Uses of Class
fr.cnes.sirius.patrius.propagation.numerical.AdditionalStateInfo

Packages that use AdditionalStateInfo

Package	Description
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.events
fr.cnes.sirius.patrius.propagation.numerical
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.propagation.precomputed
fr.cnes.sirius.patrius.propagation.sampling

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

Methods in fr.cnes.sirius.patrius.propagation that return types with arguments of type AdditionalStateInfo

Modifier and Type	Method and Description
Map<String,AdditionalStateInfo>	SpacecraftState.getAdditionalStatesInfos() Get the additional states informations map.

Constructor parameters in fr.cnes.sirius.patrius.propagation with type arguments of type AdditionalStateInfo

Constructor and Description
SpacecraftState(double[] y, OrbitType orbitType, PositionAngle angleType, AbsoluteDate date, double mu, Frame frame, Map<String,AdditionalStateInfo> addStatesInfo, Attitude attForces, Attitude attEvents) Build a spacecraft from an array (a state vector) and an additional states informations map.
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 AdditionalStateInfo in fr.cnes.sirius.patrius.propagation.events

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

Modifier and Type	Method and Description
void	AdaptedEventDetector.reinitialize(Map<String,AdditionalStateInfo> info, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDateIn, double muIn, Frame integrationFrameIn) Reinitialize reference data.

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

Constructor and Description
AdaptedEventDetector(EventDetector detectorIn, Map<String,AdditionalStateInfo> info, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, AbsoluteDate referenceDateIn, double muIn, Frame integrationFrameIn) Build a wrapped event detector.

Uses of AdditionalStateInfo in fr.cnes.sirius.patrius.propagation.numerical

Methods in fr.cnes.sirius.patrius.propagation.numerical that return AdditionalStateInfo

Modifier and Type	Method and Description
AdditionalStateInfo	AdditionalStateInfo.clone() Copy of the AdditionalStateInfo.

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

Modifier and Type	Method and Description
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.

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

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi that return types with arguments of type AdditionalStateInfo

Modifier and Type	Method and Description
Map<String,AdditionalStateInfo>	MultiStateVectorInfo.getAddStatesInfos(String satId) Get the additional states informations associated with the given spacecraft ID.

Uses of AdditionalStateInfo in fr.cnes.sirius.patrius.propagation.precomputed

Constructor parameters in fr.cnes.sirius.patrius.propagation.precomputed with type arguments of type AdditionalStateInfo

Constructor and Description
IntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeForcesProvider, AttitudeProvider attitudeEventsProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn) Creates a new instance of IntegratedEphemeris.
IntegratedEphemeris(List<AbsoluteDate> startDatesIn, List<AbsoluteDate> minDatesIn, List<AbsoluteDate> maxDatesIn, OrbitType orbitTypeIn, PositionAngle angleTypeIn, AttitudeProvider attitudeProvider, Map<String,AdditionalStateInfo> additionalStateInfos, List<ContinuousOutputModel> modelsIn, Frame referenceFrameIn, double muIn) Creates a new instance of IntegratedEphemeris.

Uses of AdditionalStateInfo in fr.cnes.sirius.patrius.propagation.sampling

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

Modifier and Type	Method and Description
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.