Uses of Class
org.orekit.propagation.numerical.AdditionalStateInfo

Packages that use AdditionalStateInfo

fr.cnes.sirius.patrius.propagation.numerical.multi
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
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 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

Map<String,AdditionalStateInfo>

MultiStateVectorInfo.getAddStatesInfos(String satId) Get the additional states informations associated with the given spacecraft ID.

Uses of AdditionalStateInfo in org.orekit.propagation

Methods in org.orekit.propagation that return types with arguments of type AdditionalStateInfo

Map<String,AdditionalStateInfo>

SpacecraftState.getAdditionalStatesInfos() Get the additional states informations map.

Constructor parameters in org.orekit.propagation with type arguments of type AdditionalStateInfo

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 org.orekit.propagation.events

Constructor parameters in org.orekit.propagation.events with type arguments of type AdditionalStateInfo

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 AdditionalStateInfo in org.orekit.propagation.numerical

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

AdditionalStateInfo

AdditionalStateInfo.clone() Copy of the AdditionalStateInfo.

Method parameters in org.orekit.propagation.numerical with type arguments of type AdditionalStateInfo

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 org.orekit.propagation.precomputed

Constructor parameters in org.orekit.propagation.precomputed with type arguments of type AdditionalStateInfo

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.

Uses of AdditionalStateInfo in org.orekit.propagation.sampling

Method parameters in org.orekit.propagation.sampling with type arguments of type AdditionalStateInfo

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.