Maneuver.java
/* Copyright 2002-2024 CS GROUP
* 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.files.ccsds.ndm.adm.apm;
import java.util.Arrays;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.files.ccsds.definitions.FrameFacade;
import org.orekit.files.ccsds.section.CommentsContainer;
import org.orekit.time.AbsoluteDate;
/**
* Maneuver in an APM file.
* @author Bryan Cazabonne
* @since 10.2
*/
public class Maneuver extends CommentsContainer {
/** Epoch of start of maneuver . */
private AbsoluteDate epochStart;
/** Coordinate system for the torque vector. */
private FrameFacade frame;
/** Duration (value is 0 for impulsive maneuver). */
private double duration;
/** Torque vector (N.m). */
private double[] torque;
/** Mass change during maneuver (kg).
* @since 12.0
*/
private double deltaMass;
/**
* Simple constructor.
*/
public Maneuver() {
duration = Double.NaN;
torque = new double[3];
deltaMass = Double.NaN;
Arrays.fill(torque, Double.NaN);
}
/** {@inheritDoc} */
@Override
public void validate(final double version) {
super.validate(version);
checkNotNull(epochStart, ManeuverKey.MAN_EPOCH_START.name());
checkNotNaN(duration, ManeuverKey.MAN_DURATION.name());
checkNotNull(frame, ManeuverKey.MAN_REF_FRAME.name());
checkNotNaN(torque[0], ManeuverKey.MAN_TOR_1.name());
checkNotNaN(torque[1], ManeuverKey.MAN_TOR_2.name());
checkNotNaN(torque[2], ManeuverKey.MAN_TOR_3.name());
}
/**
* Get epoch start.
* @return epoch start
*/
public AbsoluteDate getEpochStart() {
return epochStart;
}
/**
* Set epoch start.
* @param epochStart epoch start
*/
public void setEpochStart(final AbsoluteDate epochStart) {
refuseFurtherComments();
this.epochStart = epochStart;
}
/**
* Get Coordinate system for the torque vector.
* @return coordinate system for the torque vector
*/
public FrameFacade getFrame() {
return frame;
}
/**
* Set Coordinate system for the torque vector.
* @param frame coordinate system for the torque vector
*/
public void setFrame(final FrameFacade frame) {
refuseFurtherComments();
this.frame = frame;
}
/**
* Get duration (value is 0 for impulsive maneuver).
* @return duration (value is 0 for impulsive maneuver)
*/
public double getDuration() {
return duration;
}
/**
* Set duration (value is 0 for impulsive maneuver).
* @param duration duration (value is 0 for impulsive maneuver)
*/
public void setDuration(final double duration) {
refuseFurtherComments();
this.duration = duration;
}
/**
* Get the torque vector (N.m).
* @return torque vector
*/
public Vector3D getTorque() {
return new Vector3D(torque);
}
/**
* Set the torque vector (N.m).
* @param index vector component index (counting from 0)
* @param value component value
*/
public void setTorque(final int index, final double value) {
refuseFurtherComments();
this.torque[index] = value;
}
/**
* Get mass change during maneuver.
* @return mass change during maneuver (kg, negative)
* @since 12.0
*/
public double getDeltaMass() {
return deltaMass;
}
/**
* Set mass change during maneuver.
* @param deltaMass mass change during maneuver (kg)
* @since 12.0
*/
public void setDeltaMass(final double deltaMass) {
refuseFurtherComments();
this.deltaMass = deltaMass;
}
}