Seven tuning schemes for an ADALINE model to predict floor pressures in a subsonic cavity flow

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buir.contributor.authorÖzbay, Hitay
dc.citation.epage112en_US
dc.citation.issueNumber1en_US
dc.citation.spage97en_US
dc.citation.volumeNumber31en_US
dc.contributor.authorEfe, M. Ö.en_US
dc.contributor.authorDebiasi, M.en_US
dc.contributor.authorYan, P.en_US
dc.contributor.authorÖzbay, Hitayen_US
dc.contributor.authorSamimy, M.en_US
dc.date.accessioned2016-02-08T10:05:30Z
dc.date.available2016-02-08T10:05:30Z
dc.date.issued2009en_US
dc.departmentDepartment of Electrical and Electronics Engineeringen_US
dc.description.abstractThis paper presents a simple yet effective one-step-ahead predictor based on an adaptive linear element (ADALINE). Several tuning schemes are studied to see whether the obtained model is consistent. The process under investigation is a subsonic cavity flow system. The experimental data obtained from the system is post-processed to obtain a useful predictor. The contribution of the paper is to demonstrate that despite the spectral richness of the observed data, a simple model with various tuning schemes can help to a satisfactory extent. Seven algorithms are studied, including the least mean squares (LMS), recursive least squares (RLS), modified Kaczmarz's algorithm (MK), stochastic approximation algorithm (SA), gradient descent (GD), Levenbergĝ€ "Marquardt optimization technique (LM) and sliding mode-based tuning (SM). The model and its properties are discussed comparatively.en_US
dc.identifier.doi10.1177/0142331208090964en_US
dc.identifier.eissn1477-0369
dc.identifier.issn0142-3312
dc.identifier.urihttp://hdl.handle.net/11693/22846
dc.language.isoEnglishen_US
dc.publisherSage Publications Ltd.en_US
dc.relation.isversionofhttps://doi.org/10.1177/0142331208090964en_US
dc.source.titleTransactions of the Institute of Measurement and Controlen_US
dc.subjectADALINEen_US
dc.subjectPredictionen_US
dc.subjectSubsonic cavity flowsen_US
dc.titleSeven tuning schemes for an ADALINE model to predict floor pressures in a subsonic cavity flowen_US
dc.typeArticleen_US

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