FieldDSSTZonalContext.java
- /* Copyright 2002-2025 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.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
- import org.orekit.frames.Frame;
- import org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements;
- import org.orekit.time.AbsoluteDate;
- /**
- * This class is a container for the common "field" parameters used in {@link DSSTZonal}.
- * <p>
- * It performs parameters initialization at each integration step for the Zonal contribution
- * to the central body gravitational perturbation.
- * </p>
- * @author Bryan Cazabonne
- * @since 10.0
- * @param <T> type of the field elements
- */
- public class FieldDSSTZonalContext<T extends CalculusFieldElement<T>> extends FieldDSSTGravityContext<T> {
- /** Χ³ = 1 / B³. */
- private final T chi3;
- // Short period terms
- /** h * k. */
- private T hk;
- /** k² - h². */
- private T k2mh2;
- /** (k² - h²) / 2. */
- private T k2mh2o2;
- /** 1 / (n² * a²). */
- private T oon2a2;
- /** 1 / (n² * a) . */
- private T oon2a;
- /** χ³ / (n² * a). */
- private T x3on2a;
- /** χ / (n² * a²). */
- private T xon2a2;
- /** (C * χ) / ( 2 * n² * a² ). */
- private T cxo2n2a2;
- /** (χ²) / (n² * a² * (χ + 1 ) ). */
- private T x2on2a2xp1;
- /** B * B. */
- private T BB;
- /** Constructor with central body frame equals orbit frame.
- *
- * @param auxiliaryElements auxiliary elements related to the current orbit
- * @param provider provider for spherical harmonics
- * @param parameters values of the force model parameters (only 1 values
- * for each parameters corresponding to state date) obtained by calling the extract
- * parameter method {@link #extractParameters(double[], AbsoluteDate)}
- * to selected the right value for state date or by getting the parameters for a specific date
- * @deprecated since 12.2 and issue 1104, should be removed in 13.0
- */
- @Deprecated
- FieldDSSTZonalContext(final FieldAuxiliaryElements<T> auxiliaryElements,
- final UnnormalizedSphericalHarmonicsProvider provider,
- final T[] parameters) {
- this(auxiliaryElements, auxiliaryElements.getFrame(), provider, parameters);
- }
- /** Constructor with central body frame potentially different from orbit frame.
- *
- * @param auxiliaryElements auxiliary elements related to the current orbit
- * @param centralBodyFrame rotating body frame
- * @param provider provider for spherical harmonics
- * @param parameters values of the force model parameters (only 1 values
- * for each parameters corresponding to state date) obtained by calling the extract
- * parameter method {@link #extractParameters(double[], AbsoluteDate)}
- * to selected the right value for state date or by getting the parameters for a specific date
- * @since 12.2
- */
- FieldDSSTZonalContext(final FieldAuxiliaryElements<T> auxiliaryElements,
- final Frame centralBodyFrame,
- final UnnormalizedSphericalHarmonicsProvider provider,
- final T[] parameters) {
- super(auxiliaryElements, centralBodyFrame, provider, parameters);
- // Chi3
- final T chi = getChi();
- this.chi3 = chi.multiply(getChi2());
- // Short period terms
- // -----
- // h * k.
- hk = auxiliaryElements.getH().multiply(auxiliaryElements.getK());
- // k² - h².
- k2mh2 = auxiliaryElements.getK().multiply(auxiliaryElements.getK()).subtract(auxiliaryElements.getH().multiply(auxiliaryElements.getH()));
- // (k² - h²) / 2.
- k2mh2o2 = k2mh2.divide(2.);
- // 1 / (n² * a²) = 1 / (n * A)
- oon2a2 = (getA().multiply(getMeanMotion())).reciprocal();
- // 1 / (n² * a) = a / (n * A)
- oon2a = auxiliaryElements.getSma().multiply(oon2a2);
- // χ³ / (n² * a)
- x3on2a = chi3.multiply(oon2a);
- // χ / (n² * a²)
- xon2a2 = chi.multiply(oon2a2);
- // (C * χ) / ( 2 * n² * a² )
- cxo2n2a2 = xon2a2.multiply(auxiliaryElements.getC()).divide(2.);
- // (χ²) / (n² * a² * (χ + 1 ) )
- x2on2a2xp1 = xon2a2.multiply(chi).divide(chi.add(1.));
- // B * B
- BB = auxiliaryElements.getB().multiply(auxiliaryElements.getB());
- }
- /** Getter for the Χ³.
- * @return the Χ³
- */
- public T getChi3() {
- return chi3;
- }
- /** Get h * k.
- * @return hk
- */
- public T getHK() {
- return hk;
- }
- /** Get k² - h².
- * @return k2mh2
- */
- public T getK2MH2() {
- return k2mh2;
- }
- /** Get (k² - h²) / 2.
- * @return k2mh2o2
- */
- public T getK2MH2O2() {
- return k2mh2o2;
- }
- /** Get 1 / (n² * a²).
- * @return oon2a2
- */
- public T getOON2A2() {
- return oon2a2;
- }
- /** Get χ³ / (n² * a).
- * @return x3on2a
- */
- public T getX3ON2A() {
- return x3on2a;
- }
- /** Get χ / (n² * a²).
- * @return xon2a2
- */
- public T getXON2A2() {
- return xon2a2;
- }
- /** Get (C * χ) / ( 2 * n² * a² ).
- * @return cxo2n2a2
- */
- public T getCXO2N2A2() {
- return cxo2n2a2;
- }
- /** Get (χ²) / (n² * a² * (χ + 1 ) ).
- * @return x2on2a2xp1
- */
- public T getX2ON2A2XP1() {
- return x2on2a2xp1;
- }
- /** Get B * B.
- * @return BB
- */
- public T getBB() {
- return BB;
- }
- }