Preliminary design and test of attitude control system for lunar CubeSats

doi:10.16708/j.cnki.1000-758X.2019.0026

Chinese Space Science and Technology ›› 2019, Vol. 39 ›› Issue (4): 28-.doi: 10.16708/j.cnki.1000-758X.2019.0026

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Preliminary design and test of attitude control system for lunar CubeSats

YANG Chi-Hang, LIU Jiang-Kai, LONG Long- , SONG Huan, LI Long, ZHU Ling-Chao, YE Bing-Xu, CHEN Hong-Ru, ZHANG Hao

1.Key Laboratory of Space Utilization，Chinese Academy of Sciences; Technology and Engineer Center for Space Utilization，Chinese Academy of Sciences，Beijing 100094，China
2.University of Chinese Academy of Sciences，Beijing 100049, China
3.School of Astronautics，Northwestern Polytechnical University，Xi′an 710072，China

Received:2018-11-07 Revised:2018-12-27 Published:2019-08-25 Online:2019-04-22

Abstract

Abstract: CubeSats are miniature functional satellites The increasing interest in CubeSats has uncovered the potential for planetary missions Besides, CubeSats is an excellent educational platform. The preliminary attitude control system is designed and the corresponding hardware is built using commercial products for a lunar mission employing a CubeSat constellation to provide positioning service for landers/rovers on the far side of the moon At the same time, the basic frame and necessary subsystems including the structure, power and onboard computer subsystems, and the attitude experiment platform are constructed Based on the hardware platform, the control model is deeply understood through measuring damping coefficients by experiments A PD control method is designed to control the attitude The numerical and physical simulation results match well, and the CubeSat system achieves accurate attitude maneuver.

Key words: university CubeSats, CubeSats in deep space, system design, attitude control, CubeSats hardware system

YANG Chi-Hang, LIU Jiang-Kai, LONG Long- , SONG Huan, LI Long, ZHU Ling-Chao, YE Bing-Xu, CHEN Hong-Ru, ZHANG Hao. Preliminary design and test of attitude control system for lunar CubeSats[J]. Chinese Space Science and Technology, 2019, 39(4): 28-.

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Preliminary design and test of attitude control system for lunar CubeSats

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