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.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
org.orekit.propagation.semianalytical.dsst |
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
|
Modifier and Type | Method and Description |
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DSSTPropagator[] |
DSSTBatchLSModel.createPropagators(RealVector point)
Create the propagators and parameters corresponding to an evaluation point.
|
Modifier and Type | Method and Description |
---|---|
DSSTPropagator[] |
DSSTKalmanModel.getEstimatedPropagators()
Get the propagators estimated with the values set in the propagators builders.
|
Modifier and Type | Method and Description |
---|---|
DSSTPropagator |
DSSTPropagatorBuilder.buildPropagator(double[] normalizedParameters)
Build a propagator.
|
Constructor and Description |
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DSSTPartialDerivativesEquations(String name,
DSSTPropagator propagator,
PropagationType propagationType)
Simple constructor.
|
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