LongitudeExtremumEventFunction.java
/* Copyright 2022-2026 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,
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* See the License for the specific language governing permissions and
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*/
package org.orekit.propagation.events.functions;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.analysis.differentiation.FieldUnivariateDerivative1;
import org.hipparchus.analysis.differentiation.UnivariateDerivative1;
import org.hipparchus.analysis.differentiation.UnivariateDerivative1Field;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.orekit.bodies.BodyShape;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.time.FieldAbsoluteDate;
/** Class for longitude extremum event function.
* @author Romain Serra
* @since 14.0
*/
public class LongitudeExtremumEventFunction extends AbstractGeodeticExtremumEventFunction {
/** Constructor.
* @param body body
*/
public LongitudeExtremumEventFunction(final BodyShape body) {
super(body);
}
@Override
public double value(final SpacecraftState state) {
final UnivariateDerivative1Field field = UnivariateDerivative1Field.getInstance();
final UnivariateDerivative1 dt = new UnivariateDerivative1(0, 1);
final FieldAbsoluteDate<UnivariateDerivative1> fieldDate = new FieldAbsoluteDate<>(field, state.getDate()).shiftedBy(dt);
final FieldVector3D<UnivariateDerivative1> position = state.getPVCoordinates().toUnivariateDerivative1Vector();
return getBodyShape().getLongitude(position, state.getFrame(), fieldDate).getFirstDerivative();
}
@Override
public <T extends CalculusFieldElement<T>> T value(final FieldSpacecraftState<T> fieldState) {
final FieldAbsoluteDate<FieldUnivariateDerivative1<T>> fud1Date = fieldState.getDate().toFUD1Field();
final FieldVector3D<FieldUnivariateDerivative1<T>> fieldPosition = fieldState.getPVCoordinates().toUnivariateDerivative1Vector();
return getBodyShape().getLongitude(fieldPosition, fieldState.getFrame(), fud1Date).getFirstDerivative();
}
}