Uses of Class
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.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.sequential	The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
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.ilrs	This package provides parsers for laser ranging data stored in CDR and CPF formats.
org.orekit.files.sinex	This package provides classes related to station data.
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.clock	This package provides classes related to navigation clock files.
org.orekit.gnss.metric.messages.rtcm.ephemeris	This package provides all supported RTCM ephemeris messages.
org.orekit.gnss.navigation	This package provides classes related to RINEX navigation files.
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.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.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
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

Constructor and Description
InertialProvider(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 and 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

Constructor and Description
JPLEphemeridesLoader(String supportedNames, JPLEphemeridesLoader.EphemerisType generateType) Create a loader for JPL ephemerides binary files.

Uses of DefaultDataContext in org.orekit.data

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

Modifier and Type	Method and 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

Constructor and 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.sequential

Methods in org.orekit.estimation.sequential with annotations of type DefaultDataContext

Modifier and Type	Method and Description
protected void	TLEKalmanModel.updateReferenceTrajectories(Propagator[] propagators, PropagationType pType, PropagationType sType) Deprecated. Update the reference trajectories using the propagators as input.

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 and 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

Constructor and 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 and 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, CelestialBody body, 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, 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.ilrs

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

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

Uses of DefaultDataContext in org.orekit.files.sinex

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

Constructor and Description
SinexLoader(DataSource source) Simple constructor.
SinexLoader(String supportedNames) Simple constructor.

Uses of DefaultDataContext in org.orekit.files.sp3

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

Constructor and 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

Constructor and 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

Constructor and 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 and 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) Get the constant gravity field coefficients provider from the first supported file.
static UnnormalizedSphericalHarmonicsProvider	GravityFieldFactory.getConstantUnnormalizedProvider(int degree, int order) 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

Constructor and Description
GRGSFormatReader(String supportedNames, boolean missingCoefficientsAllowed) Simple constructor.
ICGEMFormatReader(String supportedNames, boolean missingCoefficientsAllowed) Simple constructor.
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

Constructor and Description
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider 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 and Description
static void	FramesFactory.addDefaultEOP1980HistoryLoaders(String rapidDataColumnsSupportedNames, String rapidDataXMLSupportedNames, String eopC04SupportedNames, String bulletinBSupportedNames, String bulletinASupportedNames) Add the default loaders EOP history (IAU 1980 precession/nutation).
static void	FramesFactory.addDefaultEOP2000HistoryLoaders(String rapidDataColumnsSupportedNames, String rapidDataXMLSupportedNames, String eopC04SupportedNames, String bulletinBSupportedNames, String bulletinASupportedNames) 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 FactoryManagedFrame	FramesFactory.getITRF(IERSConventions conventions, boolean simpleEOP) Get an unspecified International Terrestrial Reference Frame.
static VersionedITRF	FramesFactory.getITRF(ITRFVersion version, IERSConventions conventions, boolean simpleEOP) Get an specific 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

Constructor and Description
EclipticProvider(IERSConventions conventions) Create a transform provider from MOD to an ecliptically aligned frame.
EOPHistory(IERSConventions conventions, 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

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

Constructor and Description
RinexObservationLoader(DataSource source) Simple constructor.
RinexObservationLoader(String supportedNames) Simple constructor.
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

Constructor and Description
AntexLoader(String supportedNames) Simple constructor.

Uses of DefaultDataContext in org.orekit.gnss.clock

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

Constructor and Description
RinexClockParser() Create an clock file parser using default values.
RinexClockParser(Function<? super String,? extends Frame> frameBuilder) Create a clock file parser and specify the frame builder.

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 and Description
BeidouNavigationMessage	Rtcm1042Data.getBeidouNavigationMessage() Get the Beidou navigation message corresponding to the current RTCM data.
GalileoNavigationMessage	Rtcm1045Data.getGalileoNavigationMessage() Get the Galileo navigation message corresponding to the current RTCM data.
GLONASSNavigationMessage	Rtcm1020Data.getGlonassNavigationMessage() Get the Glonass navigation message corresponding to the current RTCM data.
GPSNavigationMessage	Rtcm1019Data.getGpsNavigationMessage() Get the GPS navigation message corresponding to the current RTCM data.
QZSSNavigationMessage	Rtcm1044Data.getQzssNavigationMessage() Get the QZSS navigation message corresponding to the current RTCM data.

Uses of DefaultDataContext in org.orekit.gnss.navigation

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

Constructor and Description
RinexNavigationParser() Constructor.

Uses of DefaultDataContext in org.orekit.models.earth

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

Modifier and Type	Method and 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

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

Constructor and Description
CssiSpaceWeatherData(String supportedNames) Simple constructor.
JB2008SpaceEnvironmentData(String supportedNamesSOL, String supportedNamesDTC) Simple constructor.
MarshallSolarActivityFutureEstimation(String supportedNames, 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

Constructor and 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

Constructor and Description
GlobalIonosphereMapModel(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(double[] alpha, double[] beta) Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
NeQuickModel(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 and 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

Constructor and Description
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.
NiellMappingFunctionModel() Builds a new instance.
SaastamoinenModel(double t0, double p0, double r0, String deltaRFileName) Create a new Saastamoinen model for the troposphere using the given environmental conditions.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel 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.
ViennaOneModel(double[] coefficientA, double[] zenithDelay) Build a new instance.
ViennaThreeModel(double[] coefficientA, double[] zenithDelay) Build a new instance.

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

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

Modifier and Type	Method and Description
void	GlobalPressureTemperatureModel.weatherParameters(double height, AbsoluteDate date)

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

Constructor and Description
GlobalPressureTemperature2Model(double latitude, double longitude, Geoid geoid) Constructor with default supported names.
GlobalPressureTemperature2Model(String supportedNames, double latitude, double longitude, Geoid geoid) Constructor with supported names given by user.
GlobalPressureTemperatureModel(double latitude, double longitude, Frame bodyFrame) 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

Constructor and Description
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements glonassOrbElt) Initializes the builder.
GNSSPropagatorBuilder(GNSSOrbitalElements gnssOrbElt) Initializes the builder.

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

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

Constructor and 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.tle

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

Modifier and Type	Method and 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) Convert Spacecraft State into TLE.
static TLE	TLE.stateToTLE(SpacecraftState state, TLE templateTLE) Convert Spacecraft State into TLE.

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

Constructor and 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(Field<T> field, String line1, String line2) Simple constructor from unparsed two lines.
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.
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.
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Protected constructor for derived classes.

Uses of DefaultDataContext in org.orekit.propagation.conversion

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

Constructor and Description
TLEPropagatorBuilder(TLE templateTLE, PositionAngle positionAngle, double positionScale) Build a new instance.
TLEPropagatorBuilder(TLE templateTLE, PositionAngle positionAngle, double positionScale, double epsilon, int maxIterations) Build a new instance.

Uses of DefaultDataContext in org.orekit.propagation.events

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

Constructor and Description
MagneticFieldDetector(double maxCheck, double threshold, double limit, GeoMagneticFieldFactory.FieldModel type, OneAxisEllipsoid body, boolean seaLevel) Build a detector.
MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel type, OneAxisEllipsoid body) Build a new detector.
MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel type, OneAxisEllipsoid body, boolean seaLevel) Build a new detector.

Uses of DefaultDataContext in org.orekit.propagation.numerical

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

Constructor and Description
FieldNumericalPropagator(Field<T> field, 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

Constructor and 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(Field<T> field, 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 and Description
static AbsoluteDate	AbsoluteDate.BEIDOU_EPOCH Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
static 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 AbsoluteDate	AbsoluteDate.FIFTIES_EPOCH Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
static AbsoluteDate	AbsoluteDate.GALILEO_EPOCH Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
static AbsoluteDate	AbsoluteDate.GLONASS_EPOCH Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
static AbsoluteDate	AbsoluteDate.GPS_EPOCH Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
static AbsoluteDate	AbsoluteDate.IRNSS_EPOCH Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
static AbsoluteDate	AbsoluteDate.J2000_EPOCH J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
static AbsoluteDate	AbsoluteDate.JAVA_EPOCH Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
static AbsoluteDate	AbsoluteDate.JULIAN_EPOCH Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
static AbsoluteDate	AbsoluteDate.MODIFIED_JULIAN_EPOCH Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
static 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 and 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	FieldAbsoluteDate.getComponents(int minutesFromUTC) Split the instance into date/time components for a local time.
DateTimeComponents	AbsoluteDate.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.
DateTimeComponents	AbsoluteDate.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 IRNSSScale	TimeScalesFactory.getIRNSS() Get the Indian Regional Navigation Satellite 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.
static <T extends CalculusFieldElement<T>> FieldAbsoluteDate<T>	FieldAbsoluteDate.getJulianEpoch(Field<T> field) Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
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 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.
FieldAbsoluteDate<T>	FieldAbsoluteDate.parseCCSDSCalendarSegmentedTimeCode(byte preambleField, byte[] timeField) Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
static AbsoluteDate	AbsoluteDate.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).
String	FieldAbsoluteDate.toString() Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
String	AbsoluteDate.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	AbsoluteDate.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.
String	AbsoluteDate.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

Constructor and Description
AbsoluteDate() Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
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)).
GLONASSDate(AbsoluteDate date) Build an instance from an absolute date.
GLONASSDate(int na, int n4, double secInNa) Build an instance corresponding to a GLONASS date.
GNSSDate(AbsoluteDate date, SatelliteSystem system) Build an instance from an absolute date.
GNSSDate(int weekNumber, double milliInWeek, SatelliteSystem system) Build an instance corresponding to a GNSS 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 and 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	TimeStampedPVCoordinates.toString() Return a string representation of this date, position, velocity, and acceleration.
String	TimeStampedFieldPVCoordinates.toString() Return a string representation of this date, position, velocity, and acceleration.