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

Class BeidouCivilianNavigationMessageFactory

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<BeidouCivilianNavigationMessage>

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

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

org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessageFactory

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<BeidouCivilianNavigationMessage>

public class BeidouCivilianNavigationMessageFactory
extends AbstractNavigationMessageFactory<BeidouCivilianNavigationMessage>

Factory for BeidouCivilianNavigationMessage.

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
BeidouCivilianNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, BeidouCivilianType beidouType, BeidouSatelliteType satelliteType)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
BeidouCivilianNavigationMessage	createFromDrivers()	Create orbital parameters from current drivers values.
BeidouCivilianType	getBeidouType()	Get the Beidou civilian message type.
int	getHealth()	Get health.
int	getIntegrityFlags()	Get B1C integrity flags.
int	getIodc()	Get the Issue Of Data Clock (IODC).
int	getIode()	Get the Issue Of Data Ephemeris (IODE).
double	getIscB1CD()	Get inter Signal Delay for B1 CD.
double	getIscB1CP()	Get inter Signal Delay for B1 CP.
double	getIscB2AD()	Get inter Signal Delay for B2 AD.
BeidouSatelliteType	getSatelliteType()	Get satellite type.
int	getSisaiOc1()	Get Signal In Space Accuracy Index (clock drift accuracy).
int	getSisaiOc2()	Get Signal In Space Accuracy Index (clock drift rate accuracy).
int	getSisaiOcb()	Get Signal In Space Accuracy Index (radial and clock).
int	getSisaiOe()	Get Signal In Space Accuracy Index (along track and across track).
int	getSismai()	Get Signal In Space Monitoring Accuracy Index.
double	getTgdB1Cp()	Get B1/B3 Group Delay Differential (s).
double	getTgdB2ap()	Get B2 AP Group Delay Differential (s).
double	getTgdB2bI()	Get B2B_i / B3I Group Delay Differential (s).
void	setHealth(int health)	Set health.
void	setIntegrityFlags(int integrityFlags)	Set B1C integrity flags.
void	setIodc(int iodc)	Set the Issue Of Data Clock (IODC).
void	setIode(int iode)	Set the Issue Of Data Ephemeris (IODE).
void	setIscB1CD(double iscB1CD)	Set inter Signal Delay for B1 CD.
void	setIscB1CP(double iscB1CP)	Set inter Signal Delay for B1 CP.
void	setIscB2AD(double iscB2AD)	Set inter Signal Delay for B2 AD.
void	setSatelliteType(BeidouSatelliteType satelliteType)	Set satellite type.
void	setSisaiOc1(int sisaiOc1)	Set Signal In Space Accuracy Index (clock drift accuracy).
void	setSisaiOc2(int sisaiOc2)	Set Signal In Space Accuracy Index (clock drift rate accuracy).
void	setSisaiOcb(int sisaiOcb)	Set Signal In Space Accuracy Index (radial and clock).
void	setSisaiOe(int sisaiOe)	Set Signal In Space Accuracy Index (along track and across track).
void	setSismai(int sismai)	Set Signal In Space Monitoring Accuracy Index.
void	setTgdB1Cp(double tgdB1Cp)	Set B1/B3 Group Delay Differential (s).
void	setTgdB2ap(double tgdB2ap)	Set B2 AP Group Delay Differential (s).
void	setTgdB2bI(double tgdB2bI)	Set B2B_i / B3I Group Delay Differential (s).

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

BeidouCivilianNavigationMessageFactory

public BeidouCivilianNavigationMessageFactory(TimeScales timeScales,
 SatelliteSystem system,
 String type,
 Frame inertial,
 Frame bodyFixed,
 BeidouCivilianType beidouType,
 BeidouSatelliteType satelliteType)

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

beidouType - Beidou civilian message type

satelliteType - satellite type

Method Details

getBeidouType

public BeidouCivilianType getBeidouType()

Get the Beidou civilian message type.

Returns:

Beidou civilian message type

getSatelliteType

public BeidouSatelliteType getSatelliteType()

Get satellite type.

Returns:

satellite type

setSatelliteType

public void setSatelliteType(BeidouSatelliteType satelliteType)

Set satellite type.

Parameters:

satelliteType - satellite type

getIode

public int getIode()

Get the Issue Of Data Ephemeris (IODE).

Returns:

the Issue Of Data Ephemeris (IODE)

setIode

public void setIode(int iode)

Set the Issue Of Data Ephemeris (IODE).

Parameters:

iode - the Issue Of Data Ephemeris (IODE)

getIodc

public int getIodc()

Get the Issue Of Data Clock (IODC).

Returns:

the Issue Of Data Clock (IODC)

setIodc

public void setIodc(int iodc)

Set the Issue Of Data Clock (IODC).

Parameters:

iodc - the Issue Of Data Clock (IODC)

getIscB1CD

public double getIscB1CD()

Get inter Signal Delay for B1 CD.

Returns:

inter signal delay

setIscB1CD

public void setIscB1CD(double iscB1CD)

Set inter Signal Delay for B1 CD.

Parameters:

iscB1CD - inter signal delay

getIscB2AD

public double getIscB2AD()

Get inter Signal Delay for B2 AD.

Returns:

inter signal delay

setIscB2AD

public void setIscB2AD(double iscB2AD)

Set inter Signal Delay for B2 AD.

Parameters:

iscB2AD - inter signal delay

getIscB1CP

public double getIscB1CP()

Get inter Signal Delay for B1 CP.

Returns:

inter signal delay

setIscB1CP

public void setIscB1CP(double iscB1CP)

Set inter Signal Delay for B1 CP.

Parameters:

iscB1CP - inter signal delay

getSisaiOe

public int getSisaiOe()

Get Signal In Space Accuracy Index (along track and across track).

Returns:

Signal In Space Accuracy Index (along track and across track)

setSisaiOe

public void setSisaiOe(int sisaiOe)

Set Signal In Space Accuracy Index (along track and across track).

Parameters:

sisaiOe - Signal In Space Accuracy Index (along track and across track)

getSisaiOcb

public int getSisaiOcb()

Get Signal In Space Accuracy Index (radial and clock).

Returns:

Signal In Space Accuracy Index (radial and clock)

setSisaiOcb

public void setSisaiOcb(int sisaiOcb)

Set Signal In Space Accuracy Index (radial and clock).

Parameters:

sisaiOcb - Signal In Space Accuracy Index (radial and clock)

getSisaiOc1

public int getSisaiOc1()

Get Signal In Space Accuracy Index (clock drift accuracy).

Returns:

Signal In Space Accuracy Index (clock drift accuracy)

setSisaiOc1

public void setSisaiOc1(int sisaiOc1)

Set Signal In Space Accuracy Index (clock drift accuracy).

Parameters:

sisaiOc1 - Signal In Space Accuracy Index (clock drift accuracy)

getSisaiOc2

public int getSisaiOc2()

Get Signal In Space Accuracy Index (clock drift rate accuracy).

Returns:

Signal In Space Accuracy Index (clock drift rate accuracy)

setSisaiOc2

public void setSisaiOc2(int sisaiOc2)

Set Signal In Space Accuracy Index (clock drift rate accuracy).

Parameters:

sisaiOc2 - Signal In Space Accuracy Index (clock drift rate accuracy)

getSismai

public int getSismai()

Get Signal In Space Monitoring Accuracy Index.

Returns:

Signal In Space Monitoring Accuracy Index

setSismai

public void setSismai(int sismai)

Set Signal In Space Monitoring Accuracy Index.

Parameters:

sismai - Signal In Space Monitoring Accuracy Index

getHealth

public int getHealth()

Get health.

Returns:

health

setHealth

public void setHealth(int health)

Set health.

Parameters:

health - health

getIntegrityFlags

public int getIntegrityFlags()

Get B1C integrity flags.

Returns:

B1C integrity flags

setIntegrityFlags

public void setIntegrityFlags(int integrityFlags)

Set B1C integrity flags.

Parameters:

integrityFlags - B1C integrity flags

getTgdB1Cp

public double getTgdB1Cp()

Get B1/B3 Group Delay Differential (s).

Returns:

B1/B3 Group Delay Differential (s)

setTgdB1Cp

public void setTgdB1Cp(double tgdB1Cp)

Set B1/B3 Group Delay Differential (s).

Parameters:

tgdB1Cp - B1/B3 Group Delay Differential (s)

getTgdB2ap

public double getTgdB2ap()

Get B2 AP Group Delay Differential (s).

Returns:

B2 AP Group Delay Differential (s)

setTgdB2ap

public void setTgdB2ap(double tgdB2ap)

Set B2 AP Group Delay Differential (s).

Parameters:

tgdB2ap - B2 AP Group Delay Differential (s)

getTgdB2bI

public double getTgdB2bI()

Get B2B_i / B3I Group Delay Differential (s).

Returns:

B2B_i / B3I Group Delay Differential (s)

setTgdB2bI

public void setTgdB2bI(double tgdB2bI)

Set B2B_i / B3I Group Delay Differential (s).

Parameters:

tgdB2bI - B2B_i / B3I Group Delay Differential (s)

createFromDrivers

public BeidouCivilianNavigationMessage createFromDrivers()

Create orbital parameters from current drivers values.

Returns:

created orbital parameters