Uses of Interface
org.orekit.propagation.AdditionalStateProvider

Packages that use AdditionalStateProvider
fr.cnes.sirius.patrius.propagation   
fr.cnes.sirius.patrius.stela.propagation   
org.orekit.propagation This package provides tools to propagate orbital states with different methods. 
 

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

Classes in fr.cnes.sirius.patrius.propagation that implement AdditionalStateProvider
 class SimpleAdditionalStateProvider
           This class is a simple implementation of additionalStateProvider.
 

Constructor parameters in fr.cnes.sirius.patrius.propagation with type arguments of type AdditionalStateProvider
PVCoordinatePropagator(PVCoordinatesProvider pvCoordProvider, AbsoluteDate initDate, double mu, Frame frame, AttitudeProvider attProviderForces, AttitudeProvider attProviderEvents, List<AdditionalStateProvider> additionalStateProviders)
          Creates an instance of PVCoordinatePropagator with PV, attitude for forces, attitude for events, and additional state providers given by the user.
 

Uses of AdditionalStateProvider in fr.cnes.sirius.patrius.stela.propagation
 

Methods in fr.cnes.sirius.patrius.stela.propagation with parameters of type AdditionalStateProvider
 void StelaAbstractPropagator.addAdditionalStateProvider(AdditionalStateProvider additionalStateProvider)
          Add a set of user-specified state parameters to be computed along with the orbit propagation.
 

Method parameters in fr.cnes.sirius.patrius.stela.propagation with type arguments of type AdditionalStateProvider
 void StelaBasicInterpolator.setAdditionalStateProviders(List<AdditionalStateProvider> additionalStateProvidersIn)
          sets the additionalStateProviders
 

Uses of AdditionalStateProvider in org.orekit.propagation
 

Methods in org.orekit.propagation with parameters of type AdditionalStateProvider
 void AbstractPropagator.addAdditionalStateProvider(AdditionalStateProvider additionalStateProvider)
          Add a set of user-specified state parameters to be computed along with the orbit propagation.
 



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