AbstractEphemerisMessage.java
/* Copyright 2002-2022 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;
import org.orekit.time.AbsoluteDate;
/**
* Base class for ephemeris-based navigation messages.
* @author Bryan Cazabonne
* @since 11.0
*
* @see GLONASSNavigationMessage
* @see SBASNavigationMessage
*/
public abstract class AbstractEphemerisMessage {
/** Ephemeris reference epoch. */
private AbsoluteDate date;
/** Time of clock epoch. */
private AbsoluteDate epochToc;
/** PRN number of the satellite. */
private int prn;
/** Satellite X position in meters. */
private double x;
/** Satellite X velocity in meters per second. */
private double xDot;
/** Satellite X acceleration in meters per second². */
private double xDotDot;
/** Satellite Y position in meters. */
private double y;
/** Satellite Y velocity in meters per second. */
private double yDot;
/** Satellite Y acceleration in meters per second². */
private double yDotDot;
/** Satellite Z position in meters. */
private double z;
/** Satellite Z velocity in meters per second. */
private double zDot;
/** Satellite Z acceleration in meters per second². */
private double zDotDot;
/** Health status. */
private double health;
/** Constructor. */
public AbstractEphemerisMessage() {
// Nothing to do ...
}
/**
* Getter for the reference date of the ephemeris.
* @return the reference date of the ephemeris
*/
public AbsoluteDate getDate() {
return date;
}
/**
* Setter for the reference date of the ephemeris.
* @param date the date to set
*/
public void setDate(final AbsoluteDate date) {
this.date = date;
}
/**
* Getter for the time of clock epoch.
* @return the time of clock epoch
*/
public AbsoluteDate getEpochToc() {
return epochToc;
}
/**
* Setter for the time of clock epoch.
* @param epochToc the epoch to set
*/
public void setEpochToc(final AbsoluteDate epochToc) {
this.epochToc = epochToc;
}
/**
* Getter for the PRN number of the satellite.
* @return the PRN number of the satellite
*/
public int getPRN() {
return prn;
}
/**
* Setter for the PRN number of the satellite.
* @param number the prn number ot set
*/
public void setPRN(final int number) {
this.prn = number;
}
/**
* Getter for the satellite X position.
* @return the satellite X position in meters
*/
public double getX() {
return x;
}
/**
* Setter for the satellite X position.
* @param x satellite X position (meters) to set
*/
public void setX(final double x) {
this.x = x;
}
/**
* Getter for the satellite X velocity.
* @return the satellite X velocity in m/s
*/
public double getXDot() {
return xDot;
}
/**
* Setter for the satellite X velocity.
* @param vx the satellite X velocity (m/s) to set
*/
public void setXDot(final double vx) {
this.xDot = vx;
}
/**
* Getter for the satellite X acceleration.
* @return the satellite X acceleration in m/s²
*/
public double getXDotDot() {
return xDotDot;
}
/**
* Setter for the satellite X acceleration.
* @param ax the satellite X acceleration (m/s²) to set
*/
public void setXDotDot(final double ax) {
this.xDotDot = ax;
}
/**
* Getter for the satellite Y position.
* @return the satellite Y position in meters
*/
public double getY() {
return y;
}
/**
* Setter for the satellite Y position.
* @param y satellite Y position (meters) to set
*/
public void setY(final double y) {
this.y = y;
}
/**
* Getter for the satellite Y velocity.
* @return the satellite Y velocity in m/s
*/
public double getYDot() {
return yDot;
}
/**
* Setter for the satellite Y velocity.
* @param vy the satellite Y velocity (m/s) to set
*/
public void setYDot(final double vy) {
this.yDot = vy;
}
/**
* Getter for the satellite Y acceleration.
* @return the satellite Y acceleration in m/s²
*/
public double getYDotDot() {
return yDotDot;
}
/**
* Setter for the satellite Y acceleration.
* @param ay the satellite Y acceleration (m/s²) to set
*/
public void setYDotDot(final double ay) {
this.yDotDot = ay;
}
/**
* Getter for the satellite Z position.
* @return the satellite Z position in meters
*/
public double getZ() {
return z;
}
/**
* Setter for the satellite Z position.
* @param z satellite Z position (meters) to set
*/
public void setZ(final double z) {
this.z = z;
}
/**
* Getter for the satellite Z velocity.
* @return the satellite Z velocity in m/s
*/
public double getZDot() {
return zDot;
}
/**
* Setter for the satellite Z velocity.
* @param vz the satellite Z velocity (m/s) to set
*/
public void setZDot(final double vz) {
this.zDot = vz;
}
/**
* Getter for the satellite Z acceleration.
* @return the satellite Z acceleration in m/s²
*/
public double getZDotDot() {
return zDotDot;
}
/**
* Setter for the satellite Z acceleration.
* @param az the satellite Z acceleration (m/s²) to set
*/
public void setZDotDot(final double az) {
this.zDotDot = az;
}
/**
* Getter for the health status.
* @return the health status
*/
public double getHealth() {
return health;
}
/**
* Setter for the health status.
* @param health the health status to set
*/
public void setHealth(final double health) {
this.health = health;
}
}