Method of State Estimation and Identification of the Arial Vehicle under Destabilizing Action of Weather Conditions

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/29400

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DC Field	Value	Language
dc.contributor.author	Tymoshenko, N	-
dc.contributor.author	Shevchuk, D	-
dc.contributor.author	Prochorenko, I	-
dc.date.accessioned	2017-06-15T15:22:22Z	-
dc.date.available	2017-06-15T15:22:22Z	-
dc.date.issued	2016	-
dc.identifier.isbn	978-1-5090-1052-3	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/29400	-
dc.description.abstract	Here we explain method and models for hover mode of aerial vehicle (helicopter) as well as measurements of parameters of this flight mode that requires smaller volume of calculation and preserves high speed and accuracy of stabilization. Also we investigate reduction of number of state vectors and volume of calculation via usage of extended Kalman filter and standard sensors.	uk_UA
dc.language.iso	en	uk_UA
dc.publisher	IEEE 4th International Conference «Methods and Systems of Navigation and Motion Control» Conference Proceedings, 18-20 October 2016, Kyiv, Ukraine. – Р. 241-244.	uk_UA
dc.relation.ispartofseries	IEEE Catalolog Number;CFP1652Y-PRT	-
dc.subject	control, control system, helicopter, filter, perturbation, stabilization	uk_UA
dc.title	Method of State Estimation and Identification of the Arial Vehicle under Destabilizing Action of Weather Conditions	uk_UA
dc.type	Other	uk_UA
Appears in Collections:	Публікації Scopus кафедри автоматизації та енергоменеджменту

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