/* 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.orbits;
  
  import org.hipparchus.geometry.euclidean.threed.Vector3D;
  import org.hipparchus.util.MathUtils;
  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.time.AbsoluteDate;
  import org.orekit.time.TimeOffset;
  import org.orekit.utils.PVCoordinates;
  import org.orekit.utils.TimeStampedPVCoordinates;
  
  
  class OrbitTest {
  
      @Test
      void testGetPosition() {
          // GIVEN
          final double aIn = 1.;
          final TestOrbit testOrbit = new TestOrbit(aIn);
          final AbsoluteDate date = testOrbit.getDate().shiftedBy(0.);
          // WHEN
          final Vector3D actualPosition = testOrbit.getPosition(date, testOrbit.getFrame());
          // THEN
          final Vector3D expectedPosition = testOrbit.getPVCoordinates(date, testOrbit.getFrame()).getPosition();
          Assertions.assertEquals(expectedPosition, actualPosition);
      }
  
      @Test
      void testKeplerianMeanMotionAndPeriod() {
          // GIVEN
          final double aIn = 1.;
          final TestOrbit testOrbit = new TestOrbit(aIn);
          // WHEN
          final double meanMotion = testOrbit.getKeplerianMeanMotion();
          final double period = testOrbit.getKeplerianPeriod();
          final double actualValue = period * meanMotion;
          // THEN
          final double expectedValue = MathUtils.TWO_PI;
          Assertions.assertEquals(expectedValue, actualValue, 1e-10);
      }
  
      @Test
      void testIsElliptical() {
          templateTestIsElliptical(1.);
      }
  
      @Test
      void testIsNotElliptical() {
          templateTestIsElliptical(-1.);
      }
  
      private void templateTestIsElliptical(final double aIn) {
          // GIVEN
          final TestOrbit testOrbit = new TestOrbit(aIn);
          // WHEN
          final boolean actualValue = testOrbit.isElliptical();
          // THEN
          final boolean expectedValue = aIn > 0.;
          Assertions.assertEquals(expectedValue, actualValue);
      }
  
      private static class TestOrbit extends Orbit {
  
          final double a;
  
          protected TestOrbit(final double aIn) throws IllegalArgumentException {
              super(FramesFactory.getGCRF(), AbsoluteDate.ARBITRARY_EPOCH, 1.);
              this.a = aIn;
          }
  
          @Override
          public OrbitType getType() {
              return null;
          }
  
          @Override
          public double getA() {
              return this.a;
          }
  
          @Override
         public double getADot() {
             return 0;
         }
 
         @Override
         public double getEquinoctialEx() {
             return 0;
         }
 
         @Override
         public double getEquinoctialExDot() {
             return 0;
         }
 
         @Override
         public double getEquinoctialEy() {
             return 0;
         }
 
         @Override
         public double getEquinoctialEyDot() {
             return 0;
         }
 
         @Override
         public double getHx() {
             return 0;
         }
 
         @Override
         public double getHxDot() {
             return 0;
         }
 
         @Override
         public double getHy() {
             return 0;
         }
 
         @Override
         public double getHyDot() {
             return 0;
         }
 
         @Override
         public double getLE() {
             return 0;
         }
 
         @Override
         public double getLEDot() {
             return 0;
         }
 
         @Override
         public double getLv() {
             return 0;
         }
 
         @Override
         public double getLvDot() {
             return 0;
         }
 
         @Override
         public double getLM() {
             return 0;
         }
 
         @Override
         public double getLMDot() {
             return 0;
         }
 
         @Override
         public double getE() {
             return 0;
         }
 
         @Override
         public double getEDot() {
             return 0;
         }
 
         @Override
         public double getI() {
             return 0;
         }
 
         @Override
         public double getIDot() {
             return 0;
         }
 
         @Override
         protected Vector3D initPosition() {
             return new Vector3D(a, 0., 0.);
         }
 
         @Override
         protected TimeStampedPVCoordinates initPVCoordinates() {
             return new TimeStampedPVCoordinates(getDate(), new PVCoordinates(initPosition(), Vector3D.ZERO));
         }
 
         @Override
         public Orbit inFrame(Frame inertialFrame) {
             return null;
         }
 
         @Override
         public Orbit shiftedBy(double dt) {
             return new TestOrbit(a);
         }
 
         @Override
         public Orbit shiftedBy(TimeOffset dt) {
             return new TestOrbit(a);
         }
 
         @Override
         protected double[][] computeJacobianMeanWrtCartesian() {
             return new double[0][];
         }
 
         @Override
         protected double[][] computeJacobianEccentricWrtCartesian() {
             return new double[0][];
         }
 
         @Override
         protected double[][] computeJacobianTrueWrtCartesian() {
             return new double[0][];
         }
 
         @Override
         public void addKeplerContribution(PositionAngleType type, double gm, double[] pDot) {
 
         }
     }
 
 }