| Package | Description |
|---|---|
| org.orekit.estimation.leastsquares |
The leastsquares package provides an implementation of a batch least
squares estimator engine to perform an orbit determination.
|
| org.orekit.estimation.sequential |
The sequential package provides an implementation of a
Kalman Filter engine to perform an orbit determination.
|
| org.orekit.forces |
This package provides the interface for force models that will be used by the
NumericalPropagator, as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...). |
| org.orekit.forces.gravity |
This package provides all gravity-related forces.
|
| org.orekit.forces.maneuvers |
This package provides models of simple maneuvers.
|
| org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
| 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.utils |
This package provides useful objects.
|
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| Class and Description |
|---|
| FieldTimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| FieldTimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| FieldTimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| TimeDerivativesEquations
Interface summing up the contribution of several forces into orbit and mass derivatives.
|
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| Class and Description |
|---|
| AbsoluteJacobiansMapper
Mapper between two-dimensional Jacobian matrices and one-dimensional
additional state arrays. |
| GLONASSNumericalPropagator
This class propagates GLONASS orbits using numerical integration.
|
| GLONASSNumericalPropagator.Builder
This nested class aims at building a GLONASSNumericalPropagator.
|
| JacobiansMapper
Mapper between two-dimensional Jacobian matrices and one-dimensional
additional state arrays. |
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| PartialDerivativesEquations
Set of
additional equations computing the partial derivatives
of the state (orbit) with respect to initial state and force models parameters. |
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
| Class and Description |
|---|
| NumericalPropagator
This class propagates
orbits using
numerical integration. |
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