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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (1): 114-118.

• 论文 • Previous Articles     Next Articles

ROBUST PI DECOUPLING DESIGN OF HELICOPTER FLIGHT CONTROL SYSTEM

Wang Yandong, Cheng Peng   

  1. Faculty 301 of Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1993-09-13 Revised:1994-12-08 Online:1996-02-25 Published:1996-02-25

Abstract: This paper studies a design method for the stabilizing systems of a multivariable robust PI controller. A necessary condition that a robust PI controller exists is given,and static decoupling is discussed with regard to the PI controller. Finally,a helicopter flight control systems is designed by this method. A satisfactory result of imitation is illustrated.

Key words: robustness, multivariable control, decoupling

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