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| Packages that use ContinuousOutputModel | |
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| fr.cnes.sirius.patrius.propagation.precomputed.multi | |
| org.apache.commons.math3.ode | This package provides classes to solve Ordinary Differential Equations problems. |
| org.orekit.propagation.precomputed | |
| Uses of ContinuousOutputModel in fr.cnes.sirius.patrius.propagation.precomputed.multi |
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| Constructor parameters in fr.cnes.sirius.patrius.propagation.precomputed.multi with type arguments of type ContinuousOutputModel | |
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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. |
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| Uses of ContinuousOutputModel in org.apache.commons.math3.ode |
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| Methods in org.apache.commons.math3.ode with parameters of type ContinuousOutputModel | |
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void |
ContinuousOutputModel.append(ContinuousOutputModel model)
Append another model at the end of the instance. |
| Uses of ContinuousOutputModel in org.orekit.propagation.precomputed |
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| Constructor parameters in org.orekit.propagation.precomputed with type arguments of type ContinuousOutputModel | |
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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. |
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