Uses of Package
org.orekit.propagation.semianalytical.dsst.forces

Package
Description
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
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.
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).
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).