Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
- Авторы: Gainutdinova T.Y.1, Gainutdinov V.G.2, Levshonkov N.V.2, Gainutdinova A.V.2
-
Учреждения:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 4 (2018)
- Страницы: 605-612
- Раздел: 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
Цитировать
Аннотация
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.
Об авторах
T. Gainutdinova
Kazan (Volga region) Federal University
Автор, ответственный за переписку.
Email: tgainut@mail.ru
Россия, ul. Kremlevskaya 18, Kazan, 420008
V. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
N. Levshonkov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
A. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
Дополнительные файлы
