Adaptive Control System Designs for Aircraft Wing Rock
نویسندگان
چکیده
منابع مشابه
Design of a Sliding Mode Control for Wing Rock Suppression in Highly-Swept Wing Aircraft
W ing rock is an oscillatory ro lling motion which arises at high angles of attack in aircraft with highly-swept wings. In the present paper, a method to suppress wing rock through sliding mode control is proposed. Sliding mode control is designed to min imize together roll angle error and command input through a cost function. The procedure is performed on a wing-only analytical model, the con...
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ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2011
ISSN: 1225-1348
DOI: 10.5139/jksas.2011.39.8.725