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

Class GalileoAlmanacFactory

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<GalileoAlmanac>

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

org.orekit.propagation.analytical.gnss.data.GalileoAlmanacFactory

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<GalileoAlmanac>

public class GalileoAlmanacFactory
extends GNSSOrbitalElementsFactory<GalileoAlmanac>

Factory for GalileoAlmanac.

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
GalileoAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
GalileoAlmanac	createFromDrivers()	Create orbital parameters from current drivers values.
int	getHealthE1()	Get the E1-B/C signal health status.
int	getHealthE5a()	Get the E5a signal health status.
int	getHealthE5b()	Get the E5b signal health status.
int	getIod()	Get the Issue of Data (IOD).
void	setHealthE1(int healthE1)	Set the E1-B/C signal health status.
void	setHealthE5a(int healthE5a)	Set the E5a signal health status.
void	setHealthE5b(int healthE5b)	Set the E5b signal health status.
void	setIod(int iod)	Set the Issue of Data (IOD).

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

GalileoAlmanacFactory

public GalileoAlmanacFactory(TimeScales timeScales,
 SatelliteSystem system,
 Frame inertial,
 Frame bodyFixed)

Simple constructor.

Parameters:

timeScales - known time scales

system - satellite system to use for interpreting week number

inertial - reference inertial frame

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

Method Details

getHealthE1

public int getHealthE1()

Get the E1-B/C signal health status.

Returns:

the E1-B/C signal health status

setHealthE1

public void setHealthE1(int healthE1)

Set the E1-B/C signal health status.

Parameters:

healthE1 - the E1-B/C signal health status

getHealthE5a

public int getHealthE5a()

Get the E5a signal health status.

Returns:

the E5a signal health status

setHealthE5a

public void setHealthE5a(int healthE5a)

Set the E5a signal health status.

Parameters:

healthE5a - the E5a signal health status

getHealthE5b

public int getHealthE5b()

Get the E5b signal health status.

Returns:

the E5b signal health status

setHealthE5b

public void setHealthE5b(int healthE5b)

Set the E5b signal health status.

Parameters:

healthE5b - the E5b signal health status

getIod

public int getIod()

Get the Issue of Data (IOD).

Returns:

the Issue Of Data

setIod

public void setIod(int iod)

Set the Issue of Data (IOD).

Parameters:

iod - the Issue Of Data

createFromDrivers

public GalileoAlmanac createFromDrivers()

Create orbital parameters from current drivers values.

Returns:

created orbital parameters