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

Class LegacyNavigationMessage<O extends LegacyNavigationMessage<O>>

java.lang.Object

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

org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements<O>

org.orekit.propagation.analytical.gnss.data.CommonGnssData<O>

org.orekit.propagation.analytical.gnss.data.AbstractAlmanac<O>

org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage<O>

org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage<O>

Type Parameters:

O - type of the orbital elements

All Implemented Interfaces:

GNSSClockElements, NavigationMessage, TimeStamped, ParameterDriversProvider

Direct Known Subclasses:

GPSLegacyNavigationMessage, NavICLegacyNavigationMessage, QZSSLegacyNavigationMessage

public abstract class LegacyNavigationMessage<O extends LegacyNavigationMessage<O>>
extends AbstractNavigationMessage<O>
implements GNSSClockElements

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

Since:

11.0

Author:

Bryan Cazabonne

Field Summary

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

AF0, AF1, AF2

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

ARGUMENT_OF_PERIGEE, ECCENTRICITY, INCLINATION, MEAN_ANOMALY, NODE_LONGITUDE, SEMI_MAJOR_AXIS

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

Modifier	Constructor	Description
protected	LegacyNavigationMessage(double mu, double angularVelocity, int weeksInCycle, TimeScales timeScales, SatelliteSystem system, String type)	Constructor.
protected	LegacyNavigationMessage(FieldLegacyNavigationMessage<T,A> original)	Constructor from field 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.
double	getSvAccuracy()	Getter for the user SV accuray (meters).
int	getSvHealth()	Getter for the satellite health status.
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	setL2Codes(int l2Codes)	Set the codes on L2 channel.
void	setL2PFlags(int l2PFlags)	Set the L2 P data flags.
void	setSvAccuracy(double svAccuracy)	Setter for the user SV accuracy.
void	setSvHealth(int svHealth)	Setter for the satellite health status.

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

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

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

getPropagator, getPropagator

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

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

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, toField

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.propagation.analytical.gnss.data.GNSSClockElements

getAf0, getAf1, getAf2, getTGD, getToc

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

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

Methods inherited from interface org.orekit.time.TimeStamped

durationFrom, getDate

Constructor Details

LegacyNavigationMessage

protected LegacyNavigationMessage(double mu,
 double angularVelocity,
 int weeksInCycle,
 TimeScales timeScales,
 SatelliteSystem system,
 String type)

Constructor.

Parameters:

mu - Earth's universal gravitational parameter

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

weeksInCycle - number of weeks in the GNSS cycle

timeScales - known time scales

system - 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

LegacyNavigationMessage

protected LegacyNavigationMessage(FieldLegacyNavigationMessage<T,A> original)

Constructor from field instance.

Type Parameters:

T - type of the field elements

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

Parameters:

original - regular field instance

Method Details

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

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

getL2Codes

public int getL2Codes()

Get the codes on L2 channel.

Returns:

codes on L2 channel

Since:

14.0

setL2Codes

public void setL2Codes(int l2Codes)

Set the codes on L2 channel.

Parameters:

l2Codes - 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

setL2PFlags

public void setL2PFlags(int l2PFlags)

Set the L2 P data flags.

Parameters:

l2PFlags - L2 P data flags

Since:

14.0