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 RealFieldElement<T>> |
Differential equations for the main state (orbit, attitude and mass).
|
| FieldAdditionalEquations<T extends RealFieldElement<T>> |
This interface allows users to add their own differential equations to a numerical propagator.
|
| FieldModeHandler<T extends RealFieldElement<T>> |
Common interface for all propagator mode handlers initialization.
|
| ModeHandler |
Common interface for all propagator mode handlers initialization.
|
| Class | Description |
|---|---|
| AbstractDSConverter |
Converter for states and parameters arrays
for both
numerical and semi-analytical propagators. |
| AbstractGradientConverter |
Converter for states and parameters arrays
for both
numerical and semi-analytical propagators. |
| AbstractIntegratedPropagator |
Common handling of
Propagator
methods for both numerical and semi-analytical propagators. |
| AbstractJacobiansMapper |
Base class for jacobian mapper.
|
| FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>> |
Common handling of
FieldPropagator
methods for both numerical and semi-analytical propagators. |
| FieldIntegratedEphemeris<T extends RealFieldElement<T>> |
This class stores sequentially generated orbital parameters for
later retrieval.
|
| FieldStateMapper<T extends 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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