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Robust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade

Authors
Na, SungsooLee, BokheeChoo, JeonghwanMarzocca, Piergiovanni
Issue Date
7월-2011
Publisher
ASCE-AMER SOC CIVIL ENGINEERS
Keywords
Robust control; Sliding mode control; Thin-walled beams; Rotating blade; Piezo-actuators
Citation
JOURNAL OF AEROSPACE ENGINEERING, v.24, no.3, pp.298 - 308
Indexed
SCIE
SCOPUS
Journal Title
JOURNAL OF AEROSPACE ENGINEERING
Volume
24
Number
3
Start Page
298
End Page
308
URI
https://scholar.korea.ac.kr/handle/2021.sw.korea/112156
DOI
10.1061/(ASCE)AS.1943-5525.0000076
ISSN
0893-1321
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. DOI: 10.1061/(ASCE)AS.1943-5525.0000076. (C) 2011 American Society of Civil Engineers.
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