| Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession |
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| 作者姓名： | Zhou Di Zhou Jingyang |
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| 作者单位： | Zhou Di，Zhou Jingyang Department of Control Science and Engineering，Harbin Institute of Technology，Harbin 150001，China |
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| 基金项目： | 国家自然科学基金
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Scientific Research Foundation for the Returned Overseas Chinese Scholars, State Education Ministry of China |
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| 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.
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| 关 键 词： | 适应控制 姿态控制 线性化反应 同步化 |
| 收稿时间： | 9 June 2006 |
| 修稿时间： | 2006-06-092006-12-22 |
Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession |
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| Zhou Di Zhou Jingyang.Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession[J].Chinese Journal of Aeronautics,2007,20(4):332-338. |
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| Authors: | Zhou Di Zhou Jingyang |
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| Institution: | Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China |
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| 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. |
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| Keywords: | adaptive control attitude control feedback linearization CMG synchronization Precession Synchronous Driven Truss Spacecraft Motion Control Adaptive Performance simulation adaptive nonlinear control controller deal with items help feedback linearization recursive Lyapunov design method angular momentum |
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