FieldDSSTZonalContext.java
/* Copyright 2002-2024 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;
}
}