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

Class FieldLegacyNavigationMessage<T extends CalculusFieldElement<T>,O extends LegacyNavigationMessage<O>>

java.lang.Object

org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements<T,O>

org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage<T,O>

org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage<T,O>

Type Parameters:

T - type of the field elements

O - type of the orbital elements (non-field version)

All Implemented Interfaces:

FieldOrbitalParameters<T>, FieldGNSSClockElements<T>, FieldTimeStamped<T>

Direct Known Subclasses:

FieldGPSLegacyNavigationMessage, FieldNavicLegacyNavigationMessage, FieldQZSSLegacyNavigationMessage

public abstract class FieldLegacyNavigationMessage<T extends CalculusFieldElement<T>,O extends LegacyNavigationMessage<O>>
extends FieldAbstractNavigationMessage<T,O>

Container for data contained in a GPS/QZNSS legacy navigation message.

Since:

13.0

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor	Description
FieldLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Creates a new instance.

Method Summary

Modifier and Type	Method	Description
int	getFitInterval()	Getter for the fit interval.
int	getIODC()	Getter for the Issue Of Data Clock (IODC).
int	getIODE()	Getter for the Issue Of Data Ephemeris (IODE).
int	getL2Codes()	Get the codes on L2 channel.
int	getL2PFlags()	Get the L2 P data flags.
T	getSvAccuracy()	Getter for the user SV accuray (meters).
int	getSvHealth()	Getter for the satellite health status.

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

getTransmissionTime

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

getADot, getAf0, getAf1, getAf2, getAngularVelocity, getCic, getCis, getCrc, getCrs, getCuc, getCus, getCycleDuration, getDate, getDeltaN0, getDeltaN0Dot, getIDot, getOmegaDot, getOrbit, getPrn, getTgd, getTimeOfClock, getTimeOfEphemeris, getTimeScales, getType, getWeeksInCycle, isCivilianMessage, toArray, toField, toNonField

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.time.FieldTimeStamped

durationFrom, durationFrom

Constructor Details

FieldLegacyNavigationMessage

public FieldLegacyNavigationMessage(double angularVelocity,
 int weeksInCycle,
 TimeScales timeScales,
 String type,
 int prn,
 FieldGNSSDate<T> toe,
 FieldKeplerianOrbit<T> orbit,
 T[] nonKeplerian,
 T tgd,
 FieldGNSSDate<T> toc,
 FieldGNSSDate<T> transmissionTime,
 int iode,
 int iodc,
 T svAccuracy,
 int svHealth,
 int fitInterval,
 int l2Codes,
 int l2PFlags)

Creates a new instance.

Parameters:

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

weeksInCycle - number of weeks in the GNSS cycle

timeScales - known time scales

type - type (null if not a navigation message)

prn - PRN number of the satellite

toe - time of ephemeris (must be consistent with orbit)

orbit - Keplerian orbit in Earth-frozen frame

nonKeplerian - 15 non-Keplerian parameters (in the order given by NonKeplerianDriversFactory

tgd - group delay differential TGD for L1-L2 correction

toc - time of clock

transmissionTime - transmission time

iode - issue of data, ephemeris

iodc - issue of data, clock

svAccuracy - user SV accuracy (m)

svHealth - satellite health status

fitInterval - fit interval

l2Codes - codes on L2 channel

l2PFlags - L2 P data flags.

Since:

14.0

Method Details

getIODE

public int getIODE()

Getter for the Issue Of Data Ephemeris (IODE).

Returns:

the Issue Of Data Ephemeris (IODE)

getIODC

public int getIODC()

Getter for the Issue Of Data Clock (IODC).

Returns:

the Issue Of Data Clock (IODC)

getSvAccuracy

public T getSvAccuracy()

Getter for the user SV accuray (meters).

Returns:

the user SV accuracy

getSvHealth

public int getSvHealth()

Getter for the satellite health status.

Returns:

the satellite health status

getFitInterval

public int getFitInterval()

Getter for the fit interval.

Returns:

the fit interval

getL2Codes

public int getL2Codes()

Get the codes on L2 channel.

Returns:

codes on L2 channel

Since:

14.0

getL2PFlags

public int getL2PFlags()

Get the L2 P data flags.

Returns:

L2 P data flags

Since:

14.0