Uses of Class
org.orekit.attitudes.Attitude

Packages that use Attitude

fr.cnes.sirius.patrius.guidance
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.precomputed

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

Methods in fr.cnes.sirius.patrius.guidance that return Attitude

Attitude	GuidanceProfile.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	QuaternionHarmonicProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	QuaternionPolynomialProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AngularVelocitiesPolynomialProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate userDate, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AngularVelocitiesHarmonicProfile.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate userDate, Frame frame) Compute the attitude corresponding to an orbital state.

Uses of Attitude in org.orekit.attitudes

Methods in org.orekit.attitudes that return Attitude

Attitude	Slew.getAttitude(AbsoluteDate date, Frame frame) Compute the attitude.
Attitude	ConstantSpinSlew.getAttitude(AbsoluteDate date, Frame frame)
Attitude	AbstractIsisSpinBiasSlew.getAttitude(AbsoluteDate date, Frame frame) Compute the attitude.
Attitude	TwoSpinBiasSlew.getAttitude(AbsoluteDate date, Frame frame)
Attitude	AbstractAttitudeLaw.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLawLeg.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	RelativeTabulatedAttitudeLaw.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLegLaw.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeProvider.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	TabulatedAttitude.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AbstractSlew.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLegsSequence.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	RelativeTabulatedAttitudeLeg.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	AttitudesSequence.getAttitude(Orbit orbit) Compute the attitude corresponding to an orbital state.
Attitude	ComposedAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Attitude	BodyCenterPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TargetPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	ConstantAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLawLeg.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Attitude	YawCompensation.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	YawSteering.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	LofOffset.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	RelativeTabulatedAttitudeLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	IsisSunPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TwoDirectionsAttitude.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeLegLaw.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	TabulatedAttitude.getAttitude(PVCoordinatesProvider pvProvider, AbsoluteDate date, Frame inFrame) Compute the attitude corresponding to an orbital state.
Attitude	CelestialBodyPointed.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AbstractSlew.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Attitude	AttitudeLegsSequence.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Gets the attitude from the sequence. The AttitudeLeg matching the date is called to compute the attitude.
Attitude	RelativeTabulatedAttitudeLeg.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	LofOffsetPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	SpinStabilized.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	FixedRate.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	GroundPointing.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	AttitudesSequence.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	GroundPointingWrapper.getBaseState(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the base system state at given date, without compensation.
Attitude	AttitudeLegsSequence.getOldAttitudeOnTransition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Returns the attitude at a transition date for the old attitude law (the law previous to the valid transition law).
Attitude	FixedRate.getReferenceAttitude() Get the reference attitude.
Attitude	Attitude.interpolate(AbsoluteDate interpolationDate, Collection<Attitude> sample) Get an interpolated instance.
Attitude	Attitude.interpolate(AbsoluteDate interpolationDate, Collection<Attitude> sample, boolean computeSpinDerivatives) Interpolates attitude.
Attitude	Attitude.shiftedBy(double dt) Get a time-shifted attitude.
static Attitude	Attitude.slerp(AbsoluteDate date, Attitude attitude1, Attitude attitude2, Frame frame, boolean computeSpinDerivative) The slerp interpolation method is efficient but is less accurate than the interpolate method.
Attitude	Attitude.withReferenceFrame(Frame newReferenceFrame) Get a similar attitude with a specific reference frame.
Attitude	Attitude.withReferenceFrame(Frame newReferenceFrame, boolean spinDerivativesComputation) Get a similar attitude with a specific reference frame.

Methods in org.orekit.attitudes that return types with arguments of type Attitude

SortedSet<Attitude>	AbstractAttitudeEphemerisGenerator.generateEphemeris(AbsoluteDateInterval ephemerisInterval, Frame frame) Computes attitude ephemeris using a fixed or variable time step and choosing the interval of validity.
SortedSet<Attitude>	AbstractAttitudeEphemerisGenerator.generateEphemeris(Frame frame) Computes attitude ephemeris using a fixed or variable time step.
List<Attitude>	TabulatedAttitude.getAttitudes() Get the non-interpolated and rightly ordered attitudes.

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

int	AttitudeChronologicalComparator.compare(Attitude o1, Attitude o2) Compare two Attitude instances.
abstract TimeStampedAngularCoordinates	GroundPointingWrapper.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
TimeStampedAngularCoordinates	YawCompensation.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame orbitFrame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
TimeStampedAngularCoordinates	YawSteering.getCompensation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame orbitFrame, Attitude base) Compute the TimeStampedAngularCoordinates at a given time.
static Attitude	Attitude.slerp(AbsoluteDate date, Attitude attitude1, Attitude attitude2, Frame frame, boolean computeSpinDerivative) The slerp interpolation method is efficient but is less accurate than the interpolate method.

Method parameters in org.orekit.attitudes with type arguments of type Attitude

Attitude	Attitude.interpolate(AbsoluteDate interpolationDate, Collection<Attitude> sample) Get an interpolated instance.
Attitude	Attitude.interpolate(AbsoluteDate interpolationDate, Collection<Attitude> sample, boolean computeSpinDerivatives) Interpolates attitude.

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

FixedRate(Attitude pReferenceAttitude)
Creates a new instance.

Constructor parameters in org.orekit.attitudes with type arguments of type Attitude

TabulatedAttitude(List<Attitude> inAttitudes)
Constructor with default number N of points used for interpolation.

TabulatedAttitude(List<Attitude> inAttitudes, int nbInterpolationPoints)
Constructor with number of points used for interpolation

Uses of Attitude in org.orekit.propagation

Methods in org.orekit.propagation that return Attitude

Attitude	SpacecraftState.getAttitude() Get the default attitude : the attitude for forces computation.
Attitude	SpacecraftState.getAttitude(Frame outputFrame) Get the default attitude : the attitude for forces computation in given output frame.
Attitude	SpacecraftState.getAttitude(LOFType lofType) Get the default attitude : the attitude for forces computation in given local orbital frame.
Attitude	SpacecraftState.getAttitudeEvents() Get the attitude for events computation.
Attitude	SpacecraftState.getAttitudeEvents(Frame outputFrame) Get the attitude for events computation in given output frame.
Attitude	SpacecraftState.getAttitudeEvents(LOFType lofType) Get the attitude for events computation in given local orbital frame.
Attitude	SpacecraftState.getAttitudeForces() Get the attitude for forces computation.
Attitude	SpacecraftState.getAttitudeForces(Frame outputFrame) Get the attitude for forces computation in given output frame.
Attitude	SpacecraftState.getAttitudeForces(LOFType lofType) Get the attitude for forces computation in given local orbital frame.

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

SpacecraftState

SpacecraftState.addAttitude(Attitude newAttitude, AttitudeEquation.AttitudeType type) Add attitude to the additional states map.

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

SpacecraftState(Orbit orbit, Attitude attitude)
Build a spacecraft state from orbit and a single attitude.

SpacecraftState(Orbit orbit, Attitude attForces, Attitude attEvents)
Build a spacecraft state from orbit, attitude for forces and events computation.

SpacecraftState(Orbit orbit, Attitude attForces, Attitude attEvents, Map<String,double[]> addStates)
Build a spacecraft state from orbit, attitude for forces and events computation and additional states map.

SpacecraftState(Orbit orbit, Attitude attForces, Attitude attEvents, MassProvider massProvider)
Build a spacecraft state from orbit, attitude for forces and events computation and mass provider.

SpacecraftState(Orbit orbit, Attitude attForces, Attitude attEvents, MassProvider massProvider, Map<String,double[]> additionalStates)
Build a spacecraft state from orbit, attitude for forces and events computation, mass provider and additional states map.

SpacecraftState(Orbit orbit, Attitude attitude, MassProvider massProvider)
Build a spacecraft state from orbit, attitude and mass provider.

Uses of Attitude in org.orekit.propagation.precomputed

Methods in org.orekit.propagation.precomputed that return Attitude

protected Attitude[]

AbstractEphemeris.attitudesInterpolation(SpacecraftState[] tab, int order, int i0, AbsoluteDate date) This method is called only if attitudes are supported.