航空学报 > 1996, Vol. 17 Issue (1): 114-118

直升机飞行控制系统鲁棒PI解耦设计

王艳东, 程鹏   

  1. 北京航空航天大学301教研室, 北京, 100083
  • 收稿日期:1993-09-13 修回日期:1994-12-08 出版日期:1996-02-25 发布日期:1996-02-25

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

摘要: 研究了多变量鲁棒PI控制器实现系统稳定的设计方法,给出了鲁棒PI控制器存在的必要条件,并对PI控制器实现系统静态解耦进行了讨论。用该方法对某直升机飞行控制系统进行设计,给出了仿真结果

关键词: 鲁棒性, 多变量控制, 解耦

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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