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| Packages that use StelaAdditionalEquations | |
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| fr.cnes.sirius.patrius.stela.propagation | |
| Uses of StelaAdditionalEquations in fr.cnes.sirius.patrius.stela.propagation |
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| Classes in fr.cnes.sirius.patrius.stela.propagation that implement StelaAdditionalEquations | |
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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 | |
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List<StelaAdditionalEquations> |
StelaGTOPropagator.getAddEquations()
Get the additional equations. |
| Methods in fr.cnes.sirius.patrius.stela.propagation with parameters of type StelaAdditionalEquations | |
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void |
StelaGTOPropagator.addAdditionalEquations(StelaAdditionalEquations addEquations)
Add a set of user-specified additional equations to be integrated along with the orbit propagation. |
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