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

Packages that use StelaAdditionalEquations

Package	Description
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

Modifier and Type	Class and Description
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

Modifier and Type	Method and Description
List<StelaAdditionalEquations>	StelaGTOPropagator.getAddEquations() Get the additional equations.

Methods in fr.cnes.sirius.patrius.stela.propagation with parameters of type StelaAdditionalEquations

Modifier and Type	Method and Description
void	StelaGTOPropagator.addAdditionalEquations(StelaAdditionalEquations addEquations) Add a set of user-specified additional equations to be integrated along with the orbit propagation.