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

Class QZSSCivilianNavigationMessageFactory

java.lang.Object

org.orekit.orbits.AbstractOrbitalParameterFactory<QZSSCivilianNavigationMessage>

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

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

org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessageFactory<QZSSCivilianNavigationMessage>

org.orekit.propagation.analytical.gnss.data.QZSSCivilianNavigationMessageFactory

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<QZSSCivilianNavigationMessage>

public class QZSSCivilianNavigationMessageFactory
extends CivilianNavigationMessageFactory<QZSSCivilianNavigationMessage>

Factory for QZSSCivilianNavigationMessage.

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
QZSSCivilianNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, boolean cnv2)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
QZSSCivilianNavigationMessage	createFromDrivers()	Create orbital parameters from current drivers values.

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

getFlags, getIscL1CA, getIscL1CD, getIscL1CP, getIscL2C, getIscL5I5, getIscL5Q5, getSvAccuracy, getSvHealth, getUraiEd, getUraiNed0, getUraiNed1, getUraiNed2, isCnv2, setFlags, setIscL1CA, setIscL1CD, setIscL1CP, setIscL2C, setIscL5I5, setIscL5Q5, setSvAccuracy, setSvHealth, setUraiEd, setUraiNed0, setUraiNed1, setUraiNed2

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

QZSSCivilianNavigationMessageFactory

public QZSSCivilianNavigationMessageFactory(TimeScales timeScales,
 SatelliteSystem system,
 String type,
 Frame inertial,
 Frame bodyFixed,
 boolean cnv2)

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

cnv2 - indicator for CNV 2 messages

Method Details

createFromDrivers

public QZSSCivilianNavigationMessage createFromDrivers()

Create orbital parameters from current drivers values.

Returns:

created orbital parameters