Email this article Control of Hybrid Unmanned Aerial Vehicle Motion in Transitional Modes
- Authors: Belokon S.A.1, Derishev D.S.2, Zolotukhin Y.N.1, Nesterov A.A.1, Filippov M.N.1
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Affiliations:
- Institute of Automation and Electrometry, Siberian Branch
- Novosibirsk Research Institute of Aviation Technology and Production Engineering
- Issue: Vol 55, No 4 (2019)
- Pages: 346-355
- Section: 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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Abstract
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.
About the authors
S. A. Belokon
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Russian Federation, pr. Akademika Koptyuga 1, Novosibirsk, 630090
D. S. Derishev
Novosibirsk Research Institute of Aviation Technology and Production Engineering
Email: zol@idisys.iae.nsk.su
Russian Federation, ul. Polzunova 15, Novosibirsk, 630051
Yu. N. Zolotukhin
Institute of Automation and Electrometry, Siberian Branch
Author for correspondence.
Email: zol@idisys.iae.nsk.su
Russian Federation, pr. Akademika Koptyuga 1, Novosibirsk, 630090
A. A. Nesterov
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Russian Federation, pr. Akademika Koptyuga 1, Novosibirsk, 630090
M. N. Filippov
Institute of Automation and Electrometry, Siberian Branch
Email: zol@idisys.iae.nsk.su
Russian Federation, pr. Akademika Koptyuga 1, Novosibirsk, 630090
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