EcksteinHechlerGradientConverter.java
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package org.orekit.propagation.analytical;
import java.util.Collections;
import java.util.List;
import org.hipparchus.analysis.differentiation.Gradient;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.utils.ParameterDriver;
/**
* Converter for Eckstein-Hechler propagator.
*
* @author Bryan Cazabonne
* @since 11.1
*/
class EcksteinHechlerGradientConverter extends AbstractAnalyticalGradientConverter {
/** Fixed dimension of the state. */
public static final int FREE_STATE_PARAMETERS = 6;
/** Orbit propagator. */
private final EcksteinHechlerPropagator propagator;
/** Simple constructor.
* @param propagator orbit propagator used to access initial orbit
*/
EcksteinHechlerGradientConverter(final EcksteinHechlerPropagator propagator) {
super(propagator, propagator.getMu(), FREE_STATE_PARAMETERS);
// Initialize fields
this.propagator = propagator;
}
/** {@inheritDoc} */
@Override
public FieldEcksteinHechlerPropagator<Gradient> getPropagator(final FieldSpacecraftState<Gradient> state,
final Gradient[] parameters) {
// Zero
final Gradient zero = state.getA().getField().getZero();
// Model parameters
final double[] ck0 = propagator.getCk0();
final double radius = propagator.getReferenceRadius();
final AttitudeProvider provider = propagator.getAttitudeProvider();
// Central attraction coefficient
final Gradient mu = zero.newInstance(propagator.getMu());
// Return the "Field" propagator
return new FieldEcksteinHechlerPropagator<>(state.getOrbit(), provider, radius, mu,
ck0[2], ck0[3], ck0[4], ck0[5], ck0[6]);
}
/** {@inheritDoc} */
@Override
public List<ParameterDriver> getParametersDrivers() {
return Collections.emptyList();
}
}