Class LegacyNavigationMessage
- java.lang.Object
-
- org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
- org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
- org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
-
- All Implemented Interfaces:
GNSSClockElements
,GNSSOrbitalElements
,TimeStamped
- Direct Known Subclasses:
GPSLegacyNavigationMessage
,QZSSLegacyNavigationMessage
public class LegacyNavigationMessage extends AbstractNavigationMessage implements GNSSClockElements
Container for data contained in a GPS/QZNSS legacy navigation message.- Since:
- 11.0
- Author:
- Bryan Cazabonne
-
-
Constructor Summary
Constructors Modifier Constructor Description protected
LegacyNavigationMessage(double mu, double angularVelocity, int weekNumber)
Constructor.
-
Method Summary
All Methods Instance Methods Concrete Methods 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).double
getSvAccuracy()
Getter for the user SV accuray (meters).int
getSvHealth()
Getter for the satellite health status.double
getTGD()
Getter for the Group Delay Differential (s).void
setFitInterval(int fitInterval)
Setter for the fit interval.void
setIODC(int value)
Setter for the Issue of Data Clock.void
setIODE(double value)
Setter for the Issue of Data Ephemeris.void
setSvAccuracy(double svAccuracy)
Setter for the user SV accuracy.void
setSvHealth(int svHealth)
Setter for the satellite health status.void
setTGD(double time)
Setter for the Group Delay Differential (s).-
Methods inherited from class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
getAf2, getCic, getCis, getCrc, getCrs, getCuc, getCus, getDeltaN, getEpochToc, getIDot, getMeanMotion, getSqrtA, getTransmissionTime, setAf2, setCic, setCis, setCrc, setCrs, setCuc, setCus, setDeltaN, setEpochToc, setIDot, setSqrtA, setTransmissionTime
-
Methods inherited from class org.orekit.propagation.analytical.gnss.data.CommonGnssData
getAf0, getAf1, getAngularVelocity, getCycleDuration, getDate, getE, getI0, getM0, getMu, getOmega0, getOmegaDot, getPa, getPRN, getSma, getTime, getWeek, setAf0, setAf1, setDate, setE, setI0, setM0, setOmega0, setOmegaDot, setPa, setPRN, setSma, 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.propagation.analytical.gnss.data.GNSSClockElements
getAf0, getAf1, getAf2, getCycleDuration, getToc
-
Methods inherited from interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
getAngularVelocity, getCycleDuration, getE, getI0, getM0, getMu, getOmega0, getOmegaDot, getPa, getPRN, getPropagator, getPropagator, getPropagator, getSma, getTime, getWeek
-
Methods inherited from interface org.orekit.time.TimeStamped
durationFrom, getDate
-
-
-
-
Field Detail
-
LNAV
public static final String LNAV
Identifier for message type.- See Also:
- Constant Field Values
-
-
Constructor Detail
-
LegacyNavigationMessage
protected LegacyNavigationMessage(double mu, double angularVelocity, int weekNumber)
Constructor.- Parameters:
mu
- Earth's universal gravitational parameterangularVelocity
- mean angular velocity of the Earth for the GNSS modelweekNumber
- number of weeks in the GNSS cycle
-
-
Method Detail
-
getIODE
public int getIODE()
Getter for the Issue Of Data Ephemeris (IODE).- Returns:
- the Issue Of Data Ephemeris (IODE)
-
setIODE
public void setIODE(double value)
Setter for the Issue of Data Ephemeris.- Parameters:
value
- the IODE to set
-
getIODC
public int getIODC()
Getter for the Issue Of Data Clock (IODC).- Returns:
- the Issue Of Data Clock (IODC)
-
setIODC
public void setIODC(int value)
Setter for the Issue of Data Clock.- Parameters:
value
- the IODC to set
-
getTGD
public double getTGD()
Getter for the Group Delay Differential (s).- Specified by:
getTGD
in interfaceGNSSClockElements
- Returns:
- the Group Delay Differential in seconds
-
setTGD
public void setTGD(double time)
Setter for the Group Delay Differential (s).- Parameters:
time
- the group delay differential to set
-
getSvAccuracy
public double getSvAccuracy()
Getter for the user SV accuray (meters).- Returns:
- the user SV accuracy
-
setSvAccuracy
public void setSvAccuracy(double svAccuracy)
Setter for the user SV accuracy.- Parameters:
svAccuracy
- the value to set
-
getSvHealth
public int getSvHealth()
Getter for the satellite health status.- Returns:
- the satellite health status
-
setSvHealth
public void setSvHealth(int svHealth)
Setter for the satellite health status.- Parameters:
svHealth
- the value to set
-
getFitInterval
public int getFitInterval()
Getter for the fit interval.- Returns:
- the fit interval
- Since:
- 12.0
-
setFitInterval
public void setFitInterval(int fitInterval)
Setter for the fit interval.- Parameters:
fitInterval
- fit interval- Since:
- 12.0
-
-