KeplerianPropagatorBuilder.java

  1. /* Copyright 2002-2018 CS Systèmes d'Information
  2.  * Licensed to CS Systèmes d'Information (CS) under one or more
  3.  * contributor license agreements.  See the NOTICE file distributed with
  4.  * this work for additional information regarding copyright ownership.
  5.  * CS licenses this file to You under the Apache License, Version 2.0
  6.  * (the "License"); you may not use this file except in compliance with
  7.  * the License.  You may obtain a copy of the License at
  8.  *
  9.  *   http://www.apache.org/licenses/LICENSE-2.0
  10.  *
  11.  * Unless required by applicable law or agreed to in writing, software
  12.  * distributed under the License is distributed on an "AS IS" BASIS,
  13.  * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
  14.  * See the License for the specific language governing permissions and
  15.  * limitations under the License.
  16.  */
  17. package org.orekit.propagation.conversion;

  18. import org.orekit.errors.OrekitException;
  19. import org.orekit.orbits.Orbit;
  20. import org.orekit.orbits.PositionAngle;
  21. import org.orekit.propagation.Propagator;
  22. import org.orekit.propagation.analytical.KeplerianPropagator;

  23. /** Builder for Keplerian propagator.
  24.  * @author Pascal Parraud
  25.  * @since 6.0
  26.  */
  27. public class KeplerianPropagatorBuilder extends AbstractPropagatorBuilder {

  28.     /** Build a new instance.
  29.      * <p>
  30.      * The template orbit is used as a model to {@link
  31.      * #createInitialOrbit() create initial orbit}. It defines the
  32.      * inertial frame, the central attraction coefficient, the orbit type, and is also
  33.      * used together with the {@code positionScale} to convert from the {@link
  34.      * org.orekit.utils.ParameterDriver#setNormalizedValue(double) normalized} parameters used by the
  35.      * callers of this builder to the real orbital parameters.
  36.      * </p>
  37.      * @param templateOrbit reference orbit from which real orbits will be built
  38.      * @param positionAngle position angle type to use
  39.      * @param positionScale scaling factor used for orbital parameters normalization
  40.      * (typically set to the expected standard deviation of the position)
  41.      * @exception OrekitException if parameters drivers cannot be scaled
  42.      * @since 8.0
  43.      */
  44.     public KeplerianPropagatorBuilder(final Orbit templateOrbit, final PositionAngle positionAngle,
  45.                                       final double positionScale)
  46.         throws OrekitException {
  47.         super(templateOrbit, positionAngle, positionScale, true);
  48.     }

  49.     /** {@inheritDoc} */
  50.     public Propagator buildPropagator(final double[] normalizedParameters)
  51.         throws OrekitException {
  52.         setParameters(normalizedParameters);
  53.         return new KeplerianPropagator(createInitialOrbit());
  54.     }

  55. }