Package org.orekit.estimation.sequential

Class AbstractKalmanEstimator

java.lang.Object

org.orekit.estimation.sequential.AbstractKalmanEstimator

Direct Known Subclasses:

KalmanEstimator, SemiAnalyticalKalmanEstimator, SemiAnalyticalUnscentedKalmanEstimator, UnscentedKalmanEstimator

public abstract class AbstractKalmanEstimator
extends Object

Base class for Kalman estimators.

Since:

11.3

Author:

Romain Gerbaud, Maxime Journot, Luc Maisonobe

Constructor Summary

Constructors

Modifier	Constructor	Description
protected	AbstractKalmanEstimator(List<? extends PropagatorBuilder> builders)	Constructor.

Method Summary

Modifier and Type	Method	Description
AbsoluteDate	getCurrentDate()	Get the current date.
int	getCurrentMeasurementNumber()	Get the current measurement number.
ParameterDriversList	getEstimatedMeasurementsParameters()	Get the list of estimated measurements parameters.
protected abstract KalmanEstimation	getKalmanEstimation()	Get the provider for kalman filter estimations.
ParameterDriversList	getOrbitalParametersDrivers(boolean estimatedOnly)	Get the orbital parameters supported by this estimator.
RealMatrix	getPhysicalEstimatedCovarianceMatrix()	Get the "physical" estimated covariance matrix (i.e.
RealVector	getPhysicalEstimatedState()	Get the "physical" estimated state (i.e.
ParameterDriversList	getPropagationParametersDrivers(boolean estimatedOnly)	Get the propagator parameters supported by this estimator.

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

AbstractKalmanEstimator

protected AbstractKalmanEstimator(List<? extends PropagatorBuilder> builders)

Constructor.

Parameters:

builders - list of propagator builders

Method Detail

getOrbitalParametersDrivers

public ParameterDriversList getOrbitalParametersDrivers(boolean estimatedOnly)

Get the orbital parameters supported by this estimator.

If there are more than one propagator builder, then the names of the drivers have an index marker in square brackets appended to them in order to distinguish the various orbits. So for example with one builder generating Keplerian orbits the names would be simply "a", "e", "i"... but if there are several builders the names would be "a[0]", "e[0]", "i[0]"..."a[1]", "e[1]", "i[1]"...

Parameters:

estimatedOnly - if true, only estimated parameters are returned

Returns:

orbital parameters supported by this estimator

getPropagationParametersDrivers

public ParameterDriversList getPropagationParametersDrivers(boolean estimatedOnly)

Get the propagator parameters supported by this estimator.

Parameters:

estimatedOnly - if true, only estimated parameters are returned

Returns:

propagator parameters supported by this estimator

getCurrentMeasurementNumber

public int getCurrentMeasurementNumber()

Get the current measurement number.

Returns:

current measurement number

getCurrentDate

public AbsoluteDate getCurrentDate()

Get the current date.

Returns:

current date

getPhysicalEstimatedState

public RealVector getPhysicalEstimatedState()

Get the "physical" estimated state (i.e. not normalized)

For the Semi-analytical Kalman Filters it corresponds to the corrected filter correction. In other words, it doesn't represent an orbital state.

Returns:

the "physical" estimated state

getPhysicalEstimatedCovarianceMatrix

public RealMatrix getPhysicalEstimatedCovarianceMatrix()

Get the "physical" estimated covariance matrix (i.e. not normalized)

Returns:

the "physical" estimated covariance matrix

getEstimatedMeasurementsParameters

public ParameterDriversList getEstimatedMeasurementsParameters()

Get the list of estimated measurements parameters.

Returns:

the list of estimated measurements parameters

getKalmanEstimation

protected abstract KalmanEstimation getKalmanEstimation()

Get the provider for kalman filter estimations.

Returns:

the provider for Kalman filter estimations