ON ONE APPROACH OF OBSERVER-BASED FLIGHT CONTROL SYSTEM DESIGN

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/28613

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DC Field	Value	Language
dc.contributor.author	Komnatska, M. M.	-
dc.contributor.author	Klipa, A. M.	-
dc.contributor.author	Berezanskyi, Y. A.	-
dc.contributor.author	Kiliian, I. V.	-
dc.date.accessioned	2017-05-30T07:25:33Z	-
dc.date.available	2017-05-30T07:25:33Z	-
dc.date.issued	2015	-
dc.identifier.issn	1990-5548	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/28613	-
dc.description.abstract	This paper presents a novel approach of observer design for aircraft motion control. The novelty of design procedure is based on the application of linear matrix inequality technique. The design procedure treats the design of both observer and controller by solving the set of linear inequalities simultaneously. The proposed approach is free of observer poles placement location. Simulation results demonstrate the validity and effectiveness of the proposed design approach	uk_UA
dc.language.iso	en	uk_UA
dc.publisher	Kyiv, "Osvita Ukrainy"	uk_UA
dc.subject	Flight control system; linear matrix inequalities; observer design; state feedback; separa- tion principle; state estimation	uk_UA
dc.title	ON ONE APPROACH OF OBSERVER-BASED FLIGHT CONTROL SYSTEM DESIGN	uk_UA
dc.title.alternative	Про один підхід до синтезу системи управління польотом зі спостерігачем	uk_UA
dc.type	Article	uk_UA
dc.subject.udc	UDC 629.735.051'622 (045)	-
Appears in Collections:	Наукові статті кафедри аерокосмічних систем управління

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