Flexible Satellite Attitude Control via Adaptive Fuzzy Linearization
The adaptive fuzzy control is combined with input-output linearization control to constitute the hybrid controller. The control method is then applied to the attitude maneuver control of the flexible satellite.The basic control structure is given. The rules of the controller parameter selection, which guarantee the attitude stabilization of the satellite with parameter uncertainties, have been analyzed. Simulation results show that the precise attitude control is accomplished in spite of the uncertainty in the system.
作 者： GUAN Ping LIU Xiang-dong CHEN Jia-bin LIU Xiao-he 作者单位： 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)
LIU Xiao-he(Department of Automation, Beijing Institute of Machinery, Beijing 100085, China)
刊 名： 北京理工大学学报（英文版） EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY 年，卷(期)： 2005 14(2) 分类号： V448.22 关键词： adaptive fuzzy control input-output linerization attitude maneuver flexible satellite