Package | Description |
---|---|
org.orekit.forces.maneuvers.jacobians |
Generators for columns of Jacobian matrices related to maneuver parameters.
|
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.numerical.cr3bp |
Top level package for CR3BP Models used with a numerical propagator.
|
org.orekit.propagation.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
Modifier and Type | Class and Description |
---|---|
class |
MassDepletionDelay
Generator for effect of delaying mass depletion when delaying a maneuver.
|
Modifier and Type | Method and Description |
---|---|
protected List<AdditionalDerivativesProvider> |
AbstractPropagatorBuilder.getAdditionalDerivativesProviders()
Get the list of additional equations.
|
Modifier and Type | Method and Description |
---|---|
void |
AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider provider)
Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).
|
Modifier and Type | Class and Description |
---|---|
class |
AdditionalEquationsAdapter
Deprecated.
must be removed in 12.0 when
AdditionalEquations is removed |
Modifier and Type | Method and Description |
---|---|
List<AdditionalDerivativesProvider> |
AbstractIntegratedPropagator.getAdditionalDerivativesProviders()
Get an unmodifiable list of providers for additional derivatives.
|
Modifier and Type | Method and Description |
---|---|
void |
AbstractIntegratedPropagator.addAdditionalDerivativesProvider(AdditionalDerivativesProvider provider)
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
|
Modifier and Type | Class and Description |
---|---|
class |
AbsolutePartialDerivativesEquations
Deprecated.
as of 11.1, this class is not used anymore
|
class |
EpochDerivativesEquations
This class is a copy of
AbsolutePartialDerivativesEquations
The computation of the derivatives of the acceleration due to a ThirdBodyAttraction
has been added. |
class |
PartialDerivativesEquations
Deprecated.
|
Modifier and Type | Class and Description |
---|---|
class |
STMEquations
Class calculating the state transition matrix coefficient for CR3BP Computation.
|
Modifier and Type | Class and Description |
---|---|
class |
DSSTPartialDerivativesEquations
Deprecated.
|
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