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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): 1119-1122.
Huang You. LQ optimal simulation for aircraft anti-skid brake control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1119-1122. (in Chinese)
Citation: Huang You. LQ optimal simulation for aircraft anti-skid brake control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1119-1122. (in Chinese)
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LQ optimal simulation for aircraft anti-skid brake control system

  • Chengdu Aircraft Design and Research Institute, Chengdu 610041, China

  • Received Date: 20 Jun 2003
  • Publish Date: 31 Dec 2003
    Abstract
  • Linear-Quadratic optimal control technique, Matlab optimal toolbox and Simulink were applied for aircraft anti-skid brake control system, according to aircraft body,tyre,ground and brake device. The dynamic model was given by modern state-space method, optimal state-feedback gain was calculated and the robust controller of aircraft anti-skid brake system was designed.

     

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    • References(1)
  • [1] 胡寿松.自动控制原理[M].北京:科学出版社,2002 Hu Shousong. Automatic control theory[M]. Beijing:Science Press, 2002(in Chinese) [2] 程 军.汽车防抱死制动系统的理论与实践[M].北京:北京理工大学出版社,1999 Cheng Jun. Theory and application for anti-lock braking system[M]. Beijing:Beijing Institute of Technology Press, 1999(in Chinese) [3] 韩利竹, 王 华.MATLAB电子仿真与应用[M].北京:国防工业出版社,2001 Han Lizhu, Wang Hua. Electronic simulation and application of Matlab[M]. Beijing:National Defence Industry Press,2001(in Chinese)
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