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contributor authorSeok-Ju Cha
contributor authorJi-Seok Song
contributor authorHwan-Hee Lee
contributor authorSungsoo Na
contributor authorJae-Hong Shim
contributor authorPiergiovanni Marzocca
date accessioned2017-05-08T22:07:12Z
date available2017-05-08T22:07:12Z
date copyrightSeptember 2014
date issued2014
identifier other29607260.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/71729
description abstractA study of the dynamic control of a rotating blade subjected to external excitations is presented. A tapered thin-walled beam of closed cross-section contour with fiber-reinforced composite material is used for present study. Since a rotating blade may be exposed to a severe environment such as high angular velocity, large external load, and so on, robust control methodology is implemented to extend the blade’s life and improve its efficiency. To verify the performance of the state estimator, a sliding mode observer is introduced, and an associated robustness test is conducted in case of model uncertainty. A robust control methodology using sliding mode control in conjunction with a sliding mode observer is implemented, and its performance toward reducing the flapping dynamic responses of a rotating blade under initial conditions and various external loadings such blast load and distributed load is demonstrated. Moreover, its control performance is compared with that of the conventional linear quadratic Gaussian implementation.
publisherAmerican Society of Civil Engineers
titleDynamic Response Control of Rotating Thin-Walled Composite Blade Exposed to External Excitations
typeJournal Paper
journal volume27
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000335
treeJournal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 005
contenttypeFulltext


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