Uses of Class
org.orekit.time.GNSSDate

Packages that use GNSSDate

Package	Description
org.orekit.propagation.analytical.gnss.data	This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
org.orekit.time	This independent package provides classes to handle epochs, time scales, and to compare instants together.

Uses of GNSSDate in org.orekit.propagation.analytical.gnss.data

Methods in org.orekit.propagation.analytical.gnss.data that return GNSSDate

Modifier and Type	Method	Description
GNSSDate	GNSSClockElements.getTimeOfClock()	Get the time of clock.
GNSSDate	GNSSOrbitalElements.getTimeOfClock()	Get the time of clock.
GNSSDate	GNSSOrbitalElementsFactory.getTimeOfClock()	Get the time of clock.
GNSSDate	GNSSOrbitalElements.getTimeOfEphemeris()	Get the time of ephemeris.
GNSSDate	GNSSOrbitalElementsFactory.getTimeOfEphemeris()	Get the time of ephemeris.
GNSSDate	AbstractNavigationMessage.getTransmissionTime()	Get transmission time.
GNSSDate	AbstractNavigationMessageFactory.getTransmissionTime()	Get transmission time.

Methods in org.orekit.propagation.analytical.gnss.data with parameters of type GNSSDate

Modifier and Type	Method	Description
void	GNSSOrbitalElementsFactory.setTimeOfClock(GNSSDate timeOfClock)	Set the time of clock.
void	GNSSOrbitalElementsFactory.setTimeOfEphemeris(GNSSDate timeOfEphemeris)	Set the time of ephemeris.
void	AbstractNavigationMessageFactory.setTransmissionTime(GNSSDate transmissionTime)	Set transmission time.

Constructors in org.orekit.propagation.analytical.gnss.data with parameters of type GNSSDate

Modifier	Constructor	Description
protected	AbstractNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime)	Constructor.
	BeidouAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, int health)	Build a new almanac.
	BeidouCivilianNavigationMessage(BeidouCivilianType beidouType, TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iode, int iodc, double iscB1CD, double iscB1CP, double iscB2AD, int sisaiOe, int sisaiOcb, int sisaiOc1, int sisaiOc2, int sismai, int health, int integrityFlags, double tgdB1Cp, double tgdB2ap, double tgdB2bI, BeidouSatelliteType satelliteType)	Constructor.
	BeidouLegacyNavigationMessage(boolean d2, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int aode, int aodc, int satH1, double tgd1, double tgd2, double svAccuracy)	Constructor.
protected	CivilianNavigationMessage(boolean cnv2, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, double svAccuracy, int svHealth, double iscL1CA, double iscL1CD, double iscL1CP, double iscL2C, double iscL5I5, double iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags)	Constructor.
	GalileoAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, int healthE5a, int healthE5b, int healthE1, int iod)	Build a new almanac.
	GalileoNavigationMessage(TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iodNav, int dataSource, double bgdE1E5a, double bgdE5bE1, double sisa, double svHealth)	Constructor.
protected	GNSSOrbitalElements(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc)	Creates a new instance.
	GPSAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, String source, int svn, int health, int ura, int satConfiguration)	Constructor.
	GPSCivilianNavigationMessage(boolean cnv2, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, double svAccuracy, int svHealth, double iscL1CA, double iscL1CD, double iscL1CP, double iscL2C, double iscL5I5, double iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags)	Constructor.
	GPSLegacyNavigationMessage(TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iode, int iodc, double svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Constructor.
protected	LegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iode, int iodc, double svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Constructor.
	NavICAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc)	Constructor.
	NavICL1NvNavigationMessage(TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int referenceSignalFlag, int urai, int l1SpsHealth, double tgdSL5, double iscSL1P, double iscL1DL1P, double iscL1PS, double iscL1DS)	Constructor.
	NavICLegacyNavigationMessage(TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iode, int iodc, double svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Constructor.
	QZSSAlmanac(TimeScales timeScales, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, String source, int health)	Constructor.
	QZSSCivilianNavigationMessage(boolean cnv2, TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, double svAccuracy, int svHealth, double iscL1CA, double iscL1CD, double iscL1CP, double iscL2C, double iscL5I5, double iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags)	Constructor.
	QZSSLegacyNavigationMessage(TimeScales timeScales, String type, int prn, GNSSDate toe, KeplerianOrbit orbit, double aDot, double deltaN0, double deltaN0Dot, double iDot, double omegaDot, double cuc, double cus, double crc, double crs, double cic, double cis, double af0, double af1, double af2, double tgd, GNSSDate toc, GNSSDate transmissionTime, int iode, int iodc, double svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags)	Constructor.

Uses of GNSSDate in org.orekit.time

Methods in org.orekit.time that return GNSSDate

Modifier and Type	Method	Description
GNSSDate	FieldGNSSDate.getGnssDate()	Get the underlying GNSS date.

Constructors in org.orekit.time with parameters of type GNSSDate

Modifier	Constructor	Description
	FieldGNSSDate(Field<T> field, GNSSDate gnssDate)	Build an instance from a GNSSDate.