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

Class BeidouLegacyNavigationMessageFactory

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<BeidouLegacyNavigationMessage>

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

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

org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessageFactory

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<BeidouLegacyNavigationMessage>

public class BeidouLegacyNavigationMessageFactory
extends AbstractNavigationMessageFactory<BeidouLegacyNavigationMessage>

Factory for BeidouLegacyNavigationMessage.

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
BeidouLegacyNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, boolean d2)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
BeidouLegacyNavigationMessage	createFromDrivers()	Create orbital parameters from current drivers values.
int	getAodc()	Get the Age Of Data Clock (AODC).
int	getAode()	Get the Age Of Data Ephemeris (AODE).
int	getSatH1()	Get the health identifier.
double	getSvAccuracy()	Get the user SV accuray (meters).
double	getTgd1()	Get the estimated group delay differential TGD1 for B1I signal.
double	getTgd2()	Get the estimated group delay differential TGD for B2I signal.
boolean	isD2()	Check if message is a D2 message.
void	setAodc(int aodc)	Set the Age Of Data Clock (AODC).
void	setAode(int aode)	Set the Age Of Data Ephemeris (AODE).
void	setSatH1(int satH1)	Set the health identifier.
void	setSvAccuracy(double svAccuracy)	Set the user SV accuray (meters).
void	setTgd1(double tgd1)	Set the estimated group delay differential TGD1 for B1I signal.
void	setTgd2(double tgd2)	Set the estimated group delay differential TGD for B2I signal.

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

BeidouLegacyNavigationMessageFactory

public BeidouLegacyNavigationMessageFactory(TimeScales timeScales,
 SatelliteSystem system,
 String type,
 Frame inertial,
 Frame bodyFixed,
 boolean d2)

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

d2 - indicator for D2 messages

Method Details

isD2

public boolean isD2()

Check if message is a D2 message.

Returns:

true if message is a D2 message

getAodc

public int getAodc()

Get the Age Of Data Clock (AODC).

Returns:

the Age Of Data Clock (AODC)

setAodc

public void setAodc(int aodc)

Set the Age Of Data Clock (AODC).

Parameters:

aodc - the Age Of Data Clock (AODC)

getAode

public int getAode()

Get the Age Of Data Ephemeris (AODE).

Returns:

the Age Of Data Ephemeris (AODE)

setAode

public void setAode(int aode)

Set the Age Of Data Ephemeris (AODE).

Parameters:

aode - the Age Of Data Ephemeris (AODE)

getTgd1

public double getTgd1()

Get the estimated group delay differential TGD1 for B1I signal.

Returns:

the estimated group delay differential TGD1 for B1I signal (s)

setTgd1

public void setTgd1(double tgd1)

Set the estimated group delay differential TGD1 for B1I signal.

Parameters:

tgd1 - the estimated group delay differential TGD1 for B1I signal (s)

getTgd2

public double getTgd2()

Get the estimated group delay differential TGD for B2I signal.

Returns:

the estimated group delay differential TGD2 for B2I signal (s)

setTgd2

public void setTgd2(double tgd2)

Set the estimated group delay differential TGD for B2I signal.

Parameters:

tgd2 - the estimated group delay differential TGD2 for B2I signal (s)

getSvAccuracy

public double getSvAccuracy()

Get the user SV accuray (meters).

Returns:

the user SV accuracy

setSvAccuracy

public void setSvAccuracy(double svAccuracy)

Set the user SV accuray (meters).

Parameters:

svAccuracy - the user SV accuracy

getSatH1

public int getSatH1()

Get the health identifier.

Returns:

health identifier

setSatH1

public void setSatH1(int satH1)

Set the health identifier.

Parameters:

satH1 - health identifier

createFromDrivers

public BeidouLegacyNavigationMessage createFromDrivers()

Create orbital parameters from current drivers values.

Returns:

created orbital parameters