Quaternion-based finite time control for spacecraft attitude tracking

Acta Astronautica - Tập 69 Số 1-2 - Trang 48-58 - 2011
Shunan Wu1,2, Gianmarco Radice2, Yongsheng Gao3, Zhaowei Sun1
1Research Center of Satellite Technology, Harbin Institute of Technology, Harbin, PR China
2Space Advanced Research Team, School of Engineering, University of Glasgow, Glasgow G12 8QQ, UK
3Robotic Institute, Harbin Institute of Technology, Harbin, PR China

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