java.lang.Object
- org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

All Implemented Interfaces:

NavigationMessage, TimeStamped

Direct Known Subclasses:

GLONASSFdmaNavigationMessage, SBASNavigationMessage
```
public abstract class AbstractEphemerisMessage
extends Object
implements TimeStamped, NavigationMessage
```
Base class for ephemeris-based navigation messages.

Since:

11.0

Author:

Bryan Cazabonne

See Also:

GLONASSFdmaNavigationMessage, SBASNavigationMessage

Constructor Summary

Constructors
Modifier Constructor Description

protected AbstractEphemerisMessage()
Constructor.

Method Summary

All Methods Instance Methods Concrete Methods
Modifier and Type	Method	Description
`AbsoluteDate`	`getDate()`	Getter for the reference date of the ephemeris.
`AbsoluteDate`	`getEpochToc()`	Getter for the time of clock epoch.
`double`	`getHealth()`	Getter for the health status.
`int`	`getPRN()`	Getter for the PRN number of the satellite.
`double`	`getX()`	Getter for the satellite X position.
`double`	`getXDot()`	Getter for the satellite X velocity.
`double`	`getXDotDot()`	Getter for the satellite X acceleration.
`double`	`getY()`	Getter for the satellite Y position.
`double`	`getYDot()`	Getter for the satellite Y velocity.
`double`	`getYDotDot()`	Getter for the satellite Y acceleration.
`double`	`getZ()`	Getter for the satellite Z position.
`double`	`getZDot()`	Getter for the satellite Z velocity.
`double`	`getZDotDot()`	Getter for the satellite Z acceleration.
`void`	`setDate(AbsoluteDate date)`	Setter for the reference date of the ephemeris.
`void`	`setEpochToc(AbsoluteDate epochToc)`	Setter for the time of clock epoch.
`void`	`setHealth(double health)`	Setter for the health status.
`void`	`setPRN(int number)`	Setter for the PRN number of the satellite.
`void`	`setX(double x)`	Setter for the satellite X position.
`void`	`setXDot(double vx)`	Setter for the satellite X velocity.
`void`	`setXDotDot(double ax)`	Setter for the satellite X acceleration.
`void`	`setY(double y)`	Setter for the satellite Y position.
`void`	`setYDot(double vy)`	Setter for the satellite Y velocity.
`void`	`setYDotDot(double ay)`	Setter for the satellite Y acceleration.
`void`	`setZ(double z)`	Setter for the satellite Z position.
`void`	`setZDot(double vz)`	Setter for the satellite Z velocity.
`void`	`setZDotDot(double az)`	Setter for the satellite Z acceleration.

Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.propagation.analytical.gnss.data.NavigationMessage
getNavigationMessageSubType, getNavigationMessageType

Methods inherited from interface org.orekit.time.TimeStamped
durationFrom

- Constructor Detail
  - AbstractEphemerisMessage
```
protected AbstractEphemerisMessage()
```
    Constructor.
- Method Detail
  - getDate
```
public AbsoluteDate getDate()
```
    Getter for the reference date of the ephemeris.
    
    Specified by:
    
    getDate in interface TimeStamped
    
    Returns:
    
    the reference date of the ephemeris
  - setDate
```
public void setDate(AbsoluteDate date)
```
    Setter for the reference date of the ephemeris.
    
    Parameters:
    
    date - the date to set
  - getEpochToc
```
public AbsoluteDate getEpochToc()
```
    Getter for the time of clock epoch.
    
    Returns:
    
    the time of clock epoch
  - setEpochToc
```
public void setEpochToc(AbsoluteDate epochToc)
```
    Setter for the time of clock epoch.
    
    Parameters:
    
    epochToc - the epoch to set
  - getPRN
```
public int getPRN()
```
    Getter for the PRN number of the satellite.
    
    Returns:
    
    the PRN number of the satellite
  - setPRN
```
public void setPRN(int number)
```
    Setter for the PRN number of the satellite.
    
    Parameters:
    
    number - the prn number ot set
  - getX
```
public double getX()
```
    Getter for the satellite X position.
    
    Returns:
    
    the satellite X position in meters
  - setX
```
public void setX(double x)
```
    Setter for the satellite X position.
    
    Parameters:
    
    x - satellite X position (meters) to set
  - getXDot
```
public double getXDot()
```
    Getter for the satellite X velocity.
    
    Returns:
    
    the satellite X velocity in m/s
  - setXDot
```
public void setXDot(double vx)
```
    Setter for the satellite X velocity.
    
    Parameters:
    
    vx - the satellite X velocity (m/s) to set
  - getXDotDot
```
public double getXDotDot()
```
    Getter for the satellite X acceleration.
    
    Returns:
    
    the satellite X acceleration in m/s²
  - setXDotDot
```
public void setXDotDot(double ax)
```
    Setter for the satellite X acceleration.
    
    Parameters:
    
    ax - the satellite X acceleration (m/s²) to set
  - getY
```
public double getY()
```
    Getter for the satellite Y position.
    
    Returns:
    
    the satellite Y position in meters
  - setY
```
public void setY(double y)
```
    Setter for the satellite Y position.
    
    Parameters:
    
    y - satellite Y position (meters) to set
  - getYDot
```
public double getYDot()
```
    Getter for the satellite Y velocity.
    
    Returns:
    
    the satellite Y velocity in m/s
  - setYDot
```
public void setYDot(double vy)
```
    Setter for the satellite Y velocity.
    
    Parameters:
    
    vy - the satellite Y velocity (m/s) to set
  - getYDotDot
```
public double getYDotDot()
```
    Getter for the satellite Y acceleration.
    
    Returns:
    
    the satellite Y acceleration in m/s²
  - setYDotDot
```
public void setYDotDot(double ay)
```
    Setter for the satellite Y acceleration.
    
    Parameters:
    
    ay - the satellite Y acceleration (m/s²) to set
  - getZ
```
public double getZ()
```
    Getter for the satellite Z position.
    
    Returns:
    
    the satellite Z position in meters
  - setZ
```
public void setZ(double z)
```
    Setter for the satellite Z position.
    
    Parameters:
    
    z - satellite Z position (meters) to set
  - getZDot
```
public double getZDot()
```
    Getter for the satellite Z velocity.
    
    Returns:
    
    the satellite Z velocity in m/s
  - setZDot
```
public void setZDot(double vz)
```
    Setter for the satellite Z velocity.
    
    Parameters:
    
    vz - the satellite Z velocity (m/s) to set
  - getZDotDot
```
public double getZDotDot()
```
    Getter for the satellite Z acceleration.
    
    Returns:
    
    the satellite Z acceleration in m/s²
  - setZDotDot
```
public void setZDotDot(double az)
```
    Setter for the satellite Z acceleration.
    
    Parameters:
    
    az - the satellite Z acceleration (m/s²) to set
  - getHealth
```
public double getHealth()
```
    Getter for the health status.
    
    Returns:
    
    the health status
  - setHealth
```
public void setHealth(double health)
```
    Setter for the health status.
    
    Parameters:
    
    health - the health status to set

Class AbstractEphemerisMessage

Constructor Summary

Method Summary

Methods inherited from class java.lang.Object

Methods inherited from interface org.orekit.propagation.analytical.gnss.data.NavigationMessage

Methods inherited from interface org.orekit.time.TimeStamped

Constructor Detail

AbstractEphemerisMessage

Method Detail

getDate

setDate

getEpochToc

setEpochToc

getPRN

setPRN

getX

setX

getXDot

setXDot

getXDotDot

setXDotDot

getY

setY

getYDot

setYDot

getYDotDot

setYDotDot

getZ

setZ

getZDot

setZDot

getZDotDot

setZDotDot

getHealth

setHealth