/* Contributed in the public domain.
    * Licensed to CS Systèmes d'Information (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.models.earth;
  
  import org.hipparchus.Field;
  import org.hipparchus.RealFieldElement;
  import org.hipparchus.analysis.RealFieldUnivariateFunction;
  import org.hipparchus.analysis.UnivariateFunction;
  import org.hipparchus.analysis.solvers.AllowedSolution;
  import org.hipparchus.analysis.solvers.BracketingNthOrderBrentSolver;
  import org.hipparchus.analysis.solvers.FieldBracketingNthOrderBrentSolver;
  import org.hipparchus.analysis.solvers.UnivariateSolver;
  import org.hipparchus.exception.MathRuntimeException;
  import org.hipparchus.geometry.euclidean.threed.FieldLine;
  import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
  import org.hipparchus.geometry.euclidean.threed.Line;
  import org.hipparchus.geometry.euclidean.threed.Vector3D;
  import org.hipparchus.util.FastMath;
  import org.orekit.bodies.FieldGeodeticPoint;
  import org.orekit.bodies.GeodeticPoint;
  import org.orekit.errors.OrekitException;
  import org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel;
  import org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider;
  import org.orekit.forces.gravity.potential.TideSystem;
  import org.orekit.frames.FieldTransform;
  import org.orekit.frames.Frame;
  import org.orekit.frames.Transform;
  import org.orekit.time.AbsoluteDate;
  import org.orekit.time.FieldAbsoluteDate;
  import org.orekit.utils.TimeStampedPVCoordinates;
  
  /**
   * A geoid is a level surface of the gravity potential of a body. The gravity
   * potential, W, is split so W = U + T, where U is the normal potential (defined
   * by the ellipsoid) and T is the anomalous potential.[3](eq. 2-137)
   *
   * <p> The {@link #getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate)}
   * method is tailored specifically for Earth's geoid. All of the other methods
   * in this class are general and will work for an arbitrary body.
   *
   * <p> There are several components that are needed to define a geoid[1]:
   *
   * <ul> <li>Geopotential field. These are the coefficients of the spherical
   * harmonics: S<sub>n,m</sub> and C<sub>n,m</sub></li>
   *
   * <li>Reference Ellipsoid. The ellipsoid is used to define the undulation of
   * the geoid (distance between ellipsoid and geoid) and U<sub>0</sub> the value
   * of the normal gravity potential at the surface of the ellipsoid.</li>
   *
   * <li>W<sub>0</sub>, the potential at the geoid. The value of the potential on
   * the level surface. This is taken to be U<sub>0</sub>, the normal gravity
   * potential at the surface of the {@link ReferenceEllipsoid}.</li>
   *
   * <li>Permanent Tide System. This implementation assumes that the geopotential
   * field and the reference ellipsoid use the same permanent tide system. If the
   * assumption is false it will produce errors of about 0.5 m. Conversion between
   * tide systems is a possible improvement.[1,2]</li>
   *
   * <li>Topographic Masses. That is mass outside of the geoid, e.g. mountains.
   * This implementation ignores topographic masses, which causes up to 3m error
   * in the Himalayas, and ~ 1.5m error in the Rockies. This could be improved
   * through the use of DTED and calculating height anomalies or using the
   * correction coefficients.[1]</li> </ul>
   *
   * <p> This implementation also assumes that the normal to the reference
   * ellipsoid is the same as the normal to the geoid. This assumption enables the
   * equation: (height above geoid) = (height above ellipsoid) - (undulation),
   * which is used in {@link #transform(GeodeticPoint)} and {@link
   * #transform(Vector3D, Frame, AbsoluteDate)}.
   *
   * <p> In testing, the error in the undulations calculated by this class were
   * off by less than 3 meters, which matches the assumptions outlined above.
   *
   * <p> References:
   *
   * <ol> <li>Dru A. Smith. There is no such thing as "The" EGM96 geoid: Subtle
   * points on the use of a global geopotential model. IGeS Bulletin No. 8:17-28,
   * 1998. <a href= "http://www.ngs.noaa.gov/PUBS_LIB/EGM96_GEOID_PAPER/egm96_geoid_paper.html"
   * >http ://www.ngs.noaa.gov/PUBS_LIB/EGM96_GEOID_PAPER/egm96_geoid_paper.html</a></li>
   *
   * <li> Martin Losch, Verena Seufer. How to Compute Geoid Undulations (Geoid
   * Height Relative to a Given Reference Ellipsoid) from Spherical Harmonic
   * Coefficients for Satellite Altimetry Applications. , 2003. <a
   * href="http://mitgcm.org/~mlosch/geoidcookbook.pdf">mitgcm.org/~mlosch/geoidcookbook.pdf</a>
   * </li>
  *
  * <li>Weikko A. Heiskanen, Helmut Moritz. Physical Geodesy. W. H. Freeman and
  * Company, 1967. (especially sections 2.13 and equation 2-144 Bruns
  * Formula)</li>
  *
  * <li>S. A. Holmes, W. E. Featherstone. A unified approach to the Clenshaw
  * summation and the recursive computation of very high degree and order
  * normalised associated Legendre functions. Journal of Geodesy, 76(5):279,
  * 2002.</li>
  *
  * <li>DMA TR 8350.2. 1984.</li>
  *
  * <li>Department of Defense World Geodetic System 1984. 2000. NIMA TR 8350.2
  * Third Edition, Amendment 1.</li> </ol>
  *
  * @author Evan Ward
  */
 public class Geoid implements EarthShape {
 
     /**
      * uid is date of last modification.
      */
     private static final long serialVersionUID = 20150312L;
 
     /**
      * A number larger than the largest undulation. Wikipedia says the geoid
      * height is in [-106, 85]. I chose 100 to be safe.
      */
     private static final double MAX_UNDULATION = 100;
     /**
      * A number smaller than the smallest undulation. Wikipedia says the geoid
      * height is in [-106, 85]. I chose -150 to be safe.
      */
     private static final double MIN_UNDULATION = -150;
     /**
      * the maximum number of evaluations for the line search in {@link
      * #getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate)}.
      */
     private static final int MAX_EVALUATIONS = 100;
 
     /**
      * the default date to use when evaluating the {@link #harmonics}. Used when
      * no other dates are available. Should be removed in a future release.
      */
     private final AbsoluteDate defaultDate;
     /**
      * the reference ellipsoid.
      */
     private final ReferenceEllipsoid referenceEllipsoid;
     /**
      * the geo-potential combined with an algorithm for evaluating the spherical
      * harmonics. The Holmes and Featherstone method is very robust.
      */
     private final transient HolmesFeatherstoneAttractionModel harmonics;
 
     /**
      * Creates a geoid from the given geopotential, reference ellipsoid and the
      * assumptions in the comment for {@link Geoid}.
      *
      * @param geopotential       the gravity potential. Only the anomalous
      *                           potential will be used. It is assumed that the
      *                           {@code geopotential} and the {@code
      *                           referenceEllipsoid} are defined in the same
      *                           frame. Usually a {@link org.orekit.forces.gravity.potential.GravityFieldFactory#getConstantNormalizedProvider(int,
      *                           int) constant geopotential} is used to define a
      *                           time-invariant Geoid.
      * @param referenceEllipsoid the normal gravity potential.
      * @throws NullPointerException if {@code geopotential == null ||
      *                              referenceEllipsoid == null}
      */
     public Geoid(final NormalizedSphericalHarmonicsProvider geopotential,
                  final ReferenceEllipsoid referenceEllipsoid) {
         // parameter check
         if (geopotential == null || referenceEllipsoid == null) {
             throw new NullPointerException();
         }
 
         // subtract the ellipsoid from the geopotential
         final SubtractEllipsoid potential = new SubtractEllipsoid(geopotential,
                 referenceEllipsoid);
 
         // set instance parameters
         this.referenceEllipsoid = referenceEllipsoid;
         this.harmonics = new HolmesFeatherstoneAttractionModel(
                 referenceEllipsoid.getBodyFrame(), potential);
         this.defaultDate = geopotential.getReferenceDate();
     }
 
     @Override
     public Frame getBodyFrame() {
         // same as for reference ellipsoid.
         return this.getEllipsoid().getBodyFrame();
     }
 
     /**
      * Gets the Undulation of the Geoid, N at the given position. N is the
      * distance between the {@link #getEllipsoid() reference ellipsoid} and the
      * geoid. The latitude and longitude parameters are both defined with
      * respect to the reference ellipsoid. For EGM96 and the WGS84 ellipsoid the
      * undulation is between -107m and +86m.
      *
      * <p> NOTE: Restrictions are not put on the range of the arguments {@code
      * geodeticLatitude} and {@code longitude}.
      *
      * @param geodeticLatitude geodetic latitude (angle between the local normal
      *                         and the equatorial plane on the reference
      *                         ellipsoid), in radians.
      * @param longitude        on the reference ellipsoid, in radians.
      * @param date             of evaluation. Used for time varying geopotential
      *                         fields.
      * @return the undulation in m, positive means the geoid is higher than the
      * ellipsoid.
      * @see Geoid
      * @see <a href="http://en.wikipedia.org/wiki/Geoid">Geoid on Wikipedia</a>
      */
     public double getUndulation(final double geodeticLatitude,
                                 final double longitude,
                                 final AbsoluteDate date) {
         /*
          * equations references are to the algorithm printed in the geoid
          * cookbook[2]. See comment for Geoid.
          */
         // reference ellipsoid
         final ReferenceEllipsoid ellipsoid = this.getEllipsoid();
 
         // position in geodetic coordinates
         final GeodeticPoint.html#GeodeticPoint">GeodeticPoint gp = new GeodeticPoint(geodeticLatitude, longitude, 0);
         // position in Cartesian coordinates, is converted to geocentric lat and
         // lon in the Holmes and Featherstone class
         final Vector3D position = ellipsoid.transform(gp);
 
         // get normal gravity from ellipsoid, eq 15
         final double normalGravity = ellipsoid
                 .getNormalGravity(geodeticLatitude);
 
         // calculate disturbing potential, T, eq 30.
         final double mu = this.harmonics.getMu();
         final double T  = this.harmonics.nonCentralPart(date, position, mu);
         // calculate undulation, eq 30
         return T / normalGravity;
     }
 
     @Override
     public ReferenceEllipsoid getEllipsoid() {
         return this.referenceEllipsoid;
     }
 
     /**
      * This class implements equations 20-24 in the geoid cook book.(Losch and
      * Seufer) It modifies C<sub>2n,0</sub> where n = 1,2,...,5.
      *
      * @see "DMA TR 8350.2. 1984."
      */
     private static final class SubtractEllipsoid implements
             NormalizedSphericalHarmonicsProvider {
         /**
          * provider of the fully normalized coefficients, includes the reference
          * ellipsoid.
          */
         private final NormalizedSphericalHarmonicsProvider provider;
         /**
          * the reference ellipsoid to subtract from {@link #provider}.
          */
         private final ReferenceEllipsoid ellipsoid;
 
         /**
          * @param provider  potential used for GM<sub>g</sub> and a<sub>g</sub>,
          *                  and of course the coefficients Cnm, and Snm.
          * @param ellipsoid Used to calculate the fully normalized
          *                  J<sub>2n</sub>
          */
         private SubtractEllipsoid(
                 final NormalizedSphericalHarmonicsProvider provider,
                 final ReferenceEllipsoid ellipsoid) {
             super();
             this.provider = provider;
             this.ellipsoid = ellipsoid;
         }
 
         @Override
         public int getMaxDegree() {
             return this.provider.getMaxDegree();
         }
 
         @Override
         public int getMaxOrder() {
             return this.provider.getMaxOrder();
         }
 
         @Override
         public double getMu() {
             return this.provider.getMu();
         }
 
         @Override
         public double getAe() {
             return this.provider.getAe();
         }
 
         @Override
         public AbsoluteDate getReferenceDate() {
             return this.provider.getReferenceDate();
         }
 
         @Override
         public double getOffset(final AbsoluteDate date) {
             return this.provider.getOffset(date);
         }
 
         @Override
         public NormalizedSphericalHarmonics onDate(final AbsoluteDate date) {
             return new NormalizedSphericalHarmonics() {
 
                 /** the original harmonics */
                 private final NormalizedSphericalHarmonics delegate = provider.onDate(date);
 
                 @Override
                 public double getNormalizedCnm(final int n, final int m) {
                     return getCorrectedCnm(n, m, this.delegate.getNormalizedCnm(n, m));
                 }
 
                 @Override
                 public double getNormalizedSnm(final int n, final int m) {
                     return this.delegate.getNormalizedSnm(n, m);
                 }
 
                 @Override
                 public AbsoluteDate getDate() {
                     return date;
                 }
             };
         }
 
         /**
          * Get the corrected Cnm for different GM or a values.
          *
          * @param n              degree
          * @param m              order
          * @param uncorrectedCnm uncorrected Cnm coefficient
          * @return the corrected Cnm coefficient.
          */
         private double getCorrectedCnm(final int n,
                                        final int m,
                                        final double uncorrectedCnm) {
             double Cnm = uncorrectedCnm;
             // n = 2,4,6,8, or 10 and m = 0
             if (m == 0 && n <= 10 && n % 2 == 0 && n > 0) {
                 // correction factor for different GM and a, 1 if no difference
                 final double gmRatio = this.ellipsoid.getGM() / this.getMu();
                 final double aRatio = this.ellipsoid.getEquatorialRadius() /
                         this.getAe();
                 /*
                  * eq 20 in the geoid cook book[2], with eq 3-61 in chapter 3 of
                  * DMA TR 8350.2
                  */
                 // halfN = 1,2,3,4,5 for n = 2,4,6,8,10, respectively
                 final int halfN = n / 2;
                 Cnm = Cnm - gmRatio * FastMath.pow(aRatio, halfN) *
                         this.ellipsoid.getC2n0(halfN);
             }
             // return is a modified Cnm
             return Cnm;
         }
 
         @Override
         public TideSystem getTideSystem() {
             return this.provider.getTideSystem();
         }
 
     }
 
     /**
      * {@inheritDoc}
      *
      * <p> The intersection point is computed using a line search along the
      * specified line. This is accurate when the geoid is slowly varying.
      */
     @Override
     public GeodeticPoint getIntersectionPoint(final Line lineInFrame,
                                               final Vector3D closeInFrame,
                                               final Frame frame,
                                               final AbsoluteDate date) {
         /*
          * It is assumed that the geoid is slowly varying over it's entire
          * surface. Therefore there will one local intersection.
          */
         // transform to body frame
         final Frame bodyFrame = this.getBodyFrame();
         final Transform frameToBody = frame.getTransformTo(bodyFrame, date);
         final Vector3D close = frameToBody.transformPosition(closeInFrame);
         final Line lineInBodyFrame = frameToBody.transformLine(lineInFrame);
 
         // set the line's direction so the solved for value is always positive
         final Line line;
         if (lineInBodyFrame.getAbscissa(close) < 0) {
             line = lineInBodyFrame.revert();
         } else {
             line = lineInBodyFrame;
         }
 
         final ReferenceEllipsoid ellipsoid = this.getEllipsoid();
         // calculate end points
         // distance from line to center of earth, squared
         final double d2 = line.pointAt(0.0).getNormSq();
         // the minimum abscissa, squared
         final double n = ellipsoid.getPolarRadius() + MIN_UNDULATION;
         final double minAbscissa2 = n * n - d2;
         // smaller end point of the interval = 0.0 or intersection with
         // min_undulation sphere
         final double lowPoint = FastMath.sqrt(FastMath.max(minAbscissa2, 0.0));
         // the maximum abscissa, squared
         final double x = ellipsoid.getEquatorialRadius() + MAX_UNDULATION;
         final double maxAbscissa2 = x * x - d2;
         // larger end point of the interval
         final double highPoint = FastMath.sqrt(maxAbscissa2);
 
         // line search function
         final UnivariateFunction heightFunction = new UnivariateFunction() {
             @Override
             public double value(final double x) {
                 try {
                     final GeodeticPoint geodetic =
                             transform(line.pointAt(x), bodyFrame, date);
                     return geodetic.getAltitude();
                 } catch (OrekitException e) {
                     // due to frame transform -> re-throw
                     throw new RuntimeException(e);
                 }
             }
         };
 
         // compute answer
         if (maxAbscissa2 < 0) {
             // ray does not pierce bounding sphere -> no possible intersection
             return null;
         }
         // solve line search problem to find the intersection
         final UnivariateSolver solver = new BracketingNthOrderBrentSolver();
         try {
             final double abscissa = solver.solve(MAX_EVALUATIONS, heightFunction, lowPoint, highPoint);
             // return intersection point
             return this.transform(line.pointAt(abscissa), bodyFrame, date);
         } catch (MathRuntimeException e) {
             // no intersection
             return null;
         }
     }
 
     @Override
     public Vector3D projectToGround(final Vector3D point,
                                     final AbsoluteDate date,
                                     final Frame frame) {
         final GeodeticPoint gp = this.transform(point, frame, date);
         final GeodeticPoint gpZero =
                 new GeodeticPoint(gp.getLatitude(), gp.getLongitude(), 0);
         final Transform bodyToFrame = this.getBodyFrame().getTransformTo(frame, date);
         return bodyToFrame.transformPosition(this.transform(gpZero));
     }
 
     /**
      * {@inheritDoc}
      *
      * <p> The intersection point is computed using a line search along the
      * specified line. This is accurate when the geoid is slowly varying.
      */
     @Override
     public <T extends RealFieldElement<T>> FieldGeodeticPoint<T> getIntersectionPoint(final FieldLine<T> lineInFrame,
                                                                                       final FieldVector3D<T> closeInFrame,
                                                                                       final Frame frame,
                                                                                       final FieldAbsoluteDate<T> date) {
 
         final Field<T> field = date.getField();
         /*
          * It is assumed that the geoid is slowly varying over it's entire
          * surface. Therefore there will one local intersection.
          */
         // transform to body frame
         final Frame bodyFrame = this.getBodyFrame();
         final FieldTransform<T> frameToBody = frame.getTransformTo(bodyFrame, date);
         final FieldVector3D<T> close = frameToBody.transformPosition(closeInFrame);
         final FieldLine<T> lineInBodyFrame = frameToBody.transformLine(lineInFrame);
 
         // set the line's direction so the solved for value is always positive
         final FieldLine<T> line;
         if (lineInBodyFrame.getAbscissa(close).getReal() < 0) {
             line = lineInBodyFrame.revert();
         } else {
             line = lineInBodyFrame;
         }
 
         final ReferenceEllipsoid ellipsoid = this.getEllipsoid();
         // calculate end points
         // distance from line to center of earth, squared
         final T d2 = line.pointAt(0.0).getNormSq();
         // the minimum abscissa, squared
         final double n = ellipsoid.getPolarRadius() + MIN_UNDULATION;
         final T minAbscissa2 = d2.negate().add(n * n);
         // smaller end point of the interval = 0.0 or intersection with
         // min_undulation sphere
         final T lowPoint = minAbscissa2.getReal() < 0 ? field.getZero() : minAbscissa2.sqrt();
         // the maximum abscissa, squared
         final double x = ellipsoid.getEquatorialRadius() + MAX_UNDULATION;
         final T maxAbscissa2 = d2.negate().add(x * x);
         // larger end point of the interval
         final T highPoint = maxAbscissa2.sqrt();
 
         // line search function
         final RealFieldUnivariateFunction<T> heightFunction = z -> {
             try {
                 final FieldGeodeticPoint<T> geodetic =
                         transform(line.pointAt(z), bodyFrame, date);
                 return geodetic.getAltitude();
             } catch (OrekitException e) {
                 // due to frame transform -> re-throw
                 throw new RuntimeException(e);
             }
         };
 
         // compute answer
         if (maxAbscissa2.getReal() < 0) {
             // ray does not pierce bounding sphere -> no possible intersection
             return null;
         }
         // solve line search problem to find the intersection
         final FieldBracketingNthOrderBrentSolver<T> solver =
                         new FieldBracketingNthOrderBrentSolver<>(field.getZero().add(1.0e-14),
                                                                  field.getZero().add(1.0e-6),
                                                                  field.getZero().add(1.0e-15),
                                                                  5);
         try {
             final T abscissa = solver.solve(MAX_EVALUATIONS, heightFunction, lowPoint, highPoint,
                                             AllowedSolution.ANY_SIDE);
             // return intersection point
             return this.transform(line.pointAt(abscissa), bodyFrame, date);
         } catch (MathRuntimeException e) {
             // no intersection
             return null;
         }
     }
 
     @Override
     public TimeStampedPVCoordinates projectToGround(
             final TimeStampedPVCoordinates pv,
             final Frame frame) {
         throw new UnsupportedOperationException();
     }
 
     /**
      * {@inheritDoc}
      *
      * @param date date of the conversion. Used for computing frame
      *             transformations and for time dependent geopotential.
      * @return The surface relative point at the same location. Altitude is
      * orthometric height, that is height above the {@link Geoid}. Latitude and
      * longitude are both geodetic and defined with respect to the {@link
      * #getEllipsoid() reference ellipsoid}.
      * @see #transform(GeodeticPoint)
      * @see <a href="http://en.wikipedia.org/wiki/Orthometric_height">Orthometric_height</a>
      */
     @Override
     public GeodeticPoint transform(final Vector3D point, final Frame frame,
                                    final AbsoluteDate date) {
         // convert using reference ellipsoid, altitude referenced to ellipsoid
         final GeodeticPoint ellipsoidal = this.getEllipsoid().transform(
                 point, frame, date);
         // convert altitude to orthometric using the undulation.
         final double undulation = this.getUndulation(ellipsoidal.getLatitude(),
                 ellipsoidal.getLongitude(), date);
         // add undulation to the altitude
         return new GeodeticPoint(
                 ellipsoidal.getLatitude(),
                 ellipsoidal.getLongitude(),
                 ellipsoidal.getAltitude() - undulation
         );
     }
 
     /**
      * {@inheritDoc}
      *
      * @param date date of the conversion. Used for computing frame
      *             transformations and for time dependent geopotential.
      * @return The surface relative point at the same location. Altitude is
      * orthometric height, that is height above the {@link Geoid}. Latitude and
      * longitude are both geodetic and defined with respect to the {@link
      * #getEllipsoid() reference ellipsoid}.
      * @see #transform(GeodeticPoint)
      * @see <a href="http://en.wikipedia.org/wiki/Orthometric_height">Orthometric_height</a>
      */
     @Override
     public <T extends RealFieldElement<T>> FieldGeodeticPoint<T> transform(final FieldVector3D<T> point, final Frame frame,
                                                                            final FieldAbsoluteDate<T> date) {
         // convert using reference ellipsoid, altitude referenced to ellipsoid
         final FieldGeodeticPoint<T> ellipsoidal = this.getEllipsoid().transform(
                 point, frame, date);
         // convert altitude to orthometric using the undulation.
         final double undulation = this.getUndulation(ellipsoidal.getLatitude().getReal(),
                                                      ellipsoidal.getLongitude().getReal(),
                                                      date.toAbsoluteDate());
         // add undulation to the altitude
         return new FieldGeodeticPoint<>(
                 ellipsoidal.getLatitude(),
                 ellipsoidal.getLongitude(),
                 ellipsoidal.getAltitude().subtract(undulation)
         );
     }
 
     /**
      * {@inheritDoc}
      *
      * @param point The surface relative point to transform. Altitude is
      *              orthometric height, that is height above the {@link Geoid}.
      *              Latitude and longitude are both geodetic and defined with
      *              respect to the {@link #getEllipsoid() reference ellipsoid}.
      * @return point at the same location but as a Cartesian point in the {@link
      * #getBodyFrame() body frame}.
      * @see #transform(Vector3D, Frame, AbsoluteDate)
      */
     @Override
     public Vector3D transform(final GeodeticPoint point) {
         try {
             // convert orthometric height to height above ellipsoid using undulation
             // TODO pass in date to allow user to specify
             final double undulation = this.getUndulation(
                     point.getLatitude(),
                     point.getLongitude(),
                     this.defaultDate
             );
             final GeodeticPointdeticPoint">GeodeticPoint ellipsoidal = new GeodeticPoint(
                     point.getLatitude(),
                     point.getLongitude(),
                     point.getAltitude() + undulation
             );
             // transform using reference ellipsoid
             return this.getEllipsoid().transform(ellipsoidal);
         } catch (OrekitException e) {
             //this method, as defined in BodyShape, is not permitted to throw
             //an OrekitException, so wrap in an exception we can throw.
             throw new RuntimeException(e);
         }
     }
 
     /**
      * {@inheritDoc}
      *
      * @param point The surface relative point to transform. Altitude is
      *              orthometric height, that is height above the {@link Geoid}.
      *              Latitude and longitude are both geodetic and defined with
      *              respect to the {@link #getEllipsoid() reference ellipsoid}.
      * @param <T> type of the field elements
      * @return point at the same location but as a Cartesian point in the {@link
      * #getBodyFrame() body frame}.
      * @see #transform(Vector3D, Frame, AbsoluteDate)
      * @since 9.0
      */
     @Override
     public <T extends RealFieldElement<T>> FieldVector3D<T> transform(final FieldGeodeticPoint<T> point) {
         try {
             // convert orthometric height to height above ellipsoid using undulation
             // TODO pass in date to allow user to specify
             final double undulation = this.getUndulation(
                     point.getLatitude().getReal(),
                     point.getLongitude().getReal(),
                     this.defaultDate
             );
             final FieldGeodeticPoint<T> ellipsoidal = new FieldGeodeticPoint<>(
                     point.getLatitude(),
                     point.getLongitude(),
                     point.getAltitude().add(undulation)
             );
             // transform using reference ellipsoid
             return this.getEllipsoid().transform(ellipsoidal);
         } catch (OrekitException e) {
             //this method, as defined in BodyShape, is not permitted to throw
             //an OrekitException, so wrap in an exception we can throw.
             throw new RuntimeException(e);
         }
     }
 
 }