org.orekit.propagation.analytical.gnss.data

Class AbstractEphemerisMessage

java.lang.Object

org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage

Direct Known Subclasses:

GLONASSNavigationMessage, SBASNavigationMessage

public abstract class AbstractEphemerisMessage
extends Object

Base class for ephemeris-based navigation messages.

Since:

11.0

Author:

Bryan Cazabonne

See Also:

GLONASSNavigationMessage, SBASNavigationMessage

Constructor Summary

Constructors

Constructor and Description
AbstractEphemerisMessage() Constructor.

Method Summary

Modifier and Type	Method and 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

Constructor Detail

AbstractEphemerisMessage

public AbstractEphemerisMessage()

Constructor.

Method Detail

getDate

public AbsoluteDate getDate()

Getter for the reference date of the ephemeris.

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