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contributor authorOluseyi O. Onawola
contributor authorS. C. Sinha
date accessioned2017-05-09T00:42:41Z
date available2017-05-09T00:42:41Z
date copyrightJuly, 2011
date issued2011
identifier issn1555-1415
identifier otherJCNDDM-25779#031006_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145536
description abstractPanel flutter suppression by exact state transformations and feedback control using piezoelectric actuation is presented. A nonlinear control system is designed for a simply supported rectangular panel with bonded piezoelectric layers based on the von Kármán large-deflection plate theory. The governing nonlinear partial differential equation for the panel is reduced to a set of ordinary differential equations using a two mode approximation. Distributed piezoelectric actuators and sensors connected to processing networks are used as modal actuators and sensors to actively control panel vibrations. The control inputs are given by the electric fields required to drive the actuators based on piezoelectric actuation. Nonlinear feedback control laws are formulated through a transformation of the discretized nonlinear system into an equivalent controllable linear system. The simulated results show that the resulting closed-loop system based on feedback linearized controllers effectively suppress panel flutter limit-cycle motions.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation
typeJournal Paper
journal volume6
journal issue3
journal titleJournal of Computational and Nonlinear Dynamics
identifier doi10.1115/1.4002391
journal fristpage31006
identifier eissn1555-1423
keywordsFlutter (Aerodynamics)
keywordsFeedback
keywordsDeflection
keywordsControl equipment
keywordsActuators
keywordsStress AND Sensors
treeJournal of Computational and Nonlinear Dynamics:;2011:;volume( 006 ):;issue: 003
contenttypeFulltext


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