摘要
An attitude control system of a spinning spacecraft with internal moving mass is presented in this paper. This system consists of a rigid body and two internal radial moving masses. The mathematical model, including attitude kinematics and nonlinear dynamics equations, is established based on Newtonian mechanics. The control law is designed based on the linearquadratic- regulator (LQR) theory. The performance of the controller is demonstrated in numerical simulation, and the response shows that the attitude control system is stable and effective.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Optoelectronics Engineering and Information Technologies in Industry |
| 页 | 1216-1220 |
| 页数 | 5 |
| DOI | |
| 出版状态 | 已出版 - 2013 |
| 活动 | 2nd International Conference on Opto-Electronics Engineering and Materials Research, OEMR 2013 - Zhengzhou, Henan, 中国 期限: 19 10月 2013 → 20 10月 2013 |
出版系列
| 姓名 | Advanced Materials Research |
|---|---|
| 卷 | 760-762 |
| ISSN（印刷版） | 1022-6680 |
会议
| 会议 | 2nd International Conference on Opto-Electronics Engineering and Materials Research, OEMR 2013 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Zhengzhou, Henan |
| 时期 | 19/10/13 → 20/10/13 |
指纹
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Guo, P. F., & Zhao, L. Y. (2013). Modeling and attitude control of a spinning spacecraft with internal moving mass. 在 Optoelectronics Engineering and Information Technologies in Industry (页码 1216-1220). (Advanced Materials Research; 卷 760-762). https://doi.org/10.4028/www.scientific.net/AMR.760-762.1216