Мақаланы E-mail арқылы жіберу Numerical and Experimental Analysis in Adjustment of the VTOL UAV Control Hardware
- Авторлар: Gainutdinova T.Y.1, Gainutdinov V.G.2, Levshonkov N.V.2, Gainutdinova A.V.2
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Мекемелер:
- Kazan (Volga region) Federal University
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 61, № 4 (2018)
- Беттер: 605-612
- Бөлім: 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
Дәйексөз келтіру
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Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
T. Gainutdinova
Kazan (Volga region) Federal University
Хат алмасуға жауапты Автор.
Email: tgainut@mail.ru
Ресей, ul. Kremlevskaya 18, Kazan, 420008
V. Gainutdinov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
N. Levshonkov
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
A. Gainutdinova
Tupolev Kazan National Research Technical University
Email: tgainut@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
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