| Package | Description |
|---|---|
| org.orekit.forces |
This package provides the interface for force models that will be used by the
NumericalPropagator, as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...). |
| org.orekit.forces.drag | |
| org.orekit.forces.gravity |
This package provides all gravity-related forces.
|
| org.orekit.forces.maneuvers |
This package provides models of simple maneuvers.
|
| org.orekit.forces.radiation | |
| org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
| org.orekit.propagation.numerical |
| Class and Description |
|---|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| Class and Description |
|---|
| JacobiansMapper
Mapper between two-dimensional Jacobian matrices and one-dimensional
additional state arrays. |
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| ParameterConfiguration
Simple container associating a parameter name with a step to compute its jacobian
and the provider that manages it.
|
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