电邮这篇文章 Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
- 作者: Gainutdinova T.Y.1, Gainutdinov V.G.2, Levshonkov N.V.2, Gainutdinova A.V.2
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隶属关系:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 4 (2018)
- 页面: 605-612
- 栏目: Aircraft Instruments and Instrumentation Computer Complexes
- URL: https://journals.rcsi.science/1068-7998/article/view/230728
- DOI: https://doi.org/10.3103/S1068799818040153
- ID: 230728
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详细
Problems associated with determining the angular attitude of the unmanned aerial vehicle (UAV) with an inertial navigation system are considered. Some ways of its practical implementation using special test benches are proposed.
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
V. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
N. Levshonkov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
A. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
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