider in org.orekit.files.ilrs

Methods in org.orekit.files.ilrs with parameters of type AttitudeProvider

Modifier and Type	Method	Description
BoundedPropagator	CPF.CPFEphemeris.getPropagator(AttitudeProvider attitudeProvider)	View this ephemeris as a propagator, combining data from all segments.

Uses of AttitudeProvider in org.orekit.files.sp3

Methods in org.orekit.files.sp3 with parameters of type AttitudeProvider

Modifier and Type	Method	Description
BoundedPropagator	SP3Segment.getPropagator(AttitudeProvider attitudeProvider)	View this ephemeris segment as a propagator.

Uses of AttitudeProvider in org.orekit.forces.empirical

Methods in org.orekit.forces.empirical that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	AbstractParametricAcceleration.getAttitudeOverride()	Getter for attitude override.

Constructors in org.orekit.forces.empirical with parameters of type AttitudeProvider

Modifier	Constructor	Description
protected	AbstractParametricAcceleration(Vector3D direction, boolean isInertial, AttitudeProvider attitudeOverride)	Constructor.
	ParametricAcceleration(Vector3D direction, AttitudeProvider attitudeOverride, AccelerationModel accelerationModel)	Simple constructor.
	TimeSpanParametricAcceleration(Vector3D direction, AttitudeProvider attitudeOverride, AccelerationModel accelerationModel)	Simple constructor.

Uses of AttitudeProvider in org.orekit.forces.maneuvers

Methods in org.orekit.forces.maneuvers that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	AbstractImpulseManeuver.getAttitudeOverride()	Get the Attitude Provider to use during maneuver.

Constructors in org.orekit.forces.maneuvers with parameters of type AttitudeProvider

Modifier	Constructor	Description
protected	AbstractImpulseManeuver(AttitudeProvider attitudeOverride, Control3DVectorCostType control3DVectorCostType)	Protected constructor.
	ConstantThrustManeuver(AttitudeProvider attitudeOverride, DateBasedManeuverTriggers dateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel constantThrustPropulsionModel)	Simple constructor for a constant direction and constant thrust.
	ConstantThrustManeuver(AbsoluteDate date, double duration, double thrust, double isp, AttitudeProvider attitudeOverride, Vector3D direction)	Simple constructor for a constant direction and constant thrust.
	ConstantThrustManeuver(AbsoluteDate date, double duration, double thrust, double isp, AttitudeProvider attitudeOverride, Vector3D direction, String name)	Simple constructor for a constant direction and constant thrust.
	ConstantThrustManeuver(AbsoluteDate date, double duration, double thrust, double isp, AttitudeProvider attitudeOverride, Vector3D direction, Control3DVectorCostType control3DVectorCostType, String name)	Simple constructor for a constant direction and constant thrust.
	ConstantThrustManeuver(AbsoluteDate date, double duration, AttitudeProvider attitudeOverride, AbstractConstantThrustPropulsionModel constantThrustPropulsionModel)	Simple constructor for a constant direction and constant thrust.
	FieldImpulseManeuver(FieldEventDetector<T> trigger, AttitudeProvider attitudeOverride, FieldVector3D<T> deltaVSat, T isp)	Build a new instance.
	FieldImpulseManeuver(FieldEventDetector<T> trigger, AttitudeProvider attitudeOverride, FieldImpulseProvider<T> fieldImpulseProvider, T isp, Control3DVectorCostType control3DVectorCostType)	Build a new instance.
	ImpulseManeuver(EventDetector trigger, AttitudeProvider attitudeOverride, Vector3D deltaVSat, double isp)	Build a new instance.
	ImpulseManeuver(EventDetector trigger, AttitudeProvider attitudeOverride, ImpulseProvider impulseProvider, double isp, Control3DVectorCostType control3DVectorCostType)	Build a new instance.

Uses of AttitudeProvider in org.orekit.gnss.attitude

Subinterfaces of AttitudeProvider in org.orekit.gnss.attitude

Modifier and Type	Interface	Description
interface	GNSSAttitudeProvider	Attitude providers for navigation satellites.

Classes in org.orekit.gnss.attitude that implement AttitudeProvider

Modifier and Type	Class	Description
class	BeidouGeo	Attitude providers for Beidou geostationary orbit navigation satellites.
class	BeidouIGSO	Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.
class	BeidouMeo	Attitude providers for Beidou Medium Earth Orbit navigation satellites.
class	Galileo	Attitude providers for Galileo navigation satellites.
class	GenericGNSS	Attitude providers for navigation satellites for which no specialized model is known.
class	Glonass	Attitude providers for Glonass navigation satellites.
class	GPSBlockIIA	Attitude providers for GPS block IIA navigation satellites.
class	GPSBlockIIF	Attitude providers for GPS block IIF navigation satellites.
class	GPSBlockIIR	Attitude providers for GPS block IIR navigation satellites.

Uses of AttitudeProvider in org.orekit.propagation

Methods in org.orekit.propagation that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	AbstractPropagator.getAttitudeProvider()	Get attitude provider.
AttitudeProvider	FieldAbstractPropagator.getAttitudeProvider()	Get attitude provider.
AttitudeProvider	FieldPropagator.getAttitudeProvider()	Get attitude provider.
AttitudeProvider	Propagator.getAttitudeProvider()	Get attitude provider.
static AttitudeProvider	Propagator.getDefaultLaw(Frames frames)	Get a default law using the given frames.

Methods in org.orekit.propagation with parameters of type AttitudeProvider

Modifier and Type	Method	Description
void	AbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	FieldAbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	FieldPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	Propagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.

Uses of AttitudeProvider in org.orekit.propagation.analytical

Constructors in org.orekit.propagation.analytical with parameters of type AttitudeProvider

Modifier	Constructor	Description
protected	AbstractAnalyticalPropagator(AttitudeProvider attitudeProvider)	Build a new instance.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double m2Value)	Build a propagator from orbit, attitude provider and potential.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, double epsilon, int maxIterations)	Build a propagator from orbit, attitude provider, mass and potential.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, OsculatingToMeanConverter converter)	Build a propagator from orbit, attitude provider, mass and potential.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential provider.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential provider.
	BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double m2Value)	Build a propagator from orbit, attitude provider and potential provider.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60)	Build a propagator from orbit, attitude provider and potential.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60)	Build a propagator from orbit, attitude provider, mass and potential.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType)	Build a propagator from orbit, attitude provider, mass and potential.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations)	Build a propagator from orbit, attitude provider, mass and potential.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, OsculatingToMeanConverter converter)	Build a propagator from orbit, attitude provider, mass and potential.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider)	Build a propagator from orbit, attitude provider, mass and potential provider.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics)	Private helper constructor.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitude, double mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType)	Private helper constructor.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType)	Build a propagator from orbit, attitude provider, mass and potential provider.
	EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider)	Build a propagator from orbit, attitude provider and potential provider.
	Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider)	Constructor with tabulated states and associated covariances.
	Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, AttitudeProvider attitudeProvider)	Constructor with tabulated states.
protected	FieldAbstractAnalyticalPropagator(Field<T> field, AttitudeProvider attitudeProvider)	Build a new instance.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double m2Value)	Build a propagator from orbit, attitude provider and potential.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double m2Value)	Build a propagator from orbit, attitude provider and potential provider.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, double epsilon, int maxIterations)	Build a propagator from orbit, attitude provider, mass and potential.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, OsculatingToMeanConverter converter)	Build a propagator from orbit, attitude provider, mass and potential.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential provider.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double m2Value)	Private helper constructor.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType, double m2Value)	Private helper constructor.
	FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double m2Value)	Build a propagator from orbit, attitude provider, mass and potential provider.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)	Build a propagator from FieldOrbit, attitude provider and potential.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider)	Build a propagator from FieldOrbit, attitude provider and potential provider.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)	Build a propagator from FieldOrbit, attitude provider, mass and potential.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType)	Build a propagator from FieldOrbit, attitude provider, mass and potential.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations)	Build a propagator from FieldOrbit, attitude provider, mass and potential.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, OsculatingToMeanConverter converter)	Build a propagator from FieldOrbit, attitude provider, mass and potential.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider)	Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics)	Private helper constructor.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType)	Private helper constructor.
	FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType)	Build a propagator from orbit, attitude provider, mass and potential provider.
	FieldEphemeris(List<FieldSpacecraftState<T>> states, FieldTimeInterpolator<FieldSpacecraftState<T>,T> stateInterpolator, AttitudeProvider attitudeProvider)	Constructor with tabulated states and attitude provider.
	FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv)	Build a propagator from orbit and attitude provider.
	FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv, T mu)	Build a propagator from orbit, attitude provider and central attraction coefficient μ.
	FieldKeplerianPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mu, T mass)	Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
	KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv)	Build a propagator from orbit and attitude provider.
	KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu)	Build a propagator from orbit, attitude provider and central attraction coefficient μ.
	KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu, double mass)	Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

Uses of AttitudeProvider in org.orekit.propagation.analytical.gnss

Methods in org.orekit.propagation.analytical.gnss with parameters of type AttitudeProvider

Modifier and Type	Method	Description
GLONASSAnalyticalPropagatorBuilder	GLONASSAnalyticalPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider)	Sets the attitude provider.
SBASPropagatorBuilder	SBASPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider)	Sets the attitude provider.

Constructors in org.orekit.propagation.analytical.gnss with parameters of type AttitudeProvider

Modifier	Constructor	Description
	FieldGnssPropagator(FieldGnssOrbitalElements<T,?> orbitalElements, Frame eci, Frame ecef, AttitudeProvider provider, T mass)	Build a new instance.
	FieldGnssPropagator(FieldSpacecraftState<T> initialState, FieldGnssOrbitalElements<T,?> nonKeplerianElements, Frame ecef, AttitudeProvider provider, T mass)	Build a new instance from an initial state.
	GNSSExtendedPositionProvider(GNSSOrbitalElements<?> orbitalElements, Frame eci, Frame ecef, AttitudeProvider provider, double mass)	Build a new instance.

Uses of AttitudeProvider in org.orekit.propagation.analytical.gnss.data

Methods in org.orekit.propagation.analytical.gnss.data with parameters of type AttitudeProvider

Modifier and Type	Method	Description
GNSSPropagator	AbstractAlmanac.getPropagator(AttitudeProvider provider, Frame inertial, Frame bodyFixed, double mass)	Get the propagator corresponding to the navigation message.
FieldGnssPropagator<T>	FieldAbstractAlmanac.getPropagator(AttitudeProvider provider, Frame inertial, Frame bodyFixed, T mass)	Get the propagator corresponding to the navigation message.
GLONASSAnalyticalPropagator	GLONASSAlmanac.getPropagator(DataContext context, AttitudeProvider provider, Frame inertial, Frame bodyFixed, double mass)	Get the propagator corresponding to the navigation message.
GLONASSNumericalPropagator	GLONASSFdmaNavigationMessage.getPropagator(double step, DataContext context, AttitudeProvider provider, Frame inertial, double mass)	Get the propagator corresponding to the navigation message.
SBASPropagator	SBASNavigationMessage.getPropagator(Frames frames, AttitudeProvider provider, Frame inertial, Frame bodyFixed, double mass, double mu)	Get the propagator corresponding to the navigation message.

Uses of AttitudeProvider in org.orekit.propagation.analytical.intelsat

Constructors in org.orekit.propagation.analytical.intelsat with parameters of type AttitudeProvider

Modifier	Constructor	Description
	FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T> elements, Frame inertialFrame, Frame ecefFrame, AttitudeProvider attitudeProvider, T mass)	Constructor.
	IntelsatElevenElementsPropagator(IntelsatElevenElements elements, Frame inertialFrame, Frame ecefFrame, AttitudeProvider attitudeProvider, double mass)	Constructor.

Uses of AttitudeProvider in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle with parameters of type AttitudeProvider

Modifier and Type	Method	Description
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters)	Selects the extrapolator to use with the selected TLE.
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass, Frame teme)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, Frame teme, AttitudeProvider attitudeProvider)	Selects the extrapolator to use with the selected TLE.

Constructors in org.orekit.propagation.analytical.tle with parameters of type AttitudeProvider

Modifier	Constructor	Description
	DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Constructor for a unique initial TLE.
	DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme)	Constructor for a unique initial TLE.
	FieldDeepSDP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters)	Constructor for a unique initial TLE.
	FieldDeepSDP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Constructor for a unique initial TLE.
	FieldSGP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters)	Constructor for a unique initial TLE.
	FieldSGP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Constructor for a unique initial TLE.
protected	FieldTLEPropagator(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, Frame teme, T[] parameters)	Protected constructor for derived classes.
protected	FieldTLEPropagator(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Protected constructor for derived classes.
	SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Constructor for a unique initial TLE.
	SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme)	Constructor for a unique initial TLE.
protected	TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Protected constructor for derived classes.
protected	TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme)	Protected constructor for derived classes.

Uses of AttitudeProvider in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	AbstractPropagatorBuilder.getAttitudeProvider()	Get the attitude provider.
AttitudeProvider	PropagatorBuilder.getAttitudeProvider()	Get the attitude provider.

Methods in org.orekit.propagation.conversion with parameters of type AttitudeProvider

Modifier and Type	Method	Description
void	AbstractPropagatorBuilder.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set the attitude provider.

Constructors in org.orekit.propagation.conversion with parameters of type AttitudeProvider

Modifier	Constructor	Description
protected	AbstractAnalyticalPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider, double initialMass)	Build a new instance.
protected	AbstractIntegratedPropagatorBuilder(Orbit templateOrbit, ODEIntegratorBuilder builder, PositionAngleType positionAngleType, double positionScale, PropagationType propagationType, AttitudeProvider attitudeProvider, double mass)	Build a new instance.
protected	AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider)	Build a new instance.
protected	AbstractPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, boolean addDriverForCentralAttraction, AttitudeProvider attitudeProvider, double initialMass)	Build a new instance.
	BrouwerLyddanePropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider, double M2)	Build a new instance.
	DSSTPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, double positionScale, PropagationType propagationType, PropagationType stateType, AttitudeProvider attitudeProvider)	Build a new instance.
	EcksteinHechlerPropagatorBuilder(Orbit templateOrbit, UnnormalizedSphericalHarmonicsProvider provider, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	EphemerisPropagatorBuilder(List<SpacecraftState> states, int interpolationPoints, double extrapolationThreshold, AttitudeProvider attitudeProvider)	Constructor.
	EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider)	Constructor.
	EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, AttitudeProvider attitudeProvider)	Constructor.
	KeplerianPropagatorBuilder(Orbit templateOrbit, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	NumericalPropagatorBuilder(Orbit referenceOrbit, ODEIntegratorBuilder builder, PositionAngleType positionAngleType, double positionScale, AttitudeProvider attitudeProvider)	Build a new instance.
	TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, DataContext dataContext, TleGenerationAlgorithm generationAlgorithm, AttitudeProvider attitudeProvider)	Build a new instance.

Uses of AttitudeProvider in org.orekit.propagation.conversion.osc2mean

Constructors in org.orekit.propagation.conversion.osc2mean with parameters of type AttitudeProvider

Modifier	Constructor	Description
	DSSTTheory(Collection<DSSTForceModel> forceModels, AttitudeProvider attitudeProvider, double mass)	Full constructor.

Uses of AttitudeProvider in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return AttitudeProvider

Modifier and Type	Method	Description
AttitudeProvider	FieldStateMapper.getAttitudeProvider()	Get the attitude provider.
AttitudeProvider	StateMapper.getAttitudeProvider()	Get the attitude provider.
protected AttitudeProvider	AbstractIntegratedPropagator.getFrozenAttitudeProvider()	Getter for the frozen attitude provider, used for performance when possible.
protected AttitudeProvider	FieldAbstractIntegratedPropagator.getFrozenAttitudeProvider()	Getter for the frozen attitude provider, used for performance when possible.
protected AttitudeProvider	AbstractIntegratedPropagator.initializeAttitudeProviderForDerivatives()	Method called when initializing the attitude provider used when evaluating derivatives.
protected AttitudeProvider	FieldAbstractIntegratedPropagator.initializeAttitudeProviderForDerivatives()	Method called when initializing the attitude provider used when evaluating derivatives.

Methods in org.orekit.propagation.integration with parameters of type AttitudeProvider

Modifier and Type	Method	Description
protected static FieldSpacecraftState<Gradient>	AbstractGradientConverter.buildBasicGradientSpacecraftState(SpacecraftState state, int freeStateParameters, AttitudeProvider provider)	Process a state into a Gradient version without force model parameter.
protected abstract StateMapper	AbstractIntegratedPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
void	AbstractIntegratedPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	FieldAbstractIntegratedPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	FieldStateMapper.setAttitudeProvider(AttitudeProvider attitudeProvider)	Setter for the attitude provider.
void	IntegratedEphemeris.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	StateMapper.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set the attitude provider.

Constructors in org.orekit.propagation.integration with parameters of type AttitudeProvider

Modifier	Constructor	Description
	FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, AttitudeProvider attitudeProvider, PropagationType type, FieldDenseOutputModel<T> model, FieldDataDictionary<T> unmanaged, List<FieldAdditionalDataProvider<?,T>> providers, String[] equations, int[] dimensions)	Creates a new instance of IntegratedEphemeris.
protected	FieldStateMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.
	IntegratedEphemeris(AbsoluteDate startDate, AbsoluteDate minDate, AbsoluteDate maxDate, StateMapper mapper, AttitudeProvider attitudeProvider, PropagationType type, DenseOutputModel model, DataDictionary unmanaged, List<AdditionalDataProvider<?>> providers, String[] equations, int[] dimensions)	Creates a new instance of IntegratedEphemeris.
protected	StateMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Simple constructor.

Uses of AttitudeProvider in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical that return AttitudeProvider

Modifier and Type	Method	Description
protected AttitudeProvider	FieldNumericalPropagator.initializeAttitudeProviderForDerivatives()	Method called when initializing the attitude provider used when evaluating derivatives.
protected AttitudeProvider	NumericalPropagator.initializeAttitudeProviderForDerivatives()	Method called when initializing the attitude provider used when evaluating derivatives.

Methods in org.orekit.propagation.numerical with parameters of type AttitudeProvider

Modifier and Type	Method	Description
GLONASSNumericalPropagatorBuilder	GLONASSNumericalPropagatorBuilder.attitudeProvider(AttitudeProvider userProvider)	Sets the attitude provider.
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected StateMapper	GLONASSNumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)
protected StateMapper	NumericalPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType orbitType, PositionAngleType positionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.

Constructors in org.orekit.propagation.numerical with parameters of type AttitudeProvider

Modifier	Constructor	Description
	FieldNumericalPropagator(FieldODEIntegrator<T> integrator, AttitudeProvider attitudeProvider)	Create a new instance of NumericalPropagator, based on orbit definition mu.
	GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator integrator, GLONASSOrbitalElements glonassOrbit, Frame eci, AttitudeProvider provider, double mass, DataContext context, boolean isAccAvailable)	Private constructor.
	NumericalPropagator(ODEIntegrator integrator, AttitudeProvider attitudeProvider)	Create a new instance of NumericalPropagator, based on orbit definition mu.

Uses of AttitudeProvider in org.orekit.propagation.semianalytical.dsst

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type AttitudeProvider

Modifier and Type	Method	Description
static SpacecraftState	DSSTPropagator.computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels)	Conversion from osculating to mean orbit.
static SpacecraftState	DSSTPropagator.computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels, double epsilon, int maxIterations)	Conversion from osculating to mean orbit.
static SpacecraftState	DSSTPropagator.computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels, OsculatingToMeanConverter converter)	Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel)	Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel, double epsilon, int maxIterations)	Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel, OsculatingToMeanConverter converter)	Conversion from osculating to mean orbit.
static SpacecraftState	DSSTPropagator.computeOsculatingState(SpacecraftState mean, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forces)	Conversion from mean to osculating orbit.
static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>	FieldDSSTPropagator.computeOsculatingState(FieldSpacecraftState<T> mean, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forces)	Conversion from mean to osculating orbit.
protected StateMapper	DSSTPropagator.createMapper(AbsoluteDate referenceDate, double mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)	Create a mapper between raw double components and spacecraft state. /** Simple constructor.
void	DSSTPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.
void	FieldDSSTPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider)	Set attitude provider.

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

Modifier	Constructor	Description
	DSSTPropagator(ODEIntegrator integrator, PropagationType propagationType, AttitudeProvider attitudeProvider)	Create a new instance of DSSTPropagator.
	FieldDSSTPropagator(Field<T> field, FieldODEIntegrator<T> integrator, AttitudeProvider attitudeProvider)	Create a new instance of DSSTPropagator.
	FieldDSSTPropagator(FieldODEIntegrator<T> integrator, PropagationType propagationType, AttitudeProvider attitudeProvider)	Create a new instance of DSSTPropagator.

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

Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type AttitudeProvider

Modifier and Type	Method	Description
void	AbstractGaussianContribution.registerAttitudeProvider(AttitudeProvider provider)	Register an attitude provider.
void	DSSTForceModel.registerAttitudeProvider(AttitudeProvider provider)	Register an attitude provider.
void	DSSTJ2SquaredClosedForm.registerAttitudeProvider(AttitudeProvider attitudeProvider)	Register an attitude provider.
void	DSSTNewtonianAttraction.registerAttitudeProvider(AttitudeProvider provider)	Register an attitude provider.
void	DSSTTesseral.registerAttitudeProvider(AttitudeProvider attitudeProvider)	Register an attitude provider.
void	DSSTThirdBody.registerAttitudeProvider(AttitudeProvider provider)	Register an attitude provider.
void	DSSTZonal.registerAttitudeProvider(AttitudeProvider attitudeProvider)	Register an attitude provider.

Uses of AttitudeProvider in org.orekit.utils

Methods in org.orekit.utils with parameters of type AttitudeProvider

Modifier and Type	Method	Description
static FieldSpacecraftState<Gradient>	DerivativeStateUtils.buildSpacecraftStateGradient(GradientField field, SpacecraftState state, AttitudeProvider attitudeProvider)	Method creating a Gradient version of the input state, using the state vector as the independent variables of a first- order Taylor algebra.
static FieldSpacecraftState<Gradient>	DerivativeStateUtils.buildSpacecraftStateTransitionGradient(SpacecraftState state, RealMatrix partialDerivatives, AttitudeProvider attitudeProvider)	Method creating a Gradient version of the input state from a given transition matrix.
static StateJacobian	Differentiation.differentiate(StateFunction function, int dimension, AttitudeProvider provider, OrbitType orbitType, PositionAngleType positionAngleType, double dP, int nbPoints)	Differentiate a vector function using finite differences.