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dc.contributor.author | Gainutdinova T. | |
dc.contributor.author | Gainutdinova A. | |
dc.contributor.author | Gainutdinov V. | |
dc.date.accessioned | 2020-01-15T21:45:58Z | |
dc.date.available | 2020-01-15T21:45:58Z | |
dc.date.issued | 2019 | |
dc.identifier.issn | 1068-7998 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/155747 | |
dc.description.abstract | © 2019, Allerton Press, Inc. A solution of initial attitude estimation is considered for the UAV with an inertial navigation system including a standard set of three-degree micro-electro-mechanical gyroscopic angular velocity sensors, accelerometers, and magnetometers. | |
dc.relation.ispartofseries | Russian Aeronautics | |
dc.subject | initial attitude estimation | |
dc.subject | three-degree micro-electro-mechanical sensors | |
dc.title | About the Efficient Scheme of Initial Attitude Estimation Using Low Accuracy Micro-Electro-Mechanical Sensors | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 3 | |
dc.relation.ispartofseries-volume | 62 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 387 | |
dc.source.id | SCOPUS10687998-2019-62-3-SID85076515279 |