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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