Package | Description |
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org.orekit.forces.maneuvers.jacobians |
Generators for columns of Jacobian matrices related to maneuver parameters.
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org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
org.orekit.propagation.numerical |
Top level package for numerical propagators.
|
org.orekit.propagation.numerical.cr3bp |
Top level package for CR3BP Models used with a numerical propagator.
|
Modifier and Type | Method and Description |
---|---|
CombinedDerivatives |
MassDepletionDelay.combinedDerivatives(SpacecraftState state)
Compute the derivatives related to the additional state (and optionally main state increments).
|
Modifier and Type | Method and Description |
---|---|
CombinedDerivatives |
AdditionalDerivativesProvider.combinedDerivatives(SpacecraftState s)
Compute the derivatives related to the additional state (and optionally main state increments).
|
Modifier and Type | Method and Description |
---|---|
CombinedDerivatives |
EpochDerivativesEquations.combinedDerivatives(SpacecraftState s)
Compute the derivatives related to the additional state (and optionally main state increments).
|
Modifier and Type | Method and Description |
---|---|
CombinedDerivatives |
STMEquations.combinedDerivatives(SpacecraftState s)
Compute the derivatives related to the additional state (and optionally main state increments).
|
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