Measuring Model of Helicopter’s Hovering Stabilization Parameters Against Point Objects

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/29398

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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	2017-06-15T15:07:53Z	-
dc.date.available	2017-06-15T15:07:53Z	-
dc.date.issued	2016	-
dc.identifier.issn	1990-5548	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/29398	-
dc.description.abstract	Here we explain measuring model of helicopter's hovering stabilization parameters against point object 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	Electronics and control systems. – 2016. – №3(49). – С.121-125.	uk_UA
dc.relation.ispartofseries	;№3(49)	-
dc.subject	control, control system, helicopter, filter, perturbation, stabilization	uk_UA
dc.title	Measuring Model of Helicopter’s Hovering Stabilization Parameters Against Point Objects	uk_UA
dc.type	Article	uk_UA
Appears in Collections:	Наукові статті кафедри автоматизації та енергоменеджменту

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