DSSTNewtonianAttractionContext.java
- /* Copyright 2002-2023 CS GROUP
- * Licensed to CS GROUP (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.semianalytical.dsst.forces;
- import org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements;
- /**
- * This class is a container for the common parameters used in {@link DSSTNewtonianAttraction}.
- * <p>
- * It performs parameters initialization at each integration step for the central body attraction.
- * </p>
- * @author Bryan Cazabonne
- * @since 10.0
- */
- public class DSSTNewtonianAttractionContext extends ForceModelContext {
- /** Standard gravitational parameter μ for the body in m³/s². */
- private final double gm;
- /**
- * Simple constructor.
- *
- * @param auxiliaryElements auxiliary elements related to the current orbit
- * @param parameters values of the force model parameters
- */
- public DSSTNewtonianAttractionContext(final AuxiliaryElements auxiliaryElements, final double[] parameters) {
- super(auxiliaryElements);
- this.gm = parameters[0];
- }
- /** Get standard gravitational parameter μ for the body in m³/s².
- * @return gm
- */
- public double getGM() {
- return gm;
- }
- }