/* 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;
  
  import org.hipparchus.CalculusFieldElement;
  import org.hipparchus.Field;
  import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
  import org.hipparchus.geometry.euclidean.threed.Vector3D;
  import org.orekit.propagation.FieldSpacecraftState;
  import org.orekit.propagation.SpacecraftState;
  import org.orekit.propagation.events.EventDetector;
  import org.orekit.propagation.events.FieldEventDetector;
  import org.orekit.time.AbsoluteDate;
  import org.orekit.time.FieldAbsoluteDate;
  import org.orekit.utils.ParameterDriver;
  
  import java.util.List;
  import java.util.stream.Stream;
  
  /**
   * Interface to wrap another force model.
   * By default, methods do not modify anything.
   *
   * @since 13.0
   * @author Romain Serra
   *
   */
  public interface ForceModelModifier extends ForceModel {
  
      /**
       * Get the underlying force model.
       * @return underlying model
       */
      ForceModel getUnderlyingModel();
  
      /** {@inheritDoc} */
      @Override
      default void init(SpacecraftState initialState, AbsoluteDate target) {
          getUnderlyingModel().init(initialState, target);
      }
  
      /** {@inheritDoc} */
      @Override
      default <T extends CalculusFieldElement<T>> void init(FieldSpacecraftState<T> initialState, FieldAbsoluteDate<T> target) {
          getUnderlyingModel().init(initialState, target);
      }
  
      /** {@inheritDoc} */
      @Override
      default Vector3D acceleration(SpacecraftState s, double[] parameters) {
          return getUnderlyingModel().acceleration(s, parameters);
      }
  
      /** {@inheritDoc} */
      @Override
      default <T extends CalculusFieldElement<T>> FieldVector3D<T> acceleration(FieldSpacecraftState<T> s,
                                                                                T[] parameters) {
          return getUnderlyingModel().acceleration(s, parameters);
      }
  
      /** {@inheritDoc} */
      @Override
      default boolean dependsOnPositionOnly() {
          return getUnderlyingModel().dependsOnPositionOnly();
      }
  
      /** {@inheritDoc} */
      @Override
      default boolean dependsOnAttitudeRate() {
          return getUnderlyingModel().dependsOnAttitudeRate();
      }
  
      /** {@inheritDoc} */
      @Override
      default Stream<EventDetector> getEventDetectors() {
          return getUnderlyingModel().getEventDetectors();
      }
  
      /** {@inheritDoc} */
      @Override
      default <T extends CalculusFieldElement<T>> Stream<FieldEventDetector<T>> getFieldEventDetectors(Field<T> field) {
          return getUnderlyingModel().getFieldEventDetectors(field);
      }
  
      /** {@inheritDoc} */
     @Override
     default List<ParameterDriver> getParametersDrivers() {
         return getUnderlyingModel().getParametersDrivers();
     }
 }