LegacyNavigationMessage.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.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;
- }
- }