Adaptive Fuzzy Attitude Control of Flexible Satellite

The adaptive fuzzy control is applied in the attitude stabilization of flexible satellite. The detailed design procedure of the adaptive fuzzy control system is presented. Two T-S models are used as both controller and identifier. The parameters of the controller could be modified according to the information of the identifier. Simulation results show that the method can effectively cope with the uncertainty of flexible satellite by on-line learning and thus posses the good robustness. With the proposed method, the precise attitude control is accomplished.

作 者： GUAN Ping LIU Xiang-dong CHEN Jia-bin   作者單位： GUAN Ping(School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China;Department of Automation, Beijing Institute of Machinery, Beijing 100085, China)

LIU Xiang-dong,CHEN Jia-bin(School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China) 

刊 名： 北京理工大學(xué)學(xué)報(bào)（英文版）  EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年，卷(期)： 2005 14(1)  分類(lèi)號(hào)： V448.22  關(guān)鍵詞： attitude control   adaptive fuzzy control   self-learning   flexible satellite  

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