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Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements

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dc.contributor.author Gainutdinova T.Y.
dc.contributor.author Trusfus M.V.
dc.contributor.author Gainutdinov V.G.
dc.date.accessioned 2021-02-25T20:38:33Z
dc.date.available 2021-02-25T20:38:33Z
dc.date.issued 2020
dc.identifier.issn 1068-7998
dc.identifier.uri https://dspace.kpfu.ru/xmlui/handle/net/162132
dc.description.abstract © 2020, Allerton Press, Inc. The paper describes the computational and experimental investigation in selecting the design parameters of control surfaces and characteristics of the lift engines of a VTOL unmanned aerial vehicle. The general structural scheme of equations to roll, pitch and yaw control and stabilization is analyzed. Results of numerical simulation of the point-to-point autonomous flight are given.
dc.relation.ispartofseries Russian Aeronautics
dc.subject control design parameters
dc.subject flight simulation
dc.subject unmanned aerial vehicle (UAV)
dc.title Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements
dc.type Article
dc.relation.ispartofseries-issue 1
dc.relation.ispartofseries-volume 63
dc.collection Публикации сотрудников КФУ
dc.source.id SCOPUS10687998-2020-63-1-SID85085034769


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  • Публикации сотрудников КФУ Scopus [22633]
    Коллекция содержит публикации сотрудников Казанского федерального (до 2010 года Казанского государственного) университета, проиндексированные в БД Scopus, начиная с 1970г.

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