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    * 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
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    *
    *   http://www.apache.org/licenses/LICENSE-2.0
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   * Unless required by applicable law or agreed to in writing, software
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  package org.orekit.propagation.semianalytical.dsst.forces;
  
  import org.hipparchus.CalculusFieldElement;
  import org.hipparchus.util.FastMath;
  import org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider;
  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 FieldForceModelContext<T> {
  
      // Common factors for potential computation
      /** A = sqrt(μ * a). */
      private final T A;
      /** &Chi; = 1 / sqrt(1 - e²) = 1 / B. */
      private T X;
      /** &Chi;². */
      private T XX;
      /** &Chi;³. */
      private T XXX;
      /** 1 / (A * B) . */
      private T ooAB;
      /** B / A . */
      private T BoA;
      /** B / A(1 + B) . */
      private T BoABpo;
      /** -C / (2 * A * B) . */
      private T mCo2AB;
      /** -2 * a / A . */
      private T m2aoA;
      /** μ / a . */
      private T muoa;
      /** R / a . */
      private T roa;
  
      /** Keplerian mean motion. */
      private final T n;
  
      // 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;
  
      /**
       * Simple constructor.
       *
       * @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
       */
      FieldDSSTZonalContext(final FieldAuxiliaryElements<T> auxiliaryElements,
                                   final UnnormalizedSphericalHarmonicsProvider provider,
                                   final T[] parameters) {
  
         super(auxiliaryElements);
 
         final T mu = parameters[0];
 
         // Keplerian mean motion
         final T absA = FastMath.abs(auxiliaryElements.getSma());
         n = FastMath.sqrt(mu.divide(absA)).divide(absA);
 
         A = FastMath.sqrt(mu.multiply(auxiliaryElements.getSma()));
 
         // &Chi; = 1 / B
         X = auxiliaryElements.getB().reciprocal();
         XX = X.square();
         XXX = X.multiply(XX);
 
         // 1 / AB
         ooAB = (A.multiply(auxiliaryElements.getB())).reciprocal();
         // B / A
         BoA = auxiliaryElements.getB().divide(A);
         // -C / 2AB
         mCo2AB = auxiliaryElements.getC().multiply(ooAB).divide(2.).negate();
         // B / A(1 + B)
         BoABpo = BoA.divide(auxiliaryElements.getB().add(1.));
         // -2 * a / A
         m2aoA = auxiliaryElements.getSma().divide(A).multiply(2.).negate();
         // μ / a
         muoa = mu.divide(auxiliaryElements.getSma());
         // R / a
         roa = auxiliaryElements.getSma().divide(provider.getAe()).reciprocal();
 
         // 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 = (A.multiply(n)).reciprocal();
         // 1 / (n² * a) = a / (n * A)
         oon2a = auxiliaryElements.getSma().multiply(oon2a2);
         // χ³ / (n² * a)
         x3on2a = XXX.multiply(oon2a);
         // χ / (n² * a²)
         xon2a2 = X.multiply(oon2a2);
         // (C * χ) / ( 2 * n² * a² )
         cxo2n2a2 = xon2a2.multiply(auxiliaryElements.getC()).divide(2.);
         // (χ²) / (n² * a² * (χ + 1 ) )
         x2on2a2xp1 = xon2a2.multiply(X).divide(X.add(1.));
         // B * B
         BB = auxiliaryElements.getB().multiply(auxiliaryElements.getB());
 
     }
 
     /** Get &Chi; = 1 / sqrt(1 - e²) = 1 / B.
      * @return &Chi;
      */
     public T getX() {
         return X;
     }
 
     /** Get &Chi;².
      * @return &Chi;².
      */
     public T getXX() {
         return XX;
     }
 
     /** Get &Chi;³.
      * @return &Chi;³
      */
     public T getXXX() {
         return XXX;
     }
 
     /** Get m2aoA = -2 * a / A.
      * @return m2aoA
      */
     public T getM2aoA() {
         return m2aoA;
     }
 
     /** Get B / A.
      * @return BoA
      */
     public T getBoA() {
         return BoA;
     }
 
     /** Get ooAB = 1 / (A * B).
      * @return ooAB
      */
     public T getOoAB() {
         return ooAB;
     }
 
     /** Get mCo2AB = -C / 2AB.
      * @return mCo2AB
      */
     public T getMCo2AB() {
         return mCo2AB;
     }
 
     /** Get BoABpo = B / A(1 + B).
      * @return BoABpo
      */
     public T getBoABpo() {
         return BoABpo;
     }
 
     /** Get μ / a .
      * @return muoa
      */
     public T getMuoa() {
         return muoa;
     }
 
     /** Get roa = R / a.
      * @return roa
      */
     public T getRoa() {
         return roa;
     }
 
     /** Get the Keplerian mean motion.
      * <p>The Keplerian mean motion is computed directly from semi major axis
      * and central acceleration constant.</p>
      * @return Keplerian mean motion in radians per second
      */
     public T getMeanMotion() {
         return n;
     }
 
     /** 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;
     }
 
 }