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

页码：346 / 355

页数：10

共 7 条

[1] Control of Hybrid Unmanned Aerial Vehicle Motion in Transitional Modes
S. A. Belokon
D. S. Derishev
Yu. N. Zolotukhin
A. A. Nesterov
M. N. Filippov
[J]. Optoelectronics, Instrumentation and Data Processing, 2019, 55 : 346 - 355
[2] Simulation of Hybrid Unmanned Aerial Vehicle Motion
S. A. Belokon
D. S. Derishev
Yu. N. Zolotukhin
A. P. Yan
[J]. Optoelectronics, Instrumentation and Data Processing, 2019, 55 : 356 - 363
[3] Simulation of Hybrid Unmanned Aerial Vehicle Motion
Belokon, S. A.
Derishev, D. S.
Zolotukhin, Yu N.
Yan, A. P.
[J]. OPTOELECTRONICS INSTRUMENTATION AND DATA PROCESSING, 2019, 55 (04) : 356 - 363
[4] Autonomous performance maximization of research-based hybrid unmanned aerial vehicle
Coban, Sezer
[J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2020, 92 (04) : 645 - 651
[5] Configuration design and topology optimization of a single wing for the hybrid unmanned aerial vehicle
Zhang Q.
Jia S.
Chen J.
Xu Y.
She Z.
Cai C.
Pan Y.
[J]. Qinghua Daxue Xuebao/Journal of Tsinghua University, 2023, 63 (03): : 423 - 432
[6] Indirect engine sizing via distributed hybrid-electric unmanned aerial vehicle state-of-charge-based parametrisation criteria
Wang, S.
Economou, J. T.
Tsourdos, A.
[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (14) : 5360 - 5368
[7] A new tilt-arm transitioning unmanned aerial vehicle: Introduction and conceptual design
Zeng, Chen
Abnous, Rosa
Gabani, Krushang
Chowdhury, Souma
Maldonado, Victor
[J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 99

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