Flight Control Using only Synthetic Jet Actuators in   High-Angle-of-Attack

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	Flight Control Using only Synthetic Jet Actuators in High-Angle-of-Attack
	Li Chunzhi ; Yang Jianying
	2016
关键词	synthetic jet flight control high angle of attack
英文摘要	This paper proposes a novel airfoil active flow control method using only synthetic jet to achieve triple-channel flight attitude control at high angle of attack. It's a feasible and effective control method to solve the difficult problem of flight control at high attack angle when stall occurs. As a first step, we build a model of the aircraft, and derive the relationship between the synthetic-jet peak velocity and moments. Under these conditions, we design a controller to the system. A nonlinear integrated flight control and flow control system was developed and tested in simulations. Simulation results showed that the proposed control method, can effectively control the aircraft at high angle of attack.; National Natural Science Key Foundation of China [11332001, 61573025]; Foundation of national astronautical key lab; CPCI-S(ISTP); 10662-10667
会议录	35th Chinese Control Conference (CCC)
语种	英语
内容类型	会议论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/470230]
专题	工学院
推荐引用方式 GB/T 7714	Li Chunzhi,Yang Jianying. Flight Control Using only Synthetic Jet Actuators in High-Angle-of-Attack[C]. 见:.