contributor author | Sungsoo Na | |
contributor author | Bokhee Lee | |
contributor author | Jeonghwan Choo | |
contributor author | Piergiovanni Marzocca | |
date accessioned | 2017-05-08T21:33:46Z | |
date available | 2017-05-08T21:33:46Z | |
date copyright | July 2011 | |
date issued | 2011 | |
identifier other | %28asce%29as%2E1943-5525%2E0000076.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56218 | |
description abstract | This 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. | |
publisher | American Society of Civil Engineers | |
title | Robust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade | |
type | Journal Paper | |
journal volume | 24 | |
journal issue | 3 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)AS.1943-5525.0000076 | |
tree | Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003 | |
contenttype | Fulltext | |