- g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
-
- g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
-
- g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Compute the value of the detection function.
- g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Equinoctial frame g vector.
- G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
-
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
- GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
- GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
-
Reference epoch for Galileo System Time: 1999-08-22.
- GalileoScale - Class in org.orekit.time
-
Galileo system time scale.
- GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
-
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
- GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Simple constructor.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
-
- generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
-
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
-
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
-
Generate a
KeplerianOrbit
from the OPM Keplerian elements if hasKeplerianElements is true,
or from the state vector data otherwise.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile
-
Generate spacecraft state from the
KeplerianOrbit
generated by generateKeplerianOrbit.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile
-
Generate spacecraft state from the
CartesianOrbit
generated by generateCartesianOrbit.
- generateTLE() - Method in class org.orekit.files.ccsds.OMMFile
-
Generate TLE from OMM file.
- GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
-
- GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
-
Simple constructor.
- GeodeticPoint - Class in org.orekit.bodies
-
Point location relative to a 2D body surface.
- GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
-
Build a new instance.
- GeographicZoneDetector - Class in org.orekit.propagation.events
-
Detector for entry/exit of a zone defined by geographic boundaries.
- GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a new detector.
- GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a detector.
- Geoid - Class in org.orekit.models.earth
-
A geoid is a level surface of the gravity potential of a body.
- Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
-
Creates a geoid from the given geopotential, reference ellipsoid and the
assumptions in the comment for
Geoid
.
- GeoMagneticElements - Class in org.orekit.models.earth
-
Contains the elements to represent a magnetic field at a single point.
- GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
-
Construct a new element with the given field vector.
- GeoMagneticField - Class in org.orekit.models.earth
-
Used to calculate the geomagnetic field at a given geodetic point on earth.
- GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
-
Create a new geomagnetic field model with the given parameters.
- GeoMagneticFieldFactory - Class in org.orekit.models.earth
-
- GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
-
The currently supported geomagnetic field models.
- GeoMagneticModelLoader - Class in org.orekit.models.earth
-
Loads geomagnetic field models from a given input stream.
- GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
-
- get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
-
Get the entry valid at a specified date.
- get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
-
Get the entry valid at a specified date.
- get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
The Kp index is derived from the Ap index.
- get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Get the last 24H mean geomagnetic index.
- getA() - Method in class org.orekit.bodies.Ellipse
-
Get the semi major axis.
- getA() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the first semi-axis.
- getA() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the orbit semi-major axis.
- getA() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.CircularOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.Orbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the semi-major axis.
- getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get A = sqrt(μ * a).
- getA() - Method in class org.orekit.propagation.SpacecraftState
-
Get the semi-major axis.
- getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
-
Returns a copy of the abscissa grid for the interpolation function.
- getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the transition field absolute date.
- getAcceleration() - Method in class org.orekit.frames.FieldTransform
-
Get the second time derivative of the translation.
- getAcceleration() - Method in class org.orekit.frames.Transform
-
Get the second time derivative of the translation.
- getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the acceleration.
- getAcceleration() - Method in class org.orekit.utils.PVCoordinates
-
Gets the acceleration.
- getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
Get the formal accuracy for this satellite.
- getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
-
Get the user requested action.
- getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
-
Get the user requested action.
- getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the adapted propagator.
- getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
-
Get the additional state.
- getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
-
Get the additional state.
- getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an additional state.
- getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
-
Get an additional state.
- getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Compute the length of the one-dimensional additional state array needed.
- getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an unmodifiable map of additional states.
- getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
-
Get an unmodifiable map of additional states.
- getADot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.Orbit
-
Get the semi-major axis derivative.
- getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the value of the central body reference radius.
- getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the central body reference radius.
- getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the value of the central body reference radius.
- getAf0() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the Zeroth Order Clock Correction.
- getAf1() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the First Order Clock Correction.
- getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the entry valid after transition.
- getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the entry valid after transition.
- getAgency() - Method in class org.orekit.files.sp3.SP3File
-
Returns the agency that prepared this SP3 file.
- getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
-
Get the alignment angle (rad).
- getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
Get all of the data in this cache.
- getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAlmanacs() - Method in class org.orekit.gnss.SEMParser
-
- getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
-
- getAlpha() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
-
Returns the alpha coefficients array.
- getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
-
Get the latitude argument.
- getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the latitude argument.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine α for central body.
- getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
-
Get the latitude argument derivative.
- getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the latitude argument derivative.
- getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric latitude argument.
- getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric latitude argument.
- getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric latitude argument derivative.
- getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric latitude argument derivative.
- getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean latitude argument.
- getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean latitude argument.
- getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean latitude argument derivative.
- getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean latitude argument derivative.
- getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true latitude argument.
- getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true latitude argument.
- getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true latitude argument derivative.
- getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true latitude argument derivative.
- getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the altitude.
- getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the altitude.
- getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
-
Get the threshold altitude value.
- getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Get the threshold altitude value.
- getAncestor(int) - Method in class org.orekit.frames.Frame
-
Get the nth ancestor of the frame.
- getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Get the fixed angle to be crossed (radians).
- getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for angleType.
- getAngular() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary angular part.
- getAngular() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary angular part.
- getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
-
Get the angular velocity (spin) of this point as seen from the origin.
- getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
-
Get the angular velocity (spin) of this point as seen from the origin.
- getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the orbit anomaly.
- getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the anomaly.
- getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the anomaly.
- getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the anomaly derivative.
- getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the anomaly derivative.
- getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the type of anomaly (true or mean).
- getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the Ap geomagnetic indices.
- getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
-
Get facet area.
- getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
-
Get astronomical amplitudes map.
- getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the atmospheric model.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the attitude corresponding to an orbital state.
- getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the attitude.
- getAttitude() - Method in class org.orekit.propagation.SpacecraftState
-
Get the attitude.
- getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the Attitude Provider to use during maneuver.
- getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get the attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
-
Get the attitude provider.
- getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
-
Get attitude provider.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the available satellite numbers.
- getAverageFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the value of the 81 day average of F10.7 solar flux centered on current day.
- getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the azimuth of a point with regards to the topocentric frame center point.
- getB() - Method in class org.orekit.bodies.Ellipse
-
Get the semi minor axis.
- getB() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the second semi-axis.
- getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get B = sqrt(1 - e²).
- getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the base frame associated with the station.
- getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the base system state at given date, without compensation.
- getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the base system state at given date, without compensation.
- getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the base system state at given date, without compensation.
- getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the base system state at given date, without compensation.
- getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the base weight associated with the measurement
- getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the base weight associated with the measurement
- getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get state vector dimension without additional parameters.
- getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get state vector dimension without additional parameters.
- getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Get the beacon at the center of the proximity zone.
- getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the entry valid before transition.
- getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the entry valid before transition.
- getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
-
Returns the beta coefficients array.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine β for central body.
- getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get a celestial body.
- getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get third body.
- getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
-
Get the body frame.
- getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
-
Get body frame related to body shape.
- getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get body frame related to body shape.
- getBodyFrame() - Method in class org.orekit.models.earth.Geoid
-
- getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
-
Get a body oriented, body centered frame.
- getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
-
Get the body shape.
- getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Get the body shape.
- getBStar() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the SGP/SGP4 drag-like coefficient.
- getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the ballistic coefficient.
- getC() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the third semi-axis.
- getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get C = 1 + p² + q².
- getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the fully normalized coefficient C2n,0 for the normal
gravity potential.
- getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
-
Get the number of slots to use in caches.
- getCalendarWeek() - Method in class org.orekit.time.DateComponents
-
Get the calendar week number.
- getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the number of calls to the differential equations computation method.
- getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the number of calls to the differential equations computation method.
- getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
-
Get the capitalized three letters abbreviation.
- getCapitalizedName() - Method in enum org.orekit.time.Month
-
Get the capitalized full name.
- getCartesian() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary Cartesian part.
- getCartesian() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary Cartesian part.
- getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
1958-01-01T00:00:00 International Atomic Time (not UTC).
- getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
-
Get the celestial body corresponding to the CCSDS constant.
- getCenter() - Method in class org.orekit.bodies.Ellipse
-
Get the center of the 2D ellipse.
- getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
-
Get the center point.
- getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
-
Get the direction of FOV center.
- getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData
-
- getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
-
Get the CCSDS center name.
- getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the origin of reference frame.
- getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
-
Find the center of curvature (point on the evolute) at the nadir of a point.
- getChildren() - Method in class org.orekit.frames.OrphanFrame
-
Get all children of the instance.
- getCic() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
- getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the circular eccentricity vector.
- getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the circular eccentricity vector.
- getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the circular eccentricity vector derivative.
- getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the circular eccentricity vector derivative.
- getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the circular eccentricity vector.
- getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the circular eccentricity vector.
- getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the circular eccentricity vector derivative.
- getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the circular eccentricity vector derivative.
- getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the CIRF2000 reference frame.
- getCis() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
- getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the Cj coefficient.
- getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the classification.
- getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the classification type.
- getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
-
Returns the clock correction value.
- getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
-
Returns the clock rate.
- getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the closest TLE to the selected date.
- getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
-
Get the load deformation coefficients for ocean tides.
- getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
-
Get the coefficients for a given site.
- getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Computes the coefficients involved in the contributions.
- getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Get the prefix for short period coefficients keys.
- getComment() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the meta-data comment.
- getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
- getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Get the meta-data comment.
- getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components.
- getComponents(int) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components.
- getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a time zone.
- getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the constant gravity field coefficients provider from the first supported file.
- getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get a time-independent provider for read spherical harmonics coefficients.
- getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the constant gravity field coefficients provider from the first supported file.
- getConventions() - Method in class org.orekit.files.ccsds.ODMFile
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.ODMParser
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.TDMParser
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.frames.EOPHistory
-
Get the IERS conventions to which these EOP apply.
- getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get Cartesian coordinates as derivatives.
- getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the coordinates for this ephemeris segment.
- getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
-
Returns the coordinate system of the entries in this orbit file.
- getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionAngle1.
- getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionAngle2.
- getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionDoppler.
- getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionRange.
- getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionReceive.
- getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionApplied.
- getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionTransmit.
- getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the evaluations counter.
- getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for covariance.
- getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the list of Covariance Matrices.
- getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the Position/Velocity covariance matrix.
- getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile
-
Get coordinate system for covariance matrix, for absolute frames.
- getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile
-
Get coordinate system for covariance matrix, for Local Orbital Frames.
- getCrc() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
- getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the file creation date and time in UTC.
- getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the file creation date and time in UTC.
- getCrs() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
- getCuc() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
- getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at previous grid point date.
- getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at current grid point date.
- getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the current weight.
- getCus() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
- getD() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean elongation of the Moon from the Sun.
- getD() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean elongation of the Moon from the Sun.
- getDailyFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the value of the daily F10.7 solar flux for previous day.
- getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the dataQuality.
- getDataUsed() - Method in class org.orekit.files.sp3.SP3File
-
Returns the data used indicator from the SP3 file.
- getDate() - Method in class org.orekit.attitudes.Attitude
-
Get the date of attitude parameters.
- getDate() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the date of attitude parameters.
- getDate() - Method in class org.orekit.data.DelaunayArguments
-
Get the date.
- getDate() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the date.
- getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the date of the maneuver.
- getDate() - Method in class org.orekit.frames.EOPEntry
-
Get the date.
- getDate() - Method in class org.orekit.frames.FieldTransform
-
Get the date.
- getDate() - Method in class org.orekit.frames.Transform
-
Get the date.
- getDate() - Method in class org.orekit.gnss.DOP
-
Gets the calculation date of the DOP.
- getDate() - Method in class org.orekit.gnss.GPSAlmanac
-
- getDate() - Method in class org.orekit.orbits.FieldOrbit
-
Get the date of orbital parameters.
- getDate() - Method in class org.orekit.orbits.Orbit
-
Get the date of orbital parameters.
- getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the TLE current date.
- getDate() - Method in class org.orekit.propagation.events.DateDetector
-
Get the current event date according to the propagator.
- getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
-
Get the current event date according to the propagator.
- getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the date.
- getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the date of the orbit.
- getDate() - Method in class org.orekit.propagation.SpacecraftState
-
Get the date.
- getDate() - Method in class org.orekit.time.AbsoluteDate
-
Get the date.
- getDate() - Method in class org.orekit.time.DateTimeComponents
-
Get the date component.
- getDate() - Method in class org.orekit.time.FieldAbsoluteDate
-
Get the date.
- getDate() - Method in interface org.orekit.time.FieldTimeStamped
-
Get the date.
- getDate() - Method in interface org.orekit.time.TimeStamped
-
Get the date.
- getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the transition absolute date.
- getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the transition date.
- getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
-
Get the date.
- getDay() - Method in class org.orekit.time.DateComponents
-
Get the day.
- getDayFraction() - Method in class org.orekit.files.sp3.SP3File
-
Returns the day fraction for this SP3 file.
- getDayOfWeek() - Method in class org.orekit.time.DateComponents
-
Get the day of week.
- getDayOfYear() - Method in class org.orekit.time.DateComponents
-
Get the day number in year.
- getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dh coefficient.
- getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dk coefficient.
- getDdEps() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for nutation in obliquity δΔε.
- getDDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean elongation of the Moon from the Sun time derivative.
- getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean elongation of the Moon from the Sun time derivative.
- getDdPsi() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for nutation in longitude δΔΨ.
- getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
-
Utility function to get a decimal year for a given day.
- getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the declination of the magnetic field in degrees.
- getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the decreasing events time shift.
- getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay
-
Returns the default model, loading delay values from the file
"tropospheric-delay.txt".
- getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
- getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get mass change during maneuver (value is < 0).
- getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the velocity increment in satellite frame.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the local density.
- getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density.
- getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density with initial entries.
- getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density with initial entries.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density.
- getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput
-
Get one of the stored densities.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
- getDepth() - Method in class org.orekit.frames.Frame
-
Get the depth of the frame.
- getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Get Γ function derivative.
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
-
Compute the value of the derivative dKj-n-1, s / de².
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
-
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
-
Get the dK₀-n-1,s / dΧ coefficient derivative.
- getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get all the drivers with set derivatives.
- getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
-
Get the detector.
- getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dα coefficient.
- getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dβ coefficient.
- getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dh coefficient.
- getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dk coefficient.
- getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dα coefficient.
- getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dβ coefficient.
- getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dh coefficient.
- getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dk coefficient.
- getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dα coefficient.
- getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dβ coefficient.
- getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dh coefficient.
- getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dk coefficient.
- getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dα coefficient.
- getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dβ coefficient.
- getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dh coefficient.
- getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dk coefficient.
- getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dα coefficient.
- getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dβ coefficient.
- getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dh coefficient.
- getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dk coefficient.
- getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the dimension of the measurement.
- getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the dimension of the measurement.
- getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the displacement models.
- getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dα coefficient.
- getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dβ coefficient.
- getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dh coefficient.
- getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dk coefficient.
- getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
-
Get the value of dLns / dγ (γ).
- getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
-
Get the upper bound value Dnl(Χ).
- getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the Doodson number for the wave.
- getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
- getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the Doodson number.
- getDragArea() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the drag area.
- getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the drag coefficient.
- getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get the drivers for supported parameters.
- getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
-
Get the drivers for supported parameters.
- getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
-
Get the drivers for supported parameters.
- getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
-
Get parameters drivers initialized from a reference orbit.
- getDrivers() - Method in class org.orekit.utils.ParameterDriversList
-
Get delegating drivers for all parameters.
- getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dh coefficient.
- getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dk coefficient.
- getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the temperature change computed from Dst index.
- getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get duration (value is 0 for impulsive maneuver).
- getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get velocity increment.
- getDx() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
- getDy() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
- getE() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the orbit eccentricity.
- getE() - Method in class org.orekit.gnss.GPSAlmanac
-
- getE() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.Orbit
-
Get the eccentricity.
- getE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Eccentricity.
- getE() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.SpacecraftState
-
Get the eccentricity.
- getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the earliest cached entry.
- getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
- getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
-
Get the earliest entry in this cache.
- getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth singleton body.
- getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth-Moon barycenter singleton bodies pair.
- getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the raw Earth Orientation Angle.
- getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction to the east of point, expressed in parent shape frame.
- getEast() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction to the east of point, expressed in parent shape frame.
- getEast() - Method in class org.orekit.frames.TopocentricFrame
-
Get the east direction of topocentric frame, expressed in parent shape frame.
- getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station position along East axis.
- getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the eccentricity.
- getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric anomaly.
- getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric anomaly.
- getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric anomaly derivative.
- getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric anomaly derivative.
- getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
- getECI() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Gets the Earth Centered Inertial frame used to propagate the orbit.
- getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
-
Get the ecliptic frame.
- getEDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.Orbit
-
Get the eccentricity derivative.
- getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the differential effects.
- getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Get the value of an element.
- getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the element number.
- getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the element set number for this satellite.
- getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the elevation of a point with regards to the local point.
- getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
-
Get the elevation value.
- getElevation(double) - Method in class org.orekit.utils.ElevationMask
-
Get the interpolated elevation for a given azimuth according to the mask.
- getElevationMask() - Method in class org.orekit.gnss.DOPComputer
-
Get the elevation mask.
- getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
-
Returns the currently configured elevation mask.
- getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Returns the currently configured elevation mask.
- getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
-
Get the underlying ellipsoid model that defines latitude and longitude.
- getEllipsoid() - Method in class org.orekit.models.earth.Geoid
-
- getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
- getEME2000() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique EME2000 frame.
- getEndDate() - Method in class org.orekit.frames.EOPHistory
-
Get the date of the last available Earth Orientation Parameters.
- getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the total number of entries cached.
- getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
-
Get the EOP history.
- getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get Earth Orientation Parameters history.
- getEOPHistory() - Method in class org.orekit.frames.GTODProvider
-
Get the EOP history.
- getEOPHistory() - Method in class org.orekit.time.UT1Scale
-
Get the EOP history.
- getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing tidal corrections for Earth Orientation Parameters.
- getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile
-
Get the list of ephemerides blocks as an unmodifiable list.
- getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the ephemerides data lines comment.
- getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the ephemeris type.
- getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the type of ephemeris.
- getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get the epoch relative to the covariance matrix.
- getEpoch() - Method in class org.orekit.files.ccsds.OGMFile
-
Get epoch of state vector, Keplerian elements and covariance matrix data.
- getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the epoch.
- getEpoch() - Method in class org.orekit.files.sp3.SP3File
-
Returns the start epoch of the orbit file.
- getEpoch() - Method in class org.orekit.frames.HelmertTransformation
-
Get the reference epoch of the transform.
- getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
-
Returns the epoch for this magnetic field model.
- getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for epoch.
- getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get epoch ignition.
- getEpochInterval() - Method in class org.orekit.files.sp3.SP3File
-
Returns the time interval between epochs (in seconds).
- getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the equatorial radius of the body.
- getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the central body equatorial radius.
- getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the first component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
-
Get the first component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the second component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
-
Get the second component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for equinox-based paradigm.
- getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for equinox-based paradigm.
- getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
- getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
-
Get one estimated measurement.
- getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the estimated UT1 time scale.
- getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
- getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the estimated value.
- getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the number of objective function evaluations.
- getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the number of evaluations used for last estimation.
- getEventDate() - Method in class org.orekit.propagation.events.EventState
-
Get the occurrence time of the event triggered in the current
step.
- getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
-
Get the occurrence time of the event triggered in the current
step.
- getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
-
Get the event detector triggered.
- getEventDetector() - Method in class org.orekit.propagation.events.EventState
-
Get the underlying event detector.
- getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
-
Get the event detector triggered.
- getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
-
Get the underlying event detector.
- getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
-
Get the events passed to this handler.
- getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the discrete events related to the model.
- getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper
-
Get the wrapped exception.
- getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the maximum timespan outside of the stored ephemeris that is allowed
for extrapolation.
- getF() - Method in class org.orekit.data.DelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon.
- getF() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon.
- getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the value of the instantaneous solar flux index
(1e-22*Watt/(m²*Hertz)).
- getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the value of the mean solar flux.
- getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
-
Get the key of the frame within the factory.
- getFDot() - Method in class org.orekit.data.DelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon time derivative.
- getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon time derivative.
- getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
- getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Field getter.
- getField() - Method in class org.orekit.time.FieldAbsoluteDate
-
Get the field.
- getFieldDate() - Method in class org.orekit.frames.FieldTransform
-
Get the date.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.AbstractParametricAcceleration
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the discrete events related to the model.
- getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Get the Field Of View.
- getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the Field Of View.
- getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Get the Field Of View.
- getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the magnetic field vector in nTesla.
- getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
- getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the date of the file from which data at the specified date comes from.
- getFileFormat() - Method in class org.orekit.files.ccsds.TDMParser
-
Get file format.
- getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
-
Get the filter corresponding to a maximum derivation order.
- getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
-
Get the filter corresponding to a maximum derivation order.
- getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the first TLE.
- getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the start date of the series.
- getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
-
Get the date of the first known leap second.
- getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get a copy of the last fitted parameters.
- getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the fixed step size.
- getFixedStepSize() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the fixed step size.
- getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the flattening of the body: f = (a-b)/a.
- getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the flow rate.
- getForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the CCSDS ODM (OPM, OMM or OEM) format version.
- getFormatVersion() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the CCSDS TDM format version.
- getFrame() - Method in class org.orekit.bodies.Ellipse
-
Get the defining frame.
- getFrame() - Method in class org.orekit.bodies.Ellipsoid
-
Get the ellipsoid central frame.
- getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame
-
Get the frame corresponding to the CCSDS constant.
- getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the reference frame in which data are given: used for state vector and
Keplerian elements data (and for the covariance reference frame if none is given).
- getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get coordinate system for covariance matrix, for absolute frames.
- getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
Get the frame of the central body.
- getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
-
Get one of the predefined frames.
- getFrame() - Method in class org.orekit.frames.OrphanFrame
-
Get the associated
frame
.
- getFrame() - Method in class org.orekit.orbits.FieldOrbit
-
Get the frame in which the orbital parameters are defined.
- getFrame() - Method in class org.orekit.orbits.Orbit
-
Get the frame in which the orbital parameters are defined.
- getFrame() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
-
- getFrame() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the frame of the initial state.
- getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
-
Get the frame in which the equator is defined.
- getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Get the sensor reference frame.
- getFrame() - Method in class org.orekit.propagation.events.NodeDetector
-
Get the frame in which the equator is defined.
- getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the inertial frame.
- getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
- getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get the inertial frame.
- getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
- getFrame() - Method in class org.orekit.propagation.integration.StateMapper
-
Get the inertial frame.
- getFrame() - Method in interface org.orekit.propagation.Propagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the definition frame of the orbit.
- getFrame() - Method in class org.orekit.propagation.SpacecraftState
-
Get the inertial frame.
- getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the name of the center of the coordinate system the ephemeris is provided
in.
- getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the reference frame specifier as it appeared in the file.
- getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the defining frame for this ephemeris segment.
- getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the freqOffset.
- getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
-
Get a new version of the instance, frozen with respect to a reference frame.
- getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Dummy date at infinity in the future direction.
- getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
- getGamma() - Method in class org.orekit.data.DelaunayArguments
-
Get the tide parameter γ = GMST + π.
- getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the tide parameter γ = GMST + π.
- getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine γ for central body.
- getGammaDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the tide parameter γ = GMST + π time derivative.
- getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the tide parameter γ = GMST + π time derivative.
- getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich apparent sidereal time, in radians.
- getGCRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique GCRF frame.
- getGdop() - Method in class org.orekit.gnss.DOP
-
Gets the geometric dilution of precision.
- getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the number of calls to the generate method.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
-
Get the ephemeris generated during propagation.
- getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the generator.
- getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
- getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Gjs coefficient.
- getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the GLObal NAvigation Satellite System time scale.
- getGM() - Method in interface org.orekit.bodies.CelestialBody
-
Get the attraction coefficient of the body.
- getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Gets the gravitational parameter that is part of the definition of the
reference ellipsoid.
- getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the Gmsj coefficient.
- getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Greenwich Mean Sidereal Time scale.
- getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time, in radians.
- getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time rate, in radians per second.
- getGnssNb() - Method in class org.orekit.gnss.DOP
-
Gets the number of GNSS satellites taken into account for DOP computation.
- getGPS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Global Positioning System scale.
- getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
- getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Gets the underlying GPS orbital elements.
- getGpsWeek() - Method in class org.orekit.files.sp3.SP3File
-
Returns the GPS week as contained in the SP3 file.
- getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the number of interpolation grid points.
- getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the number of interpolation grid points.
- getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
-
Get grid points that are within the current step.
- getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the GRS80 ellipsoid, attached to the given body frame.
- getGST() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Galileo System Time scale.
- getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the GTOD reference frame.
- getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the GTOD reference frame.
- getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the y component of eccentricity vector.
- getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
-
Get FOV half aperture angle.
- getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get the handler.
- getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get the handler.
- getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get an upper bound of the fitted harmonic amplitude.
- getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get boolean testing whether the body corresponding to the centerName
attribute can be created through the
CelestialBodyFactory
.
- getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile
-
Get boolean testing whether the OPM contains at least one maneuver.
- getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get boolean testing whether the reference frame has an epoch associated to it.
- getHdop() - Method in class org.orekit.gnss.DOP
-
Gets the horizontal dilution of precision.
- getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the header comment.
- getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the header comment.
- getHealth() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the Health status.
- getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Hjs coefficient.
- getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the Hmsj coefficient.
- getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the horizontal intensity of the magnetic field (= norm of the
vector in the plane spanned by the x/y components of the field vector).
- getHour() - Method in class org.orekit.time.TimeComponents
-
Get the hour number.
- getHx() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the first component of the inclination vector (as per equinoctial parameters).
- getHx() - Method in class org.orekit.propagation.SpacecraftState
-
Get the first component of the inclination vector (as per equinoctial parameters).
- getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the inclination vector derivative.
- getHy() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the second component of the inclination vector (as per equinoctial parameters).
- getHy() - Method in class org.orekit.propagation.SpacecraftState
-
Get the second component of the inclination vector (as per equinoctial parameters).
- getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the inclination vector derivative.
- getI() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the orbit inclination.
- getI() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.CircularOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.Orbit
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.SpacecraftState
-
Get the inclination.
- getI0() - Method in class org.orekit.gnss.GPSAlmanac
-
- getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Inclination Angle at Reference Time.
- getICRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique ICRF frame.
- getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
-
Get the identity transform.
- getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
-
Fixed orientation parallel with reference frame
(identity rotation, zero rotation rate and acceleration).
- getIDot() - Method in class org.orekit.gnss.GPSAlmanac
-
- getIDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.Orbit
-
Get the inclination derivative.
- getIDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Rate of Inclination Angle.
- getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
Get the IGRF model for the given year.
- getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Ijs coefficient.
- getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
-
Get the imaginary part of a nominal Love numbers.
- getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the inclination of the magnetic field in degrees.
- getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the increasing events time shift.
- getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the inertial velocity increment of the maneuver.
- getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the inertial frame in which the velocity increment is defined.
- getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
-
Get an inertially oriented, body centered frame.
- getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the initial state for integration.
- getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the initial state for integration.
- getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the initial state for integration.
- getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the date of the initial orbit.
- getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the date of the initial orbit.
- getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the propagator initial state.
- getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the propagator initial state.
- getInitialState() - Method in interface org.orekit.propagation.Propagator
-
Get the propagator initial state.
- getInstance() - Static method in class org.orekit.data.DataProvidersManager
-
Get the unique instance.
- getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the instantaneous solar flux.
- getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Get the value of the instantaneous solar flux.
- getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the integrationInterval.
- getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the integrationRef.
- getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the integrator used by the propagator.
- getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the integrator used by the propagator.
- getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
-
Get an interpolated point inside the tile.
- getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the interpolation degree.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the interpolation method to be used.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
-
Get the intersection point of a line with the surface of the body.
- getInverse() - Method in class org.orekit.frames.FieldTransform
-
Get the inverse transform of the instance.
- getInverse() - Method in class org.orekit.frames.Transform
-
Get the inverse transform of the instance.
- getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the specific impulse.
- getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the specific impulse.
- getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the iteration number.
- getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the number of iterations used for last estimation.
- getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the ITRF2008 reference frame, using IERS 2010 conventions.
- getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the equinox-based ITRF reference frame.
- getJ2000Day() - Method in class org.orekit.time.DateComponents
-
Get the day number with respect to J2000 epoch.
- getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
- getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Compute the Jacobian of the orbit with respect to maneuver parameters.
- getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
-
- getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
-
- getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
- getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Jjs coefficient.
- getJulianDay() - Method in class org.orekit.files.sp3.SP3File
-
Returns the julian day for this SP3 file.
- getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
- getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Jupiter singleton body.
- getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the x component of eccentricity vector.
- getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for Keplerian elements.
- getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
-
Get the Keplerian mean motion.
- getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
-
Get the Keplerian period.
- getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the keyword.
- getL() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Moon.
- getL() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Moon.
- getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the longitude argument.
- getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the longitude argument.
- getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the last TLE.
- getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the last date of the series.
- getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the last estimations performed.
- getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
-
Get the date of the last known leap second.
- getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the latest cached entry.
- getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
- getLatest() - Method in interface org.orekit.utils.TimeStampedCache
-
Get the latest entry in this cache.
- getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the latitude.
- getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the latitude.
- getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Get the fixed latitude to be crossed (radians).
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch number.
- getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch piece.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch year.
- getLDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Moon time derivative.
- getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Moon time derivative.
- getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the longitude argument derivative.
- getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the longitude argument derivative.
- getLE() - Method in class org.orekit.data.BodiesElements
-
Get the mean Earth longitude.
- getLE() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Earth longitude.
- getLE() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.Orbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the eccentric latitude argument (as per equinoctial parameters).
- getLE() - Method in class org.orekit.propagation.SpacecraftState
-
Get the eccentric latitude argument (as per equinoctial parameters).
- getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
-
Get the value of the previous leap.
- getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
-
Get the value of the previous leap.
- getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
-
Get the value of the previous leap.
- getLEDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Earth longitude time derivative.
- getLEDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Earth longitude time derivative.
- getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.Orbit
-
Get the eccentric longitude argument derivative.
- getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the eccentric longitude.
- getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the first line.
- getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the second line.
- getLJu() - Method in class org.orekit.data.BodiesElements
-
Get the mean Jupiter longitude.
- getLJu() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Jupiter longitude.
- getLJuDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Jupiter longitude time derivative.
- getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Jupiter longitude time derivative.
- getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Compute the limits in L, the true longitude, for integration.
- getLM() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.Orbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the mean latitude argument (as per equinoctial parameters).
- getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the mean longitude.
- getLM() - Method in class org.orekit.propagation.SpacecraftState
-
Get the mean latitude argument (as per equinoctial parameters).
- getLMa() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mars longitude.
- getLMa() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mars longitude.
- getLMaDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mars longitude time derivative.
- getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mars longitude time derivative.
- getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.Orbit
-
Get the mean longitude argument derivative.
- getLMe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mercury longitude.
- getLMe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mercury longitude.
- getLMeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mercury longitude time derivative.
- getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mercury longitude time derivative.
- getLNe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Neptune longitude.
- getLNe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Neptune longitude.
- getLNeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Neptune longitude time derivative.
- getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Neptune longitude time derivative.
- getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
-
Get the value of Lns(γ).
- getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get astronomical unit.
- getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get a constant defined in the ephemerides headers.
- getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
-
Get an unmodifiable view of the set of data file names that have been loaded.
- getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get Earth/Moon mass ratio.
- getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get the gravitational coefficient of a body.
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
- getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
- getLocation() - Method in class org.orekit.gnss.DOP
-
Gets the location with respect to the Earth where DOP was calculated.
- getLOD() - Method in class org.orekit.frames.EOPEntry
-
Get the LoD (Length of Day) value.
- getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the LoD (Length of Day) value.
- getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the LoD (Length of Day) value.
- getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame
-
Get the type of Local Orbital frame.
- getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get coordinate system for covariance matrix, for Local Orbital Frames.
- getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
-
Get an immutable copy of the logged events.
- getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
-
Get an immutable copy of the logged events.
- getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the longitude.
- getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the longitude.
- getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Get the fixed longitude to be crossed (radians).
- getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
-
Get the Love numbers.
- getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
-
Get the lower case three letters abbreviation.
- getLowerCaseName() - Method in enum org.orekit.time.Month
-
Get the lower case full name.
- getLPrime() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Sun.
- getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Sun.
- getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Sun time derivative.
- getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Sun time derivative.
- getLSa() - Method in class org.orekit.data.BodiesElements
-
Get the mean Saturn longitude.
- getLSa() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Saturn longitude.
- getLSaDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Saturn longitude time derivative.
- getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Saturn longitude time derivative.
- getLUr() - Method in class org.orekit.data.BodiesElements
-
Get the mean Uranus longitude.
- getLUr() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Uranus longitude.
- getLUrDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Uranus longitude time derivative.
- getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Uranus longitude time derivative.
- getLv() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.Orbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the true latitude argument (as per equinoctial parameters).
- getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the true longitude.
- getLv() - Method in class org.orekit.propagation.SpacecraftState
-
Get the true latitude argument (as per equinoctial parameters).
- getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.Orbit
-
Get the true longitude argument derivative.
- getLVe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Venus longitude.
- getLVe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Venus longitude.
- getLVeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Venus longitude time derivative.
- getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Venus longitude time derivative.
- getM0() - Method in class org.orekit.gnss.GPSAlmanac
-
- getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Mean Anomaly at Reference Time.
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the differential equations to integrate (for main state only).
- getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
-
Get all the names of all managed states.
- getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
-
Get a maneuver.
- getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
-
Get a list of all maneuvers.
- getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMargin() - Method in class org.orekit.propagation.events.FieldOfView
-
Get the angular margin to apply (radians).
- getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Get the angular margin to apply (radians).
- getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mars singleton body.
- getMass() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the spacecraft mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Gets the current mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.SpacecraftState
-
Gets the current mass.
- getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
-
Get the master ground station from which measurement is performed.
- getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get the covariance matrix.
- getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Get a line of the matrix.
- getMaxAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the maximal altitude for the model.
- getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the maximal degree available in the last file parsed.
- getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the maximal order available in the last file parsed.
- getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Get maximal time interval between switching function checks.
- getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get the maximal chunks duration.
- getMaxDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the last date of the range.
- getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
-
Get the last date of the range.
- getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the last date of the range.
- getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the maximal supported degree.
- getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the maximum supported degree.
- getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the maximal supported degree.
- getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Get maximal number of iterations in the event time search.
- getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the maximal supported order.
- getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the maximum supported order.
- getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the maximal supported order.
- getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
-
Get the maximum derivation order.
- getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
-
Get the maximum derivation order.
- getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the degree limit for the next file parsing.
- getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the degree limit for the next file parsing.
- getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the order limit for the next file parsing.
- getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the order limit for the next file parsing.
- getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the maximum number of independent cached time slots.
- getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the maximum duration span in seconds of one slot.
- getMaxValue() - Method in class org.orekit.utils.ParameterDriver
-
Get maximum parameter value.
- getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean anomaly.
- getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean anomaly.
- getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean anomaly.
- getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean anomaly derivative.
- getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean anomaly derivative.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData
-
Get the description of the Mean Element Theory.
- getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the mean solar flux.
- getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Get the value of the mean solar flux.
- getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the orbit mean motion.
- getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
-
- getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Mean Motion.
- getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the Keplerian mean motion.
- getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the first time derivative of the mean motion.
- getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the second time derivative of the mean motion.
- getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion first derivative.
- getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion second derivative.
- getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing mean obliquity of the ecliptic.
- getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the measurement.
- getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the measurements parameters supported by this estimator (including measurements and modifiers).
- getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mercury singleton body.
- getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitInternalError
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitParseException
- getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the meta-data for the block.
- getMetaData() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
-
Get the meta-data for the block.
- getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the comment for meta-data.
- getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the minimal altitude for the model.
- getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the first date of the range.
- getMinDate() - Method in interface org.orekit.propagation.