Deprecated List (OREKIT 13.1.2 API)

Interfaces
Interface Description

org.orekit.utils.ExtendedPVCoordinatesProvider
since 13.0. Use ExtendedPositionProvider instead.

Classes
Class	Description
org.orekit.propagation.events.AdapterDetector	since 13.0. Use `DetectorModifier` instead.
org.orekit.propagation.events.FieldAdapterDetector	since 13.0. Use `FieldDetectorModifier` instead.

Fields
Field Description

org.orekit.propagation.AbstractMatricesHarvester.STATE_DIMENSION
as of 13.1, use DEFAULT_STATE_DIMENSION

Methods
Method	Description
org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType.outputField(TimeConverter, OrbitManeuver)	since 13.0, because formatter should be specified. Use `ManeuverFieldType.outputField(TimeConverter, OrbitManeuver, Formatter)` instead.
org.orekit.propagation.analytical.tle.FieldTLE.stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TleGenerationAlgorithm)	As of release 13.0, use `FieldTLE.stateToTLE(FieldSpacecraftState, FieldTLE, OsculatingToMeanConverter)` instead.
org.orekit.propagation.analytical.tle.TLE.stateToTLE(SpacecraftState, TLE, TleGenerationAlgorithm)	As of release 13.0, use `TLE.stateToTLE(SpacecraftState, TLE, OsculatingToMeanConverter)` instead.
org.orekit.propagation.events.EventSlopeFilter.getFilter()	since 13.0 (use getFilterType)
org.orekit.propagation.numerical.FieldNumericalPropagator.tolerances(T, FieldOrbit<T>, OrbitType)	since 13.0. Use `ToleranceProvider` for default and custom tolerances.
org.orekit.propagation.numerical.NumericalPropagator.tolerances(double, AbsolutePVCoordinates)	since 13.0. Use `ToleranceProvider` for default and custom tolerances.
org.orekit.propagation.semianalytical.dsst.DSSTPropagator.tolerances(double, Orbit)	since 13.0. Use `ToleranceProvider` for default and custom tolerances.
org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator.tolerances(T, FieldOrbit<T>)	since 13.0. Use `ToleranceProvider` for default and custom tolerances.
org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext.getMoa()	since 12.2 Use getMuoa() instead
org.orekit.propagation.StateCovariance.getStm(Orbit, double)	since 13.1. If you must, do: final RealMatrix stm = MatrixUtils.createRealIdentityMatrix(STATE_DIMENSION); double contribution = initialOrbit.getMeanAnomalyDotWrtA() * dt; stm.setEntry(5, 0, contribution);
org.orekit.utils.AccurateFormatter.format(int, int, int, int, int, double)	As of 13.0, because static method does not utilize inheritance benefits from `Formatter` and does not check format standards of date time. Use `AccurateFormatter.toString(int, int, int, int, int, double)` instead.
org.orekit.utils.ExtendedPositionProvider.toExtendedPVCoordinatesProvider()	since 13.0. Only there to help transition out.
org.orekit.utils.FieldTimeSpanMap.addValidAfter(T, FieldAbsoluteDate<F>)	as of 13.1, replaced by `FieldTimeSpanMap.addValidAfter(Object, FieldAbsoluteDate, boolean)`
org.orekit.utils.FieldTimeSpanMap.addValidBefore(T, FieldAbsoluteDate<F>)	as of 13.1, replaced by `FieldTimeSpanMap.addValidBefore(Object, FieldAbsoluteDate, boolean)`
org.orekit.utils.FieldTimeSpanMap.getTransitions()	as of 13.1, this method is replaced by `FieldTimeSpanMap.getFirstTransition()` and then following intertwined links between `Span` and `Transition`

Constructors
Constructor	Description
org.orekit.files.ccsds.utils.generation.AbstractGenerator(Appendable, String, double, boolean)	since 13.0, since does not allow user to specify formatter. This defaults to `AccurateFormatter` Use `AbstractGenerator(Appendable, String, double, boolean, Formatter)` instead.
org.orekit.forces.maneuvers.FieldImpulseManeuver(FieldEventDetector<T>, AttitudeProvider, FieldVector3D<T>, T, Control3DVectorCostType)	since 13.0
org.orekit.forces.maneuvers.ImpulseManeuver(EventDetector, AttitudeProvider, Vector3D, double, Control3DVectorCostType)	since 13.0
org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale)	as of 13.1.1, replaced by `GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale, TimeInterpolator)`
org.orekit.propagation.FieldSpacecraftState(FieldOrbit<T>, T)	since 13.0, use withXXX
org.orekit.propagation.SpacecraftState(Orbit, double)	since 13.0, use withXXX
org.orekit.time.TimeStampedDouble(double, AbsoluteDate)
org.orekit.time.TimeStampedDoubleAndDerivative(double, double, AbsoluteDate)