Uses of Interface org.orekit.propagation.conversion.osc2mean.OsculatingToMeanConverter (OREKIT 13.0-SNAPSHOT API)

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Packages that use OsculatingToMeanConverter
Package	Description
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion.osc2mean	This package provides the ability to convert osculating orbits into mean orbits according to different theories (Brouwer-Lyddane, Eckstein-Hechler, SGP4/SDP4, DSST) with different conversion algorithms (fixed-point, least-squares).
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Uses of OsculatingToMeanConverter in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical with parameters of type OsculatingToMeanConverter
Modifier and Type	Method	Description
`static KeplerianOrbit`	BrouwerLyddanePropagator.`computeMeanOrbit(Orbit osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double m2Value, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`static KeplerianOrbit`	BrouwerLyddanePropagator.`computeMeanOrbit(Orbit osculating, UnnormalizedSphericalHarmonicsProvider provider, double m2Value, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`static CircularOrbit`	EcksteinHechlerPropagator.`computeMeanOrbit(Orbit osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`static <T extends CalculusFieldElement<T>> FieldKeplerianOrbit<T>`	FieldBrouwerLyddanePropagator.`computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double m2Value, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`static <T extends CalculusFieldElement<T>> FieldCircularOrbit<T>`	FieldEcksteinHechlerPropagator.`computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`void`	BrouwerLyddanePropagator.`resetInitialState(SpacecraftState state, PropagationType stateType, OsculatingToMeanConverter converter)`	Reset the propagator initial state.
`void`	EcksteinHechlerPropagator.`resetInitialState(SpacecraftState state, PropagationType stateType, OsculatingToMeanConverter converter)`	Reset the propagator initial state.
`void`	FieldBrouwerLyddanePropagator.`resetInitialState(FieldSpacecraftState<T> state, PropagationType stateType, OsculatingToMeanConverter converter)`	Reset the propagator initial state.
`void`	FieldEcksteinHechlerPropagator.`resetInitialState(FieldSpacecraftState<T> state, PropagationType stateType, OsculatingToMeanConverter converter)`	Reset the propagator initial state.
`protected void`	BrouwerLyddanePropagator.`resetIntermediateState(SpacecraftState state, boolean forward, OsculatingToMeanConverter converter)`	Reset an intermediate state.
`protected void`	EcksteinHechlerPropagator.`resetIntermediateState(SpacecraftState state, boolean forward, OsculatingToMeanConverter converter)`	Reset an intermediate state.
`protected void`	FieldBrouwerLyddanePropagator.`resetIntermediateState(FieldSpacecraftState<T> state, boolean forward, OsculatingToMeanConverter converter)`	Reset an intermediate state.
`protected void`	FieldEcksteinHechlerPropagator.`resetIntermediateState(FieldSpacecraftState<T> state, boolean forward, OsculatingToMeanConverter converter)`	Reset an intermediate state.

Constructors in org.orekit.propagation.analytical with parameters of type OsculatingToMeanConverter
Constructor	Description
`BrouwerLyddanePropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, OsculatingToMeanConverter converter)`	Build a propagator from orbit, attitude provider, mass and potential.
`EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mass, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, OsculatingToMeanConverter converter)`	Build a propagator from orbit, attitude provider, mass and potential.
`FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double m2Value, OsculatingToMeanConverter converter)`	Build a propagator from orbit, attitude provider, mass and potential.
`FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, OsculatingToMeanConverter converter)`	Build a propagator from FieldOrbit, attitude provider, mass and potential.

Uses of OsculatingToMeanConverter in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle with parameters of type OsculatingToMeanConverter
Modifier and Type	Method	Description
`static <T extends CalculusFieldElement<T>> FieldTLE<T>`	FieldTLE.`stateToTLE(FieldSpacecraftState<T> state, FieldTLE<T> templateTLE, OsculatingToMeanConverter converter)`	Convert Spacecraft State into TLE.
`static <T extends CalculusFieldElement<T>> FieldTLE<T>`	FieldTLE.`stateToTLE(FieldSpacecraftState<T> state, FieldTLE<T> templateTLE, OsculatingToMeanConverter converter, DataContext dataContext)`	Convert Spacecraft State into TLE.
`static TLE`	TLE.`stateToTLE(SpacecraftState state, TLE templateTLE, OsculatingToMeanConverter converter)`	Convert Spacecraft State into TLE.
`static TLE`	TLE.`stateToTLE(SpacecraftState state, TLE templateTLE, OsculatingToMeanConverter converter, DataContext dataContext)`	Convert Spacecraft State into TLE.

Uses of OsculatingToMeanConverter in org.orekit.propagation.conversion.osc2mean

Classes in org.orekit.propagation.conversion.osc2mean that implement OsculatingToMeanConverter
Modifier and Type	Class	Description
`class`	`FixedPointConverter`	Class enabling conversion from osculating to mean orbit for a given theory using a fixed-point algorithm.
`class`	`LeastSquaresConverter`	Class enabling conversion from osculating to mean orbit for a given theory using a least-squares algorithm.

Uses of OsculatingToMeanConverter in org.orekit.propagation.semianalytical.dsst

Methods in org.orekit.propagation.semianalytical.dsst with parameters of type OsculatingToMeanConverter
Modifier and Type	Method	Description
`static SpacecraftState`	DSSTPropagator.`computeMeanState(SpacecraftState osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModels, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.
`static <T extends CalculusFieldElement<T>> FieldSpacecraftState<T>`	FieldDSSTPropagator.`computeMeanState(FieldSpacecraftState<T> osculating, AttitudeProvider attitudeProvider, Collection<DSSTForceModel> forceModel, OsculatingToMeanConverter converter)`	Conversion from osculating to mean orbit.