| 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 and 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.
|
| StateMapper
This class maps between raw double elements and
SpacecraftState instances. |
| Class and 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.
|
| StateMapper
This class maps between raw double elements and
SpacecraftState instances. |
| Class and 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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