PolynomialThrustSegment.java
/* Copyright 2023 Luc Maisonobe
* 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.maneuvers.propulsion;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.analysis.polynomials.PolynomialFunction;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
/** One polynomial segment of a thrust profile.
* @author Luc Maisonobe
* @since 12.0
*/
public class PolynomialThrustSegment {
/** Reference date. */
private final AbsoluteDate referenceDate;
/** Thrust along X direction (N). */
private final PolynomialFunction xThrust;
/** Thrust along Y direction (N). */
private final PolynomialFunction yThrust;
/** Thrust along Z direction (N). */
private final PolynomialFunction zThrust;
/** Simple constructor.
* @param referenceDate reference date of the polynomials
* @param xThrust thrust along X direction (N)
* @param yThrust thrust along Y direction (N)
* @param zThrust thrust along Z direction (N)
*/
public PolynomialThrustSegment(final AbsoluteDate referenceDate,
final PolynomialFunction xThrust,
final PolynomialFunction yThrust,
final PolynomialFunction zThrust) {
this.referenceDate = referenceDate;
this.xThrust = xThrust;
this.yThrust = yThrust;
this.zThrust = zThrust;
}
/** Get thrust vector at a specified date.
* @param date date to consider
* @return thrust at {@code date} (N)
*/
public Vector3D getThrustVector(final AbsoluteDate date) {
final double dt = date.durationFrom(referenceDate);
return new Vector3D(xThrust.value(dt), yThrust.value(dt), zThrust.value(dt));
}
/** Get thrust vector at a specified date.
* @param <T> type of the field elements
* @param date date to consider
* @return thrust at {@code date} (N)
*/
public <T extends CalculusFieldElement<T>> FieldVector3D<T> getThrustVector(final FieldAbsoluteDate<T> date) {
final T dt = date.durationFrom(referenceDate);
return new FieldVector3D<>(xThrust.value(dt), yThrust.value(dt), zThrust.value(dt));
}
}