DSSTZonalContext.java
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package org.orekit.propagation.semianalytical.dsst.forces;
import org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
import org.orekit.frames.Frame;
import org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements;
/**
* This class is a container for the common 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
*/
public class DSSTZonalContext extends DSSTGravityContext {
/** Χ³ = 1 / B³. */
private final double chi3;
// Short period terms
/** h * k. */
private double hk;
/** k² - h². */
private double k2mh2;
/** (k² - h²) / 2. */
private double k2mh2o2;
/** 1 / (n² * a²). */
private double oon2a2;
/** 1 / (n² * a) . */
private double oon2a;
/** χ³ / (n² * a). */
private double x3on2a;
/** χ / (n² * a²). */
private double xon2a2;
/** (C * χ) / ( 2 * n² * a² ). */
private double cxo2n2a2;
/** (χ²) / (n² * a² * (χ + 1 ) ). */
private double x2on2a2xp1;
/** B * B. */
private double BB;
/**
* Constructor with central body frame potentially different than orbit frame.
*
* @param auxiliaryElements auxiliary elements related to the current orbit
* @param bodyFixedFrame rotating body frame
* @param provider provider for spherical harmonics
* @param parameters values of the force model parameters
* @since 12.2
*/
DSSTZonalContext(final AuxiliaryElements auxiliaryElements,
final Frame bodyFixedFrame,
final UnnormalizedSphericalHarmonicsProvider provider,
final double[] parameters) {
super(auxiliaryElements, bodyFixedFrame, provider, parameters);
// Chi3
final double chi = getChi();
this.chi3 = chi * getChi2();
// Short period terms
// -----
// h * k.
hk = auxiliaryElements.getH() * auxiliaryElements.getK();
// k² - h².
k2mh2 = auxiliaryElements.getK() * auxiliaryElements.getK() - auxiliaryElements.getH() * auxiliaryElements.getH();
// (k² - h²) / 2.
k2mh2o2 = k2mh2 / 2.;
// 1 / (n² * a²) = 1 / (n * A)
oon2a2 = 1 / (getA() * getMeanMotion());
// 1 / (n² * a) = a / (n * A)
oon2a = auxiliaryElements.getSma() * oon2a2;
// χ³ / (n² * a)
x3on2a = chi3 * oon2a;
// χ / (n² * a²)
xon2a2 = getChi() * oon2a2;
// (C * χ) / ( 2 * n² * a² )
cxo2n2a2 = xon2a2 * auxiliaryElements.getC() / 2;
// (χ²) / (n² * a² * (χ + 1 ) )
x2on2a2xp1 = xon2a2 * chi / (chi + 1);
// B * B
BB = auxiliaryElements.getB() * auxiliaryElements.getB();
}
/** Getter for the Χ³.
* @return the Χ³
*/
public double getChi3() {
return chi3;
}
/** Get h * k.
* @return hk
*/
public double getHK() {
return hk;
}
/** Get k² - h².
* @return k2mh2
*/
public double getK2MH2() {
return k2mh2;
}
/** Get (k² - h²) / 2.
* @return k2mh2o2
*/
public double getK2MH2O2() {
return k2mh2o2;
}
/** Get 1 / (n² * a²).
* @return oon2a2
*/
public double getOON2A2() {
return oon2a2;
}
/** Get χ³ / (n² * a).
* @return x3on2a
*/
public double getX3ON2A() {
return x3on2a;
}
/** Get χ / (n² * a²).
* @return xon2a2
*/
public double getXON2A2() {
return xon2a2;
}
/** Get (C * χ) / ( 2 * n² * a² ).
* @return cxo2n2a2
*/
public double getCXO2N2A2() {
return cxo2n2a2;
}
/** Get (χ²) / (n² * a² * (χ + 1 ) ).
* @return x2on2a2xp1
*/
public double getX2ON2A2XP1() {
return x2on2a2xp1;
}
/** Get B * B.
* @return BB
*/
public double getBB() {
return BB;
}
}