KeplerianPropagatorBuilder.java
- /* Copyright 2002-2018 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 org.orekit.errors.OrekitException;
- import org.orekit.orbits.Orbit;
- import org.orekit.orbits.PositionAngle;
- import org.orekit.propagation.Propagator;
- import org.orekit.propagation.analytical.KeplerianPropagator;
- /** Builder for Keplerian propagator.
- * @author Pascal Parraud
- * @since 6.0
- */
- public class KeplerianPropagatorBuilder extends AbstractPropagatorBuilder {
- /** Build a new instance.
- * <p>
- * The template orbit is used as a model to {@link
- * #createInitialOrbit() create initial orbit}. It defines the
- * inertial frame, the central attraction coefficient, the orbit type, and is also
- * used together with the {@code positionScale} to convert from the {@link
- * org.orekit.utils.ParameterDriver#setNormalizedValue(double) normalized} parameters used by the
- * callers of this builder to the real orbital parameters.
- * </p>
- * @param templateOrbit reference orbit from which real orbits will be built
- * @param positionAngle position angle type to use
- * @param positionScale scaling factor used for orbital parameters normalization
- * (typically set to the expected standard deviation of the position)
- * @exception OrekitException if parameters drivers cannot be scaled
- * @since 8.0
- */
- public KeplerianPropagatorBuilder(final Orbit templateOrbit, final PositionAngle positionAngle,
- final double positionScale)
- throws OrekitException {
- super(templateOrbit, positionAngle, positionScale, true);
- }
- /** {@inheritDoc} */
- public Propagator buildPropagator(final double[] normalizedParameters)
- throws OrekitException {
- setParameters(normalizedParameters);
- return new KeplerianPropagator(createInitialOrbit());
- }
- }