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.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).
|
org.orekit.utils |
This package provides useful objects.
|
Modifier and Type | Method and Description |
---|---|
protected List<AdditionalEquations> |
AbstractPropagatorBuilder.getAdditionalEquations()
Deprecated.
as of 11.1, replaced by
AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider) |
Modifier and Type | Method and Description |
---|---|
void |
AbstractPropagatorBuilder.addAdditionalEquations(AdditionalEquations additional)
Deprecated.
as of 11.1, replaced by
AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider) |
Modifier and Type | Method and Description |
---|---|
void |
AbstractIntegratedPropagator.addAdditionalEquations(AdditionalEquations additional)
Deprecated.
as of 11.1, replaced by
AbstractIntegratedPropagator.addAdditionalDerivativesProvider(AdditionalDerivativesProvider) |
Constructor and Description |
---|
AdditionalEquationsAdapter(AdditionalEquations equations,
Supplier<SpacecraftState> stateSupplier)
Deprecated.
Simple constructor.
|
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.
|
Constructor and Description |
---|
CR3BPMultipleShooter(List<SpacecraftState> initialGuessList,
List<NumericalPropagator> propagatorList,
List<AdditionalEquations> additionalEquations,
double arcDuration,
double tolerance)
Deprecated.
as of 11.1, replaced by
CR3BPMultipleShooter.CR3BPMultipleShooter(List, List, List, double, double, int) |
Modifier and Type | Class and Description |
---|---|
class |
DSSTPartialDerivativesEquations
Deprecated.
|
Modifier and Type | Method and Description |
---|---|
protected SpacecraftState |
AbstractMultipleShooting.getAugmentedInitialState(SpacecraftState initialState,
AdditionalEquations additionalEquations2)
Deprecated.
as of 11.1, replaced by
AbstractMultipleShooting.getAugmentedInitialState(int) |
Constructor and Description |
---|
AbstractMultipleShooting(List<SpacecraftState> initialGuessList,
List<NumericalPropagator> propagatorList,
List<AdditionalEquations> additionalEquations,
double arcDuration,
double tolerance,
String additionalName)
Deprecated.
as of 11.1, replaced by
AbstractMultipleShooting.AbstractMultipleShooting(List, List, double, double, int, String) |
MultipleShooter(List<SpacecraftState> initialGuessList,
List<NumericalPropagator> propagatorList,
List<AdditionalEquations> additionalEquations,
double arcDuration,
double tolerance)
Deprecated.
as of 11.1, replaced by
MultipleShooter.MultipleShooter(List, List, List, double, double, int) |
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