Deprecated API

Contents

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

Deprecated Interfaces

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

Deprecated 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

Deprecated Enums

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

Deprecated Exceptions

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

Deprecated Fields

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

Deprecated Methods

Method	Description
org.orekit.propagation.events.FunctionalDetector.GFunction.apply(SpacecraftState)	Use ToDoubleFunction.applyAsDouble(Object) instead. Will be removed in next major release.
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.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)
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.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.estimation.measurements.EstimatedMeasurement.getCurrentWeight()	as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status
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.events.FunctionalDetector.getGFunction()	use FunctionalDetector.getFunction() instead. Will be removed in next major release.
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.gnss.RinexLoader.getObservations()	as of 9.3 replaced by RinexLoader.getObservationDataSets()
org.orekit.estimation.measurements.GroundStation.getOffsetGeodeticPoint()	as of 9.1, replaced by GroundStation.getOffsetGeodeticPoint(AbsoluteDate)
org.orekit.estimation.measurements.AbstractMeasurement.getPropagatorsIndices()	as of 9.3, replaced by AbstractMeasurement.getSatellites()
org.orekit.estimation.measurements.ObservedMeasurement.getPropagatorsIndices()	as of 9.3, replaced by ObservedMeasurement.getSatellites()
org.orekit.propagation.numerical.JacobiansMapper.getStateDimension()	as of 9.0, replaced with JacobiansMapper.STATE_DIMENSION
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.sampling.OrekitFixedStepHandler.init(SpacecraftState, AbsoluteDate)	as of 9.0, replaced by OrekitFixedStepHandler.init(SpacecraftState, AbsoluteDate, double)
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.propagation.numerical.PartialDerivativesEquations.setInitialJacobians(SpacecraftState, int)	as of 9.0, replaced by PartialDerivativesEquations.setInitialJacobians(SpacecraftState)
org.orekit.propagation.events.FunctionalDetector.withGFunction(FunctionalDetector.GFunction)	Use FunctionalDetector.withFunction(ToDoubleFunction) instead. Will be removed in next major release.

Deprecated 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.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.AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], int)	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.AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int)	since 9.3, replaced by AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite)
org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double)	as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double)
org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double)	as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double)
org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive)	as of 9.2 replaced by DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)
org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive)	as of 9.2 replaced by {DSSTSolarRadiationPressure(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.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.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.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.Phase(GroundStation, AbsoluteDate, double, double, double, double, int)	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.Position(AbsoluteDate, Vector3D, double[][], double, int)	as of 9.3, replaced by Position(AbsoluteDate, Vector3D, 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.Position(AbsoluteDate, Vector3D, double[], double, int)	as of 9.3, replaced by Position(AbsoluteDate, Vector3D, 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.Position(AbsoluteDate, Vector3D, double, double, int)	as of 9.3, replaced by Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite)
org.orekit.estimation.measurements.PV(AbsoluteDate, Vector3D, Vector3D, double[][], double)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, 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.PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, int)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite)
org.orekit.estimation.measurements.PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, int)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite)
org.orekit.estimation.measurements.PV(AbsoluteDate, Vector3D, Vector3D, double[], double)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, 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.PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, int)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite)
org.orekit.estimation.measurements.PV(AbsoluteDate, Vector3D, Vector3D, double[], double, int)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, 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.PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, int)	as of 9.3, replaced by PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite)
org.orekit.estimation.measurements.Range(GroundStation, boolean, AbsoluteDate, double, double, double, int)	as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, 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.Range(GroundStation, AbsoluteDate, double, double, double, boolean)	as of 9.3, replaced by Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite)
org.orekit.estimation.measurements.Range(GroundStation, AbsoluteDate, double, double, double, int)	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.RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, int)	since 9.3 replaced by RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite)
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.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.forces.radiation.SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive)	as of 9.2 replaced by SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive)
org.orekit.forces.radiation.SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive)	as of 9.2 replaced by SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive)
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.estimation.measurements.TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, int)	as of 9.3, replaced by TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite)