1. Репозиторий Самарского национального исследовательского университета имени академика С.П. Королёва
  2. 04. Материалы конференций
  3. Информационные технологии и нанотехнологии
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dc.contributor.authorGuerra Guerra D.J.ru
dc.contributor.authorHoang V. H.ru
dc.contributor.authorKurkina E. V.ru
dc.contributor.authorLukyanov О. Е.ru
dc.date.accessioned2026-01-23T11:29:00Z-
dc.date.available2026-01-23T11:29:00Z-
dc.date.issued2025-
dc.identifierRU\НТБ СГАУ\582263ru
dc.identifier.citationConstruction of a multilayer perceptron architecture for predicting the aerodynamic characteristics of aircraft with different aerodynamic configurations / О. Е. Lukyanov, V. H. Hoang, D.J. Guerra Guerra, E. V. Kurkina // Информационные технологии и нанотехнологии (ИТНТ-2025) : материалы XI междунар. конф. и молодеж. шк. (г. Самарканд, Узбекистан, 7-9 окт. 2025 г.) / М-во науки и высш. образования Рос. Федерации, Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т). - Самара : Изд-во Самар. ун-та, 2025. - С. 030642.ru
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dc.description.abstractThe proposed method has built a complete MLP model topredict the three main aerodynamic properties of the aircraftwith high accuracy (R2 up to 0.993, 0.997 and 0.995 for Cd,Cl, Cm respectively) as well as significantly reduced therequired computational time and cost when compared withnumerical mathematical models based on the vortex latticemethod and empirical equations.ru
dc.description.firstpage030642ru
dc.format.extentru
dc.format.mimetypeTextru
dc.language.isoengru
dc.publisherPublisherru
dc.rightsLicenseru
dc.sourceSourceru
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dc.subjectaerodynamic characteristicsru
dc.subjectaircraftru
dc.subjectarchitecture hyperparameterru
dc.subjectmultilayer perceptronru
dc.subject.rubbkru
dc.subject.rugasntiru
dc.subject.udcru
dc.titleConstruction of a multilayer perceptron architecture for predicting the aerodynamic characteristics of aircraft with different aerodynamic configurationsru
dc.title.alternativeru
dc.typeType Textru
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