Please use this identifier to cite or link to this item: https://doi.org/10.1109/TCST.2007.912242
DC FieldValue
dc.titleAdaptive neural network control for helicopters in vertical flight
dc.contributor.authorTee, K.P.
dc.contributor.authorGe, S.S.
dc.contributor.authorTay, F.E.H.
dc.date.accessioned2014-06-17T02:36:58Z
dc.date.available2014-06-17T02:36:58Z
dc.date.issued2008-07
dc.identifier.citationTee, K.P., Ge, S.S., Tay, F.E.H. (2008-07). Adaptive neural network control for helicopters in vertical flight. IEEE Transactions on Control Systems Technology 16 (4) : 753-762. ScholarBank@NUS Repository. https://doi.org/10.1109/TCST.2007.912242
dc.identifier.issn10636536
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/54915
dc.description.abstractIn this brief, robust adaptive neural network (NN) control is presented for helicopters in vertical flight, with dynamics in single-input-single-output (SISO) nonlinear nonaffine form. Based on the use of the implicit function theorem and the mean value theorem, we propose a constructive approach for adaptive NN control design with guaranteed stability. Considering both full-state and output feedback cases, it is shown that the output tracking error converges to a small neighborhood of the origin, while the remaining closed-loop signals remain bounded. The simulation study demonstrates the effectiveness of the proposed control. © 2008 IEEE.
dc.description.urihttp://libproxy1.nus.edu.sg/login?url=http://dx.doi.org/10.1109/TCST.2007.912242
dc.sourceScopus
dc.subjectAdaptive control
dc.subjectHelicopters
dc.subjectNeural networks (NNs)
dc.subjectOutput feedback
dc.subjectUncertain systems
dc.typeArticle
dc.contributor.departmentELECTRICAL & COMPUTER ENGINEERING
dc.contributor.departmentMECHANICAL ENGINEERING
dc.description.doi10.1109/TCST.2007.912242
dc.description.sourcetitleIEEE Transactions on Control Systems Technology
dc.description.volume16
dc.description.issue4
dc.description.page753-762
dc.description.codenIETTE
dc.identifier.isiut000257138900016
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