Package org.orekit.propagation.analytical.gnss.data

Class GalileoNavigationMessageFactory

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<GalileoNavigationMessage>

org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory<GalileoNavigationMessage>

org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessageFactory<GalileoNavigationMessage>

org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessageFactory

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<GalileoNavigationMessage>

public class GalileoNavigationMessageFactory
extends AbstractNavigationMessageFactory<GalileoNavigationMessage>

Factory for GalileoNavigationMessage.

Since:

14.0

Author:

Luc Maisonobe

Field Summary

Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory

ARGUMENT_OF_PERIAPSIS, ECCENTRICITY, FROZEN, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS

Constructor Summary

Constructors

Constructor	Description
GalileoNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
GalileoNavigationMessage	createFromDrivers()	Create orbital parameters from current drivers values.
double	getBGDE1E5a()	Get the E1/E5a broadcast group delay.
double	getBGDE5bE1()	Get the Broadcast Group Delay E5b/E1.
int	getDataSource()	Get the data source.
int	getIodNav()	Get the Issue Of Data (IOD).
double	getSisa()	Get the signal in space accuracy (m).
double	getSvHealth()	Get the SV health status.
void	setBGDE1E5a(double newBgdE1E5a)	Set the E1/E5a broadcast group delay.
void	setBGDE5bE1(double newBgdE5bE1)	Set the Broadcast Group Delay E5b/E1.
void	setDataSource(int dataSource)	Set the data source.
void	setIodNav(int iodNav)	Set the Issue Of Data (IOD).
void	setSisa(double sisa)	Set the signal in space accuracy (m).
void	setSvHealth(double svHealth)	Set the SV health status.

Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessageFactory

getTransmissionTime, setTransmissionTime

Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsFactory

buildOrbitalDrivers, createOrbitFromDrivers, getADotDriver, getAf0Driver, getAf1Driver, getAf2Driver, getAngularVelocity, getBodyFixed, getCicDriver, getCisDriver, getCrcDriver, getCrsDriver, getCucDriver, getCusDriver, getDeltaN0DotDriver, getDeltaN0Driver, getIDotDriver, getInertial, getJacobianWrtParameters, getNonKeplerianParametersDrivers, getOmegaDotDriver, getPrn, getSystem, getTgd, getTimeDriver, getTimeOfClock, getTimeOfEphemeris, getTimeScales, getType, jacobianWrtParameters, setDate, setPrn, setTgd, setTimeOfClock, setTimeOfEphemeris, toArray

Methods inherited from class org.orekit.orbits.AbstractOrbitalParameterFactory

clone, getDate, getFrame, getJacobianWrtCartesian, getMu, getOrbitalParametersDrivers, getOrbitType, getPositionAngleType, reset, setFrame, setMu, setPositionAngleType

Methods inherited from class java.lang.Object

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

Constructor Details

GalileoNavigationMessageFactory

public GalileoNavigationMessageFactory(TimeScales timeScales,
 SatelliteSystem system,
 String type,
 Frame inertial,
 Frame bodyFixed)

Simple constructor.

Parameters:

timeScales - known time scales

system - satellite system to use for interpreting week number

type - message type (null if not a navigation message)

inertial - reference inertial frame

bodyFixed - body fixed frame (will be frozen at date to build the orbital elements

Method Details

getIodNav

public int getIodNav()

Get the Issue Of Data (IOD).

Returns:

Issue Of Data (IOD)

setIodNav

public void setIodNav(int iodNav)

Set the Issue Of Data (IOD).

Parameters:

iodNav - Issue Of Data (IOD)

getDataSource

public int getDataSource()

Get the data source.

Returns:

the data source

setDataSource

public void setDataSource(int dataSource)

Set the data source.

Parameters:

dataSource - data source

getBGDE1E5a

public double getBGDE1E5a()

Get the E1/E5a broadcast group delay.

Returns:

the E1/E5a broadcast group delay (s)

setBGDE1E5a

public void setBGDE1E5a(double newBgdE1E5a)

Set the E1/E5a broadcast group delay.

Parameters:

newBgdE1E5a - the E1/E5a broadcast group delay (s)

getBGDE5bE1

public double getBGDE5bE1()

Get the Broadcast Group Delay E5b/E1.

Returns:

the Broadcast Group Delay E5b/E1 (s)

setBGDE5bE1

public void setBGDE5bE1(double newBgdE5bE1)

Set the Broadcast Group Delay E5b/E1.

Parameters:

newBgdE5bE1 - the Broadcast Group Delay E5b/E1 (s)

getSisa

public double getSisa()

Get the signal in space accuracy (m).

Returns:

the signal in space accuracy

setSisa

public void setSisa(double sisa)

Set the signal in space accuracy (m).

Parameters:

sisa - the signal in space accuracy

getSvHealth

public double getSvHealth()

Get the SV health status.

Returns:

the SV health status

setSvHealth

public void setSvHealth(double svHealth)

Set the SV health status.

Parameters:

svHealth - the SV health status

createFromDrivers

public GalileoNavigationMessage createFromDrivers()

Create orbital parameters from current drivers values.

Returns:

created orbital parameters