Uses of Class
fr.cnes.sirius.patrius.math.ode.ContinuousOutputModel

Packages that use ContinuousOutputModel

Package	Description
fr.cnes.sirius.patrius.math.ode	This package provides classes to solve Ordinary Differential Equations problems.
fr.cnes.sirius.patrius.propagation.precomputed
fr.cnes.sirius.patrius.propagation.precomputed.multi

Uses of ContinuousOutputModel in fr.cnes.sirius.patrius.math.ode

Methods in fr.cnes.sirius.patrius.math.ode with parameters of type ContinuousOutputModel

Modifier and Type	Method and Description
void	ContinuousOutputModel.append(ContinuousOutputModel model) Append another model at the end of the instance.

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

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

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.

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

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

Constructor and Description

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.