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Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession

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【Author】 Zhou Di, Zhou Jingyang Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

【摘要】 The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.

【Abstract】 The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.

【基金】 National Natural Science Foundation of China(60674102, 60475027);Scientific Research Foundation for the Returned Overseas Chinese Scholars, State Education Ministry of China
  • 【文献出处】 Chinese Journal of Aeronautics ,中国航空学报(英文版) , 编辑部邮箱 ,2007年04期
  • 【分类号】V448
  • 【被引频次】5
  • 【下载频次】57
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