/* Copyright 2022-2025 Romain Serra
    * 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.forces.maneuvers;
  
  import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
  import org.hipparchus.geometry.euclidean.threed.Vector3D;
  import org.hipparchus.util.Binary64;
  import org.hipparchus.util.Binary64Field;
  import org.junit.jupiter.api.Assertions;
  import org.junit.jupiter.api.Test;
  import org.junit.jupiter.params.ParameterizedTest;
  import org.junit.jupiter.params.provider.ValueSource;
  import org.orekit.TestUtils;
  import org.orekit.frames.FramesFactory;
  import org.orekit.orbits.CartesianOrbit;
  import org.orekit.orbits.FieldCartesianOrbit;
  import org.orekit.orbits.Orbit;
  import org.orekit.propagation.FieldSpacecraftState;
  import org.orekit.propagation.SpacecraftState;
  import org.orekit.time.AbsoluteDate;
  import org.orekit.utils.PVCoordinates;
  
  class FieldImpulseProviderTest {
  
      @Test
      void testOfVector3D() {
          // GIVEN
          final Vector3D forwardImpulse = new Vector3D(1, 2, 3);
          final Binary64Field field = Binary64Field.getInstance();
          final FieldImpulseProvider<Binary64> provider = FieldImpulseProvider.of(field, forwardImpulse);
          // WHEN
          final Vector3D vector3D = provider.getImpulse(null, true).toVector3D();
          // THEN
          Assertions.assertEquals(forwardImpulse, vector3D);
          Assertions.assertEquals(forwardImpulse.negate(), provider.getImpulse(null, false).toVector3D());
      }
  
      @Test
      void testOfFieldVector3D() {
          // GIVEN
          final Vector3D forwardImpulse = new Vector3D(1, 2, 3);
          final Binary64Field field = Binary64Field.getInstance();
          final Orbit orbit = TestUtils.getDefaultOrbit(AbsoluteDate.ARBITRARY_EPOCH);
          final SpacecraftState state = new SpacecraftState(orbit, 100);
          final FieldSpacecraftState<Binary64> fieldState = new FieldSpacecraftState<>(field, state);
          // WHEN
          final FieldImpulseProvider<Binary64> provider = FieldImpulseProvider.of(new FieldVector3D<>(field, forwardImpulse));
          final Vector3D vector3D = provider.getImpulse(fieldState, true).toVector3D();
          // THEN
          Assertions.assertEquals(forwardImpulse, vector3D);
          Assertions.assertEquals(forwardImpulse.negate(), provider.getImpulse(fieldState, false).toVector3D());
      }
  
      @ParameterizedTest
      @ValueSource(booleans = {true, false})
      void testOfImpulseProvider(final boolean isForward) {
          // GIVEN
          final Vector3D forwardImpulse = new Vector3D(1, 2, 3);
          final ImpulseProvider impulseProvider = ImpulseProvider.of(forwardImpulse);
          final FieldImpulseProvider<Binary64> fieldImpulseProvider = FieldImpulseProvider.of(impulseProvider);
          final FieldSpacecraftState<Binary64> fieldSpacecraftState = buildFieldState();
          // WHEN
          final Vector3D vector3D = fieldImpulseProvider.getImpulse(fieldSpacecraftState, isForward).toVector3D();
          // THEN
          Assertions.assertEquals(impulseProvider.getImpulse(fieldSpacecraftState.toSpacecraftState(), isForward), vector3D);
      }
  
      private static FieldSpacecraftState<Binary64> buildFieldState() {
          return new FieldSpacecraftState<>(new FieldCartesianOrbit<>(Binary64Field.getInstance(),
                  new CartesianOrbit(new PVCoordinates(Vector3D.MINUS_J, Vector3D.MINUS_K), FramesFactory.getEME2000(), AbsoluteDate.ARBITRARY_EPOCH, 1)));
      }
  }