Control of Hybrid Unmanned Aerial Vehicle Motion in Transitional Modes


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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.

作者简介

S. Belokon

Institute of Automation and Electrometry, Siberian Branch

Email: zol@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090

D. Derishev

Novosibirsk Research Institute of Aviation Technology and Production Engineering

Email: zol@idisys.iae.nsk.su
俄罗斯联邦, ul. Polzunova 15, Novosibirsk, 630051

Yu. Zolotukhin

Institute of Automation and Electrometry, Siberian Branch

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Email: zol@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090

A. Nesterov

Institute of Automation and Electrometry, Siberian Branch

Email: zol@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090

M. Filippov

Institute of Automation and Electrometry, Siberian Branch

Email: zol@idisys.iae.nsk.su
俄罗斯联邦, pr. Akademika Koptyuga 1, Novosibirsk, 630090

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