Abstract Design of the Korea Lunar Pathfinder Orbiter (KPLO) attitude control subsystem is a unique challenge that requires refined models that simulate the cis-lunar and lunar orbital environments including coordinate frame changes, and a new sun-pointing control mode that satisfies Sun and communication pointing constraints. This paper introduces LUNASIM, a simulator for verifying the attitude control performance of KPLO. The simulation architecture is described, and attitude control performance verification results of the sun-pointing control sub-mode are presented.
Attitude Control Simulator for the Korea Pathfinder Lunar Orbiter
The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018) ; 4 ; 2521-2532
Lecture Notes in Electrical Engineering ; 459 , 4
2019-01-01
12 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
The Lunar Orbiter attitude control simulator.
NTRS | 1967
|The Lunar Orbiter Attitude Control Simulator
IEEE | 1967
|Lunar Orbiter Attitude Control System.
NTRS | 1967
|