| 直升机飞行控制系统鲁棒PI解耦设计 |
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| 引用本文： | 王艳东,程鹏.直升机飞行控制系统鲁棒PI解耦设计[J].航空学报,1996,17(1):114-118. |
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| 作者姓名： | 王艳东 程鹏 |
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| 作者单位： | 北京航空航天大学３０１教研室 |
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| 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
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| 关 键 词： | 鲁棒性 多变量控制 解耦 |
ROBUST PI DECOUPLING DESIGN OF HELICOPTER FLIGHT CONTROL SYSTEM |
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| Wang Yandong,Cheng Peng.ROBUST PI DECOUPLING DESIGN OF HELICOPTER FLIGHT CONTROL SYSTEM[J].Acta Aeronautica et Astronautica Sinica,1996,17(1):114-118. |
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| Authors: | Wang Yandong Cheng Peng |
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| Institution: | Faculty 301 of Beijing University of Aeronautics and Astronautics,Beijing,100083 |
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| 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. |
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| Keywords: | robustness multivariable control decoupling |
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