KeplerianPropagatorBuilder.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.frames.Frame;
- import org.orekit.orbits.KeplerianOrbit;
- import org.orekit.propagation.Propagator;
- import org.orekit.propagation.analytical.KeplerianPropagator;
- import org.orekit.time.AbsoluteDate;
- import org.orekit.utils.PVCoordinates;
- /** Builder for Keplerian propagator.
- * @author Pascal Parraud
- * @since 6.0
- */
- public class KeplerianPropagatorBuilder extends AbstractParameterizable
- implements PropagatorBuilder {
- /** Central attraction coefficient (m<sup>3</sup>/s<sup>2</sup>). */
- private final double mu;
- /** 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 mu central attraction coefficient (m<sup>3</sup>/s<sup>2</sup>)
- * @param frame the frame in which the orbit is propagated
- * (<em>must</em> be a {@link Frame#isPseudoInertial pseudo-inertial frame})
- */
- public KeplerianPropagatorBuilder(final double mu,
- final Frame frame) {
- this.mu = mu;
- this.frame = frame;
- }
- /** {@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 KeplerianOrbit orb = new KeplerianOrbit(new PVCoordinates(new Vector3D(parameters[0],
- parameters[1],
- parameters[2]),
- new Vector3D(parameters[3],
- parameters[4],
- parameters[5])),
- frame, date, mu);
- return new KeplerianPropagator(orb);
- }
- /** {@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 {
- }
- }