FieldDSSTNewtonianAttractionContext.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.hipparchus.CalculusFieldElement;
  19. import org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements;

  20. /**
  21.  * This class is a container for the common "field" parameters used in {@link DSSTNewtonianAttraction}.
  22.  * <p>
  23.  * It performs parameters initialization at each integration step for the central body attraction.
  24.  * </p>
  25.  * @author Bryan Cazabonne
  26.  * @since 10.0
  27.  * @param <T> type of the field elements
  28.  */
  29. public class FieldDSSTNewtonianAttractionContext<T extends CalculusFieldElement<T>> extends FieldForceModelContext<T> {

  30.     /** Standard gravitational parameter μ for the body in m³/s². */
  31.     private final T gm;

  32.     /**
  33.      * Simple constructor.
  34.      *
  35.      * @param auxiliaryElements auxiliary elements related to the current orbit
  36.      * @param parameters        values of the force model parameters
  37.      */
  38.     FieldDSSTNewtonianAttractionContext(final FieldAuxiliaryElements<T> auxiliaryElements, final T[] parameters) {

  39.         super(auxiliaryElements);
  40.         this.gm = parameters[0];
  41.     }

  42.     /** Get standard gravitational parameter μ for the body in m³/s².
  43.      * @return gm
  44.      */
  45.     public T getGM() {
  46.         return gm;
  47.     }
  48. }