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Volume 29 Issue 12
Dec.  2003
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Journal of Beijing University of Aeronautics and Astronautics  > 2003  >  29(12): 1127-1129.
Wang Yueping. Design of fuzzy flight control system based on LMI[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1127-1129. (in Chinese)
Citation: Wang Yueping. Design of fuzzy flight control system based on LMI[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1127-1129. (in Chinese)
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Design of fuzzy flight control system based on LMI

  • Flight Automatic Control Research Institute, Xi'an 710065, China

  • Received Date: 20 Jun 2003
  • Publish Date: 31 Dec 2003
    Abstract
  • A fuzzy flight control system model was established. Through using linear matrix inequality, a design method was gained which guarantees the fuzzy system is global asymptotic stability and the poles were assigned to anticipant areas. The numerical simulations of a fuzzy flight control system designed by this method show the system possesses not only satisfactory performances but also strong robustness.

     

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  • [1] Hua O Wang, Kazuo Tanaka, Michael F Griffin. An approach to fuzzy control of nonlinear systems:stability and design issues[J]. IEEE Trans Fuzzy Systems,1996,4:14~23 [2] Joongseon Joh, Reza Langari, Eun Tae Jeung, et al. A new design method for continuous Takagi-Sugeon fuzzy controller with pole placement constraints:an LMI approach[J]. IEEE, 1997,2969~2974 [3] GJB 185-186,有人驾驶飞机(固定翼)飞行品质[S],1986 GJB185186,Flight qualities of piloted airplanes(fixed wing)[S],1986(in Chinese) [4] Tanaka K, Michio Sugeno.Stability analysis and design of fuzzy control systems[J]. Fuzzy Sets and Systems, 1992,45:135~156
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