Package | Description |
---|---|
org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
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.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
Modifier and Type | Method and Description |
---|---|
protected List<AdditionalEquations> |
AbstractPropagatorBuilder.getAdditionalEquations()
Get the list of additional equations.
|
Modifier and Type | Method and Description |
---|---|
void |
AbstractPropagatorBuilder.addAdditionalEquations(AdditionalEquations additional)
Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).
|
Modifier and Type | Method and Description |
---|---|
void |
AbstractIntegratedPropagator.addAdditionalEquations(AdditionalEquations additional)
Add a set of user-specified equations to be integrated along with the orbit propagation.
|
Modifier and Type | Class and Description |
---|---|
class |
PartialDerivativesEquations
Set of
additional equations computing the partial derivatives
of the state (orbit) with respect to initial state and force models parameters. |
Modifier and Type | Class and Description |
---|---|
class |
DSSTPartialDerivativesEquations
Set of
additional equations computing the partial derivatives
of the state (orbit) with respect to initial state and force models parameters. |
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