Uses of Class
org.orekit.time.FieldGNSSDate
Packages that use FieldGNSSDate
Package
Description
This package provides classes related to navigation data containing in
GNSS almanacs and navigation messages.
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Uses of FieldGNSSDate in org.orekit.propagation.analytical.gnss.data
Methods in org.orekit.propagation.analytical.gnss.data that return FieldGNSSDateModifier and TypeMethodDescriptionFieldGNSSClockElements.getTimeOfClock()Get the time of clock.FieldGnssOrbitalElements.getTimeOfClock()Get the time of clock.FieldGnssOrbitalElements.getTimeOfEphemeris()Get the time of ephemeris.FieldAbstractNavigationMessage.getTransmissionTime()Getter for transmission time.Constructors in org.orekit.propagation.analytical.gnss.data with parameters of type FieldGNSSDateModifierConstructorDescriptionFieldAbstractNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime) Creates a new instance.FieldBeidouAlmanac(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, int health) Creates a new instance.FieldBeidouCivilianNavigationMessage(BeidouCivilianType beidouType, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T iscB1CD, T iscB1CP, T iscB2AD, int sisaiOe, int sisaiOcb, int sisaiOc1, int sisaiOc2, int sismai, int health, int integrityFlags, T tgdB1Cp, T tgdB2ap, T tgdB2bI, BeidouSatelliteType satelliteType) Creates a new instance.FieldBeidouLegacyNavigationMessage(boolean d2, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int aode, int aodc, int satH1, T tgd1, T tgd2, T svAccuracy) Creates a new instance.FieldCivilianNavigationMessage(boolean cnv2, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, T svAccuracy, int svHealth, T iscL1CA, T iscL1CD, T iscL1CP, T iscL2C, T iscL5I5, T iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags) Creates a new instance.FieldGalileoAlmanac(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, int healthE5a, int healthE5b, int healthE1, int iod) Creates a new instance.FieldGalileoNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iodNav, int dataSource, T bgdE1E5a, T bgdE5bE1, T sisa, T svHealth) Creates a new instance.protectedFieldGnssOrbitalElements(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc) Creates a new instance.protectedFieldGnssOrbitalElements(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T aDot, T deltaN0, T deltaN0Dot, T iDot, T omegaDot, T cuc, T cus, T crc, T crs, T cic, T cis, T af0, T af1, T af2, T tgd, FieldGNSSDate<T> toc) Creates a new instance.FieldGPSAlmanac(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, String source, int svn, int health, int ura, int satConfiguration) Creates a new instance.FieldGPSCivilianNavigationMessage(boolean cnv2, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, T svAccuracy, int svHealth, T iscL1CA, T iscL1CD, T iscL1CP, T iscL2C, T iscL5I5, T iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags) Creates a new instance.FieldGPSLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags) Creates a new instance.FieldLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags) Creates a new instance.FieldNavICAlmanac(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc) Creates a new instance.FieldNavicL1NvNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int referenceSignalFlag, int urai, int l1SpsHealth, T tgdSL5, T iscSL1P, T iscL1DL1P, T iscL1PS, T iscL1DS) Creates a new instance.FieldNavicLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags) Creates a new instance.FieldQZSSAlmanac(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, String source, int health) Creates a new instance.FieldQZSSCivilianNavigationMessage(boolean cnv2, double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, T svAccuracy, int svHealth, T iscL1CA, T iscL1CD, T iscL1CP, T iscL2C, T iscL5I5, T iscL5Q5, int uraiEd, int uraiNed0, int uraiNed1, int uraiNed2, int flags) Creates a new instance.FieldQZSSLegacyNavigationMessage(double angularVelocity, int weeksInCycle, TimeScales timeScales, String type, int prn, FieldGNSSDate<T> toe, FieldKeplerianOrbit<T> orbit, T[] nonKeplerian, T tgd, FieldGNSSDate<T> toc, FieldGNSSDate<T> transmissionTime, int iode, int iodc, T svAccuracy, int svHealth, int fitInterval, int l2Codes, int l2PFlags) Creates a new instance.