ForceModelModifier.java
/* Copyright 2022-2024 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();
}
}