Package org.orekit.propagation.conversion

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.

See: Description

Interface Summary

Interface	Description
ODEIntegratorBuilder	This interface is the top-level abstraction to build first order integrators for propagators conversion.
PropagatorBuilder	This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter	This interface is the top-level abstraction for propagators conversions.

Class Summary

Class	Description
AbstractPropagatorBuilder	Base class for propagator builders.
AbstractPropagatorConverter	Common handling of PropagatorConverter methods for propagators conversions.
AdamsBashforthIntegratorBuilder	Builder for AdamsBashforthIntegrator.
AdamsMoultonIntegratorBuilder	Builder for AdamsMoultonIntegrator.
ClassicalRungeKuttaIntegratorBuilder	Builder for ClassicalRungeKuttaIntegrator.
DormandPrince54IntegratorBuilder	Builder for DormandPrince54Integrator.
DormandPrince853IntegratorBuilder	Builder for DormandPrince853Integrator.
EcksteinHechlerPropagatorBuilder	Builder for Eckstein-Hechler propagator.
EulerIntegratorBuilder	Builder for EulerIntegrator.
FiniteDifferencePropagatorConverter	Propagator converter using finite differences to compute the jacobian.
GillIntegratorBuilder	Builder for GillIntegrator.
GraggBulirschStoerIntegratorBuilder	Builder for GraggBulirschStoerIntegrator.
HighamHall54IntegratorBuilder	Builder for HighamHall54Integrator.
JacobianPropagatorConverter	Propagator converter using the real jacobian.
KeplerianPropagatorBuilder	Builder for Keplerian propagator.
LutherIntegratorBuilder	Builder for LutherIntegrator.
MidpointIntegratorBuilder	Builder for MidpointIntegrator.
NumericalPropagatorBuilder	Builder for numerical propagator.
OsculatingToMeanElementsConverter	This class converts osculating orbital elements into mean elements.
ThreeEighthesIntegratorBuilder	Builder for ThreeEighthesIntegrator.
TLEPropagatorBuilder	Builder for TLEPropagator.

Package org.orekit.propagation.conversion Description

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator. The conversion principle is to minimize the mean square error for positions and velocities over a given time span.

The conversion from osculating to mean elements appears as a side effect of propagation models conversion.

These package extends an original contribution from Telespazio for TLE (Orbit Converter for Two-Lines Elements) to all propagators.

Author:

Pascal Parraud