Uses of Interface
fr.cnes.sirius.patrius.stela.propagation.StelaAdditionalEquations

Packages that use StelaAdditionalEquations
fr.cnes.sirius.patrius.stela.propagation   
 

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

Classes in fr.cnes.sirius.patrius.stela.propagation that implement StelaAdditionalEquations
 class StelaAttitudeAdditionalEquations
           This abstract class allows users to add their own attitude differential equations to a Stela GTO propagator.
 class StelaPartialDerivativesEquations
          This class represents a set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state.
 

Methods in fr.cnes.sirius.patrius.stela.propagation that return types with arguments of type StelaAdditionalEquations
 List<StelaAdditionalEquations> StelaGTOPropagator.getAddEquations()
          Get the additional equations.
 

Methods in fr.cnes.sirius.patrius.stela.propagation with parameters of type StelaAdditionalEquations
 void StelaGTOPropagator.addAdditionalEquations(StelaAdditionalEquations addEquations)
          Add a set of user-specified additional equations to be integrated along with the orbit propagation.
 



Copyright © 2017 CNES. All Rights Reserved.