Package org.orekit.propagation.conversion.averaging

package org.orekit.propagation.conversion.averaging

This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.

Since:

12.1

Author:

Romain Serra

Related Packages

Package	Description
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.conversion.averaging.converters	This package wraps conversions from an osculating orbit to an averaged state according to a given theory (usually via a fixed-point algorithm using the inverse conversion).
org.orekit.propagation.conversion.averaging.elements	This package contains data classes representing averaged orbital elements (not time-stamped and in any theory compatible with this choice of coordinates).
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).

Class	Description
AbstractAveragedOrbitalState	Abstract class representing averaged orbital state.
AveragedOrbitalState	Interface representing averaged orbital elements at a specific instant.
BrouwerLyddaneOrbitalState	Class representing an averaged orbital state as in the Brouwer-Lyddane theory.
DSST6X0OrbitalState	Class representing an averaged orbital state as in the DSST theory using only the first 6 zonal harmonics as perturbations.
EcksteinHechlerOrbitalState	Class representing an averaged orbital state as in the Eckstein-Hechler theory.
SGP4OrbitalState	Class representing an averaged orbital state as in the TLE-related theory.