TLEGradientConverter.java
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* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
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*
* http://www.apache.org/licenses/LICENSE-2.0
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* Unless required by applicable law or agreed to in writing, software
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package org.orekit.propagation.analytical.tle;
import java.util.List;
import org.hipparchus.analysis.differentiation.Gradient;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.frames.Frame;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter;
import org.orekit.time.TimeScale;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.ParameterDriversProvider;
/** Converter for TLE propagator.
* @author Luc Maisonobe
* @author Bryan Cazabonne
* @author Thomas Paulet
* @since 11.0
*/
class TLEGradientConverter extends AbstractAnalyticalGradientConverter implements ParameterDriversProvider {
/** Fixed dimension of the state. */
public static final int FREE_STATE_PARAMETERS = 6;
/** Current TLE. */
private final TLE tle;
/** UTC time scale. */
private final TimeScale utc;
/** TEME frame. */
private final Frame teme;
/** Attitude provider. */
private final AttitudeProvider provider;
/** Simple constructor.
* @param propagator TLE propagator used to access initial orbit
*/
TLEGradientConverter(final TLEPropagator propagator) {
super(propagator, TLEConstants.MU, FREE_STATE_PARAMETERS);
// TLE and related parameters
this.tle = propagator.getTLE();
this.teme = propagator.getFrame();
this.utc = tle.getUtc();
this.provider = propagator.getAttitudeProvider();
}
/** {@inheritDoc} */
@Override
public FieldTLEPropagator<Gradient> getPropagator(final FieldSpacecraftState<Gradient> state,
final Gradient[] parameters) {
// Zero
final Gradient zero = state.getA().getField().getZero();
// Template TLE
final int satelliteNumber = tle.getSatelliteNumber();
final char classification = tle.getClassification();
final int launchYear = tle.getLaunchYear();
final int launchNumber = tle.getLaunchNumber();
final String launchPiece = tle.getLaunchPiece();
final int ephemerisType = tle.getEphemerisType();
final int elementNumber = tle.getElementNumber();
final int revolutionNumberAtEpoch = tle.getRevolutionNumberAtEpoch();
final double bStar = tle.getBStar(state.getDate().toAbsoluteDate());
// Initialize the new TLE
final FieldTLE<Gradient> templateTLE = new FieldTLE<>(satelliteNumber, classification,
launchYear, launchNumber, launchPiece, ephemerisType, elementNumber, state.getDate(),
zero, zero, zero, zero, zero, zero, zero, zero,
revolutionNumberAtEpoch, bStar, utc);
// TLE
final FieldTLE<Gradient> gTLE = TLEPropagator.getDefaultTleGenerationAlgorithm(utc, teme).generate(state, templateTLE);
// Return the "Field" propagator
return FieldTLEPropagator.selectExtrapolator(gTLE, provider, state.getMass(), teme, parameters);
}
/** {@inheritDoc} */
@Override
public List<ParameterDriver> getParametersDrivers() {
return tle.getParametersDrivers();
}
}