ForceModelModifier.java
- /* 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();
- }
- }