EcksteinHechlerPropagatorBuilder.java
/* Copyright 2002-2013 CS Systèmes d'Information
* Licensed to CS Systèmes d'Information (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package org.orekit.propagation.conversion;
import java.util.ArrayList;
import java.util.Collection;
import org.apache.commons.math3.exception.util.LocalizedFormats;
import org.apache.commons.math3.geometry.euclidean.threed.Vector3D;
import org.apache.commons.math3.ode.AbstractParameterizable;
import org.orekit.errors.OrekitException;
import org.orekit.forces.gravity.potential.GravityFieldFactory;
import org.orekit.forces.gravity.potential.TideSystem;
import org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
import org.orekit.frames.Frame;
import org.orekit.orbits.CircularOrbit;
import org.orekit.propagation.Propagator;
import org.orekit.propagation.analytical.EcksteinHechlerPropagator;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.PVCoordinates;
/** Builder for Eckstein-Hechler propagator.
* @author Pascal Parraud
* @since 6.0
*/
public class EcksteinHechlerPropagatorBuilder extends AbstractParameterizable
implements PropagatorBuilder {
/** Provider for un-normalized coefficients. */
private final UnnormalizedSphericalHarmonicsProvider provider;
/** Frame in which the orbit is propagated. */
private final Frame frame;
/** List of the free parameters names. */
private Collection<String> freeParameters;
/** Build a new instance.
* @param frame the frame in which the orbit is propagated
* (<em>must</em> be a {@link Frame#isPseudoInertial pseudo-inertial frame})
* @param provider for un-normalized zonal coefficients
*/
public EcksteinHechlerPropagatorBuilder(final Frame frame,
final UnnormalizedSphericalHarmonicsProvider provider) {
this.frame = frame;
this.provider = provider;
}
/** Build a new instance.
* @param frame the frame in which the orbit is propagated
* (<em>must</em> be a {@link Frame#isPseudoInertial pseudo-inertial frame})
* @param referenceRadius reference radius of the Earth for the potential model (m)
* @param mu central attraction coefficient (m<sup>3</sup>/s<sup>2</sup>)
* @param tideSystem tide system
* @param c20 un-normalized zonal coefficient (about -1.08e-3 for Earth)
* @param c30 un-normalized zonal coefficient (about +2.53e-6 for Earth)
* @param c40 un-normalized zonal coefficient (about +1.62e-6 for Earth)
* @param c50 un-normalized zonal coefficient (about +2.28e-7 for Earth)
* @param c60 un-normalized zonal coefficient (about -5.41e-7 for Earth)
*/
public EcksteinHechlerPropagatorBuilder(final Frame frame,
final double referenceRadius,
final double mu,
final TideSystem tideSystem,
final double c20,
final double c30,
final double c40,
final double c50,
final double c60) {
this(frame,
GravityFieldFactory.getUnnormalizedProvider(referenceRadius, mu, tideSystem,
new double[][] {
{
0
}, {
0
}, {
c20
}, {
c30
}, {
c40
}, {
c50
}, {
c60
}
}, new double[][] {
{
0
}, {
0
}, {
0
}, {
0
}, {
0
}, {
0
}, {
0
}
}));
}
/** {@inheritDoc} */
public Propagator buildPropagator(final AbsoluteDate date, final double[] parameters)
throws OrekitException {
if (parameters.length != (freeParameters.size() + 6)) {
throw OrekitException.createIllegalArgumentException(LocalizedFormats.DIMENSIONS_MISMATCH);
}
final CircularOrbit orb = new CircularOrbit(new PVCoordinates(new Vector3D(parameters[0],
parameters[1],
parameters[2]),
new Vector3D(parameters[3],
parameters[4],
parameters[5])),
frame, date, provider.getMu());
return new EcksteinHechlerPropagator(orb, provider);
}
/** {@inheritDoc} */
public Frame getFrame() {
return frame;
}
/** {@inheritDoc} */
public void setFreeParameters(final Collection<String> parameters)
throws IllegalArgumentException {
freeParameters = new ArrayList<String>();
for (String name : parameters) {
complainIfNotSupported(name);
}
freeParameters.addAll(parameters);
}
/** {@inheritDoc} */
public double getParameter(final String name)
throws IllegalArgumentException {
return 0;
}
/** {@inheritDoc} */
public void setParameter(final String name, final double value)
throws IllegalArgumentException {
}
}