See: Description
Interface | Description |
---|---|
AbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
AdditionalEquations |
This interface allows users to add their own differential equations to a numerical propagator.
|
FieldAbstractIntegratedPropagator.MainStateEquations<T extends org.hipparchus.RealFieldElement<T>> |
Differential equations for the main state (orbit, attitude and mass).
|
FieldAdditionalEquations<T extends org.hipparchus.RealFieldElement<T>> |
This interface allows users to add their own differential equations to a numerical propagator.
|
FieldModeHandler<T extends org.hipparchus.RealFieldElement<T>> |
Common interface for all propagator mode handlers initialization.
|
ModeHandler |
Common interface for all propagator mode handlers initialization.
|
Class | Description |
---|---|
AbstractIntegratedPropagator |
Common handling of
Propagator
methods for both numerical and semi-analytical propagators. |
FieldAbstractIntegratedPropagator<T extends org.hipparchus.RealFieldElement<T>> |
Common handling of
FieldPropagator
methods for both numerical and semi-analytical propagators. |
FieldIntegratedEphemeris<T extends org.hipparchus.RealFieldElement<T>> |
This class stores sequentially generated orbital parameters for
later retrieval.
|
FieldStateMapper<T extends org.hipparchus.RealFieldElement<T>> |
This class maps between raw double elements and
FieldSpacecraftState instances. |
IntegratedEphemeris |
This class stores sequentially generated orbital parameters for
later retrieval.
|
StateMapper |
This class maps between raw double elements and
SpacecraftState instances. |
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