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

Class FieldGalileoNavigationMessage<T extends CalculusFieldElement<T>>

java.lang.Object

org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

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

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

org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac<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:

FieldGNSSClockElements<T>, FieldTimeStamped<T>, ParameterDriversProvider

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

Field Summary

Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider

A_DOT, A_DOT_INDEX, CIC_INDEX, CIS_INDEX, CRC_INDEX, CRS_INDEX, CUC_INDEX, CUS_INDEX, DELTA_N0, DELTA_N0_DOT, DELTA_N0_DOT_INDEX, DELTA_N0_INDEX, I_DOT_INDEX, INCLINATION_COSINE, INCLINATION_RATE, INCLINATION_SINE, LATITUDE_COSINE, LATITUDE_SINE, LONGITUDE_RATE, OMEGA_DOT_INDEX, RADIUS_COSINE, RADIUS_SINE, SIZE, TIME, TIME_INDEX

Constructor Summary

Constructors

Constructor	Description
FieldGalileoNavigationMessage(Function<V,T> converter, FieldGalileoNavigationMessage<V> original)	Constructor from different field instance.
FieldGalileoNavigationMessage(Field<T> field, GalileoNavigationMessage original)	Constructor from non-field instance.

Method Summary

Modifier and Type	Method	Description
<U extends CalculusFieldElement<U>, G extends FieldGnssOrbitalElements<U, GalileoNavigationMessage>> G	changeField(Function<T,U> converter)	Create another field version of the instance.
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.
void	setBGDE1E5a(T bgd)	Setter for the E1/E5a broadcast group delay (s).
void	setBGDE5bE1(T bgd)	Setter for the E5b/E1 broadcast group delay (s).
void	setDataSource(int dataSource)	Setter for the data source.
void	setIODNav(int iod)	Setter for the Issue of Data of the navigation batch.
void	setSisa(T sisa)	Setter for the signal in space accuracy.
void	setSvHealth(T svHealth)	Setter for the SV health status.
GalileoNavigationMessage	toNonField()	Create a non-field version of the instance.

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

getEpochToc, getNavigationMessageType, getSqrtA, getTransmissionTime, setEpochToc, setSqrtA, setTransmissionTime

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

getPropagator, getPropagator

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

getAf0, getAf1, getAf2, getTGD, getToc, setAf0, setAf1, setAf2, setTGD, setToc

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

getDate, getE, getI0, getM0, getMeanMotion0, getMu, getOmega0, getPa, getSma, setE, setGnssDate, setI0, setM0, setOmega0, setPa, setSma

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

copyNonKeplerian, copySelectionSettings, createDriver, getADot, getADotDriver, getAngularVelocity, getCic, getCicDriver, getCis, getCisDriver, getCrc, getCrcDriver, getCrs, getCrsDriver, getCuc, getCucDriver, getCus, getCusDriver, getCycleDuration, getDeltaN0, getDeltaN0Dot, getDeltaN0DotDriver, getDeltaN0Driver, getIDot, getIDotDriver, getOmegaDot, getOmegaDotDriver, getParametersDrivers, getPRN, getSystem, getTime, getTimeDriver, getTimeScales, getWeek, getWeeksInCycle, isCivilianMessage, setADot, setCic, setCis, setCrc, setCrs, setCuc, setCus, setDeltaN0, setDeltaN0Dot, setIDot, setOmegaDot, setPRN, setTime, setWeek

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, getDate

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported

Constructor Details

FieldGalileoNavigationMessage

public FieldGalileoNavigationMessage(Field<T> field,
 GalileoNavigationMessage original)

Constructor from non-field instance.

Parameters:

field - field to which elements belong

original - regular non-field instance

FieldGalileoNavigationMessage

public FieldGalileoNavigationMessage(Function<V,T> converter,
 FieldGalileoNavigationMessage<V> original)

Constructor from different field instance.

Type Parameters:

V - type of the old field elements

Parameters:

converter - for field elements

original - regular non-field instance

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

changeField

public <U extends CalculusFieldElement<U>,
G extends FieldGnssOrbitalElements<U,
GalileoNavigationMessage>>
G changeField(Function<T,U> converter)

Create another field version of the instance.

Specified by:

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

Type Parameters:

U - type of the new field elements

G - type of the orbital elements (field version)

Parameters:

converter - for field 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)

setIODNav

public void setIODNav(int iod)

Setter for the Issue of Data of the navigation batch.

Parameters:

iod - the IOD to set

getDataSource

public int getDataSource()

Getter for the the data source.

Returns:

the data source

setDataSource

public void setDataSource(int dataSource)

Setter for the data source.

Parameters:

dataSource - data source

getBGDE1E5a

public T getBGDE1E5a()

Getter for the E1/E5a broadcast group delay.

Returns:

the E1/E5a broadcast group delay (s)

setBGDE1E5a

public void setBGDE1E5a(T bgd)

Setter for the E1/E5a broadcast group delay (s).

Parameters:

bgd - the E1/E5a broadcast group delay to set

setBGDE5bE1

public void setBGDE5bE1(T bgd)

Setter for the E5b/E1 broadcast group delay (s).

Parameters:

bgd - the E5b/E1 broadcast group delay to set

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

setSisa

public void setSisa(T sisa)

Setter for the signal in space accuracy.

Parameters:

sisa - the sisa to set

getSvHealth

public T getSvHealth()

Getter for the SV health status.

Returns:

the SV health status

setSvHealth

public void setSvHealth(T svHealth)

Setter for the SV health status.

Parameters:

svHealth - the SV health status to set