月球立方星姿态控制系统的初步设计与测试
月球立方星姿态控制系统的初步设计与测试
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.
Attitude control, CubeSats hardware system, CubeSats in deep space, System design, University CubeSats
28-35
Yang, Chihang
6c17b81a-41c6-44e5-aa0f-4b147eb7f801
Liu, Jiangkai
c6139422-9739-466e-8d4b-a0ac7d2e9fbd
Long, Long
438974cb-4361-4a56-be2d-3875def813c2
Song, Huan
06ec9402-43b3-427c-a7a7-9f159c71f3f2
Li, Long
ed655ab8-cc7a-4282-b7d5-0ec0a7abf321
Zhu, Lingchao
d4eb4e16-4cee-4190-abc7-755331c7c476
Ye, Bingxu
1cef54d0-2946-4c97-8e02-f69a2b86c07e
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Zhang, Hao
6b809119-4403-4075-aedd-04dcc1c674ab
25 August 2019
Yang, Chihang
6c17b81a-41c6-44e5-aa0f-4b147eb7f801
Liu, Jiangkai
c6139422-9739-466e-8d4b-a0ac7d2e9fbd
Long, Long
438974cb-4361-4a56-be2d-3875def813c2
Song, Huan
06ec9402-43b3-427c-a7a7-9f159c71f3f2
Li, Long
ed655ab8-cc7a-4282-b7d5-0ec0a7abf321
Zhu, Lingchao
d4eb4e16-4cee-4190-abc7-755331c7c476
Ye, Bingxu
1cef54d0-2946-4c97-8e02-f69a2b86c07e
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Zhang, Hao
6b809119-4403-4075-aedd-04dcc1c674ab
Yang, Chihang, Liu, Jiangkai, Long, Long, Song, Huan, Li, Long, Zhu, Lingchao, Ye, Bingxu, Chen, Hongru and Zhang, Hao
(2019)
月球立方星姿态控制系统的初步设计与测试.
Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology, 39 (4), .
(doi:10.16708/j.cnki.1000-758X.2019.0026).
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.
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More information
Published date: 25 August 2019
Alternative titles:
Preliminary design and test of attitude control system for lunar CubeSats
Keywords:
Attitude control, CubeSats hardware system, CubeSats in deep space, System design, University CubeSats
Identifiers
Local EPrints ID: 490961
URI: http://eprints.soton.ac.uk/id/eprint/490961
ISSN: 1000-758X
PURE UUID: 63f8c63c-91a2-49cc-a8fd-d5d9dd0a198e
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Date deposited: 10 Jun 2024 16:51
Last modified: 11 Jun 2024 02:10
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Contributors
Author:
Chihang Yang
Author:
Jiangkai Liu
Author:
Long Long
Author:
Huan Song
Author:
Long Li
Author:
Lingchao Zhu
Author:
Bingxu Ye
Author:
Hongru Chen
Author:
Hao Zhang
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