DSSTNewtonianAttractionContext.java

  1. /* Copyright 2002-2023 CS GROUP
  2.  * Licensed to CS GROUP (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.semianalytical.dsst.forces;

  18. import org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements;

  19. /**
  20.  * This class is a container for the common parameters used in {@link DSSTNewtonianAttraction}.
  21.  * <p>
  22.  * It performs parameters initialization at each integration step for the central body attraction.
  23.  * </p>
  24.  * @author Bryan Cazabonne
  25.  * @since 10.0
  26.  */
  27. public class DSSTNewtonianAttractionContext extends ForceModelContext {

  28.     /** Standard gravitational parameter μ for the body in m³/s². */
  29.     private final double gm;

  30.     /**
  31.      * Simple constructor.
  32.      *
  33.      * @param auxiliaryElements auxiliary elements related to the current orbit
  34.      * @param parameters        values of the force model parameters
  35.      */
  36.     public DSSTNewtonianAttractionContext(final AuxiliaryElements auxiliaryElements, final double[] parameters) {

  37.         super(auxiliaryElements);
  38.         this.gm = parameters[0];
  39.     }

  40.     /** Get standard gravitational parameter μ for the body in m³/s².
  41.      * @return gm
  42.      */
  43.     public double getGM() {
  44.         return gm;
  45.     }
  46. }