EarthOrientationParameterMessage.java
/* Copyright 2002-2024 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.files.rinex.navigation;
import org.orekit.gnss.SatelliteSystem;
import org.orekit.time.AbsoluteDate;
/** Container for data contained in a Earth Orientation Parameter navigation message.
* @author Luc Maisonobe
* @since 12.0
*/
public class EarthOrientationParameterMessage extends TypeSvMessage {
/** Reference epoch. */
private AbsoluteDate referenceEpoch;
/** X component of the pole (rad). */
private double xp;
/** X component of the pole first derivative (rad/s). */
private double xpDot;
/** X component of the pole second derivative (rad/s²). */
private double xpDotDot;
/** Y component of the pole (rad). */
private double yp;
/** Y component of the pole first derivative (rad/s). */
private double ypDot;
/** Y component of the pole second derivative (rad/s²). */
private double ypDotDot;
/** ΔUT₁ (s).
* According to Rinex 4.00 table A31, this may be either UT₁-UTC or UT₁-GPST
* depending on constellation and applicable Interface Control Document).
*/
private double dUt1;
/** ΔUT₁ first derivative (s/s). */
private double dUt1Dot;
/** ΔUT₁ second derivative (s/s²). */
private double dUt1DotDot;
/** Transmission time. */
private double transmissionTime;
/** Simple constructor.
* @param system satellite system
* @param prn satellite number
* @param navigationMessageType navigation message type
*/
public EarthOrientationParameterMessage(final SatelliteSystem system, final int prn, final String navigationMessageType) {
super(system, prn, navigationMessageType);
}
/** Get the reference epoch.
* @return the reference epoch
*/
public AbsoluteDate getReferenceEpoch() {
return referenceEpoch;
}
/** Set the reference epoch.
* @param referenceEpoch the reference epoch to set
*/
public void setReferenceEpoch(final AbsoluteDate referenceEpoch) {
this.referenceEpoch = referenceEpoch;
}
/** Get the X component of the pole.
* @return the X component of the pole (rad)
*/
public double getXp() {
return xp;
}
/** Set the X component of the pole.
* @param xp X component of the pole (rad)
*/
public void setXp(final double xp) {
this.xp = xp;
}
/** Get the X component of the pole first derivative.
* @return the X component of the pole first derivative (rad/s)
*/
public double getXpDot() {
return xpDot;
}
/** Set the X component of the pole first derivative.
* @param xpDot X component of the pole first derivative (rad/s)
*/
public void setXpDot(final double xpDot) {
this.xpDot = xpDot;
}
/** Get the X component of the pole second derivative.
* @return the X component of the pole second derivative (rad/s²)
*/
public double getXpDotDot() {
return xpDotDot;
}
/** Set the X component of the pole second derivative.
* @param xpDotDot X component of the pole second derivative (rad/s²)
*/
public void setXpDotDot(final double xpDotDot) {
this.xpDotDot = xpDotDot;
}
/** Get the Y component of the pole.
* @return the Y component of the pole (rad)
*/
public double getYp() {
return yp;
}
/** Set the Y component of the pole.
* @param yp Y component of the pole (rad)
*/
public void setYp(final double yp) {
this.yp = yp;
}
/** Get the Y component of the pole first derivative.
* @return the Y component of the pole first derivative (rad/s)
*/
public double getYpDot() {
return ypDot;
}
/** Set the Y component of the pole first derivative.
* @param ypDot Y component of the pole first derivative (rad/s)
*/
public void setYpDot(final double ypDot) {
this.ypDot = ypDot;
}
/** Get the Y component of the pole second derivative.
* @return the Y component of the pole second derivative (rad/s²)
*/
public double getYpDotDot() {
return ypDotDot;
}
/** Set the Y component of the pole second derivative.
* @param ypDotDot Y component of the pole second derivative (rad/s²)
*/
public void setYpDotDot(final double ypDotDot) {
this.ypDotDot = ypDotDot;
}
/** Get the ΔUT₁.
* @return the ΔUT₁ (s)
*/
public double getDut1() {
return dUt1;
}
/** Set the ΔUT₁.
* @param dUT1 ΔUT₁ (s)
*/
public void setDut1(final double dUT1) {
this.dUt1 = dUT1;
}
/** Get the ΔUT₁ first derivative.
* @return the ΔUT₁ first derivative (s/s)
*/
public double getDut1Dot() {
return dUt1Dot;
}
/** Set the ΔUT₁ first derivative.
* @param dUT1Dot ΔUT₁ first derivative (s/s)
*/
public void setDut1Dot(final double dUT1Dot) {
this.dUt1Dot = dUT1Dot;
}
/** Get the ΔUT₁ second derivative.
* @return the ΔUT₁ second derivative (s/s²)
*/
public double getDut1DotDot() {
return dUt1DotDot;
}
/** Set the ΔUT₁ second derivative.
* @param dUT1DotDot ΔUT₁ second derivative (s/s²)
*/
public void setDut1DotDot(final double dUT1DotDot) {
this.dUt1DotDot = dUT1DotDot;
}
/** Get the message transmission time.
* @return message transmission time
*/
public double getTransmissionTime() {
return transmissionTime;
}
/** Set the message transmission time.
* @param transmissionTime the message transmission time
*/
public void setTransmissionTime(final double transmissionTime) {
this.transmissionTime = transmissionTime;
}
}