FieldLogarithmicBarrierCartesianFuel.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.control.indirect.adjoint.cost;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.util.FastMath;
/**
* Fuel cost penalized with a logarithmic term, which is a barrier so is not defined for epsilon equal to 0 or 1.
*
* @author Romain Serra
* @since 13.0
*/
public class FieldLogarithmicBarrierCartesianFuel<T extends CalculusFieldElement<T>>
extends FieldPenalizedCartesianFuelCost<T> {
/**
* Constructor.
*
* @param name adjoint name
* @param massFlowRateFactor mass flow rate factor
* @param maximumThrustMagnitude maximum thrust magnitude
* @param epsilon penalty weight
*/
public FieldLogarithmicBarrierCartesianFuel(final String name, final T massFlowRateFactor,
final T maximumThrustMagnitude, final T epsilon) {
super(name, massFlowRateFactor, maximumThrustMagnitude, epsilon);
}
/** {@inheritDoc} */
@Override
public T evaluateFieldPenaltyFunction(final T controlNorm) {
return FastMath.log(controlNorm).add(FastMath.log(controlNorm.negate().add(1)));
}
/** {@inheritDoc} */
@Override
public FieldVector3D<T> getFieldThrustAccelerationVector(final T[] adjointVariables, final T mass) {
final T thrustForceMagnitude = getThrustForceMagnitude(adjointVariables, mass);
return getFieldThrustDirection(adjointVariables).scalarMultiply(thrustForceMagnitude.divide(mass));
}
/** {@inheritDoc} */
@Override
public void updateFieldAdjointDerivatives(final T[] adjointVariables, final T mass, final T[] adjointDerivatives) {
if (getAdjointDimension() > 6) {
adjointDerivatives[6] = adjointDerivatives[6].add(getFieldAdjointVelocityNorm(adjointVariables)
.multiply(getThrustForceMagnitude(adjointVariables, mass)).divide(mass.square()));
}
}
/**
* Computes the Euclidean norm of the thrust force.
* @param adjointVariables adjoint variables
* @param mass mass
* @return thrust force magnitude
*/
private T getThrustForceMagnitude(final T[] adjointVariables, final T mass) {
final T twoEpsilon = getEpsilon().multiply(2);
T otherTerm = getFieldAdjointVelocityNorm(adjointVariables).divide(mass).subtract(1.);
if (getAdjointDimension() > 6) {
otherTerm = otherTerm.subtract(getMassFlowRateFactor().multiply(adjointVariables[6]));
}
return twoEpsilon.multiply(getMaximumThrustMagnitude())
.divide(twoEpsilon.add(otherTerm).add(FastMath.sqrt(otherTerm.square().add(twoEpsilon.square()))));
}
/** {@inheritDoc} */
@Override
public LogarithmicBarrierCartesianFuel toCartesianCost() {
return new LogarithmicBarrierCartesianFuel(getAdjointName(), getMassFlowRateFactor().getReal(),
getMaximumThrustMagnitude().getReal(), getEpsilon().getReal());
}
}