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

Class LegacyNavigationMessageFactory<O extends LegacyNavigationMessage<O>>

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<O>

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

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

org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessageFactory<O>

Type Parameters:

O - type of the orbital elements

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<O>

Direct Known Subclasses:

GPSLegacyNavigationMessageFactory, NavICLegacyNavigationMessageFactory, QZSSLegacyNavigationMessageFactory

public abstract class LegacyNavigationMessageFactory<O extends LegacyNavigationMessage<O>>
extends AbstractNavigationMessageFactory<O>

Factory for LegacyNavigationMessage.

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
LegacyNavigationMessageFactory(double angularVelocity, TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, double mu)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
int	getFitInterval()	Get the fit interval.
int	getIodc()	Get the Issue Of Data Clock (IODC).
int	getIode()	Get the Issue Of Data Ephemeris (IODE).
int	getL2Codes()	Get the codes on L2 channel.
int	getL2PFlags()	Get the L2 P data flags.
double	getSvAccuracy()	Get the user SV accuray (meters).
int	getSvHealth()	Get the satellite health status.
void	setFitInterval(int fitInterval)	Set the fit interval.
void	setIodc(int iodc)	Set the Issue Of Data Clock (IODC).
void	setIode(int iode)	Set the Issue Of Data Ephemeris (IODE).
void	setL2Codes(int l2Codes)	Set the codes on L2 channel.
void	setL2PFlags(int l2PFlags)	Set the L2 P data flags.
void	setSvAccuracy(double svAccuracy)	Set the user SV accuray (meters).
void	setSvHealth(int svHealth)	Set the satellite 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

Methods inherited from interface org.orekit.orbits.OrbitalParameterFactory

createFromDrivers

Constructor Details

LegacyNavigationMessageFactory

public LegacyNavigationMessageFactory(double angularVelocity,
 TimeScales timeScales,
 SatelliteSystem system,
 String type,
 Frame inertial,
 Frame bodyFixed,
 double mu)

Simple constructor.

Parameters:

angularVelocity - mean angular velocity of the Earth for the GNSS model

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

mu - central attraction coefficient (m³/s²)

Method Details

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)

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

getSvHealth

public int getSvHealth()

Get the satellite health status.

Returns:

the satellite health status

setSvHealth

public void setSvHealth(int svHealth)

Set the satellite health status.

Parameters:

svHealth - the satellite health status

getFitInterval

public int getFitInterval()

Get the fit interval.

Returns:

the fit interval

setFitInterval

public void setFitInterval(int fitInterval)

Set the fit interval.

Parameters:

fitInterval - fit interval

getL2Codes

public int getL2Codes()

Get the codes on L2 channel.

Returns:

codes on L2 channel

setL2Codes

public void setL2Codes(int l2Codes)

Set the codes on L2 channel.

Parameters:

l2Codes - codes on L2 channel

getL2PFlags

public int getL2PFlags()

Get the L2 P data flags.

Returns:

L2 P data flags

setL2PFlags

public void setL2PFlags(int l2PFlags)

Set the L2 P data flags.

Parameters:

l2PFlags - L2 P data flags