| Interface | Description |
|---|---|
| AdditionalEquations |
This interface allows users to add their own differential equations to a numerical propagator.
|
| JacobianParametersProvider |
Interface for classes that can provide parameters for computing jacobians.
|
| ModeHandler |
Common interface for all propagator mode handlers initialization.
|
| TimeDerivativesEquations |
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class | Description |
|---|---|
| AbstractPartialDerivativesEquations |
Abstract class for
PartialDerivativesEquations and MultiPartialDerivativesEquations. |
| AdditionalEquationsAndTolerances |
Internal class for additional equations and tolerances management.
|
| AdditionalStateInfo |
Utility class that describes in a minimal fashion the structure of an additional state.
|
| AttitudeEquation |
This interface allows users to add their own attitude differential equations to a numerical propagator.
|
| Jacobianizer |
Class enabling basic
ForceModel instances
to be used when processing spacecraft state partial derivatives. |
| JacobiansMapper |
Mapper between two-dimensional Jacobian matrices and one-dimensional
additional state arrays.
|
| NumericalPropagator |
This class propagates
SpacecraftState using numerical integration. |
| ParameterConfiguration |
Simple container associating a parameter name with a step to compute its jacobian
and the provider thant manages it.
|
| PartialDerivativesEquations |
Set of
additional equations computing the partial derivatives
of the state (orbit) with respect to initial state and force models parameters. |
| SecondOrderMapper |
Second-order / first order integrator state mapper.
|
| Enum | Description |
|---|---|
| AttitudeEquation.AttitudeType |
Attitude type.
|
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