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.
Author supplied keywords
Cite
CITATION STYLE
Jung, D., Kwon, J. W., Baek, K., & Ahn, H. W. (2019). Attitude Control Simulator for the Korea Pathfinder Lunar Orbiter. In Lecture Notes in Electrical Engineering (Vol. 459, pp. 2521–2532). Springer Verlag. https://doi.org/10.1007/978-981-13-3305-7_202
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
