FieldDSSTNewtonianAttractionContext.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.hipparchus.CalculusFieldElement;
import org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements;
/**
* This class is a container for the common "field" 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
* @param <T> type of the field elements
*/
public class FieldDSSTNewtonianAttractionContext<T extends CalculusFieldElement<T>> extends FieldForceModelContext<T> {
/** Standard gravitational parameter μ for the body in m³/s². */
private final T gm;
/**
* Simple constructor.
*
* @param auxiliaryElements auxiliary elements related to the current orbit
* @param parameters values of the force model parameters
*/
FieldDSSTNewtonianAttractionContext(final FieldAuxiliaryElements<T> auxiliaryElements, final T[] parameters) {
super(auxiliaryElements);
this.gm = parameters[0];
}
/** Get standard gravitational parameter μ for the body in m³/s².
* @return gm
*/
public T getGM() {
return gm;
}
}