FixedPointTleGenerationAlgorithm.java
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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.generation;
import org.hipparchus.CalculusFieldElement;
import org.orekit.annotation.DefaultDataContext;
import org.orekit.data.DataContext;
import org.orekit.frames.Frame;
import org.orekit.orbits.FieldKeplerianOrbit;
import org.orekit.orbits.KeplerianOrbit;
import org.orekit.orbits.OrbitType;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.analytical.tle.FieldTLE;
import org.orekit.propagation.analytical.tle.TLE;
import org.orekit.propagation.conversion.osc2mean.FixedPointConverter;
import org.orekit.propagation.conversion.osc2mean.TLETheory;
import org.orekit.time.TimeScale;
import org.orekit.utils.ParameterDriver;
/**
* Fixed Point method to reverse SGP4 and SDP4 propagation algorithm
* and generate a usable TLE from a spacecraft state.
* <p>
* Using this algorithm, the B* value is not computed. In other words,
* the B* value from the template TLE is set to the generated one.
* </p>
* @author Thomas Paulet
* @author Bryan Cazabonne
* @since 12.0
*/
public class FixedPointTleGenerationAlgorithm implements TleGenerationAlgorithm {
/** Default value for epsilon. */
public static final double EPSILON_DEFAULT = 1.0e-10;
/** Default value for maxIterations. */
public static final int MAX_ITERATIONS_DEFAULT = 100;
/** Default value for scale. */
public static final double SCALE_DEFAULT = 1.0;
/** Osculating to mean orbit converter. */
private final FixedPointConverter converter;
/** UTC time scale. */
private final TimeScale utc;
/**
* Default constructor.
* <p>
* Uses the {@link DataContext#getDefault() default data context}
* as well as {@link #EPSILON_DEFAULT}, {@link #MAX_ITERATIONS_DEFAULT},
* {@link #SCALE_DEFAULT} for method convergence.
* </p>
*/
@DefaultDataContext
public FixedPointTleGenerationAlgorithm() {
this(EPSILON_DEFAULT, MAX_ITERATIONS_DEFAULT, SCALE_DEFAULT);
}
/**
* Constructor.
* <p>
* Uses the {@link DataContext#getDefault() default data context}.
* </p>
* @param epsilon used to compute threshold for convergence check
* @param maxIterations maximum number of iterations for convergence
* @param scale scale factor of the Fixed Point algorithm
*/
@DefaultDataContext
public FixedPointTleGenerationAlgorithm(final double epsilon,
final int maxIterations,
final double scale) {
this(epsilon, maxIterations, scale,
DataContext.getDefault().getTimeScales().getUTC(),
DataContext.getDefault().getFrames().getTEME());
}
/**
* Constructor.
* @param epsilon used to compute threshold for convergence check
* @param maxIterations maximum number of iterations for convergence
* @param scale scale factor of the Fixed Point algorithm
* @param utc UTC time scale
* @param teme TEME frame
*/
public FixedPointTleGenerationAlgorithm(final double epsilon,
final int maxIterations,
final double scale,
final TimeScale utc,
final Frame teme) {
this.converter = new FixedPointConverter(new TLETheory(utc, teme),
epsilon,
maxIterations,
scale);
this.utc = utc;
}
/** {@inheritDoc} */
@Override
public TLE generate(final SpacecraftState state, final TLE templateTLE) {
final KeplerianOrbit mean = (KeplerianOrbit) OrbitType.KEPLERIAN.convertType(converter.convertToMean(state.getOrbit()));
final TLE tle = TleGenerationUtil.newTLE(mean, templateTLE, templateTLE.getBStar(mean.getDate()), utc);
// reset estimated parameters from template to generated tle
for (final ParameterDriver templateDrivers : templateTLE.getParametersDrivers()) {
if (templateDrivers.isSelected()) {
// set to selected for the new TLE
tle.getParameterDriver(templateDrivers.getName()).setSelected(true);
}
}
return tle;
}
/** {@inheritDoc} */
@Override
public <T extends CalculusFieldElement<T>> FieldTLE<T> generate(final FieldSpacecraftState<T> state,
final FieldTLE<T> templateTLE) {
final T bStar = state.getMass().getField().getZero().newInstance(templateTLE.getBStar());
final FieldKeplerianOrbit<T> mean = (FieldKeplerianOrbit<T>) OrbitType.KEPLERIAN.convertType(converter.convertToMean(state.getOrbit()));
final FieldTLE<T> tle = TleGenerationUtil.newTLE(mean, templateTLE, bStar, utc);
// reset estimated parameters from template to generated tle
for (final ParameterDriver templateDrivers : templateTLE.getParametersDrivers()) {
if (templateDrivers.isSelected()) {
// set to selected for the new TLE
tle.getParameterDriver(templateDrivers.getName()).setSelected(true);
}
}
return tle;
}
}