Uses of Class
org.orekit.annotation.DefaultDataContext
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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.measurements The measurements package defines everything that is related to orbit determination measurements.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.ccsds.ndm.cdm This package contains class managing CCSDS Conjunction Data Message.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.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.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.metric.messages.rtcm.ephemeris This package provides all supported RTCM ephemerismessages
.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.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 ofSpacecraftState
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.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. -
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Uses of DefaultDataContext in org.orekit.attitudes
Constructors in org.orekit.attitudes with annotations of type DefaultDataContext Constructor Description 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 ofCelestialBodies
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 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 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 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
Methods in org.orekit.estimation.measurements with annotations of type DefaultDataContext Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
TAbstractMeasurement. signalTimeOfFlight(TimeStampedFieldPVCoordinates<T> adjustableEmitterPV, FieldVector3D<T> receiverPosition, FieldAbsoluteDate<T> signalArrivalDate)
static double
AbstractMeasurement. signalTimeOfFlight(TimeStampedPVCoordinates adjustableEmitterPV, Vector3D receiverPosition, AbsoluteDate signalArrivalDate)
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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, FieldTransform<Gradient> stationToInertial, Frame frame)
Natural to proper correction for aberration of light.static Gradient[]
AberrationModifier. fieldProperToNatural(Gradient[] properRaDec, FieldTransform<Gradient> stationToInertial, Frame frame)
Proper to natural correction for aberration of light.static double[]
AberrationModifier. naturalToProper(double[] naturalRaDec, GroundStation station, AbsoluteDate date, Frame frame)
Natural to proper correction for aberration of light.static double[]
AberrationModifier. properToNatural(double[] properRaDec, GroundStation station, AbsoluteDate date, Frame frame)
Proper to natural correction for aberration of light.Constructors in org.orekit.estimation.measurements.modifiers with annotations of type DefaultDataContext 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 Constructor Description ParserBuilder()
Simple constructor.WriterBuilder()
Simple constructor. -
Uses of DefaultDataContext in org.orekit.files.ccsds.ndm.cdm
Constructors in org.orekit.files.ccsds.ndm.cdm with annotations of type DefaultDataContext Constructor Description CdmMetadata()
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 generatedOrekitEphemerisFile.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 generatedOrekitEphemerisFile.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 generatedOrekitEphemerisFile.OrekitEphemerisSegment
that has been stored internally. -
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 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 Constructor Description RinexClockParser()
Create a 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.files.rinex.navigation
Constructors in org.orekit.files.rinex.navigation with annotations of type DefaultDataContext Constructor Description RinexNavigationParser()
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 Constructor Description RinexObservationParser()
Simple constructor. -
Uses of DefaultDataContext in org.orekit.files.sinex
Constructors in org.orekit.files.sinex with annotations of type DefaultDataContext Constructor Description SinexLoader(String supportedNames)
Simple constructor.SinexLoader(DataSource source)
Simple constructor. -
Uses of DefaultDataContext in org.orekit.files.sp3
Methods in org.orekit.files.sp3 with annotations of type DefaultDataContext Modifier and Type Method Description static Frame
SP3Parser. guessFrame(String name)
Deprecated.as of 12.1, replaced byIGSUtils.guessFrame(String)
Constructors in org.orekit.files.sp3 with annotations of type DefaultDataContext 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 aPropagator
from the ephemeris data. -
Uses of DefaultDataContext in org.orekit.forces.drag
Constructors in org.orekit.forces.drag with annotations of type DefaultDataContext Constructor Description TimeSpanDragForce(Atmosphere atmosphere, DragSensitive spacecraft)
Deprecated.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 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 ofGravityFields
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 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 Description ECOM2(int nD, int nB, double value, ExtendedPVCoordinatesProvider sun, double equatorialRadius)
Constructor.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 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 ofFrames
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 underlyingHelmertTransformation
.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 Description EclipticProvider(IERSConventions conventions)
Create a transform provider from MOD to an ecliptically aligned frame.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)
Constructors in org.orekit.gnss with annotations of type DefaultDataContext 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 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
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.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.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 theGeoMagneticField
for the given model type and year.static LazyLoadedGeoMagneticFields
GeoMagneticFieldFactory. getGeoMagneticFields()
Get the instance ofGeoMagneticFields
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 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 Description CssiSpaceWeatherData(String supportedNames)
Simple constructor.CssiSpaceWeatherData(DataSource source)
Simple constructor which use thedefault 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 thedefault 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 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 Constructor 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 Description static FixedTroposphericDelay
FixedTroposphericDelay. getDefaultModel()
Returns the default model, loading delay values from the file "tropospheric-delay.txt" via thedefault data context
.static SaastamoinenModel
SaastamoinenModel. getStandardModel()
Deprecated.Create a new Saastamoinen model using a standard atmosphere model.Constructors in org.orekit.models.earth.troposphere with annotations of type DefaultDataContext 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.EstimatedTroposphericModel(double t0, double p0, MappingFunction model, double totalDelay)
Deprecated.Build a new instance using the given environmental conditions.EstimatedTroposphericModel(MappingFunction model, double totalDelay)
Deprecated.Build a new instance using a standard atmosphere model.FixedTroposphericDelay(String supportedName)
Creates a newFixedTroposphericDelay
instance, and loads the delay values from the given resource via thedefault data context
.GlobalMappingFunctionModel()
Build a new instance.ModifiedSaastamoinenModel(double t0, double p0, double r0, String deltaRFileName)
Deprecated.as of 12.1.1, replaced byModifiedSaastamoinenModel(PressureTemperatureHumidityProvider, String)
ModifiedSaastamoinenModel(PressureTemperatureHumidityProvider pth0Provider, String deltaRFileName)
Create a new Saastamoinen model for the troposphere using the given environmental conditions.NiellMappingFunctionModel()
Builds a new instance.SaastamoinenModel(double t0, double p0, double r0)
Deprecated.Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.SaastamoinenModel(double t0, double p0, double r0, String deltaRFileName)
Deprecated.Create a new Saastamoinen model for the troposphere using the given environmental conditions.TimeSpanEstimatedModel(EstimatedModel model)
Constructor with default UTC time scale.TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel model)
Deprecated.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)
Deprecated.Build a new instance.ViennaThreeModel(double[] coefficientA, double[] zenithDelay)
Deprecated.Build a new instance. -
Uses of DefaultDataContext in org.orekit.models.earth.weather
Constructors in org.orekit.models.earth.weather with annotations of type DefaultDataContext Constructor Description GlobalPressureTemperature(Geoid geoid)
Build a new instance.GlobalPressureTemperature2Model(double latitude, double longitude, Geoid geoid)
Deprecated.Constructor with default supported names.GlobalPressureTemperature2Model(String supportedNames, double latitude, double longitude, Geoid geoid)
Deprecated.Constructor with supported names given by user.GlobalPressureTemperatureModel(double latitude, double longitude, Frame bodyFrame)
Deprecated.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 Description GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements glonassOrbElt)
Initializes the builder.GNSSPropagatorBuilder(GNSSOrbitalElements gnssOrbElt)
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
GLONASSNavigationMessage. getPropagator(double step)
Get the propagator corresponding to the navigation message.default GNSSPropagator
GNSSOrbitalElements. getPropagator()
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 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 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.Constructors in org.orekit.propagation.analytical.tle with annotations of type DefaultDataContext 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.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.analytical.tle.generation
Constructors in org.orekit.propagation.analytical.tle.generation with annotations of type DefaultDataContext 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 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 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 Constructor Description OsculatingToSGP4Converter()
Constructor with default data context. -
Uses of DefaultDataContext in org.orekit.propagation.events
Constructors in org.orekit.propagation.events with annotations of type DefaultDataContext 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, OneAxisEllipsoid body, boolean atSeaLevel)
Build a detector.MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel model, OneAxisEllipsoid body)
Build a new detector.MagneticFieldDetector(double limit, GeoMagneticFieldFactory.FieldModel model, OneAxisEllipsoid 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 Constructor 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 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 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 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 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 ofTimeScales
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 JavaInstant
.Instant
FieldAbsoluteDate. toInstant()
Convert the instance to a JavaInstant
.String
AbsoluteDate. toString()
Get a String representation of the instant location with up to 16 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 Constructor Description AbsoluteDate()
Create an instance with a default value (AbsoluteDate.J2000_EPOCH
).AbsoluteDate(Instant instant)
Build an instance from aninstant
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 aninstant
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(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 thereference date
.<T extends CalculusFieldElement<T>>
TIERSConventions. evaluateTC(FieldAbsoluteDate<T> date)
Evaluate the date offset between the current date and thereference 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
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.
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