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Parametric control systems design with applications in missile control

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Abstract

This paper considers parametric control of high-order descriptor linear systems via proportional plus derivative feedback. By employing general parametric solutions to a type of so-called high-order Sylvester matrix equations, complete parametric control approaches for high-order linear systems are presented. The proposed approaches give simple complete parametric expressions for the feedback gains and the closed-loop eigenvector matrices, and produce all the design degrees of freedom. Furthermore, important special cases are particularly treated. Based on the proposed parametric design approaches, a parametric method for the gain-scheduling controller design of a linear time-varying system is proposed and the design of a BTT missile ai]topilot is carried out. The simulation results show that the method is superior to the traditional one in sense of either global stability or system performance.

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Correspondence to GuangRen Duan.

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Supported by the Major Program of the National Natural Science Foundation of China (Grant No. 60710002), the Program for Changjiang Scholars and Innovative Research Team in University, Self-planed Task of State Key Laboratory of Robotics and System (Grant No. SKLRS200801A03), and the Key Programs of Heilongjiang Province (Grant No. ZJC603)

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Duan, G., Yu, H. & Tan, F. Parametric control systems design with applications in missile control. Sci. China Ser. F-Inf. Sci. 52, 2190–2200 (2009). https://doi.org/10.1007/s11432-009-0188-4

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  • DOI: https://doi.org/10.1007/s11432-009-0188-4

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