Deprecated API

Contents

• Interfaces
• Classes
• Enums
• Exceptions
• Fields
• Methods
• Constructors

Interfaces

Interface	Description
org.orekit.propagation.events.FunctionalDetector.GFunction	Use ToDoubleFunction instead. Will be removed in next major release.

Classes

Class	Description
org.orekit.propagation.analytical.tle.TLESeries	as of 9.0, this class is deprecated without replacement. The file format used was considered to be too specific and the API not really well designed. Users are encouraged to use their own parser for series of TLE

Enums

Enum	Description
org.orekit.gnss.antenna.SatelliteAntennaCode	as of 9.3 replaced by SatelliteType

Exceptions

Exceptions	Description
org.orekit.errors.OrekitExceptionWrapper	as of 9.3, this class is not used anymore, as OrekitException is now an unchecked exception

Fields

Field	Description
org.orekit.data.DataProvider.GZIP_FILE_PATTERN	as of 9.2, replaced with GzipFilter

Methods

Method	Description
org.orekit.estimation.measurements.AbstractMeasurement.getPropagatorsIndices()	as of 9.3, replaced by AbstractMeasurement.getSatellites()
org.orekit.estimation.measurements.EstimatedMeasurement.getCurrentWeight()	as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status
org.orekit.estimation.measurements.EstimatedMeasurement.setCurrentWeight(double...)	as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status
org.orekit.estimation.measurements.GroundStation.getOffsetGeodeticPoint()	as of 9.1, replaced by GroundStation.getOffsetGeodeticPoint(AbsoluteDate)
org.orekit.estimation.measurements.ObservedMeasurement.getPropagatorsIndices()	as of 9.3, replaced by ObservedMeasurement.getSatellites()
org.orekit.gnss.RinexLoader.getObservations()	as of 9.3 replaced by RinexLoader.getObservationDataSets()
org.orekit.orbits.FieldCircularOrbit.circularToPosition(T, T, T, T, T, T, double)	as of 9.3, replaced by FieldCircularOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()
org.orekit.orbits.FieldEquinoctialOrbit.equinoctialToPosition(T, T, T, T, T, T, double)	as of 9.3, replaced by FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()
org.orekit.orbits.FieldKeplerianOrbit.ellipticKeplerianToPosition(T, T, T, T, T, T, double)	as of 9.3 replaced with FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()
org.orekit.orbits.FieldKeplerianOrbit.hyperbolicKeplerianToPosition(T, T, T, T, T, T, double)	as of 9.3 replaced with FieldKeplerianOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, double) and FieldOrbit.getPVCoordinates()
org.orekit.propagation.events.FunctionalDetector.getGFunction()	use FunctionalDetector.getFunction() instead. Will be removed in next major release.
org.orekit.propagation.events.FunctionalDetector.GFunction.apply(SpacecraftState)	Use ToDoubleFunction.applyAsDouble(Object) instead. Will be removed in next major release.
org.orekit.propagation.events.FunctionalDetector.withGFunction(FunctionalDetector.GFunction)	Use FunctionalDetector.withFunction(ToDoubleFunction) instead. Will be removed in next major release.
org.orekit.propagation.numerical.FieldNumericalPropagator.getForceModels()	as of 9.1, this method is deprecated, the perturbing force models are retrieved together with the Newtonian attraction by calling FieldNumericalPropagator.getAllForceModels()
org.orekit.propagation.numerical.FieldNumericalPropagator.getNewtonianAttractionForceModel()	as of 9.1, this method is deprecated, the Newtonian attraction force model (if any) is the last in the FieldNumericalPropagator.getAllForceModels()
org.orekit.propagation.numerical.JacobiansMapper.getStateDimension()	as of 9.0, replaced with JacobiansMapper.STATE_DIMENSION
org.orekit.propagation.numerical.PartialDerivativesEquations.setInitialJacobians(SpacecraftState, int)	as of 9.0, replaced by PartialDerivativesEquations.setInitialJacobians(SpacecraftState)
org.orekit.propagation.sampling.OrekitFixedStepHandler.init(SpacecraftState, AbsoluteDate)	as of 9.0, replaced by OrekitFixedStepHandler.init(SpacecraftState, AbsoluteDate, double)
org.orekit.time.AbsoluteDate.createGPSDate(int, double)	as of 9.3, replaced by GPSDate(int, double).GPSDate.getDate()
org.orekit.utils.Differentiation.differentiate(ParameterFunction, ParameterDriver, int, double)	as of 9.3, replaced by Differentiation.differentiate(ParameterFunction, int, double)

Constructors

Constructor	Description
org.orekit.estimation.measurements.AbstractMeasurement(AbsoluteDate, double, double, double, List<Integer>, ParameterDriver...)	since 9.3, replaced bew AbstractMeasurement(AbsoluteDate, double, double, double, List) followed by AbstractMeasurement.addParameterDriver(ParameterDriver)
org.orekit.estimation.measurements.AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[])	since 9.3, replaced by AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite)
org.orekit.estimation.measurements.AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[])	since 9.3, replaced by AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)
org.orekit.estimation.measurements.InterSatellitesRange(int, int, boolean, AbsoluteDate, double, double, double)	as of 9.3, replaced by InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double)
org.orekit.estimation.measurements.Phase(GroundStation, AbsoluteDate, double, double, double, double)	since 9.3 raplced by Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite)
org.orekit.estimation.measurements.Position(AbsoluteDate, Vector3D, double, double)	as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)
org.orekit.estimation.measurements.PV(AbsoluteDate, Vector3D, Vector3D, double, double, double)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite)
org.orekit.estimation.measurements.Range(GroundStation, AbsoluteDate, double, double, double)	as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)
org.orekit.estimation.measurements.RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean)	since 9.3 replaced by RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite)
org.orekit.estimation.measurements.TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double)	as of 9.3, replaced by TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite)
org.orekit.forces.radiation.SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive)	as of 9.2 replaced by SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)
org.orekit.frames.EOPEntry(int, double, double, double, double, double, double, double, double)	as of 9.2 replaced with EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion)
org.orekit.frames.InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double)	as of 9.1, replaced by InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double)
org.orekit.frames.ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double)	as of 9.1, replaced by ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double)
org.orekit.gnss.antenna.SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, int, String, AbsoluteDate, AbsoluteDate)	since 9.3 replaced by SatelliteAntenna(String, String, Map, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate)
org.orekit.gnss.attitude.GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int)	as of 9.3 replaced by GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame)
org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double)	as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double)