NDLI: Bang-bang optimal control method with plasma actuators in airfoil roll control

Content Provider	IEEE Xplore Digital Library
Author	Wei Qingkai Chen Bao Niu Zhongguo Huang Xun
Copyright Year	2012
Description	Author affiliation: Department of Aeronautics and Astronautics, Peking University, Beijing, 100871, P.R. China (Wei Qingkai; Huang Xun) \|\| Harbin Institute of Technology, Harbin 150001, P.R. China (Chen Bao; Niu Zhongguo)
Abstract	The bang-bang optimal control method was proposed for glow discharge plasma actuators, taking account of practical issues, such as limited actuation states with instantaneously varied aerodynamic control performance. Hence, this work's contribution is to integrate flight control with active flow control in particular for plasma actuators. Flow control effects were examined in wind tunnel experiments, which show that the plasma authority for flow control is limited. Via the experimental results, flow control effects are only obvious at pitch angles near stall. However, flight control simulations suggest that even those small plasma-induced roll moments can satisfactorily fulfill the maneuver tasks and meet flight quality specifications. In addition, the disturbance from volatile plasma-induced roll moments can be rejected. Hence, the proposed bang-bang control method is a promising candidate of control design methodology for plasma actuators.
Starting Page	4674
Ending Page	4679
File Size	583259
Page Count	6
File Format	PDF
ISBN	9781467325813
ISSN	21612927
e-ISBN	9789881563811
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-07-25
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	Electrodes Actuators Roll control Bang-bang control Atmospheric modeling Aerodynamics Plasmas Automotive components Bang-bang control method
Content Type	Text
Resource Type	Article

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