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	Wind tunnel test and gust load alleviation of flexible wing including geometric nonlinearities with servo control
	Chao, A.; Changchuan, X.; Yang, M.; Chao, Y.
	2018
会议名称	AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018
会议日期	2018-01-08
关键词	Aspect ratio Atmospheric turbulence Aviation Control nonlinearities Control surfaces Finite element method Flexible wings Linearization Proportional control systems State space methods Structural dynamics Two term control systems Wind stress Geometric non-linearity Gust load alleviation Nonlinear finite element method Proportional integral derivative controllers State - space models Trailing-edge control surfaces Vertical accelerations Vortex lattice method Wind tunnels
收录类别	EI
URL标识	查看原文
内容类型	会议论文
URI标识	http://www.corc.org.cn/handle/1471x/5934187
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Chao, A.,Changchuan, X.,Yang, M.,et al. Wind tunnel test and gust load alleviation of flexible wing including geometric nonlinearities with servo control[C]. 见:AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018. 2018-01-08.

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