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

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dc.contributor.authorNa, Sungsoo-
dc.contributor.authorLee, Bokhee-
dc.contributor.authorChoo, Jeonghwan-
dc.contributor.authorMarzocca, Piergiovanni-
dc.date.accessioned2021-09-07T11:13:36Z-
dc.date.available2021-09-07T11:13:36Z-
dc.date.created2021-06-14-
dc.date.issued2011-07-
dc.identifier.issn0893-1321-
dc.identifier.urihttps://scholar.korea.ac.kr/handle/2021.sw.korea/112156-
dc.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. DOI: 10.1061/(ASCE)AS.1943-5525.0000076. (C) 2011 American Society of Civil Engineers.-
dc.languageEnglish-
dc.language.isoen-
dc.publisherASCE-AMER SOC CIVIL ENGINEERS-
dc.subjectFINITE-ELEMENT MODEL-
dc.subjectAEROELASTIC CONTROL-
dc.subjectVIBRATION ANALYSIS-
dc.subjectBEAMS-
dc.titleRobust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade-
dc.typeArticle-
dc.contributor.affiliatedAuthorNa, Sungsoo-
dc.identifier.doi10.1061/(ASCE)AS.1943-5525.0000076-
dc.identifier.scopusid2-s2.0-79960280641-
dc.identifier.wosid000292514800005-
dc.identifier.bibliographicCitationJOURNAL OF AEROSPACE ENGINEERING, v.24, no.3, pp.298 - 308-
dc.relation.isPartOfJOURNAL OF AEROSPACE ENGINEERING-
dc.citation.titleJOURNAL OF AEROSPACE ENGINEERING-
dc.citation.volume24-
dc.citation.number3-
dc.citation.startPage298-
dc.citation.endPage308-
dc.type.rimsART-
dc.type.docTypeArticle-
dc.description.journalClass1-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.relation.journalWebOfScienceCategoryEngineering, Civil-
dc.subject.keywordPlusFINITE-ELEMENT MODEL-
dc.subject.keywordPlusAEROELASTIC CONTROL-
dc.subject.keywordPlusVIBRATION ANALYSIS-
dc.subject.keywordPlusBEAMS-
dc.subject.keywordAuthorRobust control-
dc.subject.keywordAuthorSliding mode control-
dc.subject.keywordAuthorThin-walled beams-
dc.subject.keywordAuthorRotating blade-
dc.subject.keywordAuthorPiezo-actuators-
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