Uses of Interface
fr.cnes.sirius.patrius.attitudes.multi.MultiAttitudeProvider

Packages that use MultiAttitudeProvider

Package	Description
fr.cnes.sirius.patrius.attitudes.multi
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

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

Classes in fr.cnes.sirius.patrius.attitudes.multi that implement MultiAttitudeProvider

Modifier and Type	Class and Description
class	MultiAttitudeProviderWrapper Wrapper of attitude provider to make it compatible with MultiAttitudeProvider.

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

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

Modifier and Type	Method and Description
MultiAttitudeProvider	MultiPropagator.getAttitudeProvider(String satId) Get the default attitude provider.
MultiAttitudeProvider	MultiPropagator.getAttitudeProviderEvents(String satId) Get the attitude provider for events computation.
MultiAttitudeProvider	MultiPropagator.getAttitudeProviderForces(String satId) Get the attitude provider for forces computation.

Uses of MultiAttitudeProvider in fr.cnes.sirius.patrius.propagation.events.multi

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

Modifier and Type	Method and Description
void	AdaptedMonoEventDetector.reinitialize(OrbitType orbitType, PositionAngle angleType, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, AbsoluteDate referenceDate, MultiStateVectorInfo stateVectorInfo, String satId) Reinitialize data.

Method parameters in fr.cnes.sirius.patrius.propagation.events.multi with type arguments of type MultiAttitudeProvider

Modifier and Type	Method and Description
void	AdaptedMultiEventDetector.reinitialize(OrbitType orbitType, PositionAngle angleType, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo) Reinitialize data.
void	AdaptedMultiEventDetector.reinitialize(OrbitType orbitType, PositionAngle angleType, Map<String,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> attProvidersEvents, AbsoluteDate referenceDate, Map<String,Double> muMap, Map<String,Frame> framesMap, MultiStateVectorInfo stateVectorInfo) Reinitialize data.

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

Constructor and Description
AdaptedMonoEventDetector(EventDetector detector, OrbitType orbitType, PositionAngle angleType, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, AbsoluteDate referenceDate, MultiStateVectorInfo stateVectorInfo, String satId) Build a wrapped event detector.

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

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

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

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

Modifier and Type	Method and Description
MultiAttitudeProvider	MultiNumericalPropagator.getAttitudeProvider(String satId) Get the default attitude provider.
MultiAttitudeProvider	MultiNumericalPropagator.getAttitudeProviderEvents(String satId) Get the attitude provider for events computation.
MultiAttitudeProvider	MultiNumericalPropagator.getAttitudeProviderForces(String satId) Get the attitude provider for forces computation.

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

Modifier and Type	Method and Description
SpacecraftState	MultiStateVectorInfo.mapArrayToState(double[] y, AbsoluteDate currentDate, OrbitType orbitType, PositionAngle angleType, MultiAttitudeProvider attProviderForces, MultiAttitudeProvider attProviderEvents, String id) Extract a given SpacecraftState from the state vector.
void	MultiNumericalPropagator.setAttitudeProvider(MultiAttitudeProvider attitudeProvider, String satId) Set attitude provider.
void	MultiNumericalPropagator.setAttitudeProviderEvents(MultiAttitudeProvider attitudeProviderEvents, String satId) Set attitude provider for events.
void	MultiNumericalPropagator.setAttitudeProviderForces(MultiAttitudeProvider attitudeProviderForces, String satId) Set attitude provider for forces.

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

Modifier and Type	Method and Description
protected void	MultiNumericalPropagator.addEventHandlers(boolean activateHandlers, Map<String,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents) Add event handlers to integrator.
protected void	MultiNumericalPropagator.addEventHandlers(boolean activateHandlers, Map<String,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents) Add event handlers to integrator.
void	MultiEphemerisModeHandler.initialize(OrbitType orbit, PositionAngle angle, Map<String,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attitudeProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> attProvidersForces, Map<String,MultiAttitudeProvider> 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,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents, String satId) Wrap an Orekit event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(EventDetector osf, Map<String,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents, String satId) Wrap an Orekit event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(MultiEventDetector osf, Map<String,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents) Wrap an Orekit multi-sat event detector and register it to the integrator.
protected void	MultiNumericalPropagator.setUpEventDetector(MultiEventDetector osf, Map<String,MultiAttitudeProvider> localAttProvForces, Map<String,MultiAttitudeProvider> localAttProvEvents) Wrap an Orekit multi-sat event detector and register it to the integrator.

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

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

Constructor and Description

MultiIntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, MultiAttitudeProvider multiAttitudeProviderForcesIn, MultiAttitudeProvider multiAttitudeProviderEventsIn, MultiStateVectorInfo stateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, String satIdIn) Creates a new instance of IntegratedEphemeris.

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

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

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