Email this article Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
- Authors: Gainutdinova T.Y.1, Gainutdinov V.G.2, Levshonkov N.V.2, Gainutdinova A.V.2
-
Affiliations:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 4 (2018)
- Pages: 605-612
- Section: 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
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
T. Yu. Gainutdinova
Kazan (Volga region) Federal University
Author for correspondence.
Email: tgainut@mail.ru
Russian Federation, ul. Kremlevskaya 18, Kazan, 420008
V. G. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
N. V. Levshonkov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
A. V. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
Supplementary files
