LegacyNavigationMessage.java
/* Copyright 2002-2023 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.propagation.analytical.gnss.data;
/**
* Container for data contained in a GPS/QZNSS legacy navigation message.
* @author Bryan Cazabonne
* @since 11.0
*/
public class LegacyNavigationMessage extends AbstractNavigationMessage implements GNSSClockElements {
/** Identifier for message type. */
public static final String LNAV = "LNAV";
/** Issue of Data, Ephemeris. */
private int iode;
/** Issue of Data, Clock. */
private int iodc;
/** Group Delay Differential (s). */
private double tgd;
/** The user SV accuracy (m). */
private double svAccuracy;
/** Satellite health status. */
private int svHealth;
/** Fit interval.
* @since 12.0
*/
private int fitInterval;
/**
* Constructor.
* @param mu Earth's universal gravitational parameter
* @param angularVelocity mean angular velocity of the Earth for the GNSS model
* @param weekNumber number of weeks in the GNSS cycle
*/
protected LegacyNavigationMessage(final double mu,
final double angularVelocity,
final int weekNumber) {
super(mu, angularVelocity, weekNumber);
}
/**
* Getter for the Issue Of Data Ephemeris (IODE).
* @return the Issue Of Data Ephemeris (IODE)
*/
public int getIODE() {
return iode;
}
/**
* Setter for the Issue of Data Ephemeris.
* @param value the IODE to set
*/
public void setIODE(final double value) {
// The value is given as a floating number in the navigation message
this.iode = (int) value;
}
/**
* Getter for the Issue Of Data Clock (IODC).
* @return the Issue Of Data Clock (IODC)
*/
public int getIODC() {
return iodc;
}
/**
* Setter for the Issue of Data Clock.
* @param value the IODC to set
*/
public void setIODC(final int value) {
this.iodc = value;
}
/**
* Getter for the Group Delay Differential (s).
* @return the Group Delay Differential in seconds
*/
public double getTGD() {
return tgd;
}
/**
* Setter for the Group Delay Differential (s).
* @param time the group delay differential to set
*/
public void setTGD(final double time) {
this.tgd = time;
}
/**
* Getter for the user SV accuray (meters).
* @return the user SV accuracy
*/
public double getSvAccuracy() {
return svAccuracy;
}
/**
* Setter for the user SV accuracy.
* @param svAccuracy the value to set
*/
public void setSvAccuracy(final double svAccuracy) {
this.svAccuracy = svAccuracy;
}
/**
* Getter for the satellite health status.
* @return the satellite health status
*/
public int getSvHealth() {
return svHealth;
}
/**
* Setter for the satellite health status.
* @param svHealth the value to set
*/
public void setSvHealth(final int svHealth) {
this.svHealth = svHealth;
}
/**
* Getter for the fit interval.
* @return the fit interval
* @since 12.0
*/
public int getFitInterval() {
return fitInterval;
}
/**
* Setter for the fit interval.
* @param fitInterval fit interval
* @since 12.0
*/
public void setFitInterval(final int fitInterval) {
this.fitInterval = fitInterval;
}
}