/* Copyright 2002-2026 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.files.ccsds.ndm.adm;
  
  import org.hipparchus.CalculusFieldElement;
  import org.hipparchus.Field;
  import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
  import org.orekit.attitudes.Attitude;
  import org.orekit.attitudes.AttitudeBuilder;
  import org.orekit.attitudes.FieldAttitude;
  import org.orekit.errors.OrekitException;
  import org.orekit.errors.OrekitMessages;
  import org.orekit.files.ccsds.definitions.CcsdsFrameMapper;
  import org.orekit.files.ccsds.definitions.FrameFacade;
  import org.orekit.files.ccsds.definitions.OrbitRelativeFrame;
  import org.orekit.frames.Frame;
  import org.orekit.utils.AngularCoordinates;
  import org.orekit.utils.FieldAngularCoordinates;
  import org.orekit.utils.FieldPVCoordinates;
  import org.orekit.utils.FieldPVCoordinatesProvider;
  import org.orekit.utils.PVCoordinates;
  import org.orekit.utils.PVCoordinatesProvider;
  import org.orekit.utils.TimeStampedAngularCoordinates;
  import org.orekit.utils.TimeStampedFieldAngularCoordinates;
  
  /** Endpoints for attitude definition.
   * <p>
   * This class provides a bridge between two different views of attitude definition.
   * In both views, there is an external frame, based on either celestial body or orbit-relative
   * and there is a spacecraft body frame.
   * <ul>
   *   <li>CCSDS ADM view: frames are labeled as A and B but nothing tells which is which
   *   and attitude can be defined in any direction</li>
   *   <li>{@link Attitude Orekit attitude} view: attitude is always from external to
   *   spacecraft body</li>
   * </ul>
   * @author Luc Maisonobe
   * @since 11.0
   */
  public class AttitudeEndpoints implements AttitudeBuilder {
  
      /** Constant for A → B diraction. */
      public static final String A2B = "A2B";
  
      /** Constant for A ← B direction. */
      public static final String B2A = "B2A";
  
      /** For creating a {@link Frame}. */
      private final CcsdsFrameMapper frameMapper;
  
      /** Frame A. */
      private FrameFacade frameA;
  
      /** Frame B. */
      private FrameFacade frameB;
  
      /** Flag for frames direction. */
      private Boolean a2b;
  
      /**
       * Simple constructor.
       *
       * @param frameMapper for creating a {@link Frame}.
       * @since 13.1.5
       */
      public AttitudeEndpoints(final CcsdsFrameMapper frameMapper) {
          this.frameMapper = frameMapper;
      }
  
      /** Complain if a field is null.
       * @param field field to check
       * @param key key associated with the field
       */
      private void checkNotNull(final Object field, final Enum<?> key) {
          if (field == null) {
              throw new OrekitException(OrekitMessages.UNINITIALIZED_VALUE_FOR_KEY, key.name());
          }
      }
      /** Check external frame is properly initialized.
       * @param aKey key for frame A
       * @param bKey key for frame B
       */
      public void checkExternalFrame(final Enum<?> aKey, final Enum<?> bKey) {
          checkNotNull(frameA, aKey);
          checkNotNull(frameB, bKey);
         if (frameA.asSpacecraftBodyFrame() != null && frameB.asSpacecraftBodyFrame() != null) {
             // we cannot have two spacecraft body frames
             throw new OrekitException(OrekitMessages.CCSDS_INVALID_FRAME, frameB.getName());
         }
     }
 
     /** Check is mandatory entries <em>except external frame</em> have been initialized.
      * <p>
      * Either frame A or frame B must be initialized with a {@link
      * org.orekit.files.ccsds.definitions.SpacecraftBodyFrame spacecraft body frame}.
      * </p>
      * <p>
      * This method should throw an exception if some mandatory entry is missing
      * </p>
      * @param version format version
      * @param aKey key for frame A
      * @param bKey key for frame B
      * @param dirKey key for direction
      */
     public void checkMandatoryEntriesExceptExternalFrame(final double version,
                                                          final Enum<?> aKey, final Enum<?> bKey,
                                                          final Enum<?> dirKey) {
 
         if (frameA == null) {
             if (frameB == null || frameB.asSpacecraftBodyFrame() == null) {
                 throw new OrekitException(OrekitMessages.UNINITIALIZED_VALUE_FOR_KEY, aKey.name());
             }
         } else if (frameA.asSpacecraftBodyFrame() == null) {
             if (frameB == null) {
                 throw new OrekitException(OrekitMessages.UNINITIALIZED_VALUE_FOR_KEY, bKey.name());
             } else if (frameB.asSpacecraftBodyFrame() == null) {
                 // at least one of the frame must be a spacecraft body frame
                 throw new OrekitException(OrekitMessages.CCSDS_INVALID_FRAME, frameB.getName());
             }
         }
 
         if (version < 2.0) {
             // in ADM version 1, direction is mandatory
             checkNotNull(a2b, dirKey);
         } else if (!isA2b()) {
             // in ADM version 2, direction is always A → B
             throw new OrekitException(OrekitMessages.CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION,
                                       dirKey, version);
         }
 
     }
 
     /** Set frame A.
      * @param frameA frame A
      */
     public void setFrameA(final FrameFacade frameA) {
         this.frameA = frameA;
     }
 
     /** Get frame A.
      * @return frame A
      */
     public FrameFacade getFrameA() {
         return frameA;
     }
 
     /** Set frame B.
      * @param frameB frame B
      */
     public void setFrameB(final FrameFacade frameB) {
         this.frameB = frameB;
     }
 
     /** Get frame B.
      * @return frame B
      */
     public FrameFacade getFrameB() {
         return frameB;
     }
 
     /** Set rotation direction.
      * @param a2b if true, rotation is from {@link #getFrameA() frame A}
      * to {@link #getFrameB() frame B}
      */
     public void setA2b(final boolean a2b) {
         this.a2b = a2b;
     }
 
     /** Check if rotation direction is from {@link #getFrameA() frame A} to {@link #getFrameB() frame B}.
      * @return true if rotation direction is from {@link #getFrameA() frame A} to {@link #getFrameB() frame B}
      */
     public boolean isA2b() {
         return a2b == null ? true : a2b;
     }
 
     /** Get the external frame.
      * @return external frame
      * @see #getExternal()
      */
     public FrameFacade getExternalFrame() {
         return frameA.asSpacecraftBodyFrame() == null ? frameA : frameB;
     }
 
     /**
      * Get the mapping between a CCSDS frame and a {@link Frame}.
      *
      * @return the frame mapper.
      * @since 13.1.5
      */
     public CcsdsFrameMapper getFrameMapper() {
         return frameMapper;
     }
 
     /**
      * Get the external reference frame. Only the orientation is significant.
      *
      * @return the external frame.
      * @see #getExternalFrame()
      * @since 13.1.5
      */
     public Frame getExternal() {
         // no reference frame epoch
         return getFrameMapper().buildCcsdsFrame(getExternalFrame(), null);
     }
 
     /** Get the spacecraft body frame.
      * @return spacecraft body frame
      */
     public FrameFacade getSpacecraftBodyFrame() {
         return frameA.asSpacecraftBodyFrame() == null ? frameB : frameA;
     }
 
     /** Check if attitude is from external frame to spacecraft body frame.
      * <p>
      * {@link #checkMandatoryEntriesExceptExternalFrame(double, Enum, Enum, Enum)
      * Mandatory entries} must have been initialized properly to non-null
      * values before this method is called, otherwise {@code NullPointerException}
      * will be thrown.
      * </p>
      * @return true if attitude is from external frame to spacecraft body frame
      */
     public boolean isExternal2SpacecraftBody() {
         return isA2b() ^ frameB.asSpacecraftBodyFrame() == null;
     }
 
     /** Check if a endpoint is compatible with another one.
      * <p>
      * Endpoins are compatible if they refer o the same frame names,
      * in the same order and in the same direction.
      * </p>
      * @param other other endpoints to check against
      * @return true if both endpoints are compatible with each other
      */
     public boolean isCompatibleWith(final AttitudeEndpoints other) {
         return frameA.getName().equals(other.frameA.getName()) &&
                frameB.getName().equals(other.frameB.getName()) &&
                a2b.equals(other.a2b);
     }
 
     /**  {@inheritDoc} */
     @Override
     public Attitude build(final Frame frame, final PVCoordinatesProvider pvProv,
                           final TimeStampedAngularCoordinates rawAttitude) {
 
         // attitude converted to Orekit conventions
         final TimeStampedAngularCoordinates att =
                         isExternal2SpacecraftBody() ? rawAttitude : rawAttitude.revert();
 
         final FrameFacade        external = getExternalFrame();
         final OrbitRelativeFrame orf      = external.asOrbitRelativeFrame();
         if (orf != null) {
             // this is an orbit-relative attitude
             if (orf.getLofType() == null) {
                 throw new OrekitException(OrekitMessages.UNSUPPORTED_LOCAL_ORBITAL_FRAME, external.getName());
             }
 
             // construction of the local orbital frame, using PV from reference frame
             final PVCoordinates pv = pvProv.getPVCoordinates(rawAttitude.getDate(), frame);
             final AngularCoordinates frame2Lof =
                             orf.isQuasiInertial() ?
                             new AngularCoordinates(orf.getLofType().rotationFromInertial(pv)) :
                             orf.getLofType().transformFromInertial(att.getDate(), pv).getAngular();
 
             // compose with APM
             return new Attitude(frame, att.addOffset(frame2Lof));
 
         } else {
             // this is an absolute attitude
             if (external.asFrame() == null) {
                 // unknown frame
                 throw new OrekitException(OrekitMessages.CCSDS_INVALID_FRAME, external.getName());
             }
             final Attitude attitude = new Attitude(external.asFrame(), att);
             return frame == null ? attitude : attitude.withReferenceFrame(frame);
         }
 
     }
 
     /**  {@inheritDoc} */
     @Override
     public <T extends CalculusFieldElement<T>>
         FieldAttitude<T> build(final Frame frame, final FieldPVCoordinatesProvider<T> pvProv,
                                final TimeStampedFieldAngularCoordinates<T> rawAttitude) {
 
         // attitude converted to Orekit conventions
         final TimeStampedFieldAngularCoordinates<T> att =
                         isExternal2SpacecraftBody() ? rawAttitude : rawAttitude.revert();
 
         final FrameFacade        external = getExternalFrame();
         final OrbitRelativeFrame orf      = external.asOrbitRelativeFrame();
         if (orf != null) {
             // this is an orbit-relative attitude
             if (orf.getLofType() == null) {
                 throw new OrekitException(OrekitMessages.UNSUPPORTED_LOCAL_ORBITAL_FRAME, external.getName());
             }
 
             // construction of the local orbital frame, using PV from reference frame
             final FieldPVCoordinates<T> pv = pvProv.getPVCoordinates(rawAttitude.getDate(), frame);
             final Field<T> field = rawAttitude.getDate().getField();
             final FieldAngularCoordinates<T> referenceToLof =
                             orf.isQuasiInertial() ?
                             new FieldAngularCoordinates<>(orf.getLofType().rotationFromInertial(field, pv),
                                                           FieldVector3D.getZero(field)) :
                             orf.getLofType().transformFromInertial(att.getDate(), pv).getAngular();
 
             // compose with APM
             return new FieldAttitude<>(frame, att.addOffset(referenceToLof));
 
         } else {
             // this is an absolute attitude
             if (external.asFrame() == null) {
                 // this should never happen as all CelestialBodyFrame have an Orekit mapping
                 throw new OrekitException(OrekitMessages.CCSDS_INVALID_FRAME, external.getName());
             }
             final FieldAttitude<T> attitude = new FieldAttitude<>(external.asFrame(), att);
             return frame == null ? attitude : attitude.withReferenceFrame(frame);
         }
 
     }
 
     /** {@inheritDoc} */
     @Override
     public String toString() {
         return frameA.getName() + (isA2b() ? " → " : " ← ") + frameB.getName();
     }
 
 }