Package | Description |
---|---|
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).
|
Class | Description |
---|---|
AbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
AdditionalEquations |
This interface allows users to add their own differential equations to a numerical propagator.
|
FieldAbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
FieldAdditionalEquations |
This interface allows users to add their own differential equations to a numerical propagator.
|
FieldStateMapper |
This class maps between raw double elements and
FieldSpacecraftState instances. |
StateMapper |
This class maps between raw double elements and
SpacecraftState instances. |
Class | Description |
---|---|
AbstractIntegratedPropagator |
Common handling of
Propagator
methods for both numerical and semi-analytical propagators. |
AbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
AdditionalEquations |
This interface allows users to add their own differential equations to a numerical propagator.
|
FieldAbstractIntegratedPropagator |
Common handling of
FieldPropagator
methods for both numerical and semi-analytical propagators. |
FieldAbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
FieldStateMapper |
This class maps between raw double elements and
FieldSpacecraftState instances. |
StateMapper |
This class maps between raw double elements and
SpacecraftState instances. |
Class | Description |
---|---|
AbstractIntegratedPropagator |
Common handling of
Propagator
methods for both numerical and semi-analytical propagators. |
AbstractIntegratedPropagator.MainStateEquations |
Differential equations for the main state (orbit, attitude and mass).
|
StateMapper |
This class maps between raw double elements and
SpacecraftState instances. |
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