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Document Type : Latin Dissertation
Language of Document : English
Record Number : 149001
Doc. No : ET20793
Main Entry : Sushma Gujjula
Title Proper : SUPPRESSION OF LIMIT CYCLE OSCILLATIONS IN AN AEROELASTIC SYSTEM USING ROBUST AND ADAPTIVE CONTROL
Note : This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract : In this thesis control systems are designed for the flutter control of nonlinearaeroelastic system. The aeroelastic model describes the plunge and pitch motion ofa wing. The model includes plunge and pitch nonlinearities, and has both leading-and trailing edge control surfaces for the purpose of control. First the existence oflimit cycle oscillations and domain of stability (attraction) of prototypical aeroelasticwing sections with pitch structural nonlinearity using the describing function method.
Subject : Electericl tess
: برق
electronic file name : TL43938.pdf
Title and statement of responsibility and : SUPPRESSION OF LIMIT CYCLE OSCILLATIONS IN AN AEROELASTIC SYSTEM USING ROBUST AND ADAPTIVE CONTROL [Thesis]
 
 
 
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