Estimation of Vertical Take-off Unmanned Aircraft Flight Characteristics and Algorithm of Required Roll Angle Calculating for Trajectory Tracking

dc.contributor.author	Gainutdinova T.Y.
dc.contributor.author	Gainutdinova A.V.
dc.contributor.author	Trusfus M.V.
dc.contributor.author	Gainutdinov V.G.
dc.contributor.author	Zamaleev T.A.
dc.date.accessioned	2022-02-09T20:36:01Z
dc.date.available	2022-02-09T20:36:01Z
dc.date.issued	2021
dc.identifier.issn	1068-7998
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/169306
dc.description.abstract	Abstract: The paper proposes an algorithm for estimating the available and required power for the VTOL unmanned aircraft based on speed data obtained during acceleration of a plane in horizontal flight with the engine operating at maximum output power. We consider the scheme of refinement of navigation calculations for controlling the throttle of the fuel supply and elevator and lateral control of an unmanned aircraft during flight along a given route. The results of numerical simulation are presented.
dc.relation.ispartofseries	Russian Aeronautics
dc.subject	control algorithms
dc.subject	flight characteristics
dc.subject	numerical simulation
dc.subject	vertical take-off unmanned aerial vehicle
dc.title	Estimation of Vertical Take-off Unmanned Aircraft Flight Characteristics and Algorithm of Required Roll Angle Calculating for Trajectory Tracking
dc.type	Article
dc.relation.ispartofseries-issue	3
dc.relation.ispartofseries-volume	64
dc.collection	Публикации сотрудников КФУ
dc.relation.startpage	416
dc.source.id	SCOPUS10687998-2021-64-3-SID85121536342

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