Show simple item record

contributor authorSungsoo Na
contributor authorBokhee Lee
contributor authorJeonghwan Choo
contributor authorPiergiovanni Marzocca
date accessioned2017-05-08T21:33:46Z
date available2017-05-08T21:33:46Z
date copyrightJuly 2011
date issued2011
identifier other%28asce%29as%2E1943-5525%2E0000076.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56218
description abstractThis paper presents a robust control methodology for the dynamic response control of a rotating blade exposed to external excitations and modeling uncertainty. The blade is modeled as a tapered thin-walled beam with fiber-reinforced composite material. The dynamic response characteristics of a rotating composite beam are investigated; namely, ply angle, taper ratio, and various selected rotational speeds. To extend life and improve efficiency, a robust control methodology is implemented and structural tailoring composite properties are used. To this end, considering modeling uncertainties and external disturbance conditions, a sliding mode control is proposed and its performance and robustness are compared with the conventional linear quadratic Gaussian control.
publisherAmerican Society of Civil Engineers
titleRobust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade
typeJournal Paper
journal volume24
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000076
treeJournal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record