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

Packages that use OsculatingToMeanConverter

Package	Description
org.orekit.control.heuristics	This package for optimal control provides heuristics methods i.e. not involving formal optimization processes.
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.control.heuristics

Constructors in org.orekit.control.heuristics with parameters of type OsculatingToMeanConverter

Modifier	Constructor	Description
	MeanSmaChangeImpulseProvider(double maximumMagnitude, double targetSemiMajorAxis, OsculatingToMeanConverter osculatingToMeanConverter)	Constructor.
	MeanSmaChangeImpulseProvider(double targetSemiMajorAxis, OsculatingToMeanConverter osculatingToMeanConverter)	Constructor with default maximum magnitude set to positive infinity (unconstrained).

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

Modifier	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, 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.