Control of Hybrid Unmanned Aerial Vehicle Motion in Transitional Modes

被引：1
|
作者：
Belokon, S. A. [1 ]
Derishev, D. S. [2 ]
Zolotukhi, Yu N. [1 ]
Nesterov, A. A. [1 ]
Filippov, M. N. [1 ]
机构：
[1] Russian Acad Sci, Siberian Branch, Inst Automat & Electrometry, Pr Akademika Koptyuga 1, Novosibirsk 630090, Russia
[2] Novosibirsk Res Inst Aviat Technol & Prod Engn, Ul Polzunova 15, Novosibirsk 630051, Russia
来源：
OPTOELECTRONICS INSTRUMENTATION AND DATA PROCESSING | 2019年 / 55卷 / 04期
关键词：
hybrid unmanned aerial vehicle; control in transitional modes; dimensionless aerodynamic coefficients;
D O I：
10.3103/S8756699019040046
中图分类号：
O4 [物理学];
学科分类号：
0702 ;
摘要：
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.
引用
收藏
页码：346 / 355
页数：10
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