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

Class FieldGalileoNavigationMessage<T extends CalculusFieldElement<T>>

java.lang.Object

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

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

org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage<T>

Type Parameters:

T - type of the field elements

All Implemented Interfaces:

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

public class FieldGalileoNavigationMessage<T extends CalculusFieldElement<T>>
extends FieldAbstractNavigationMessage<T,GalileoNavigationMessage>

Container for data contained in a Galileo navigation message.

Since:

13.0

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor	Description
FieldGalileoNavigationMessage(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 iodNav, int dataSource, T bgdE1E5a, T bgdE5bE1, T sisa, T svHealth)	Creates a new instance.

Method Summary

Modifier and Type	Method	Description
T	getBGDE1E5a()	Getter for the E1/E5a broadcast group delay.
T	getBGDE5bE1()	Getter for the the Broadcast Group Delay E5b/E1.
int	getDataSource()	Getter for the the data source.
int	getIODNav()	Getter for the the Issue Of Data (IOD).
T	getSisa()	Getter for the signal in space accuracy (m).
T	getSvHealth()	Getter for the SV health status.
<U extends CalculusFieldElement<U>> FieldGalileoNavigationMessage<U>	toField(FieldKeplerianOrbit<U> orbit, U[] nonKeplerian, Function<T,U> converter)	Create another field version of the instance.
GalileoNavigationMessage	toNonField()	Create a non-field version of the instance.

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

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

FieldGalileoNavigationMessage

public FieldGalileoNavigationMessage(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 iodNav,
 int dataSource,
 T bgdE1E5a,
 T bgdE5bE1,
 T sisa,
 T svHealth)

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

iodNav - issue of Data of the navigation batch

dataSource - data source

bgdE1E5a - E1/E5a broadcast group delay (s)

bgdE5bE1 - E5b/E1 broadcast group delay (s)

sisa - signal in space accuracy

svHealth - satellite health status

Since:

14.0

Method Details

toNonField

public GalileoNavigationMessage toNonField()

Create a non-field version of the instance.

Specified by:

toNonField in class FieldGnssOrbitalElements<T extends CalculusFieldElement<T>,GalileoNavigationMessage>

Returns:

non-field version of the instance

toField

public <U extends CalculusFieldElement<U>>
FieldGalileoNavigationMessage<U> toField(FieldKeplerianOrbit<U> orbit,
 U[] nonKeplerian,
 Function<T,U> converter)

Create another field version of the instance.

Specified by:

toField in class FieldGnssOrbitalElements<T extends CalculusFieldElement<T>,GalileoNavigationMessage>

Type Parameters:

U - type of the new field elements

Parameters:

orbit - orbit in the correct gradient field

nonKeplerian - non-Keplerian parameters

converter - converter for remaining elements

Returns:

field version of the instance

getIODNav

public int getIODNav()

Getter for the the Issue Of Data (IOD).

Returns:

the Issue Of Data (IOD)

getDataSource

public int getDataSource()

Getter for the the data source.

Returns:

the data source

getBGDE1E5a

public T getBGDE1E5a()

Getter for the E1/E5a broadcast group delay.

Returns:

the E1/E5a broadcast group delay (s)

getBGDE5bE1

public T getBGDE5bE1()

Getter for the the Broadcast Group Delay E5b/E1.

Returns:

the Broadcast Group Delay E5b/E1 (s)

getSisa

public T getSisa()

Getter for the signal in space accuracy (m).

Returns:

the signal in space accuracy

getSvHealth

public T getSvHealth()

Getter for the SV health status.

Returns:

the SV health status