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	Controller design and simulation of aircraft's automatic landing under complex atmospheric conditions
	Zou Xin-sheng ; Li Chun-wen
	2010-05-06 ; 2010-05-06
关键词	Practical Theoretical or Mathematical/ aerospace simulation aircraft landing guidance atmospheric turbulence neurocontrollers robust control/ controller design aircrafts automatic landing complex atmospheric conditions neural network real flight altitude reference flight altitude inverse system/ B7620 Aerospace test facilities and simulation B7650 Ground support systems C3360L Aerospace control C1340N Neurocontrol C1320 Stability in control theory
中文摘要	The control of aircraft's automatic approach and landing was designed, mainly using inverse system method, compensated by neural network for robustness. The learning rule of neural network was a linear function of the neural network's sensitivity with dead zone. Some typical atmospheric conditions, such as turbulence and windshear, were analyzed, which might occur in landing. Some simulations were made to verify the control law under above-mentioned complex atmospheric conditions. The simulation results show that the automatic landing system has good robustness to complex atmospheric conditions, and the error between the real flight altitude in landing and reference flight altitude is in a reasonable range.
语种	中文 ; 中文
出版者	Editorial Committee of J. Systems Simulation ; China
内容类型	期刊论文
源URL	[http://hdl.handle.net/123456789/8888]
专题	清华大学
推荐引用方式 GB/T 7714	Zou Xin-sheng,Li Chun-wen. Controller design and simulation of aircraft's automatic landing under complex atmospheric conditions[J],2010, 2010.
APA	Zou Xin-sheng,&Li Chun-wen.(2010).Controller design and simulation of aircraft's automatic landing under complex atmospheric conditions..
MLA	Zou Xin-sheng,et al."Controller design and simulation of aircraft's automatic landing under complex atmospheric conditions".(2010).

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