TLEBatchLSModel.java
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package org.orekit.estimation.leastsquares;
import java.util.List;
import org.orekit.estimation.measurements.ObservedMeasurement;
import org.orekit.orbits.Orbit;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.tle.TLEJacobiansMapper;
import org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations;
import org.orekit.propagation.analytical.tle.TLEPropagator;
import org.orekit.propagation.conversion.OrbitDeterminationPropagatorBuilder;
import org.orekit.propagation.integration.AbstractJacobiansMapper;
import org.orekit.utils.ParameterDriversList;
/** Bridge between {@link ObservedMeasurement measurements} and {@link
* org.hipparchus.optim.nonlinear.vector.leastsquares.LeastSquaresProblem
* least squares problems}.
* <p>
* This class is an adaption of the {@link BatchLSModel} class
* but for the {@link TLEPropagator TLE propagator}.
* </p>
* @author Luc Maisonobe
* @author Bryan Cazabonne
* @author Thomas Paulet
* @since 11.0
*
*/
public class TLEBatchLSModel extends AbstractBatchLSModel {
/** Simple constructor.
* @param propagatorBuilders builders to use for propagation
* @param measurements measurements
* @param estimatedMeasurementsParameters estimated measurements parameters
* @param observer observer to be notified at model calls
*/
public TLEBatchLSModel(final OrbitDeterminationPropagatorBuilder[] propagatorBuilders,
final List<ObservedMeasurement<?>> measurements,
final ParameterDriversList estimatedMeasurementsParameters,
final ModelObserver observer) {
// call super constructor
super(propagatorBuilders, measurements, estimatedMeasurementsParameters,
new TLEJacobiansMapper[propagatorBuilders.length], observer);
}
/** {@inheritDoc} */
@Override
protected TLEJacobiansMapper configureDerivatives(final Propagator propagator) {
final String equationName = TLEBatchLSModel.class.getName() + "-derivatives";
final TLEPartialDerivativesEquations partials = new TLEPartialDerivativesEquations(equationName, (TLEPropagator) propagator);
// add the derivatives to the initial state
final SpacecraftState rawState = propagator.getInitialState();
final SpacecraftState stateWithDerivatives = partials.setInitialJacobians(rawState);
propagator.resetInitialState(stateWithDerivatives);
return partials.getMapper();
}
/** {@inheritDoc} */
@Override
protected Orbit configureOrbits(final AbstractJacobiansMapper mapper,
final Propagator propagator) {
// Directly return the propagator's initial state
return propagator.getInitialState().getOrbit();
}
}