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 |
|