Uses of Interface
org.orekit.attitudes.AttitudeProvider

Packages that use AttitudeProvider

fr.cnes.sirius.patrius.guidance
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.events.multi
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.propagation.precomputed.multi
fr.cnes.sirius.patrius.propagation.sampling.multi
fr.cnes.sirius.patrius.stela.propagation
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.analytical.twod
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.numerical
org.orekit.propagation.precomputed
org.orekit.propagation.sampling	This package provides interfaces and classes dealing with step handling during propagation.

Uses of AttitudeProvider in fr.cnes.sirius.patrius.guidance

Classes in fr.cnes.sirius.patrius.guidance that implement AttitudeProvider

class	AngularVelocitiesHarmonicProfile Represents an angular velocities guidance profile, calculated with Fourier series
class	AngularVelocitiesPolynomialProfile Represents an angular velocities guidance profile, calculated with polynomial functions
class	GuidanceProfile Represents a guidance profile
class	QuaternionHarmonicProfile Represents a quaternion guidance profile, calculated with Fourier series.
class	QuaternionPolynomialProfile Represents a quaternion guidance profile, calculated with polynomial functions

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

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

AttitudeProvider	MultiPropagator.getAttitudeProvider(String satId) Get the default attitude provider.
AttitudeProvider	MultiPropagator.getAttitudeProviderEvents(String satId) Get the attitude provider for events computation.
AttitudeProvider	MultiPropagator.getAttitudeProviderForces(String satId) Get the attitude provider for forces computation.

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

void	MultiPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider, String satId) Set attitude provider for defined spacecraft.
void	MultiPropagator.setAttitudeProviderEvents(AttitudeProvider attitudeProviderEvents, String satId) Set attitude provider for events computation.
void	MultiPropagator.setAttitudeProviderForces(AttitudeProvider attitudeProviderForces, String satId) Set attitude provider for forces computation.

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

PVCoordinatePropagator(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 AttitudeProvider in fr.cnes.sirius.patrius.propagation.events.multi

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

AdaptedMonoEventDetector(EventDetector detector, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDate, double mu, Frame integrationFrame, MultiStateVectorInfo stateVectorInfo, String satId)
Build a wrapped event detector.

Constructor parameters in fr.cnes.sirius.patrius.propagation.events.multi with type arguments of type AttitudeProvider

AdaptedMultiEventDetector(MultiEventDetector detector, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo)
Build a wrapped multi-sat event detector.

AdaptedMultiEventDetector(MultiEventDetector detector, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo)
Build a wrapped multi-sat event detector.

Uses of AttitudeProvider in fr.cnes.sirius.patrius.propagation.numerical.multi

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi that return AttitudeProvider

AttitudeProvider	MultiNumericalPropagator.getAttitudeProvider(String satId)
AttitudeProvider	MultiNumericalPropagator.getAttitudeProviderEvents(String satId)
AttitudeProvider	MultiNumericalPropagator.getAttitudeProviderForces(String satId)

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi with parameters of type AttitudeProvider

SpacecraftState	MultiStateVectorInfo.mapArrayToState(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, double mu, Frame integrationFrame, String satId) Extract a given SpacecraftState from the state vector.
void	MultiNumericalPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider, String satId)
void	MultiNumericalPropagator.setAttitudeProviderEvents(AttitudeProvider attitudeProviderEvents, String satId)
void	MultiNumericalPropagator.setAttitudeProviderForces(AttitudeProvider attitudeProviderForces, String satId)

Method parameters in fr.cnes.sirius.patrius.propagation.numerical.multi with type arguments of type AttitudeProvider

protected void	MultiNumericalPropagator.addEventHandlers(boolean activateHandlers, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents) Add event handlers to integrator.
protected void	MultiNumericalPropagator.addEventHandlers(boolean activateHandlers, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents) Add event handlers to integrator.
void	MultiEphemerisModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
void	MultiEphemerisModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
void	MultiModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
void	MultiModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attitudeProvidersForces, Map<String,AttitudeProvider> attitudeProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frame, Map<String,Double> mu) Initialize the mode handler.
Map<String,SpacecraftState>	MultiStateVectorInfo.mapArrayToStates(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, Map<String,Double> mu, Map<String,Frame> integrationFrame) Convert state vector into a Map of SpacecraftState
Map<String,SpacecraftState>	MultiStateVectorInfo.mapArrayToStates(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, Map<String,Double> mu, Map<String,Frame> integrationFrame) Convert state vector into a Map of SpacecraftState
protected void	MultiNumericalPropagator.setUpEventDetector(EventDetector osf, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents, String satId) Wrap an Orekit event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(EventDetector osf, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents, String satId) Wrap an Orekit event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(MultiEventDetector osf, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents) Wrap an Orekit multi-sat event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(MultiEventDetector osf, Map<String,AttitudeProvider> localAttProvForces, Map<String,AttitudeProvider> localAttProvEvents) Wrap an Orekit multi-sat event detector and register it to the integrator.

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

Constructors in fr.cnes.sirius.patrius.propagation.precomputed.multi with parameters of type AttitudeProvider

MultiIntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MultiStateVectorInfo stateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn, String satIdIn)
Creates a new instance of IntegratedEphemeris.

Uses of AttitudeProvider in fr.cnes.sirius.patrius.propagation.sampling.multi

Method parameters in fr.cnes.sirius.patrius.propagation.sampling.multi with type arguments of type AttitudeProvider

void	MultiAdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frameMap, Map<String,Double> muMap) Initialize the mode handler.
void	MultiAdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,AttitudeProvider> attProvidersForces, Map<String,AttitudeProvider> attProvidersEvents, MultiStateVectorInfo stateVectorInfo, boolean activateHandlers, AbsoluteDate reference, Map<String,Frame> frameMap, Map<String,Double> muMap) Initialize the mode handler.

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

Fields in fr.cnes.sirius.patrius.stela.propagation declared as AttitudeProvider

protected AttitudeProvider	StelaAbstractPropagator.attitudeProviderByDefault Attitude provider given by default for one attitude.
protected AttitudeProvider	StelaAbstractPropagator.attitudeProviderEvents Attitude provider for events computation.
protected AttitudeProvider	StelaAbstractPropagator.attitudeProviderForces Attitude provider for forces computation.

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

AttitudeProvider	StelaAbstractPropagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	StelaAbstractPropagator.getAttitudeProviderEvents() Get attitude provider for events computation.
AttitudeProvider	StelaAbstractPropagator.getAttitudeProviderForces() Get attitude provider for forces computation.

Methods in fr.cnes.sirius.patrius.stela.propagation with parameters of type AttitudeProvider

void	StelaAbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProviderIn) Set attitude provider for forces and events computation.
void	StelaGTOPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider for forces and events computation.
void	StelaAbstractPropagator.setAttitudeProviderEvents(AttitudeProvider attitudeProviderIn) Set attitude provider for events computation.
void	StelaGTOPropagator.setAttitudeProviderEvents(AttitudeProvider attitudeEventsProvider) Set attitude provider for events computation.
void	StelaAbstractPropagator.setAttitudeProviderForces(AttitudeProvider attitudeProviderIn) Set attitude provider for forces computation.
void	StelaGTOPropagator.setAttitudeProviderForces(AttitudeProvider attitudeForcesProvider) Set attitude provider for forces computation.

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

StelaAbstractPropagator(AttitudeProvider attitudeProviderInForces, AttitudeProvider attitudeProviderInEvents, StelaBasicInterpolator inInterpolator)
Build a new instance.

StelaAbstractPropagator(AttitudeProvider attitudeProviderIn, StelaBasicInterpolator inInterpolator)
Build a new instance.

StelaGTOPropagator(FirstOrderIntegrator integr, AttitudeProvider inAttitudeProviderForces, AttitudeProvider inAttitudeProviderEvents, StelaBasicInterpolator inInter, double maxShiftIn, double minStepSizeIn)
Build a StelaGTOPropagator.

StelaGTOPropagator(FirstOrderIntegrator integr, AttitudeProvider inAttitudeProvider, StelaBasicInterpolator inInter, double maxShiftIn, double minStepSizeIn)
Build a StelaGTOPropagator.

Uses of AttitudeProvider in org.orekit.attitudes

Subinterfaces of AttitudeProvider in org.orekit.attitudes

interface	AttitudeLaw This interface has been created to represent a generic attitude provider without an interval of validity: the attitude can be computed at any date.
interface	AttitudeLawModifier This interface represents an attitude law that modifies/wraps another underlying law.
interface	AttitudeLeg Interface which makes it obligatory to give an interval of validity to an attitude law. All the classes implementing this interface should have an interval of validity with CLOSED endpoints.
interface	Slew This interface represents a slew model set.

Classes in org.orekit.attitudes that implement AttitudeProvider

class	AbstractAttitudeLaw This abstract class gather all common features to classes implementing the AttitudeLaw interface.
class	AbstractIsisSpinBiasSlew Abstract class for ISIS spin bias slew: slew with trapezoidal angular velocity profile.
class	AbstractSlew This abstract class is the basic implementation of the Slew interface.
class	AttitudeLawLeg This class represents an attitude law version "attitude", with an interval of validity (whose borders are closed points).
class	AttitudeLegLaw This class represents an attitude law version "attitudeLeg", with an interval of validity (whose borders are closed points) and attitude laws outside this interval of validity.
class	AttitudeLegsSequence This class handles a sequence of different attitude providers AttitudeLeg.
class	AttitudesSequence This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
class	BodyCenterGroundPointing This class handles body center pointing attitude provider; the difference between BodyCenterPointing and this class is that the target point of the former is the body center, while that of the latter is the corresponding point on the ground.
class	BodyCenterPointing This class handles body center pointing attitude provider.
class	CelestialBodyPointed This class handles a celestial body pointed attitude provider.
class	ComposedAttitudeLaw This class represents a composed attitude law, defined by a main attitude law provider and a chained list of orientation laws. The main attitude law provides, for a given date, the dynamic frame representing the spacecraft orientation; this orientation is then progressively transformed using the orientation laws.
class	ConstantAttitudeLaw This class handles a constant attitude law.
class	ConstantSpinSlew This class extends the AbstractSlew.
class	FixedRate This class handles a simple attitude provider at constant rate around a fixed axis.
class	GroundPointing Base class for ground pointing attitude providers.
class	GroundPointingWrapper This class leverages common parts for compensation modes around ground pointing attitudes.
class	IsisAnalyticalSpinBiasSlew ISIS spin bias slew: slew with trapezoidal angular velocity profile.
class	IsisNumericalSpinBiasSlew ISIS spin bias slew: slew with trapezoidal angular velocity profile.
class	IsisSunPointing Implementation of ISIS Sun pointing attitude 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	RelativeTabulatedAttitudeLaw This class represents a relative tabulated attitude law version "attitudeLeg", with an interval of validity (whose borders are closed points) and attitude laws outside this interval of validity, which can be of two types : a ConstantAttitudeLaw, or an ExtrapolatedAttitudeLaw (private class)
class	RelativeTabulatedAttitudeLeg This class implements the tabulated attitude leg relative to a reference date.
class	SpinStabilized This class handles a spin stabilized attitude provider.
class	SunPointing This class implements a Sun pointing attitude law.
class	TabulatedAttitude This class implements the tabulated attitude leg.
class	TargetGroundPointing This class handles target pointing attitude provider; while the class TargetPointing does not guarantee the target point belongs to the body surface, this class always provides a ground point target.
class	TargetPointing This class handles target pointing attitude provider.
class	TwoDirectionsAttitude This class implements a generic two directions attitude law.
class	TwoSpinBiasSlew This class extends the AbstractSlew.
class	YawCompensation This class handles yaw compensation attitude provider.
class	YawSteering This class handles yaw steering law.

Fields in org.orekit.attitudes declared as AttitudeProvider

protected AttitudeProvider	AbstractSlew.fLaw The attitude law after the slew.
protected AttitudeProvider	AbstractSlew.iLaw The attitude law before the slew.

Methods in org.orekit.attitudes that return AttitudeProvider

AttitudeProvider

AttitudeFrame.getAttitudeLaw()

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

AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn)
Constructor with default maximum number of iterations allowed for slew duration computation's convergence.

AbstractIsisSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn, int maxIterationsNumberIn)
Constructor.

AbstractSlew(AttitudeProvider initialLaw, AttitudeProvider finalLaw, AbsoluteDate initialDate, AbsoluteDate finalDate)
Builds a slew when its interval of validity is known.

ConstantSpinSlew(AttitudeProvider initialLaw, AttitudeProvider finalLaw, AbsoluteDate initialDate, AbsoluteDate finalDate)
Builds a ConstantSpinSlew based on a given interval of dates

ConstantSpinSlew(AttitudeProvider initialLaw, AttitudeProvider finalLaw, AbsoluteDate date, boolean isStartDate, double constraintValue, ConstantSpinSlew.Constraint constraintType)
Builds a ConstantSpinSlew from a type of constraint and its value

IsisAnalyticalSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn)
Constructor with default maximum number of iterations allowed for slew duration computation's convergence.

IsisAnalyticalSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn, int maxIterationsNumberIn)
Constructor.

IsisNumericalSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn)
Constructor with default maximum number of iterations allowed for slew duration computation's convergence.

IsisNumericalSpinBiasSlew(AttitudeProvider initialLawIn, AttitudeProvider finalLawIn, AbsoluteDate initialDateIn, double dtSCAOIn, double thetaMaxAllowedIn, double durationMaxIn, double dtConvergenceThresholdIn, double[][] inertiaMatrixIn, double rwTorqueAllocAccelIn, double rwTorqueAllocDecelIn, double rwDeltaMomentumAllocIn, double[][] rwMatrixIn, double tranquillisationTimeIn, int maxIterationsNumberIn)
Constructor.

LofOffsetPointing(BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector)
Creates new instance.

TwoSpinBiasSlew(AttitudeProvider initialLaw, AttitudeProvider targetLaw, AbsoluteDate initialDate, double dtSCAOIn, double thetaMaxIn, double tauIn, double epsInRall, double omegaHigh, double thetaSwitch, double epsOutRall, double omegaLow, double tStab)
This class extends the AbstractSlew.

Uses of AttitudeProvider in org.orekit.propagation

Methods in org.orekit.propagation that return AttitudeProvider

AttitudeProvider	Propagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	AbstractPropagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	Propagator.getAttitudeProviderEvents() Get attitude provider for events computation.
AttitudeProvider	AbstractPropagator.getAttitudeProviderEvents() Get attitude provider for events computation.
AttitudeProvider	Propagator.getAttitudeProviderForces() Get attitude provider for forces computation.
AttitudeProvider	AbstractPropagator.getAttitudeProviderForces() Get attitude provider for forces computation.

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

void	Propagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider for forces and events computation.
void	AbstractPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider for forces and events computation.
void	Propagator.setAttitudeProviderEvents(AttitudeProvider attitudeProviderEvents) Set attitude provider for events computation.
void	AbstractPropagator.setAttitudeProviderEvents(AttitudeProvider attProviderEvents) Set attitude provider for events computation.
void	Propagator.setAttitudeProviderForces(AttitudeProvider attitudeProviderForces) Set attitude provider for forces computation.
void	AbstractPropagator.setAttitudeProviderForces(AttitudeProvider attProviderForces) Set attitude provider for forces computation.

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

AbstractPropagator(AttitudeProvider attitudeProvider)
Build a new instance.

AbstractPropagator(AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents)
Build a new instance.

AnalyticalIntegratedEphemeris(List<AbsoluteDate> initialDates, List<AbsoluteDate> finalDates, List<SpacecraftState> initialStates, AbstractPropagator propagator, AttitudeProvider attForcesProvider, AttitudeProvider attEventsProvider, boolean isForward)
Constructor.

SpacecraftState(double[] y, OrbitType orbitType, PositionAngle angleType, AbsoluteDate date, double mu, Frame frame, Map<String,AdditionalStateInfo> addStatesInfo, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents)
Build a spacecraft from an array (a state vector) and an additional states informations map.

Uses of AttitudeProvider in org.orekit.propagation.analytical

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

void	AnalyticalEphemerisModeHandler.setAttitudeProviderEvents(AttitudeProvider attProvEvents) Set attitude provider for events computation.
void	AnalyticalEphemerisModeHandler.setAttitudeProviderForces(AttitudeProvider attProvForces) Set attitude provider for forces computation.

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

AbstractLyddanePropagator(Orbit secularOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider)
Generic constructor.

AnalyticalEphemerisModeHandler(AbstractPropagator propagator, AttitudeProvider attForcesProvider, AttitudeProvider attEventsProvider)
Constructor.

EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double referenceRadius, double mu, Frame frame, double c20, double c30, double c40, double c50, double c60, MassProvider massProvider, ParametersType paramsType)
Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double referenceRadius, double mu, Frame frame, double c20, double c30, double c40, double c50, double c60, ParametersType paramsType)
Build a propagator from orbit, attitude provider for forces and events computation and potential.

EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, Frame frame, double c20, double c30, double c40, double c50, double c60, MassProvider massProvider, ParametersType paramsType)
Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, double mu, Frame frame, double c20, double c30, double c40, double c50, double c60, ParametersType paramsType)
Build a propagator from orbit, attitude provider and potential.

J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvider)
Constructor without mass provider.

J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents)
Constructor without mass provider.

J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider)
Generic constructor.

J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvider, MassProvider massProvider)
Generic constructor.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv)
Build a propagator from orbit and a single attitude provider.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents)
Build a propagator from orbit and attitude provider for forces and event computation.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double mu)
Build a propagator from orbit, attitude provider for forces and events computation and central attraction coefficient μ.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double mu, MassProvider massProvider)
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu)
Build a propagator from orbit, a single attitude provider and central attraction coefficient μ.

KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu, MassProvider massProvider)
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider)
Constructor without mass provider.

LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents)
Constructor without mass provider.

LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider)
Generic constructor.

LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider, MassProvider massProvider)
Generic constructor.

LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider)
Constructor without mass provider.

LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents)
Constructor without mass provider.

LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider)
Generic constructor.

LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider, MassProvider massProvider)
Generic constructor.

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

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

static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MassProvider mass) Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, MassProvider mass) Selects the extrapolator to use with the selected TLE.

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

TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MassProvider mass)
Protected constructor for derived classes.

TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, MassProvider mass)
Protected constructor for derived classes.

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

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

Analytical2DPropagator(AttitudeProvider attitudeProvider, Analytical2DOrbitModel model, AbsoluteDate initialDate)
Create an instance of a 2D propagator.

Analytical2DPropagator(AttitudeProvider attitudeProvider, Analytical2DOrbitModel model, AbsoluteDate initialDate, int[] orders)
Create an instance of a 2D propagator.

Uses of AttitudeProvider in org.orekit.propagation.events

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

AdaptedEventDetector(EventDetector detector, Map<String,AdditionalStateInfo> info, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDate, double mu, Frame integrationFrame)
Build a wrapped event detector.

Uses of AttitudeProvider in org.orekit.propagation.numerical

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

AttitudeProvider	NumericalPropagator.getAttitudeProvider() Get attitude provider.
AttitudeProvider	NumericalPropagator.getAttitudeProviderEvents() Get attitude provider for events computation.
AttitudeProvider	NumericalPropagator.getAttitudeProviderForces() Get attitude provider for forces computation.

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

void	ModeHandler.initialize(OrbitType orbit, PositionAngle angle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, Map<String,AdditionalStateInfo> additionalStateInfos, boolean activateHandlers, AbsoluteDate reference, Frame frame, double mu) Initialize the mode handler.
void	NumericalPropagator.setAttitudeLaw(AttitudeProvider provider) Deprecated. as of 6.0 replaced by NumericalPropagator.setAttitudeProvider(AttitudeProvider)
void	NumericalPropagator.setAttitudeProvider(AttitudeProvider attitudeProvider) Set attitude provider for forces and events computation.
void	NumericalPropagator.setAttitudeProviderEvents(AttitudeProvider attitudeEventsProvider) Set attitude provider for events computation.
void	NumericalPropagator.setAttitudeProviderForces(AttitudeProvider attitudeForcesProvider) Set attitude provider for forces computation.

Uses of AttitudeProvider in org.orekit.propagation.precomputed

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

static SpacecraftState[]	AbstractEphemeris.generateSpacecraftState(PVCoordinatesProvider pvProv, AttitudeProvider attProvForces, AttitudeProvider attProvEvents, double step, AbsoluteDateInterval ptsInterval, Frame frame, double mu) Creates a spacecraft array with constant step size.
void	AbstractEphemeris.setAttitudeProvider(AttitudeProvider attitudeProvider)
void	AbstractEphemeris.setAttitudeProviderEvents(AttitudeProvider attProviderEvents)
void	AbstractEphemeris.setAttitudeProviderForces(AttitudeProvider attProviderForces)

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

HermiteEphemeris(PVCoordinatesProvider pvProv, AttitudeProvider attProvForces, AttitudeProvider attProvEvents, double step, AbsoluteDateInterval intervalOfPoints, Frame frame2, double mu2)
Deprecated. Constructor n°1 using a PV coordinates provider and an AttitudeProvider to build the interpolation points.

IntegratedEphemeris(List<AbsoluteDate> startDates, List<AbsoluteDate> minDates, List<AbsoluteDate> maxDates, OrbitType orbitType, PositionAngle angleType, AttitudeProvider attitudeForcesProvider, AttitudeProvider attitudeEventsProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> models, Frame referenceFrame, double mu)
Creates a new instance of IntegratedEphemeris.

LagrangeEphemeris(PVCoordinatesProvider pvProv, AttitudeProvider attProvForces, AttitudeProvider attProvEvents, double step, AbsoluteDateInterval intervalOfPoints, Frame frame, double mu)
Deprecated. Constructor using a PV coordinates provider and an AttitudeProvider to build the interpolation points, defaulting to 8th order for the Lagrange interpolator.

LagrangeEphemeris(PVCoordinatesProvider pvProv, AttitudeProvider attProvForces, AttitudeProvider attProvEvents, double step, AbsoluteDateInterval intervalOfPoints, Frame frame, double mu, int order)
Deprecated. Constructor using a PV coordinates provider and an AttitudeProvider to build the interpolation points.

Uses of AttitudeProvider in org.orekit.propagation.sampling

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

void

AdaptedStepHandler.initialize(OrbitType orbit, PositionAngle angle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, Map<String,AdditionalStateInfo> additionalStateInfos, boolean activateHandlers, AbsoluteDate reference, Frame frame, double mu) Initialize the mode handler.