Method of State Estimation and Identification of the Arial Vehicle under Destabilizing Action of Weather Conditions
| 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.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.identifier.isbn | 978-1-5090-1052-3 | |
| dc.identifier.uri | http://er.nau.edu.ua/handle/NAU/29400 | |
| 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 |
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