Uses of Interface
org.orekit.time.TimeScales

Packages that use TimeScales

Package	Description
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.data	This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.files.rinex.clock	This package provides classes related to navigation clock files.
org.orekit.files.rinex.navigation	This package provides classes related to RINEX navigation files.
org.orekit.files.rinex.navigation.parsers	This package provides parsers for the various RINEX navigation messages.
org.orekit.files.rinex.observation	This package provides classes related to RINEX observation files.
org.orekit.files.rinex.section	This package contains class managing the sections in RINEX files.
org.orekit.files.sinex	This package provides classes related to station data.
org.orekit.files.sinex.orbex	This package provides classes related to orbex file format.
org.orekit.files.sp3	This package provides a parser for orbit data stored in SP3 format.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.gnss	This package provides classes related to GNSS applications.
org.orekit.gnss.metric.messages.rtcm.ephemeris	This package provides all supported RTCM ephemeris messages.
org.orekit.gnss.metric.ntrip	This package provides streams reading from ntrip casters.
org.orekit.gnss.metric.parser	This package provides the top level MessagesParser class that can extract messages from binary containers like ByteArrayEncodedMessages or {link org.orekit.metric.gnss.ssr.parser.InputStreamEncodedMessages InputStreamEncodedMessages}.
org.orekit.models.earth.weather	This package provides models that simulate global weather conditions on Earth.
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.
org.orekit.utils	This package provides useful objects.

Uses of TimeScales in org.orekit.bodies

Methods in org.orekit.bodies with parameters of type TimeScales

Modifier and Type	Method	Description
static PredefinedIAUPoles	PredefinedIAUPoles.getIAUPole(JPLEphemeridesLoader.EphemerisType body, TimeScales timeScales)	Get a predefined IAU pole.

Constructors in org.orekit.bodies with parameters of type TimeScales

Modifier	Constructor	Description
	JPLEphemeridesLoader(String supportedNames, JPLEphemeridesLoader.EphemerisType generateType, DataProvidersManager dataProvidersManager, TimeScales timeScales, Frame gcrf, CelestialBodies celestialBodies)	Create a loader for JPL ephemerides binary files.
	LazyLoadedCelestialBodies(DataProvidersManager dataProvidersManager, TimeScales timeScales, Frame gcrf)	Create a celestial body factory with the given auxiliary data sources.

Uses of TimeScales in org.orekit.data

Methods in org.orekit.data that return TimeScales

Modifier and Type	Method	Description
TimeScales	CompositeDataContext.getTimeScales()
TimeScales	DataContext.getTimeScales()	Get a factory for constructing TimeScales based on the auxiliary data in this context.

Constructors in org.orekit.data with parameters of type TimeScales

Modifier	Constructor	Description
	CompositeDataContext(TimeScales timeScales, Frames frames, CelestialBodies celestialBodies, GravityFields gravityFields, GeoMagneticFields geoMagneticFields)	Simple constructor.
	FundamentalNutationArguments(IERSConventions conventions, TimeScale timeScale, InputStream stream, String name, TimeScales timeScales)	Build a model of fundamental arguments from an IERS table file.
	FundamentalNutationArguments(IERSConventions conventions, TimeScale timeScale, List<double[]> coefficients, TimeScales timeScales)	Build a model of fundamental arguments from an IERS table file.

Uses of TimeScales in org.orekit.files.rinex.clock

Methods in org.orekit.files.rinex.clock with parameters of type TimeScales

Modifier and Type	Method	Description
void	RinexClockHeader.parseProgramRunByDate(String line, TimeScales timeScales)	Parse program, run/by and date.

Constructors in org.orekit.files.rinex.clock with parameters of type TimeScales

Modifier	Constructor	Description
	RinexClockParser(Function<? super String,? extends Frame> frameBuilder, Function<? super String,? extends ObservationType> typeBuilder, Function<? super String,? extends TimeSystem> timeSystemBuilder, TimeScales timeScales)	Constructor, build the IGS clock file parser.

Uses of TimeScales in org.orekit.files.rinex.navigation

Methods in org.orekit.files.rinex.navigation that return TimeScales

Modifier and Type	Method	Description
TimeScales	RinexNavigationWriter.getTimeScales()	Get the known time scales.

Methods in org.orekit.files.rinex.navigation with parameters of type TimeScales

Modifier and Type	Method	Description
void	RinexNavigationHeader.parseProgramRunByDate(String line, TimeScales timeScales)	Parse program, run/by and date.

Constructors in org.orekit.files.rinex.navigation with parameters of type TimeScales

Modifier	Constructor	Description
	RinexNavigationParser(TimeScales timeScales, Frame inertial, Frame bodyFixed)	Constructor.
	RinexNavigationWriter(Appendable output, String outputName, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Simple constructor.

Constructor parameters in org.orekit.files.rinex.navigation with type arguments of type TimeScales

Modifier	Constructor	Description
	RinexNavigationWriter(Appendable output, String outputName, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Simple constructor.

Uses of TimeScales in org.orekit.files.rinex.navigation.parsers

Methods in org.orekit.files.rinex.navigation.parsers that return TimeScales

Modifier and Type	Method	Description
TimeScales	ParseInfo.getTimeScales()	Get the time scales.

Constructors in org.orekit.files.rinex.navigation.parsers with parameters of type TimeScales

Modifier	Constructor	Description
	ParseInfo(String name, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Constructor, build the ParseInfo object.

Uses of TimeScales in org.orekit.files.rinex.observation

Methods in org.orekit.files.rinex.observation with parameters of type TimeScales

Modifier and Type	Method	Description
void	RinexObservationHeader.parseProgramRunByDate(String line, TimeScales timeScales)	Parse program, run/by and date.

Constructors in org.orekit.files.rinex.observation with parameters of type TimeScales

Modifier	Constructor	Description
	RinexObservationParser(Function<? super String,? extends ObservationType> typeBuilder, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
	RinexObservationWriter(Appendable output, String outputName, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Simple constructor.

Constructor parameters in org.orekit.files.rinex.observation with type arguments of type TimeScales

Modifier	Constructor	Description
	RinexObservationParser(Function<? super String,? extends ObservationType> typeBuilder, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
	RinexObservationWriter(Appendable output, String outputName, BiFunction<SatelliteSystem,TimeScales,? extends TimeScale> timeScaleBuilder, TimeScales timeScales)	Simple constructor.

Uses of TimeScales in org.orekit.files.rinex.section

Methods in org.orekit.files.rinex.section with parameters of type TimeScales

Modifier and Type	Method	Description
protected void	RinexBaseHeader.parseProgramRunByDate(String prgm, String run, String date, TimeScales timeScales)	Parse program, run/by and date.
abstract void	RinexBaseHeader.parseProgramRunByDate(String line, TimeScales timeScales)	Parse program, run/by and date.

Uses of TimeScales in org.orekit.files.sinex

Methods in org.orekit.files.sinex that return TimeScales

Modifier and Type	Method	Description
TimeScales	AbstractSinex.getTimeScales()	Get the time scales.
TimeScales	AbstractSinexParser.getTimeScales()	Get the time scales.
protected TimeScales	ParseInfo.getTimeScales()	Get time scales.

Constructors in org.orekit.files.sinex with parameters of type TimeScales

Modifier	Constructor	Description
	AbstractSinex(double version, TimeScales timeScales, AbsoluteDate creationDate, AbsoluteDate startDate, AbsoluteDate endDate)	Simple constructor.
protected	AbstractSinexParser(TimeScales timeScales)	Simple constructor.
protected	ParseInfo(TimeScales timeScales)	Simple constructor.
	Sinex(double version, TimeScales timeScales, AbsoluteDate creationDate, AbsoluteDate startDate, AbsoluteDate endDate, Map<SatInSystem,Map<GnssSignal,Vector3D>> satellitesPhaseCenters, Map<String,Station> stations, Map<AbsoluteDate,SinexEopEntry> eop)	Simple constructor.
	SinexBias(double version, TimeScales timeScales, AbsoluteDate creationDate, AbsoluteDate startDate, AbsoluteDate endDate, BiasDescription description, Map<String,StationDifferentialSignalBias> stationsDsb, Map<SatInSystem,SatelliteDifferentialSignalBias> satellitesDsb, Map<String,StationObservableSpecificSignalBias> stationsOsb, Map<SatInSystem,SatelliteObservableSpecificSignalBias> satellitesOsb)	Simple constructor.
	SinexBiasParser(TimeScales timeScales)	Simple constructor.
	SinexParser(TimeScales timeScales)	Simple constructor.

Uses of TimeScales in org.orekit.files.sinex.orbex

Constructors in org.orekit.files.sinex.orbex with parameters of type TimeScales

Modifier	Constructor	Description
	OrbexParser(Function<? super String,? extends Frame> frameBuilder, Function<? super String,? extends TimeSystem> timeSystemBuilder, TimeScales timeScales)	Simple constructor.

Uses of TimeScales in org.orekit.files.sp3

Constructors in org.orekit.files.sp3 with parameters of type TimeScales

Modifier	Constructor	Description
	SP3Parser(double mu, int interpolationSamples, Function<? super String,? extends Frame> frameBuilder, TimeScales timeScales)	Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
	SP3Writer(Appendable output, String outputName, TimeScales timeScales)	Simple constructor.

Uses of TimeScales in org.orekit.frames

Methods in org.orekit.frames that return TimeScales

Modifier and Type	Method	Description
protected TimeScales	AbstractFrames.getTimeScales()	Get the time scales.
TimeScales	EOPHistory.getTimeScales()	Get the time scales used in computing EOP corrections.

Methods in org.orekit.frames with parameters of type TimeScales

Modifier and Type	Method	Description
EOPHistory	LazyLoadedEop.getEOPHistory(IERSConventions conventions, boolean simpleEOP, TimeScales timeScales)	Get Earth Orientation Parameters history.
static EopHistoryLoader.Parser	EopHistoryLoader.Parser.newBulletinAParser(IERSConventions conventions, ItrfVersionProvider itrfVersionProvider, TimeScales timeScales)	Create a new parser for EOP data in the Bulletin A format.
static EopHistoryLoader.Parser	EopHistoryLoader.Parser.newBulletinBParser(IERSConventions conventions, ItrfVersionProvider itrfVersionProvider, TimeScales timeScales)	Create a new parser for EOP data in the Bulletin B format.
static EopHistoryLoader.Parser	EopHistoryLoader.Parser.newEopC04Parser(IERSConventions conventions, TimeScales timeScales)	Create a new parser for EOP data in the EOP C04 format.
static EopHistoryLoader.Parser	EopHistoryLoader.Parser.newFinalsColumnsParser(IERSConventions conventions, ItrfVersionProvider itrfVersionProvider, TimeScales timeScales, boolean isNonRotatingOrigin)	Create a new parser for EOP data in the rapid and predicted columnar format.
static EopHistoryLoader.Parser	EopHistoryLoader.Parser.newFinalsXmlParser(IERSConventions conventions, ItrfVersionProvider itrfVersionProvider, TimeScales timeScales)	Create a new parser for EOP data in the rapid and predicted XML format.
static Frames	Frames.of(TimeScales timeScales, Supplier<Frame> icrfSupplier)	Create a set of frames from the given data.
static Frames	Frames.of(TimeScales timeScales, CelestialBodies celestialBodies)	Create a set of frames from the given data.

Constructors in org.orekit.frames with parameters of type TimeScales

Modifier	Constructor	Description
protected	AbstractFrames(TimeScales timeScales, Supplier<Frame> icrfSupplier)	Simple constructor.
	EclipticProvider(IERSConventions conventions, TimeScales timeScales)	Create a transform provider from MOD to an ecliptically aligned frame.
	EOPHistory(IERSConventions conventions, int interpolationDegree, Collection<? extends EOPEntry> data, boolean simpleEOP, TimeScales timeScales)	Simple constructor.
protected	GTODProvider(IERSConventions conventions, EOPHistory eopHistory, TimeScales timeScales)	Simple constructor.
	LazyLoadedFrames(LazyLoadedEop lazyLoadedEop, TimeScales timeScales, CelestialBodies celestialBodies)	Create a collection of frames from the given auxiliary data.

Uses of TimeScales in org.orekit.gnss

Methods in org.orekit.gnss with parameters of type TimeScales

Modifier and Type	Method	Description
abstract TimeScale	ObservationTimeScale.getTimeScale(TimeScales timeScales)	Get time scale.
TimeScale	PredefinedTimeSystem.getTimeScale(TimeScales timeScales)	Get the time scale corresponding to time system.
TimeScale	TimeSystem.getTimeScale(TimeScales timeScales)	Get the time scale corresponding to time system.

Constructors in org.orekit.gnss with parameters of type TimeScales

Modifier	Constructor	Description
	SEMParser(String supportedNames, DataProvidersManager dataProvidersManager, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Create a SEM loader/parser with the given source of SEM auxiliary data files.
	YUMAParser(String supportedNames, DataProvidersManager dataProvidersManager, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Uses of TimeScales in org.orekit.gnss.metric.messages.rtcm.ephemeris

Methods in org.orekit.gnss.metric.messages.rtcm.ephemeris with parameters of type TimeScales

Modifier and Type	Method	Description
GLONASSFdmaNavigationMessage	Rtcm1020Data.getGlonassNavigationMessage(TimeScales timeScales)	Get the Glonass navigation message corresponding to the current RTCM data.

Uses of TimeScales in org.orekit.gnss.metric.ntrip

Methods in org.orekit.gnss.metric.ntrip that return TimeScales

Modifier and Type	Method	Description
TimeScales	NtripClient.getTimeScales()	Get the known time scales.

Methods in org.orekit.gnss.metric.ntrip with parameters of type TimeScales

Modifier and Type	Method	Description
abstract MessagesParser	Type.getParser(List<Integer> messages, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Get the message parser associated to the SSR type.

Constructors in org.orekit.gnss.metric.ntrip with parameters of type TimeScales

Modifier	Constructor	Description
	NtripClient(String host, int port, TimeScales timeScales, int maxRetries, Frame inertial, Frame bodyFixed)	Build a client for NTRIP.

Uses of TimeScales in org.orekit.gnss.metric.parser

Methods in org.orekit.gnss.metric.parser with parameters of type TimeScales

Modifier and Type	Method	Description
ParsedMessage	MessageType.parse(EncodedMessage encodedMessage, int messageNumber, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Parse an encoded message.

Constructors in org.orekit.gnss.metric.parser with parameters of type TimeScales

Modifier	Constructor	Description
	IgsSsrMessagesParser(List<Integer> messages, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Constructor.
protected	MessagesParser(List<Integer> messages, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Constructor.
	RtcmMessagesParser(List<Integer> messages, TimeScales timeScales, Frame inertial, Frame bodyFixed)	Constructor.

Uses of TimeScales in org.orekit.models.earth.weather

Constructors in org.orekit.models.earth.weather with parameters of type TimeScales

Modifier	Constructor	Description
	GlobalPressureTemperature2(DataSource source, TimeScales timeScales)	Constructor with source of GPT2 auxiliary data given by user.
	GlobalPressureTemperature2w(DataSource source, TimeScales timeScales)	Constructor with supported names and source of GPT2w auxiliary data given by user.

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

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

Modifier and Type	Method	Description
TimeScales	FieldGnssOrbitalElements.getTimeScales()	Get known time scales.
TimeScales	GNSSOrbitalElements.getTimeScales()	Get known time scales.
TimeScales	GNSSOrbitalElementsFactory.getTimeScales()	Get known time scales.

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

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.
	AbstractNavigationMessageFactory(double angularVelocity, TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, double mu)	Simple 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.
	BeidouAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple constructor.
	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.
	BeidouCivilianNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, BeidouCivilianType beidouType, BeidouSatelliteType satelliteType)	Simple 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.
	BeidouLegacyNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, boolean d2)	Simple 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.
	CivilianNavigationMessageFactory(double angularVelocity, TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, double mu, boolean cnv2)	Simple constructor.
	FieldAbstractNavigationMessage(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.
protected	FieldGnssOrbitalElements(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.
protected	FieldGnssOrbitalElements(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.
	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.
	GalileoAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple constructor.
	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.
	GalileoNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple 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.
protected	GNSSOrbitalElementsFactory(double angularVelocity, TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, double mu)	Simple constructor.
	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.
	GPSAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple 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.
	GPSCivilianNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, boolean cnv2)	Simple 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.
	GPSLegacyNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple 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.
	LegacyNavigationMessageFactory(double angularVelocity, TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, double mu)	Simple 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.
	NavICAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple 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.
	NavICL1NvNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple 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.
	NavICLegacyNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple 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.
	QZSSAlmanacFactory(TimeScales timeScales, SatelliteSystem system, Frame inertial, Frame bodyFixed)	Simple 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.
	QZSSCivilianNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed, boolean cnv2)	Simple 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.
	QZSSLegacyNavigationMessageFactory(TimeScales timeScales, SatelliteSystem system, String type, Frame inertial, Frame bodyFixed)	Simple constructor.

Uses of TimeScales in org.orekit.time

Classes in org.orekit.time that implement TimeScales

Modifier and Type	Class	Description
class	AbstractTimeScales	Abstract base class for TimeScales that implements some common functionality.
class	LazyLoadedTimeScales	An implementation of TimeScales that loads auxiliary data, leap seconds and UT1-UTC, when it is first accessed.

Methods in org.orekit.time that return TimeScales

Modifier and Type	Method	Description
static TimeScales	TimeScales.of(Collection<? extends OffsetModel> utcMinusTai, BiFunction<? super IERSConventions,? super TimeScales,? extends Collection<? extends EOPEntry>> eopSupplier)	Create a set of time scales where all the data is loaded from the given functions.

Methods in org.orekit.time with parameters of type TimeScales

Modifier and Type	Method	Description
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createBesselianEpoch(T besselianEpoch, TimeScales timeScales)	Build an instance corresponding to a Besselian Epoch (BE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createJulianEpoch(T julianEpoch, TimeScales timeScales)	Build an instance corresponding to a Julian Epoch (JE).
Instant	AbsoluteDate.toInstant(TimeScales timeScales)	Convert the instance to a Java Instant.
Instant	FieldAbsoluteDate.toInstant(TimeScales timeScales)	Convert the instance to a Java Instant.

Method parameters in org.orekit.time with type arguments of type TimeScales

Modifier and Type	Method	Description
static TimeScales	TimeScales.of(Collection<? extends OffsetModel> utcMinusTai, BiFunction<? super IERSConventions,? super TimeScales,? extends Collection<? extends EOPEntry>> eopSupplier)	Create a set of time scales where all the data is loaded from the given functions.

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

Modifier	Constructor	Description
	GNSSDate(int weekNumber, double secondsInWeek, SatelliteSystem system, DateComponents reference, TimeScales timeScales)	Build an instance corresponding to a GNSS date.
	GNSSDate(int weekNumber, double secondsInWeek, SatelliteSystem system, TimeScales timeScales)	Build an instance corresponding to a GNSS date.
	GNSSDate(int weekNumber, TimeOffset secondsInWeek, SatelliteSystem system, DateComponents reference, TimeScales timeScales)	Build an instance corresponding to a GNSS date.
	GNSSDate(int weekNumber, TimeOffset secondsInWeek, SatelliteSystem system, TimeScales timeScales)	Build an instance corresponding to a GNSS date.
	GNSSDate(AbsoluteDate date, SatelliteSystem system, TimeScales timeScales)	Build an instance from an absolute date.

Uses of TimeScales in org.orekit.utils

Methods in org.orekit.utils with parameters of type TimeScales

Modifier and Type	Method	Description
double	IERSConventions.evaluateTC(AbsoluteDate date, TimeScales timeScales)	Evaluate the date offset between the current date and the reference date.
<T extends CalculusFieldElement<T>> T	IERSConventions.evaluateTC(FieldAbsoluteDate<T> date, TimeScales timeScales)	Evaluate the date offset between the current date and the reference date.
abstract TimeVectorFunction	IERSConventions.getEOPTidalCorrection(TimeScales timeScales)	Get the function computing tidal corrections for Earth Orientation Parameters.
abstract TimeScalarFunction	IERSConventions.getGASTFunction(TimeScale ut1, EOPHistory eopHistory, TimeScales timeScales)	Get the function computing Greenwich apparent sidereal time, in radians.
abstract TimeScalarFunction	IERSConventions.getGMSTFunction(TimeScale ut1, TimeScales timeScales)	Get the function computing Greenwich mean sidereal time, in radians.
abstract TimeScalarFunction	IERSConventions.getGMSTRateFunction(TimeScale ut1, TimeScales timeScales)	Get the function computing Greenwich mean sidereal time rate, in radians per second.
abstract TimeScalarFunction	IERSConventions.getMeanObliquityFunction(TimeScales timeScales)	Get the function computing mean obliquity of the ecliptic.
abstract FundamentalNutationArguments	IERSConventions.getNutationArguments(TimeScale timeScale, TimeScales timeScales)	Get the fundamental nutation arguments.
protected FundamentalNutationArguments	IERSConventions.getNutationArguments(TimeScales timeScales)	Get the fundamental nutation arguments.
IERSConventions.NutationCorrectionConverter	IERSConventions.getNutationCorrectionConverter(TimeScales timeScales)	Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
abstract TimeVectorFunction	IERSConventions.getNutationFunction(TimeScales timeScales)	Get the function computing the nutation angles.
AbsoluteDate	IERSConventions.getNutationReferenceEpoch(TimeScales timeScales)	Get the reference epoch for fundamental nutation arguments.
abstract TimeVectorFunction	IERSConventions.getPrecessionFunction(TimeScales timeScales)	Get the function computing the precession angles.
abstract TimeVectorFunction	IERSConventions.getTideFrequencyDependenceFunction(TimeScale ut1, TimeScales timeScales)	Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
abstract TimeVectorFunction	IERSConventions.getXYSpXY2Function(TimeScales timeScales)	Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.