Control of Hybrid Unmanned Aerial Vehicle Motion in Transitional Modes
- Авторы: Belokon S.A.1, Derishev D.S.2, Zolotukhin Y.N.1, Nesterov A.A.1, Filippov M.N.1
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Учреждения:
- Institute of Automation and Electrometry, Siberian Branch
- Novosibirsk Research Institute of Aviation Technology and Production Engineering
- Выпуск: Том 55, № 4 (2019)
- Страницы: 346-355
- Раздел: Automation Systems in Scientific Research and Industry
- URL: https://journals.rcsi.science/8756-6990/article/view/212796
- DOI: https://doi.org/10.3103/S8756699019040046
- ID: 212796
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Аннотация
Results of investigations of the flight control system for a hybrid unmanned aerial vehicle prototype in transitional modes are presented. The hybrid vehicle is equipped with a quadrotor and main propulsion units. The control system developed in the study includes subsystems for attitude stabilization, vertical take-off, hovering, and landing, as well as a control subsystem operating in transitional modes from quadrotor to aircraft modes and back.
Об авторах
S. Belokon
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Россия, pr. Akademika Koptyuga 1, Novosibirsk, 630090
D. Derishev
Novosibirsk Research Institute of Aviation Technology and Production Engineering
Email: zol@idisys.iae.nsk.su
Россия, ul. Polzunova 15, Novosibirsk, 630051
Yu. Zolotukhin
Institute of Automation and Electrometry, Siberian Branch
Автор, ответственный за переписку.
Email: zol@idisys.iae.nsk.su
Россия, pr. Akademika Koptyuga 1, Novosibirsk, 630090
A. Nesterov
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Россия, pr. Akademika Koptyuga 1, Novosibirsk, 630090
M. Filippov
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Россия, pr. Akademika Koptyuga 1, Novosibirsk, 630090
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