FieldCartesianFuelCost.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.control.indirect.adjoint.cost;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.events.EventDetectionSettings;
import org.orekit.propagation.events.FieldEventDetectionSettings;
import org.orekit.propagation.events.FieldEventDetector;
import org.orekit.propagation.events.handlers.FieldEventHandler;
import org.orekit.propagation.events.handlers.FieldResetDerivativesOnEvent;
import java.util.stream.Stream;
/**
* Class for fuel cost with Cartesian coordinates.
* It is the integral over time of the Euclidean norm of the thrust vector.
*
* @author Romain Serra
* @see CartesianCost
* @since 13.0
*/
public class FieldCartesianFuelCost<T extends CalculusFieldElement<T>> extends FieldAbstractCartesianCost<T> {
/** Maximum value of thrust force Euclidean norm. */
private final T maximumThrustMagnitude;
/** Detection settings for singularity detection. */
private final FieldEventDetectionSettings<T> eventDetectionSettings;
/**
* Constructor with default detection settings.
* @param name name
* @param massFlowRateFactor mass flow rate factor
* @param maximumThrustMagnitude maximum thrust magnitude
*/
public FieldCartesianFuelCost(final String name, final T massFlowRateFactor, final T maximumThrustMagnitude) {
this(name, massFlowRateFactor, maximumThrustMagnitude, new FieldEventDetectionSettings<>(massFlowRateFactor.getField(),
EventDetectionSettings.getDefaultEventDetectionSettings()));
}
/**
* Constructor.
* @param name name
* @param massFlowRateFactor mass flow rate factor
* @param maximumThrustMagnitude maximum thrust magnitude
* @param eventDetectionSettings singularity event detection settings
*/
public FieldCartesianFuelCost(final String name, final T massFlowRateFactor, final T maximumThrustMagnitude,
final FieldEventDetectionSettings<T> eventDetectionSettings) {
super(name, massFlowRateFactor);
this.maximumThrustMagnitude = maximumThrustMagnitude;
this.eventDetectionSettings = eventDetectionSettings;
}
/**
* Getter for event detection settings.
* @return detection settings.
*/
public FieldEventDetectionSettings<T> getEventDetectionSettings() {
return eventDetectionSettings;
}
/** Getter for maximum thrust magnitude.
* @return maximum thrust
*/
public T getMaximumThrustMagnitude() {
return maximumThrustMagnitude;
}
/**
* Evaluate switching function (whose sign determines the bang-bang control profile).
* @param adjointVariables adjoint vector
* @param mass mass
* @return value of switch function
*/
private T evaluateFieldSwitchFunction(final T[] adjointVariables, final T mass) {
return getFieldAdjointVelocityNorm(adjointVariables).divide(mass).subtract(adjointVariables[6].multiply(getMassFlowRateFactor())).subtract(1.);
}
/**
* Computes the direction of thrust.
* @param adjointVariables adjoint vector
* @return thrust direction
*/
private FieldVector3D<T> getFieldThrustDirection(final T[] adjointVariables) {
return new FieldVector3D<>(adjointVariables[3], adjointVariables[4], adjointVariables[5]).normalize();
}
/** {@inheritDoc} */
@Override
public FieldVector3D<T> getFieldThrustAccelerationVector(final T[] adjointVariables, final T mass) {
final T switchFunction = evaluateFieldSwitchFunction(adjointVariables, mass);
if (switchFunction.getReal() > 0.) {
return getFieldThrustDirection(adjointVariables).scalarMultiply(mass.reciprocal().multiply(maximumThrustMagnitude));
} else {
return FieldVector3D.getZero(mass.getField());
}
}
/** {@inheritDoc} */
@Override
public void updateFieldAdjointDerivatives(final T[] adjointVariables, final T mass,
final T[] adjointDerivatives) {
final T switchFunction = evaluateFieldSwitchFunction(adjointVariables, mass);
if (switchFunction.getReal() > 0.) {
adjointDerivatives[6] = adjointDerivatives[6].add(getFieldAdjointVelocityNorm(adjointVariables).multiply(maximumThrustMagnitude).divide(mass.square()));
}
}
/** {@inheritDoc} */
@Override
public T getFieldHamiltonianContribution(final T[] adjointVariables, final T mass) {
final FieldVector3D<T> thrustForce = getFieldThrustAccelerationVector(adjointVariables, mass).scalarMultiply(mass);
return thrustForce.getNorm().negate();
}
/** {@inheritDoc} */
@Override
public Stream<FieldEventDetector<T>> getFieldEventDetectors(final Field<T> field) {
return Stream.of(new FieldSwitchDetector());
}
@Override
public CartesianFuelCost toCartesianCost() {
return new CartesianFuelCost(getAdjointName(), getMassFlowRateFactor().getReal(), maximumThrustMagnitude.getReal(),
getEventDetectionSettings().toEventDetectionSettings());
}
/**
* Field event detector for bang-bang switches.
*/
private class FieldSwitchDetector implements FieldEventDetector<T> {
/** Event handler. */
private final FieldResetDerivativesOnEvent<T> handler = new FieldResetDerivativesOnEvent<>();
/** {@inheritDoc} */
@Override
public T g(final FieldSpacecraftState<T> state) {
final T[] adjoint = state.getAdditionalState(getAdjointName());
return evaluateFieldSwitchFunction(adjoint, state.getMass());
}
@Override
public FieldEventDetectionSettings<T> getDetectionSettings() {
return eventDetectionSettings;
}
@Override
public FieldEventHandler<T> getHandler() {
return handler;
}
}
}