Package org.orekit.files.rinex.navigation

Class EarthOrientationParameterMessage

java.lang.Object

org.orekit.files.rinex.navigation.TypeSvMessage

org.orekit.files.rinex.navigation.EarthOrientationParameterMessage

All Implemented Interfaces:

NavigationMessage, TimeStamped

public class EarthOrientationParameterMessage
extends TypeSvMessage

Container for data contained in a Earth Orientation Parameter navigation message.

Since:

12.0

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor	Description
EarthOrientationParameterMessage(SatelliteSystem system, int prn, String type, String subType)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
AbsoluteDate	getDate()	Get the date.
double	getDut1()	Get the ΔUT₁.
double	getDut1Dot()	Get the ΔUT₁ first derivative.
double	getDut1DotDot()	Get the ΔUT₁ second derivative.
AbsoluteDate	getReferenceEpoch()	Get the reference epoch.
double	getTransmissionTime()	Get the message transmission time.
double	getXp()	Get the X component of the pole.
double	getXpDot()	Get the X component of the pole first derivative.
double	getXpDotDot()	Get the X component of the pole second derivative.
double	getYp()	Get the Y component of the pole.
double	getYpDot()	Get the Y component of the pole first derivative.
double	getYpDotDot()	Get the Y component of the pole second derivative.
void	setDut1(double dUT1)	Set the ΔUT₁.
void	setDut1Dot(double dUT1Dot)	Set the ΔUT₁ first derivative.
void	setDut1DotDot(double dUT1DotDot)	Set the ΔUT₁ second derivative.
void	setReferenceEpoch(AbsoluteDate referenceEpoch)	Set the reference epoch.
void	setTransmissionTime(double transmissionTime)	Set the message transmission time.
void	setXp(double xp)	Set the X component of the pole.
void	setXpDot(double xpDot)	Set the X component of the pole first derivative.
void	setXpDotDot(double xpDotDot)	Set the X component of the pole second derivative.
void	setYp(double yp)	Set the Y component of the pole.
void	setYpDot(double ypDot)	Set the Y component of the pole first derivative.
void	setYpDotDot(double ypDotDot)	Set the Y component of the pole second derivative.

Methods inherited from class org.orekit.files.rinex.navigation.TypeSvMessage

getIdentifier, getNavigationMessageSubType, getNavigationMessageType, getPrn, getSystem

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.time.TimeStamped

durationFrom

Constructor Details

EarthOrientationParameterMessage

public EarthOrientationParameterMessage(SatelliteSystem system,
 int prn,
 String type,
 String subType)

Simple constructor.

Parameters:

system - satellite system

prn - satellite number

type - navigation message type

subType - navigation message subtype

Method Details

getDate

public AbsoluteDate getDate()

Get the date.

Returns:

date attached to the object

getReferenceEpoch

public AbsoluteDate getReferenceEpoch()

Get the reference epoch.

Returns:

the reference epoch

setReferenceEpoch

public void setReferenceEpoch(AbsoluteDate referenceEpoch)

Set the reference epoch.

Parameters:

referenceEpoch - the reference epoch to set

getXp

public double getXp()

Get the X component of the pole.

Returns:

the X component of the pole (rad)

setXp

public void setXp(double xp)

Set the X component of the pole.

Parameters:

xp - X component of the pole (rad)

getXpDot

public double getXpDot()

Get the X component of the pole first derivative.

Returns:

the X component of the pole first derivative (rad/s)

setXpDot

public void setXpDot(double xpDot)

Set the X component of the pole first derivative.

Parameters:

xpDot - X component of the pole first derivative (rad/s)

getXpDotDot

public double getXpDotDot()

Get the X component of the pole second derivative.

Returns:

the X component of the pole second derivative (rad/s²)

setXpDotDot

public void setXpDotDot(double xpDotDot)

Set the X component of the pole second derivative.

Parameters:

xpDotDot - X component of the pole second derivative (rad/s²)

getYp

public double getYp()

Get the Y component of the pole.

Returns:

the Y component of the pole (rad)

setYp

public void setYp(double yp)

Set the Y component of the pole.

Parameters:

yp - Y component of the pole (rad)

getYpDot

public double getYpDot()

Get the Y component of the pole first derivative.

Returns:

the Y component of the pole first derivative (rad/s)

setYpDot

public void setYpDot(double ypDot)

Set the Y component of the pole first derivative.

Parameters:

ypDot - Y component of the pole first derivative (rad/s)

getYpDotDot

public double getYpDotDot()

Get the Y component of the pole second derivative.

Returns:

the Y component of the pole second derivative (rad/s²)

setYpDotDot

public void setYpDotDot(double ypDotDot)

Set the Y component of the pole second derivative.

Parameters:

ypDotDot - Y component of the pole second derivative (rad/s²)

getDut1

public double getDut1()

Get the ΔUT₁.

Returns:

the ΔUT₁ (s)

setDut1

public void setDut1(double dUT1)

Set the ΔUT₁.

Parameters:

dUT1 - ΔUT₁ (s)

getDut1Dot

public double getDut1Dot()

Get the ΔUT₁ first derivative.

Returns:

the ΔUT₁ first derivative (s/s)

setDut1Dot

public void setDut1Dot(double dUT1Dot)

Set the ΔUT₁ first derivative.

Parameters:

dUT1Dot - ΔUT₁ first derivative (s/s)

getDut1DotDot

public double getDut1DotDot()

Get the ΔUT₁ second derivative.

Returns:

the ΔUT₁ second derivative (s/s²)

setDut1DotDot

public void setDut1DotDot(double dUT1DotDot)

Set the ΔUT₁ second derivative.

Parameters:

dUT1DotDot - ΔUT₁ second derivative (s/s²)

getTransmissionTime

public double getTransmissionTime()

Get the message transmission time.

Returns:

message transmission time

setTransmissionTime

public void setTransmissionTime(double transmissionTime)

Set the message transmission time.

Parameters:

transmissionTime - the message transmission time