Full Eckstein-Hechler dynamical model realization
Both Orekit and Celestlab implement the Eckstein-Hechler model, but the modeling is not fully realized, only the perturbations of J2~J6 and J2^2 are considered.
The semi-major axis accuracy of the complete Eckstein-Hechler model can reach 1m. The full implementation can address many orbital maneuver planning problems, is anyone willing to do this difficult but cool task together?
Edited by Liao Spacefan