/* Contributed in the public domain.
    * 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.propagation.events.handlers;
  
  import org.hipparchus.ode.events.Action;
  import org.junit.jupiter.api.Assertions;
  import org.junit.jupiter.api.Test;
  import org.orekit.frames.Frame;
  import org.orekit.frames.FramesFactory;
  import org.orekit.orbits.KeplerianOrbit;
  import org.orekit.orbits.Orbit;
  import org.orekit.orbits.PositionAngleType;
  import org.orekit.propagation.SpacecraftState;
  import org.orekit.propagation.events.DateDetector;
  import org.orekit.propagation.events.handlers.RecordAndContinue.Event;
  import org.orekit.time.AbsoluteDate;
  import org.orekit.utils.Constants;
  
  import java.util.List;
  
  /**
   * Unit tests for {@link RecordAndContinue}.
   *
   * @author Evan Ward
   */
  public class RecordAndContinueTest {
  
      /**
       * check add and clear behavior.
       */
      @Test
      public void testGetEvents() {
          // setup
          RecordAndContinue handler = new RecordAndContinue();
          AbsoluteDate date = AbsoluteDate.J2000_EPOCH;
          DateDetector detector = new DateDetector(date);
          Frame eci = FramesFactory.getGCRF();
          Orbit orbit = new KeplerianOrbit(6378137 + 500e3, 0, 0, 0, 0, 0,
                  PositionAngleType.TRUE, eci, date, Constants.EIGEN5C_EARTH_MU);
          SpacecraftState s1 = new SpacecraftState(orbit);
          SpacecraftState s2 = s1.shiftedBy(-10);
          SpacecraftState s3 = s2.shiftedBy(1);
          SpacecraftState s4 = s3.shiftedBy(1);
  
          // actions
          Assertions.assertEquals(Action.CONTINUE, handler.eventOccurred(s1, detector, true));
          Assertions.assertEquals(Action.CONTINUE, handler.eventOccurred(s2, detector, true));
          Assertions.assertEquals(Action.CONTINUE, handler.eventOccurred(s3, detector, false));
  
          // verify
          List<Event> events = handler.getEvents();
          Assertions.assertEquals(3, events.size());
          Assertions.assertEquals(s1, events.get(0).getState());
          Assertions.assertEquals(s2, events.get(1).getState());
          Assertions.assertEquals(s3, events.get(2).getState());
          Assertions.assertEquals(true, events.get(0).isIncreasing());
          Assertions.assertEquals(true, events.get(1).isIncreasing());
          Assertions.assertEquals(false, events.get(2).isIncreasing());
          for (Event event : events) {
              Assertions.assertEquals(detector, event.getDetector());
          }
  
          // action: clear
          handler.clear();
  
          // verify is empty
          Assertions.assertEquals(0, handler.getEvents().size());
  
          // action add more
          Assertions.assertEquals(Action.CONTINUE, handler.eventOccurred(s4, detector, false));
  
          // verify new events
          events = handler.getEvents();
          Assertions.assertEquals(1, events.size());
          Assertions.assertEquals(s4, events.get(0).getState());
          Assertions.assertEquals(false, events.get(0).isIncreasing());
          Assertions.assertEquals(detector, events.get(0).getDetector());
      }
  
  }