Package | Description |
---|---|
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. |
Modifier and Type | Class and Description |
---|---|
class |
DSSTKalmanModel
Class defining the process model dynamics to use with a
KalmanEstimator . |
class |
KalmanModel
Class defining the process model dynamics to use with a
KalmanEstimator . |
class |
TLEKalmanModel
Class defining the process model dynamics to use with a
KalmanEstimator . |
Modifier and Type | Method and Description |
---|---|
AbstractKalmanModel |
TLEPropagatorBuilder.buildKalmanModel(List<OrbitDeterminationPropagatorBuilder> propagatorBuilders,
List<CovarianceMatrixProvider> covarianceMatricesProviders,
ParameterDriversList estimatedMeasurementsParameters,
CovarianceMatrixProvider measurementProcessNoiseMatrix) |
AbstractKalmanModel |
OrbitDeterminationPropagatorBuilder.buildKalmanModel(List<OrbitDeterminationPropagatorBuilder> propagatorBuilders,
List<CovarianceMatrixProvider> covarianceMatricesProviders,
ParameterDriversList estimatedMeasurementsParameters,
CovarianceMatrixProvider measurementProcessNoiseMatrix)
Build a new Kalman model.
|
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