Uses of Annotation Interface
org.orekit.annotation.DefaultDataContext

Packages that use DefaultDataContext

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.control.heuristics.lambert	This package provides routines related to Lambert problems.
org.orekit.control.indirect.shooting.propagation	This package provides classes relative to the propagation part of indirect shooting.
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.estimation.measurements.model	This package contains physical models for measurement prediction.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.files.ccsds.definitions	This package contains definitions for CCSDS objects (frames, time systems...).
org.orekit.files.ccsds.ndm	This package contains the base hierarchy for CCSDS ADM, ODM and TDM.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.iirv	This package provides parsers and writers for Improved Interrange Vector (IIRV) messages.
org.orekit.files.iirv.terms	This package collects classes representing the individual terms that make up an IIRV vector.
org.orekit.files.ilrs	This package provides parsers for laser ranging data stored in CDR and CPF formats.
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.observation	This package provides classes related to RINEX observation files.
org.orekit.files.sp3	This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces.drag	This package provides all drag-related forces.
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.forces.gravity.potential	This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.radiation	This package provides all radiation pressure related forces.
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.antenna	This package provides classes related to receiver and satellites antenna modeling.
org.orekit.gnss.metric.messages.rtcm.ephemeris	This package provides all supported RTCM ephemeris messages.
org.orekit.gnss.metric.messages.ssr.subtype	This package provides all supported IGS SSR Sub-Type Message.
org.orekit.models.earth	This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.atmosphere	This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.atmosphere.data	This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.
org.orekit.models.earth.displacement	This package provides models computing reference points displacements on Earth surface.
org.orekit.models.earth.ionosphere	This package provides models that simulate the impact of the ionosphere.
org.orekit.models.earth.ionosphere.nequick	This package provides classes for implementing NeQuick ionosphere models.
org.orekit.models.earth.troposphere	This package provides models that simulate the impact of the troposphere.
org.orekit.models.earth.weather	This package provides models that simulate global weather conditions on Earth.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.gnss.data	This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
org.orekit.propagation.analytical.intelsat	This package provides classes to propagate Intelsat's 11 elements.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.analytical.tle.generation	This package provides classes related to TLE generation.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.conversion.averaging	This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.
org.orekit.propagation.conversion.averaging.converters	This package wraps conversions from an osculating orbit to an averaged state according to a given theory (usually via a fixed-point algorithm using the inverse conversion).
org.orekit.propagation.conversion.osc2mean	This package provides the ability to convert osculating orbits into mean orbits according to different theories (Brouwer-Lyddane, Eckstein-Hechler, SGP4/SDP4, DSST) with different conversion algorithms (fixed-point, least-squares).
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
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 DefaultDataContext in org.orekit.attitudes

Constructors in org.orekit.attitudes with annotations of type DefaultDataContext

Modifier	Constructor	Description
	AlignedAndConstrained(Vector3D primarySat, TargetProvider primaryTarget, Vector3D secondarySat, TargetProvider secondaryTarget, ExtendedPositionProvider sun, OneAxisEllipsoid earth)	Constructor with default inertial frame.
	FrameAlignedProvider(Rotation rotation)	Creates new instance.

Uses of DefaultDataContext in org.orekit.bodies

Methods in org.orekit.bodies with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static void	CelestialBodyFactory.addCelestialBodyLoader(String name, CelestialBodyLoader loader)	Add a loader for celestial bodies.
static void	CelestialBodyFactory.addDefaultCelestialBodyLoader(String supportedNames)	Add the default loaders for all predefined celestial bodies.
static void	CelestialBodyFactory.addDefaultCelestialBodyLoader(String name, String supportedNames)	Add the default loaders for celestial bodies.
static void	CelestialBodyFactory.clearCelestialBodyCache()	Clear all loaded celestial bodies.
static void	CelestialBodyFactory.clearCelestialBodyCache(String name)	Clear the specified celestial body from the internal cache.
static void	CelestialBodyFactory.clearCelestialBodyLoaders()	Clear loaders for all celestial bodies.
static void	CelestialBodyFactory.clearCelestialBodyLoaders(String name)	Clear loaders for one celestial body.
static CelestialBody	CelestialBodyFactory.getBody(String name)	Get a celestial body.
static LazyLoadedCelestialBodies	CelestialBodyFactory.getCelestialBodies()	Get the instance of CelestialBodies that is called by the static methods in this class.
static CelestialBody	CelestialBodyFactory.getEarth()	Get the Earth singleton body.
static CelestialBody	CelestialBodyFactory.getEarthMoonBarycenter()	Get the Earth-Moon barycenter singleton bodies pair.
static CR3BPSystem	CR3BPFactory.getEarthMoonCR3BP()	Get the Earth-Moon CR3BP singleton bodies pair.
static CelestialBody	CelestialBodyFactory.getJupiter()	Get the Jupiter singleton body.
static CelestialBody	CelestialBodyFactory.getMars()	Get the Mars singleton body.
static CelestialBody	CelestialBodyFactory.getMercury()	Get the Mercury singleton body.
static CelestialBody	CelestialBodyFactory.getMoon()	Get the Moon singleton body.
static CelestialBody	CelestialBodyFactory.getNeptune()	Get the Neptune singleton body.
static CelestialBody	CelestialBodyFactory.getPluto()	Get the Pluto singleton body.
static CelestialBody	CelestialBodyFactory.getSaturn()	Get the Saturn singleton body.
static CelestialBody	CelestialBodyFactory.getSolarSystemBarycenter()	Get the solar system barycenter aggregated body.
static CelestialBody	CelestialBodyFactory.getSun()	Get the Sun singleton body.
static CR3BPSystem	CR3BPFactory.getSunEarthCR3BP(AbsoluteDate date, TimeScale timeScale)	Get the Sun-Earth CR3BP singleton bodies pair.
static CR3BPSystem	CR3BPFactory.getSunJupiterCR3BP(AbsoluteDate date, TimeScale timeScale)	Get the Sun-Jupiter CR3BP singleton bodies pair.
static CelestialBody	CelestialBodyFactory.getUranus()	Get the Uranus singleton body.
static CelestialBody	CelestialBodyFactory.getVenus()	Get the Venus singleton body.

Constructors in org.orekit.bodies with annotations of type DefaultDataContext

Modifier	Constructor	Description
	AnalyticalLunarPositionProvider()	Constructor with default data context.
	AnalyticalSolarPositionProvider()	Constructor with default data context.
	JPLEphemeridesLoader(String supportedNames, JPLEphemeridesLoader.EphemerisType generateType)	Create a loader for JPL ephemerides binary files.

Uses of DefaultDataContext in org.orekit.control.heuristics.lambert

Methods in org.orekit.control.heuristics.lambert with annotations of type DefaultDataContext

Modifier and Type	Method	Description
String	LambertBoundaryConditions.toString()
String	LambertSolution.toString()

Uses of DefaultDataContext in org.orekit.control.indirect.shooting.propagation

Constructors in org.orekit.control.indirect.shooting.propagation with annotations of type DefaultDataContext

Modifier	Constructor	Description
	ShootingPropagationSettings(List<ForceModel> forceModels, AdjointDynamicsProvider adjointDynamicsProvider, ShootingIntegrationSettings integrationSettings)	Simple constructor with default frame and attitude provider.

Uses of DefaultDataContext in org.orekit.data

Methods in org.orekit.data with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static LazyLoadedDataContext	DataContext.getDefault()	Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.

Constructors in org.orekit.data with annotations of type DefaultDataContext

Modifier	Constructor	Description
	FundamentalNutationArguments(IERSConventions conventions, TimeScale timeScale, InputStream stream, String name)	Build a model of fundamental arguments from an IERS table file.
	FundamentalNutationArguments(IERSConventions conventions, TimeScale timeScale, List<double[]> coefficients)	Build a model of fundamental arguments from an IERS table file.

Uses of DefaultDataContext in org.orekit.estimation.measurements.model

Constructors in org.orekit.estimation.measurements.model with annotations of type DefaultDataContext

Modifier	Constructor	Description
	TopocentricAzElModel(BodyShape bodyShape, SignalTravelTimeModel signalTravelTimeModel)	Constructor with default inertial frame.

Uses of DefaultDataContext in org.orekit.estimation.measurements.modifiers

Methods in org.orekit.estimation.measurements.modifiers with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static Gradient[]	AberrationModifier.fieldNaturalToProper(Gradient[] naturalRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame)	Natural to proper correction for aberration of light.
static Gradient[]	AberrationModifier.fieldProperToNatural(Gradient[] properRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame)	Proper to natural correction for aberration of light.
static double[]	AberrationModifier.naturalToProper(double[] naturalRaDec, Observer observer, AbsoluteDate date, Frame frame)	Natural to proper correction for aberration of light.
static double[]	AberrationModifier.properToNatural(double[] properRaDec, Observer observer, AbsoluteDate date, Frame frame)	Proper to natural correction for aberration of light.

Constructors in org.orekit.estimation.measurements.modifiers with annotations of type DefaultDataContext

Modifier	Constructor	Description
	AberrationModifier()	Empty constructor.

Uses of DefaultDataContext in org.orekit.files.ccsds.definitions

Methods in org.orekit.files.ccsds.definitions with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static BodyFacade	BodyFacade.create(CenterName centerName)	Create a body facade from an input center name.
CelestialBody	CenterName.getCelestialBody()	Get the celestial body corresponding to the CCSDS constant.

Uses of DefaultDataContext in org.orekit.files.ccsds.ndm

Constructors in org.orekit.files.ccsds.ndm with annotations of type DefaultDataContext

Modifier	Constructor	Description
	ParserBuilder()	Simple constructor.
	WriterBuilder()	Simple constructor.

Uses of DefaultDataContext in org.orekit.files.general

Methods in org.orekit.files.general with annotations of type DefaultDataContext

Modifier and Type	Method	Description
OrekitEphemerisFile.OrekitEphemerisSegment	OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states)	Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
OrekitEphemerisFile.OrekitEphemerisSegment	OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states, int interpolationSampleSize)	Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
OrekitEphemerisFile.OrekitEphemerisSegment	OrekitEphemerisFile.OrekitSatelliteEphemeris.addNewSegment(List<SpacecraftState> states, CelestialBody body, int interpolationSampleSize)	Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.

Uses of DefaultDataContext in org.orekit.files.iirv

Methods in org.orekit.files.iirv with annotations of type DefaultDataContext

Modifier and Type	Method	Description
Frame	IIRVSegment.getFrame()	Get the reference frame for this ephemeris segment.
Frame	IIRVVector.getFrame()	Returns the Frame associated with the IIRV vector based on its CoordinateSystemTerm.

Uses of DefaultDataContext in org.orekit.files.iirv.terms

Methods in org.orekit.files.iirv.terms with annotations of type DefaultDataContext

Modifier and Type	Method	Description
Frame	CoordinateSystemTerm.getFrame()	Returns the Frame specified within the IIRV using the default data context.

Uses of DefaultDataContext in org.orekit.files.ilrs

Methods in org.orekit.files.ilrs with annotations of type DefaultDataContext

Modifier and Type	Method	Description
String	CRDHeader.getH4CrdString()	Get a string representation of the H4 in the CRD format.
String	CRD.AnglesMeasurement.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.Calibration.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.CalibrationDetail.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.FrRangeMeasurement.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.MeteorologicalMeasurement.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.NptRangeMeasurement.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.RangeSupplement.toCrdString()	Get a string representation of the instance in the CRD format.
String	CRD.AnglesMeasurement.toString()
String	CRD.Calibration.toString()
String	CRD.FrRangeMeasurement.toString()
String	CRD.MeteorologicalMeasurement.toString()
String	CRD.NptRangeMeasurement.toString()
String	CRD.RangeSupplement.toString()

Constructors in org.orekit.files.ilrs with annotations of type DefaultDataContext

Modifier	Constructor	Description
	CPFParser()	Default constructor.
	CRDParser()	Default constructor.

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

Constructors in org.orekit.files.rinex.clock with annotations of type DefaultDataContext

Modifier	Constructor	Description
	RinexClockParser()	Create a clock file parser using default values.

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

Constructors in org.orekit.files.rinex.navigation with annotations of type DefaultDataContext

Modifier	Constructor	Description
	RinexNavigationParser()	Constructor.
	RinexNavigationWriter(Appendable output, String outputName)	Simple constructor.

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

Methods in org.orekit.files.rinex.observation with annotations of type DefaultDataContext

Modifier and Type	Method	Description
void	RinexObservationWriter.writeCompleteFile(RinexObservation rinexObservation)	Write a complete observation file.
void	RinexObservationWriter.writeHeader(RinexObservationHeader header)	Write header.

Constructors in org.orekit.files.rinex.observation with annotations of type DefaultDataContext

Modifier	Constructor	Description
	RinexObservationParser()	Simple constructor.
	RinexObservationWriter(Appendable output, String outputName)	Simple constructor.

Uses of DefaultDataContext in org.orekit.files.sp3

Constructors in org.orekit.files.sp3 with annotations of type DefaultDataContext

Modifier	Constructor	Description
	SP3Parser()	Create an SP3 parser using default values.
	SP3Parser(double mu, int interpolationSamples, Function<? super String,? extends Frame> frameBuilder)	Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.

Uses of DefaultDataContext in org.orekit.forces.drag

Constructors in org.orekit.forces.drag with annotations of type DefaultDataContext

Modifier	Constructor	Description
	TimeSpanDragForce(Atmosphere atmosphere, DragSensitive spacecraft)	Constructor with default UTC time scale for the default names of the drag parameter drivers.

Uses of DefaultDataContext in org.orekit.forces.gravity

Constructors in org.orekit.forces.gravity with annotations of type DefaultDataContext

Modifier	Constructor	Description
	DeSitterRelativity()	Constructor.
	OceanTides(Frame centralBodyFrame, double ae, double mu, boolean poleTide, double step, int nbPoints, int degree, int order, IERSConventions conventions, UT1Scale ut1)	Simple constructor.
	OceanTides(Frame centralBodyFrame, double ae, double mu, int degree, int order, IERSConventions conventions, UT1Scale ut1)	Simple constructor.

Uses of DefaultDataContext in org.orekit.forces.gravity.potential

Methods in org.orekit.forces.gravity.potential with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static void	GravityFieldFactory.addDefaultOceanTidesReaders()	Add the default READERS for ocean tides.
static void	GravityFieldFactory.addDefaultPotentialCoefficientsReaders()	Add the default readers for gravity fields.
static void	GravityFieldFactory.addOceanTidesReader(OceanTidesReader reader)	Add a reader for ocean tides.
static void	GravityFieldFactory.addPotentialCoefficientsReader(PotentialCoefficientsReader reader)	Add a reader for gravity fields.
static void	GravityFieldFactory.clearOceanTidesReaders()	Clear ocean tides readers.
static void	GravityFieldFactory.clearPotentialCoefficientsReaders()	Clear gravity field readers.
static void	GravityFieldFactory.configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients oldc)	Configure ocean load deformation coefficients.
static NormalizedSphericalHarmonicsProvider	GravityFieldFactory.getConstantNormalizedProvider(int degree, int order, AbsoluteDate freezingDate)	Get the constant gravity field coefficients provider from the first supported file.
static UnnormalizedSphericalHarmonicsProvider	GravityFieldFactory.getConstantUnnormalizedProvider(int degree, int order, AbsoluteDate freezingDate)	Get the constant gravity field coefficients provider from the first supported file.
static LazyLoadedGravityFields	GravityFieldFactory.getGravityFields()	Get the instance of GravityFields that is called by the static methods of this class.
static NormalizedSphericalHarmonicsProvider	GravityFieldFactory.getNormalizedProvider(int degree, int order)	Get the gravity field coefficients provider from the first supported file.
static OceanLoadDeformationCoefficients	GravityFieldFactory.getOceanLoadDeformationCoefficients()	Get the configured ocean load deformation coefficients.
static List<OceanTidesWave>	GravityFieldFactory.getOceanTidesWaves(int degree, int order)	Get the ocean tides waves from the first supported file.
static UnnormalizedSphericalHarmonicsProvider	GravityFieldFactory.getUnnormalizedProvider(int degree, int order)	Get the gravity field coefficients provider from the first supported file.
static PotentialCoefficientsReader	GravityFieldFactory.readGravityField(int maxParseDegree, int maxParseOrder)	Read a gravity field coefficients provider from the first supported file.

Constructors in org.orekit.forces.gravity.potential with annotations of type DefaultDataContext

Modifier	Constructor	Description
	GRGSFormatReader(String supportedNames, boolean missingCoefficientsAllowed)	Simple constructor.
	ICGEMFormatReader(String supportedNames, boolean missingCoefficientsAllowed)	Simple constructor.
protected	PotentialCoefficientsReader(String supportedNames, boolean missingCoefficientsAllowed)	Simple constructor.
	SHMFormatReader(String supportedNames, boolean missingCoefficientsAllowed)	Simple constructor.

Uses of DefaultDataContext in org.orekit.forces.radiation

Constructors in org.orekit.forces.radiation with annotations of type DefaultDataContext

Modifier	Constructor	Description
	ECOM2(int nD, int nB, double value, ExtendedPositionProvider sun, double equatorialRadius)	Constructor.
	KnockeRediffusedForceModel(ExtendedPositionProvider sun, RadiationSensitive spacecraft, double equatorialRadius, double angularResolution)	Default Constructor.

Uses of DefaultDataContext in org.orekit.frames

Methods in org.orekit.frames with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static void	FramesFactory.addDefaultEOP1980HistoryLoaders(String rapidDataColumnsSupportedNames, String rapidDataXMLSupportedNames, String eopC04SupportedNames, String bulletinBSupportedNames, String bulletinASupportedNames, String csvSupportedNames)	Add the default loaders EOP history (IAU 1980 precession/nutation).
static void	FramesFactory.addDefaultEOP2000HistoryLoaders(String rapidDataColumnsSupportedNames, String xmlSupportedNames, String eopC04SupportedNames, String bulletinBSupportedNames, String bulletinASupportedNames, String csvSupportedNames)	Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
static void	FramesFactory.addEOPHistoryLoader(IERSConventions conventions, EopHistoryLoader loader)	Add a loader for Earth Orientation Parameters history.
static void	FramesFactory.clearEOPHistoryLoaders()	Clear loaders for Earth Orientation Parameters history.
Frame	HelmertTransformation.Predefined.createTransformedITRF(Frame parent, String name)	Create an ITRF frame by transforming another ITRF frame.
static FactoryManagedFrame	FramesFactory.getCIRF(IERSConventions conventions, boolean simpleEOP)	Get the CIRF2000 reference frame.
static ITRFVersion.Converter	ITRFVersion.getConverter(ITRFVersion origin, ITRFVersion destination)	Find a converter between specified ITRF frames.
static Frame	FramesFactory.getEcliptic(IERSConventions conventions)	Get the ecliptic frame.
static FactoryManagedFrame	FramesFactory.getEME2000()	Get the unique EME2000 frame.
static EOPHistory	FramesFactory.getEOPHistory(IERSConventions conventions, boolean simpleEOP)	Get Earth Orientation Parameters history.
static Frame	FramesFactory.getFrame(Predefined factoryKey)	Get one of the predefined frames.
static LazyLoadedFrames	FramesFactory.getFrames()	Get the instance of Frames that is called by the static methods in this class.
static Frame	FramesFactory.getGCRF()	Get the unique GCRF frame.
static FactoryManagedFrame	FramesFactory.getGTOD(boolean applyEOPCorr)	Get the GTOD reference frame.
static FactoryManagedFrame	FramesFactory.getGTOD(IERSConventions conventions, boolean simpleEOP)	Get the GTOD reference frame.
static Frame	FramesFactory.getICRF()	Get the unique ICRF frame.
static VersionedITRF	FramesFactory.getITRF(ITRFVersion version, IERSConventions conventions, boolean simpleEOP)	Get a specific International Terrestrial Reference Frame.
static FactoryManagedFrame	FramesFactory.getITRF(IERSConventions conventions, boolean simpleEOP)	Get an unspecified International Terrestrial Reference Frame.
static FactoryManagedFrame	FramesFactory.getITRFEquinox(IERSConventions conventions, boolean simpleEOP)	Get the equinox-based ITRF reference frame.
static FactoryManagedFrame	FramesFactory.getMOD(boolean applyEOPCorr)	Get the MOD reference frame.
static FactoryManagedFrame	FramesFactory.getMOD(IERSConventions conventions)	Get the MOD reference frame.
static FactoryManagedFrame	FramesFactory.getPZ9011(IERSConventions convention, boolean simpleEOP)	Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
static FactoryManagedFrame	FramesFactory.getTEME()	Get the TEME reference frame.
static FactoryManagedFrame	FramesFactory.getTIRF(IERSConventions conventions)	Get the TIRF reference frame, ignoring tidal effects.
static FactoryManagedFrame	FramesFactory.getTIRF(IERSConventions conventions, boolean simpleEOP)	Get the TIRF reference frame.
static FactoryManagedFrame	FramesFactory.getTOD(boolean applyEOPCorr)	Get the TOD reference frame.
static FactoryManagedFrame	FramesFactory.getTOD(IERSConventions conventions, boolean simpleEOP)	Get the TOD reference frame.
HelmertTransformation	HelmertTransformation.Predefined.getTransformation()	Get the underlying HelmertTransformation.
static FactoryManagedFrame	FramesFactory.getVeis1950()	Get the VEIS 1950 reference frame.
static void	FramesFactory.setEOPContinuityThreshold(double threshold)	Set the threshold to check EOP continuity.

Constructors in org.orekit.frames with annotations of type DefaultDataContext

Modifier	Constructor	Description
	EclipticProvider(IERSConventions conventions)	Create a transform provider from MOD to an ecliptically aligned frame.
protected	EOPHistory(IERSConventions conventions, int interpolationDegree, Collection<? extends EOPEntry> data, boolean simpleEOP)	Simple constructor.
	ITRFVersionLoader()	Build a loader for ITRF version configuration file using the default name.
	ITRFVersionLoader(String supportedNames)	Build a loader for ITRF version configuration file.

Uses of DefaultDataContext in org.orekit.gnss

Methods in org.orekit.gnss with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static Frame	IGSUtils.guessFrame(String name)	Default string to Frame conversion for SP3Parser or RinexClockParser.

Constructors in org.orekit.gnss with annotations of type DefaultDataContext

Modifier	Constructor	Description
	SEMParser(String supportedNames)	Simple constructor.
	YUMAParser(String supportedNames)	Simple constructor.

Uses of DefaultDataContext in org.orekit.gnss.antenna

Constructors in org.orekit.gnss.antenna with annotations of type DefaultDataContext

Modifier	Constructor	Description
	AntexLoader(String supportedNames)	Simple constructor.

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

Methods in org.orekit.gnss.metric.messages.rtcm.ephemeris with annotations of type DefaultDataContext

Modifier and Type	Method	Description
BeidouLegacyNavigationMessage	Rtcm1042Data.getBeidouNavigationMessage()	Get the Beidou navigation message corresponding to the current RTCM data.
GalileoNavigationMessage	Rtcm1046Data.getGalileoNavigationMessage()	Get the Galileo navigation message corresponding to the current RTCM data.
GLONASSFdmaNavigationMessage	Rtcm1020Data.getGlonassNavigationMessage()	Get the Glonass navigation message corresponding to the current RTCM data.
GPSLegacyNavigationMessage	Rtcm1019Data.getGpsNavigationMessage()	Get the GPS navigation message corresponding to the current RTCM data.
QZSSLegacyNavigationMessage	Rtcm1044Data.getQzssNavigationMessage()	Get the QZSS navigation message corresponding to the current RTCM data.

Uses of DefaultDataContext in org.orekit.gnss.metric.messages.ssr.subtype

Methods in org.orekit.gnss.metric.messages.ssr.subtype with annotations of type DefaultDataContext

Modifier and Type	Method	Description
SsrVtecIonosphericModel	SsrIm201.getIonosphericModel()	Get the ionospheric model adapted to the current IM201 message.
SsrVtecIonosphericModel	SsrIm201.getIonosphericModel(Frame itrf)	Get the ionospheric model adapted to the current IM201 message.

Uses of DefaultDataContext in org.orekit.models.earth

Methods in org.orekit.models.earth with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static GeoMagneticField	GeoMagneticFieldFactory.getField(GeoMagneticFieldFactory.FieldModel type, double year)	Get the GeoMagneticField for the given model type and year.
static LazyLoadedGeoMagneticFields	GeoMagneticFieldFactory.getGeoMagneticFields()	Get the instance of GeoMagneticFields that is called by methods in this class.
static GeoMagneticField	GeoMagneticFieldFactory.getIGRF(double year)	Get the IGRF model for the given year.
static GeoMagneticField	GeoMagneticFieldFactory.getWMM(double year)	Get the WMM model for the given year.

Uses of DefaultDataContext in org.orekit.models.earth.atmosphere

Constructors in org.orekit.models.earth.atmosphere with annotations of type DefaultDataContext

Modifier	Constructor	Description
	DTM2000(DTM2000InputParameters parameters, ExtendedPositionProvider sun, BodyShape earth)	Simple constructor for independent computation.
	JB2006(JB2006InputParameters parameters, ExtendedPositionProvider sun, BodyShape earth)	Constructor with space environment information for internal computation.
	JB2008(JB2008InputParameters parameters, ExtendedPositionProvider sun, BodyShape earth)	Constructor with space environment information for internal computation.
	NRLMSISE00(NRLMSISE00InputParameters parameters, ExtendedPositionProvider sun, BodyShape earth)	Constructor.

Uses of DefaultDataContext in org.orekit.models.earth.atmosphere.data

Constructors in org.orekit.models.earth.atmosphere.data with annotations of type DefaultDataContext

Modifier	Constructor	Description
	CssiSpaceWeatherData(String supportedNames)	Simple constructor.
	CssiSpaceWeatherData(DataSource source)	Simple constructor which use the default data context.
	JB2008SpaceEnvironmentData(String supportedNamesSOL, String supportedNamesDTC)	Simple constructor.
	JB2008SpaceEnvironmentData(DataSource sourceSolfsmy, DataSource sourceDtc)	Simple constructor.
	MarshallSolarActivityFutureEstimation(String supportedNames, MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel)	Simple constructor.
	MarshallSolarActivityFutureEstimation(DataSource source, MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel)	Simple constructor which use the default data context.
	MarshallSolarActivityFutureEstimationLoader(MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel)	Simple constructor.

Uses of DefaultDataContext in org.orekit.models.earth.displacement

Constructors in org.orekit.models.earth.displacement with annotations of type DefaultDataContext

Modifier	Constructor	Description
	OceanLoadingCoefficientsBLQFactory(String supportedNames)	Simple constructor.

Uses of DefaultDataContext in org.orekit.models.earth.ionosphere

Constructors in org.orekit.models.earth.ionosphere with annotations of type DefaultDataContext

Modifier	Constructor	Description
	GlobalIonosphereMapModel(OneAxisEllipsoid earth, String supportedNames)	Constructor with supported names given by user.
	KlobucharIonoCoefficientsLoader()	Constructor with default supported names.
	KlobucharIonoCoefficientsLoader(String supportedNames)	Constructor with supported names given by user.
	KlobucharIonoModel(OneAxisEllipsoid earth, double[] alpha, double[] beta)	Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

Uses of DefaultDataContext in org.orekit.models.earth.ionosphere.nequick

Constructors in org.orekit.models.earth.ionosphere.nequick with annotations of type DefaultDataContext

Modifier	Constructor	Description
	NeQuickGalileo(OneAxisEllipsoid earth, double[] alpha)	Build a new instance.

Uses of DefaultDataContext in org.orekit.models.earth.troposphere

Methods in org.orekit.models.earth.troposphere with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static FixedTroposphericDelay	FixedTroposphericDelay.getDefaultModel()	Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.

Constructors in org.orekit.models.earth.troposphere with annotations of type DefaultDataContext

Modifier	Constructor	Description
	EstimatedModel(double h0, double t0, double p0, TroposphereMappingFunction model, double totalDelay)	Build a new instance using the given environmental conditions.
	EstimatedModel(TroposphereMappingFunction model, double totalDelay)	Build a new instance using a standard atmosphere model.
	FixedTroposphericDelay(String supportedName)	Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.
	GlobalMappingFunctionModel()	Build a new instance.
	ModifiedSaastamoinenModel(PressureTemperatureHumidityProvider pth0Provider, String deltaRFileName)	Create a new Saastamoinen model for the troposphere using the given environmental conditions.
	NiellMappingFunctionModel()	Builds a new instance.
	TimeSpanEstimatedModel(EstimatedModel model)	Constructor with default UTC time scale.
	ViennaModelCoefficientsLoader(double latitude, double longitude, ViennaModelType type)	Constructor with default supported names.
	ViennaModelCoefficientsLoader(String supportedNames, double latitude, double longitude, ViennaModelType type)	Constructor with supported names given by user.

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

Constructors in org.orekit.models.earth.weather with annotations of type DefaultDataContext

Modifier	Constructor	Description
	GlobalPressureTemperature(Geoid geoid)	Build a new instance.

Uses of DefaultDataContext in org.orekit.propagation.analytical.gnss

Constructors in org.orekit.propagation.analytical.gnss with annotations of type DefaultDataContext

Modifier	Constructor	Description
	GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements glonassOrbElt)	Initializes the builder.
	SBASPropagatorBuilder(SBASOrbitalElements sbasOrbElt)	Initializes the builder.

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

Methods in org.orekit.propagation.analytical.gnss.data with annotations of type DefaultDataContext

Modifier and Type	Method	Description
GLONASSAnalyticalPropagator	GLONASSAlmanac.getPropagator()	Get the propagator corresponding to the navigation message.
GLONASSNumericalPropagator	GLONASSFdmaNavigationMessage.getPropagator(double step)	Get the propagator corresponding to the navigation message.
SBASPropagator	SBASNavigationMessage.getPropagator()	Get the propagator corresponding to the navigation message.

Constructors in org.orekit.propagation.analytical.gnss.data with annotations of type DefaultDataContext

Modifier	Constructor	Description
	GLONASSAlmanac(int channel, int health, int day, int month, int year, double ta, double lambda, double deltaI, double pa, double ecc, double deltaT, double deltaTDot, double tGlo2UTC, double tGPS2Glo, double tGlo)	Constructor.
	GLONASSEphemeris(int n4, int nt, double tb, double x, double xDot, double xDotDot, double y, double yDot, double yDotDot, double z, double zDot, double zDotDot)	Build a new instance.

Uses of DefaultDataContext in org.orekit.propagation.analytical.intelsat

Constructors in org.orekit.propagation.analytical.intelsat with annotations of type DefaultDataContext

Modifier	Constructor	Description
	FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T> elements)	Default constructor.
	IntelsatElevenElementsPropagator(IntelsatElevenElements elements)	Default constructor.

Uses of DefaultDataContext in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Selects the extrapolator to use with the selected TLE.
static <T extends CalculusFieldElement<T>> FieldTLEPropagator<T>	FieldTLEPropagator.selectExtrapolator(FieldTLE<T> tle, T[] parameters)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle)	Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, double mass)	Selects the extrapolator to use with the selected TLE.
static <T extends CalculusFieldElement<T>> FieldTLE<T>	FieldTLE.stateToTLE(FieldSpacecraftState<T> state, FieldTLE<T> templateTLE, OsculatingToMeanConverter converter)	Convert Spacecraft State into TLE.

Constructors in org.orekit.propagation.analytical.tle with annotations of type DefaultDataContext

Modifier	Constructor	Description
	DeepSDP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Constructor for a unique initial TLE.
	FieldDeepSDP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Constructor for a unique initial TLE.
	FieldSGP4(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Constructor for a unique initial TLE.
	FieldTLE(int satelliteNumber, char classification, int launchYear, int launchNumber, String launchPiece, int ephemerisType, int elementNumber, FieldAbsoluteDate<T> epoch, T meanMotion, T meanMotionFirstDerivative, T meanMotionSecondDerivative, T e, T i, T pa, T raan, T meanAnomaly, int revolutionNumberAtEpoch, double bStar)	Simple constructor from already parsed elements.
	FieldTLE(Field<T> field, String line1, String line2)	Simple constructor from unparsed two lines.
protected	FieldTLEPropagator(FieldTLE<T> initialTLE, AttitudeProvider attitudeProvider, T mass, T[] parameters)	Protected constructor for derived classes.
	SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Constructor for a unique initial TLE.
	TLE(int satelliteNumber, char classification, int launchYear, int launchNumber, String launchPiece, int ephemerisType, int elementNumber, AbsoluteDate epoch, double meanMotion, double meanMotionFirstDerivative, double meanMotionSecondDerivative, double e, double i, double pa, double raan, double meanAnomaly, int revolutionNumberAtEpoch, double bStar)	Simple constructor from already parsed elements.
	TLE(String line1, String line2)	Simple constructor from unparsed two lines.
	TleExtendedPositionProvider(TLE tle)	Constructor with default TEME frame.
protected	TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass)	Protected constructor for derived classes.

Uses of DefaultDataContext in org.orekit.propagation.analytical.tle.generation

Constructors in org.orekit.propagation.analytical.tle.generation with annotations of type DefaultDataContext

Modifier	Constructor	Description
	FixedPointTleGenerationAlgorithm()	Default constructor.
	FixedPointTleGenerationAlgorithm(double epsilon, int maxIterations, double scale)	Constructor.
	LeastSquaresTleGenerationAlgorithm()	Default constructor.
	LeastSquaresTleGenerationAlgorithm(int maxIterations)	Default constructor.

Uses of DefaultDataContext in org.orekit.propagation.conversion

Constructors in org.orekit.propagation.conversion with annotations of type DefaultDataContext

Modifier	Constructor	Description
	TLEPropagatorBuilder(TLE templateTLE, PositionAngleType positionAngleType, double positionScale, TleGenerationAlgorithm generationAlgorithm)	Build a new instance.

Uses of DefaultDataContext in org.orekit.propagation.conversion.averaging

Constructors in org.orekit.propagation.conversion.averaging with annotations of type DefaultDataContext

Modifier	Constructor	Description
	SGP4OrbitalState(AbsoluteDate date, AveragedKeplerianWithMeanAngle elements)	Constructor with default data context.

Uses of DefaultDataContext in org.orekit.propagation.conversion.averaging.converters

Constructors in org.orekit.propagation.conversion.averaging.converters with annotations of type DefaultDataContext

Modifier	Constructor	Description
	OsculatingToSGP4Converter()	Constructor with default data context.

Uses of DefaultDataContext in org.orekit.propagation.conversion.osc2mean

Constructors in org.orekit.propagation.conversion.osc2mean with annotations of type DefaultDataContext

Modifier	Constructor	Description
	TLETheory()	Constructor with default data context and default TLE template.
	TLETheory(FieldTLE<T> template)	Constructor with default data context.
	TLETheory(TLE template)	Constructor with default data context.

Uses of DefaultDataContext in org.orekit.propagation.events

Constructors in org.orekit.propagation.events with annotations of type DefaultDataContext

Modifier	Constructor	Description
	BetaAngleDetector(double betaAngleThreshold)	Solar beta angle constructor.
	FieldBetaAngleDetector(T betaAngleThreshold)	Solar beta angle constructor.
	MagneticFieldDetector(double maxCheck, double threshold, double limit, GeoMagneticFieldFactory.FieldModel model, BodyShape body, boolean atSeaLevel)	Build a detector.
	MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel model, BodyShape body)	Build a new detector.
	MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel model, BodyShape body, boolean atSeaLevel)	Build a new detector.

Uses of DefaultDataContext in org.orekit.propagation.numerical

Constructors in org.orekit.propagation.numerical with annotations of type DefaultDataContext

Modifier	Constructor	Description
	FieldNumericalPropagator(FieldODEIntegrator<T> integrator)	Create a new instance of NumericalPropagator, based on orbit definition mu.
	GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator integrator, GLONASSOrbitalElements glonassOrbElt, boolean isAccAvailable)	Initializes the builder.
	NumericalPropagator(ODEIntegrator integrator)	Create a new instance of NumericalPropagator, based on orbit definition mu.

Uses of DefaultDataContext in org.orekit.propagation.semianalytical.dsst

Constructors in org.orekit.propagation.semianalytical.dsst with annotations of type DefaultDataContext

Modifier	Constructor	Description
	DSSTPropagator(ODEIntegrator integrator)	Create a new instance of DSSTPropagator.
	DSSTPropagator(ODEIntegrator integrator, PropagationType propagationType)	Create a new instance of DSSTPropagator.
	FieldDSSTPropagator(Field<T> field, FieldODEIntegrator<T> integrator)	Create a new instance of DSSTPropagator.
	FieldDSSTPropagator(FieldODEIntegrator<T> integrator, PropagationType propagationType)	Create a new instance of DSSTPropagator.

Uses of DefaultDataContext in org.orekit.time

Fields in org.orekit.time with annotations of type DefaultDataContext

Modifier and Type	Field	Description
static final AbsoluteDate	AbsoluteDate.BEIDOU_EPOCH	Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
static final AbsoluteDate	AbsoluteDate.CCSDS_EPOCH	Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
static final AbsoluteDate	AbsoluteDate.FIFTIES_EPOCH	Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
static final AbsoluteDate	AbsoluteDate.GALILEO_EPOCH	Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
static final AbsoluteDate	AbsoluteDate.GLONASS_EPOCH	Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
static final AbsoluteDate	AbsoluteDate.GPS_EPOCH	Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
static final AbsoluteDate	AbsoluteDate.J2000_EPOCH	J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
static final AbsoluteDate	AbsoluteDate.JAVA_EPOCH	Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
static final AbsoluteDate	AbsoluteDate.JULIAN_EPOCH	Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
static final AbsoluteDate	AbsoluteDate.MODIFIED_JULIAN_EPOCH	Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
static final AbsoluteDate	AbsoluteDate.NAVIC_EPOCH	Reference epoch for NavIC weeks: 1999-08-22T00:00:00 NavIC time.
static final AbsoluteDate	AbsoluteDate.QZSS_EPOCH	Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.

Methods in org.orekit.time with annotations of type DefaultDataContext

Modifier and Type	Method	Description
static void	TimeScalesFactory.addDefaultUTCTAIOffsetsLoaders()	Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
static void	TimeScalesFactory.addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader loader)	Add a loader for UTC-TAI offsets history files.
static void	TimeScalesFactory.clearUTCTAIOffsetsLoaders()	Clear loaders for UTC-TAI offsets history files.
static AbsoluteDate	AbsoluteDate.createBesselianEpoch(double besselianEpoch)	Build an instance corresponding to a Besselian Epoch (BE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createBesselianEpoch(T besselianEpoch)	Build an instance corresponding to a Besselian Epoch (BE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createGPSDate(int weekNumber, T milliInWeek)	Build an instance corresponding to a GPS date.
static AbsoluteDate	AbsoluteDate.createJulianEpoch(double julianEpoch)	Build an instance corresponding to a Julian Epoch (JE).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.createJulianEpoch(T julianEpoch)	Build an instance corresponding to a Julian Epoch (JE).
static BDTScale	TimeScalesFactory.getBDT()	Get the BeiDou Navigation Satellite System time scale.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getCCSDSEpoch(Field<T> field)	Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4).
DateTimeComponents	AbsoluteDate.getComponents(int minutesFromUTC)	Split the instance into date/time components for a local time.
DateTimeComponents	AbsoluteDate.getComponents(TimeZone timeZone)	Split the instance into date/time components for a time zone.
DateTimeComponents	FieldAbsoluteDate.getComponents(int minutesFromUTC)	Split the instance into date/time components for a local time.
DateTimeComponents	FieldAbsoluteDate.getComponents(TimeZone timeZone)	Split the instance into date/time components for a time zone.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getFiftiesEpoch(Field<T> field)	Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getGalileoEpoch(Field<T> field)	Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
static GLONASSScale	TimeScalesFactory.getGLONASS()	Get the GLObal NAvigation Satellite System time scale.
static GMSTScale	TimeScalesFactory.getGMST(IERSConventions conventions, boolean simpleEOP)	Get the Greenwich Mean Sidereal Time scale.
static GPSScale	TimeScalesFactory.getGPS()	Get the Global Positioning System scale.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getGPSEpoch(Field<T> field)	Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
static GalileoScale	TimeScalesFactory.getGST()	Get the Galileo System Time scale.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJ2000Epoch(Field<T> field)	J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJavaEpoch(Field<T> field)	Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
double	AbsoluteDate.getJD()	Return the given date as a Julian Date expressed in UTC.
T	FieldAbsoluteDate.getJD()	Return the given date as a Julian Date expressed in UTC.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJulianEpoch(Field<T> field)	Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
double	AbsoluteDate.getMJD()	Return the given date as a Modified Julian Date expressed in UTC.
T	FieldAbsoluteDate.getMJD()	Return the given date as a Modified Julian Date expressed in UTC.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getModifiedJulianEpoch(Field<T> field)	Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
static NavicScale	TimeScalesFactory.getNavIC()	Get the Navigation with Indian Constellation time scale.
static QZSSScale	TimeScalesFactory.getQZSS()	Get the Quasi-Zenith Satellite System time scale.
static TAIScale	TimeScalesFactory.getTAI()	Get the International Atomic Time scale.
static TCBScale	TimeScalesFactory.getTCB()	Get the Barycentric Coordinate Time scale.
static TCGScale	TimeScalesFactory.getTCG()	Get the Geocentric Coordinate Time scale.
static TDBScale	TimeScalesFactory.getTDB()	Get the Barycentric Dynamic Time scale.
static LazyLoadedTimeScales	TimeScalesFactory.getTimeScales()	Get the instance of TimeScales that is called by all of the static methods in this class.
static TTScale	TimeScalesFactory.getTT()	Get the Terrestrial Time scale.
static UT1Scale	TimeScalesFactory.getUT1(EOPHistory history)	Get the Universal Time 1 scale.
static UT1Scale	TimeScalesFactory.getUT1(IERSConventions conventions, boolean simpleEOP)	Get the Universal Time 1 scale.
static UTCScale	TimeScalesFactory.getUTC()	Get the Universal Time Coordinate scale.
static AbsoluteDate	AbsoluteDate.parseCCSDSCalendarSegmentedTimeCode(byte preambleField, byte[] timeField)	Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSCalendarSegmentedTimeCode(byte preambleField, byte[] timeField)	Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
static AbsoluteDate	AbsoluteDate.parseCCSDSDaySegmentedTimeCode(byte preambleField, byte[] timeField, DateComponents agencyDefinedEpoch)	Build an instance from a CCSDS Day Segmented Time Code (CDS).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSDaySegmentedTimeCode(Field<T> field, byte preambleField, byte[] timeField, DateComponents agencyDefinedEpoch)	Build an instance from a CCSDS Day Segmented Time Code (CDS).
static AbsoluteDate	AbsoluteDate.parseCCSDSUnsegmentedTimeCode(byte preambleField1, byte preambleField2, byte[] timeField, AbsoluteDate agencyDefinedEpoch)	Build an instance from a CCSDS Unsegmented Time Code (CUC).
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSUnsegmentedTimeCode(Field<T> field, byte preambleField1, byte preambleField2, byte[] timeField, FieldAbsoluteDate<T> agencyDefinedEpoch)	Build an instance from a CCSDS Unsegmented Time Code (CUC).
Instant	AbsoluteDate.toInstant()	Convert the instance to a Java Instant.
Instant	FieldAbsoluteDate.toInstant()	Convert the instance to a Java Instant.
String	AbsoluteDate.toString()	Get a String representation of the instant location with up to 18 digits of precision for the seconds value.
String	AbsoluteDate.toString(int minutesFromUTC)	Get a String representation of the instant location for a local time.
String	AbsoluteDate.toString(TimeZone timeZone)	Get a String representation of the instant location for a time zone.
String	FieldAbsoluteDate.toString()	Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
String	FieldAbsoluteDate.toString(int minutesFromUTC)	Get a String representation of the instant location for a local time.
String	FieldAbsoluteDate.toString(TimeZone timeZone)	Get a String representation of the instant location for a time zone.

Constructors in org.orekit.time with annotations of type DefaultDataContext

Modifier	Constructor	Description
	AbsoluteDate()	Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
	AbsoluteDate(Instant instant)	Build an instance from an instant in utc time scale.
	AGILeapSecondFilesLoader(String supportedNames)	Build a loader for LeapSecond.dat file from AGI.
	FieldAbsoluteDate(Field<T> field)	Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
	FieldAbsoluteDate(Field<T> field, Instant instant)	Build an instance from an instant in utc time scale.
	GLONASSDate(int na, int n4, double secInNa)	Build an instance corresponding to a GLONASS date.
	GLONASSDate(AbsoluteDate date)	Build an instance from an absolute date.
	GNSSDate(int weekNumber, double secondsInWeek, SatelliteSystem system)	Build an instance corresponding to a GNSS date.
	GNSSDate(int weekNumber, TimeOffset secondsInWeek, SatelliteSystem system)	Build an instance corresponding to a GNSS date.
	GNSSDate(AbsoluteDate date, SatelliteSystem system)	Build an instance from an absolute date.
	TAIUTCDatFilesLoader(String supportedNames)	Build a loader for tai-utc.dat file from USNO.
	UTCTAIBulletinAFilesLoader(String supportedNames)	Build a loader for IERS bulletins A files.
	UTCTAIHistoryFilesLoader()	Build a loader for UTC-TAI history file.

Uses of DefaultDataContext in org.orekit.utils

Methods in org.orekit.utils with annotations of type DefaultDataContext

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