Numerical and Experimental Design Parameter Analysis of VTOL Airframe Control Elements

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

Files in this item

Size: 83.66Kb

Format: PDF

Публикации сотрудников КФУ Scopus [24551]
Коллекция содержит публикации сотрудников Казанского федерального (до 2010 года Казанского государственного) университета, проиндексированные в БД Scopus, начиная с 1970г.