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http://dx.doi.org/10.5139/JKSAS.2011.39.8.725

Adaptive Control System Designs for Aircraft Wing Rock  

Shin, Yoong-Hyun (국방과학연구소 제1연구개발본부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.39, no.8, 2011 , pp. 725-734 More about this Journal
Abstract
At high angles of attack, aircraft dynamics can display an oscillatory lateral behavior that manifests itself as a limit cycle known as wing rock. In this paper, a classical and neural network based adaptive control design methods of adaptively stabilizing the oscillatory motion by adapting uncertainties are described in detail. All methods are simulated and compared using a model for an 80o swept delta wing.
Keywords
Aircraft Wing Rock; Classical Adaptive Control; Neural Network based Adaptive Control;
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