OPTIMAL OBSERVER-BASED CONTROL DESIGN   FOR AIRCRAFT LATERAL MOTION

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/29961

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DC Field	Value	Language
dc.contributor.author	Komnatska M.M.	-
dc.date.accessioned	2017-07-04T09:03:32Z	-
dc.date.available	2017-07-04T09:03:32Z	-
dc.date.issued	2015-10-08	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/29961	-
dc.description.abstract	The paper presents an alternative approach of observer-based flight control system design. This approach 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	Національний авіаційний університет	uk_UA
dc.relation.ispartofseries	Проблеми інформатизації та управління;3(51)’2015	-
dc.subject	aircraft lateral motion	uk_UA
dc.title	OPTIMAL OBSERVER-BASED CONTROL DESIGN FOR AIRCRAFT LATERAL MOTION	uk_UA
dc.type	Article	uk_UA
dc.subject.udc	629.735.051'622 (045)	-
Appears in Collections:	Наукові статті кафедри аерокосмічних систем управління

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