Class GalileoNavigationMessage
- java.lang.Object
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- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider
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- org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements<O>
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- org.orekit.propagation.analytical.gnss.data.CommonGnssData<O>
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- org.orekit.propagation.analytical.gnss.data.AbstractAlmanac<O>
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- org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage<GalileoNavigationMessage>
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- org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
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- All Implemented Interfaces:
GNSSClockElements,NavigationMessage,TimeStamped,ParameterDriversProvider
public class GalileoNavigationMessage extends AbstractNavigationMessage<GalileoNavigationMessage>
Container for data contained in a Galileo navigation message.- Since:
- 11.0
- Author:
- Bryan Cazabonne
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Field Summary
Fields Modifier and Type Field Description static StringFNAVMessage type.static StringINAVMessage type.-
Fields inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData
AF0, AF1, AF2
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Fields inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
ARGUMENT_OF_PERIGEE, ECCENTRICITY, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS
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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
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Constructor Summary
Constructors Constructor Description GalileoNavigationMessage(FieldGalileoNavigationMessage<T> original)Constructor from field instance.GalileoNavigationMessage(TimeScales timeScales, SatelliteSystem system, String type)Constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description doublegetBGDE1E5a()Getter for the E1/E5a broadcast group delay.doublegetBGDE5bE1()Getter for the the Broadcast Group Delay E5b/E1.intgetDataSource()Getter for the the data source.intgetIODNav()Getter for the the Issue Of Data (IOD).doublegetSisa()Getter for the signal in space accuracy (m).doublegetSvHealth()Getter for the SV health status.voidsetBGDE1E5a(double bgd)Setter for the E1/E5a broadcast group delay (s).voidsetBGDE5bE1(double bgd)Setter for the E5b/E1 broadcast group delay (s).voidsetDataSource(int dataSource)Setter for the data source.voidsetIODNav(int iod)Setter for the Issue of Data of the navigation batch.voidsetSisa(double sisa)Setter for the signal in space accuracy.voidsetSvHealth(double svHealth)Setter for the SV health status.<T extends CalculusFieldElement<T>,F extends FieldGnssOrbitalElements<T,GalileoNavigationMessage>>
FtoField(Field<T> field)Create a field version of the instance.-
Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
getEpochToc, getNavigationMessageSubType, getNavigationMessageType, getSqrtA, getTransmissionTime, setEpochToc, setSqrtA, setTransmissionTime
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
getPropagator, getPropagator
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData
getAf0, getAf1, getAf2, getTGD, getToc, setAf0, setAf1, setAf2, setTGD, setToc
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Methods inherited from class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
getDate, getE, getEDriver, getI0, getI0Driver, getM0, getM0Driver, getMeanMotion0, getMu, getOmega0, getOmega0Driver, getPa, getPaDriver, getSma, getSmaDriver, setE, setGnssDate, setI0, setM0, setOmega0, setPa, setSma
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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
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Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
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Methods inherited from interface org.orekit.time.TimeStamped
durationFrom, getDate
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Field Detail
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INAV
public static final String INAV
Message type.- Since:
- 14.0
- See Also:
- Constant Field Values
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FNAV
public static final String FNAV
Message type.- Since:
- 14.0
- See Also:
- Constant Field Values
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Constructor Detail
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GalileoNavigationMessage
public GalileoNavigationMessage(TimeScales timeScales, SatelliteSystem system, String type)
Constructor.- Parameters:
timeScales- known time scalessystem- satellite system to consider for interpreting week number (may be different from real system, for example in Rinex nav, weeks are always according to GPS)type- message type
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GalileoNavigationMessage
public GalileoNavigationMessage(FieldGalileoNavigationMessage<T> original)
Constructor from field instance.- Type Parameters:
T- type of the field elements- Parameters:
original- regular field instance
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Method Detail
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toField
public <T extends CalculusFieldElement<T>,F extends FieldGnssOrbitalElements<T,GalileoNavigationMessage>> F toField(Field<T> field)
Create a field version of the instance.- Specified by:
toFieldin classGNSSOrbitalElements<GalileoNavigationMessage>- Type Parameters:
T- type of the field elementsF- type of the orbital elements (field version)- Parameters:
field- field to which elements belong- Returns:
- field version of the instance
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getIODNav
public int getIODNav()
Getter for the the Issue Of Data (IOD).- Returns:
- the Issue Of Data (IOD)
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setIODNav
public void setIODNav(int iod)
Setter for the Issue of Data of the navigation batch.- Parameters:
iod- the IOD to set
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getDataSource
public int getDataSource()
Getter for the the data source.- Returns:
- the data source
- Since:
- 12.0
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setDataSource
public void setDataSource(int dataSource)
Setter for the data source.- Parameters:
dataSource- data source- Since:
- 12.0
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getBGDE1E5a
public double getBGDE1E5a()
Getter for the E1/E5a broadcast group delay.- Returns:
- the E1/E5a broadcast group delay (s)
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setBGDE1E5a
public void setBGDE1E5a(double bgd)
Setter for the E1/E5a broadcast group delay (s).- Parameters:
bgd- the E1/E5a broadcast group delay to set
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setBGDE5bE1
public void setBGDE5bE1(double bgd)
Setter for the E5b/E1 broadcast group delay (s).- Parameters:
bgd- the E5b/E1 broadcast group delay to set
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getBGDE5bE1
public double getBGDE5bE1()
Getter for the the Broadcast Group Delay E5b/E1.- Returns:
- the Broadcast Group Delay E5b/E1 (s)
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getSisa
public double getSisa()
Getter for the signal in space accuracy (m).- Returns:
- the signal in space accuracy
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setSisa
public void setSisa(double sisa)
Setter for the signal in space accuracy.- Parameters:
sisa- the sisa to set
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getSvHealth
public double getSvHealth()
Getter for the SV health status.- Returns:
- the SV health status
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setSvHealth
public void setSvHealth(double svHealth)
Setter for the SV health status.- Parameters:
svHealth- the SV health status to set
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