电邮这篇文章 About the Efficient Scheme of Initial Attitude Estimation Using Low Accuracy Micro-Electro-Mechanical Sensors
- 作者: Gainutdinova T.Y.1, Gainutdinova A.V.2, Gainutdinov V.G.2
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隶属关系:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- 期: 卷 62, 编号 3 (2019)
- 页面: 387-393
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/231021
- DOI: https://doi.org/10.3103/S106879981903005X
- ID: 231021
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详细
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.
作者简介
T. Gainutdinova
Kazan (Volga region) Federal University
编辑信件的主要联系方式.
Email: tgainut@mail.ru
俄罗斯联邦, ul. Kremlevskaya 18, Kazan, 420008 Tatarstan
A. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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