直升机飞行/推进综合控制器的设计  

On Simplifying Design of Helicopter IFPC System Designed with H_∞ Theory

作　　者：王志峰[1] 姜广伦[1] 安锦文[1] 

机构地区：[1]西北工业大学自动控制系,陕西西安710072

出　　处：《西北工业大学学报》2000年第4期621-624,共4页Journal of Northwestern Polytechnical University

摘　　要：用 H∞ 控制理论设计直升机飞行 /推进综合控制器 ,提出了一种基于性能指标要求的加权阵选择方法 ,整个设计过程简单明了且效果很好 。When designing helicopter IFPC (integrated flight/propulsion control) system with H ∞ theory, its robustness performance depends on the very complicated to design matrices W 1 and W 3 . We now present a relatively simple method for their design. Section 2 gives the details of our relatively simple method for designing W 1 , the sensitivity weighting matrix, and W 3 , the complementary sensitivity weighting matrix. Our method is so simple that engineers can use the details in section 2 to design W 1 and W 3 without having to glance through section 1, in which H ∞ theory is briefly summarized. The simulation results in Fig. 4 show preliminarily that the helicopter IFPC system designed by our method is decoupled and possesses strong robustness.

关 键 词：H∞控制 奇异值灵敏度 加权函数阵 直升机 飞行/推进综合控制器 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计] V249