Automated identification system baseds on the changing of the temperature field of aircraft elements

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/38379

Full metadata record

DC Field	Value	Language
dc.contributor.author	Шевчук, Д.О.	uk_UA
dc.date.accessioned	2019-04-11T10:05:35Z	-
dc.date.available	2019-04-11T10:05:35Z	-
dc.date.issued	2013	-
dc.identifier.issn	1990-5548	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/38379	-
dc.description.abstract	In this article, system of identification collisions (structural damage) in the air, based on the change of the temperature field was given. Identification system provides information about type and size of aircraft damage to all systems during recovering the controllability of the aircraft when an unexpected problem occurs during a flight is proposed	en
dc.language.iso	en	en
dc.publisher	National Aviation University	en
dc.subject	identification system	en
dc.subject	aircraft	en
dc.subject	structural damage	en
dc.subject	reconfiguration	en
dc.subject	flight control system	en
dc.subject	loss of control in flight	en
dc.subject	stability and controllability	en
dc.title	Automated identification system baseds on the changing of the temperature field of aircraft elements	en
dc.type	Article	en
Appears in Collections:	Наукові статті кафедри автоматизації та енергоменеджменту

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