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

Class AbstractNavigationMessageFactory<O extends AbstractNavigationMessage<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>

Type Parameters:

O - type of the orbital elements

All Implemented Interfaces:

Cloneable, OrbitalParameterFactory<O>

Direct Known Subclasses:

BeidouCivilianNavigationMessageFactory, BeidouLegacyNavigationMessageFactory, CivilianNavigationMessageFactory, GalileoNavigationMessageFactory, LegacyNavigationMessageFactory, NavICL1NvNavigationMessageFactory

public abstract class AbstractNavigationMessageFactory<O extends AbstractNavigationMessage<O>>
extends GNSSOrbitalElementsFactory<O>

Factory for AbstractNavigationMessage.

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

Method Summary

Modifier and Type	Method	Description
GNSSDate	getTransmissionTime()	Get transmission time.
void	setTransmissionTime(GNSSDate transmissionTime)	Set transmission time.

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

AbstractNavigationMessageFactory

public AbstractNavigationMessageFactory(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

getTransmissionTime

public GNSSDate getTransmissionTime()

Get transmission time.

Returns:

transmission time

setTransmissionTime

public void setTransmissionTime(GNSSDate transmissionTime)

Set transmission time.

Parameters:

transmissionTime - transmission time