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simulation results show that

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The attitude tracking control problem for a satellite with parameter uncertainties and external disturbances is considered in this paper. For this class of multi-input multi-output uncertain nonlinear systems, a design method of robust output tracking controllers is proposed based on the upper-bounds of the uncertainties. Using the input/output feedback linearization approach and Lyapunov method, a control law is designed, which guarantees that the system output exponentially tracks the given desired output. The proposed controller is easy to compute and complement. Simulation results show that, in the closed-loop system, precise attitude control is accomplished in spite of the uncertainties in the system.

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simulation results show that

仿真结果表明:

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    通过模拟实验证明失超保护系统满足设计要求

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    模拟结果表明,各异性模型各向同性模型可以更好描述实际介质

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    仿真结果表明开关磁阻电机智能滑模结构控制方法简单良好动态性能,较好的鲁棒性。

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