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Structural feedback linearization based on nonlinearities rejection

dc.creatorBlas L.A.spa
dc.creatorBonilla M.spa
dc.creatorMalabre M.spa
dc.creatorAzhmyakov V.spa
dc.creatorSalazar S.spa
dc.date.accessioned2017-12-19T19:36:41Z
dc.date.available2017-12-19T19:36:41Z
dc.date.created2017
dc.identifier.issn24058963
dc.identifier.urihttp://hdl.handle.net/11407/4249
dc.description.abstractIn this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying. © 2017eng
dc.language.isoeng
dc.publisherElsevier B.V.spa
dc.relation.isversionofhttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85031776095&doi=10.1016%2fj.ifacol.2017.08.090&partnerID=40&md5=8dfa35de87143f0594e830d4b729452espa
dc.sourceScopusspa
dc.titleStructural feedback linearization based on nonlinearities rejectionspa
dc.typeArticleeng
dc.rights.accessrightsinfo:eu-repo/semantics/restrictedAccess
dc.contributor.affiliationBlas, L.A., CINVESTAV-IPN, DCA, Mexicospa
dc.contributor.affiliationBonilla, M., CINVESTAV-IPN, DCA, UMI 3175, CINVESTAV-CNRS, Mexicospa
dc.contributor.affiliationMalabre, M., CNRS, LS2N (Laboratoire des Sciences du Numérique de Nantes), UMR 6004, Francespa
dc.contributor.affiliationAzhmyakov, V., Universidad de Medellin, Department of Basic Sciences, Medellin, Colombiaspa
dc.contributor.affiliationSalazar, S., CINVESTAV-IPN, SANAS, UMI 3175, CINVESTAV-CNRS, Mexicospa
dc.identifier.doi10.1016/j.ifacol.2017.08.090
dc.subject.keywordfailure reconstructioneng
dc.subject.keywordfeedback linearizationeng
dc.subject.keywordNonlinear systemseng
dc.publisher.facultyFacultad de Ciencias Básicasspa
dc.abstractIn this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying. © 2017eng
dc.creator.affiliationCINVESTAV-IPN, DCA, Mexicospa
dc.creator.affiliationCINVESTAV-IPN, DCA, UMI 3175, CINVESTAV-CNRS, Mexicospa
dc.creator.affiliationCNRS, LS2N (Laboratoire des Sciences du Numérique de Nantes), UMR 6004, Francespa
dc.creator.affiliationUniversidad de Medellin, Department of Basic Sciences, Medellin, Colombiaspa
dc.creator.affiliationCINVESTAV-IPN, SANAS, UMI 3175, CINVESTAV-CNRS, Mexicospa
dc.relation.ispartofesIFAC-PapersOnLinespa
dc.relation.ispartofesIFAC-PapersOnLine Volume 50, Issue 1, July 2017, Pages 922-927spa
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dc.relation.referencesPowers, C., Mellinger, D., & Kumar, V. (2014). Quadrotor kinematics and dynamics. Chapter 16 of Handbook of Unmanned Aerial Vehicles.spa
dc.relation.referencesSaberi, A., Stoorvogel, A. A., Sannuti, P., & Niemann, H. (2000). Fundamental problems in fault detection and identification. International Journal of Robust and Nonlinear Control, 10(14), 1209-1236. doi:10.1002/1099-1239(20001215)10:14<1209spa
dc.relation.referencesVidyasagar, M. (1993). Nonlinear Systems Analysis.spa
dc.type.versioninfo:eu-repo/semantics/publishedVersion
dc.type.driverinfo:eu-repo/semantics/article
dc.identifier.reponamereponame:Repositorio Institucional Universidad de Medellínspa
dc.identifier.instnameinstname:Universidad de Medellínspa


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