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Design of Fail-Safe Quadrocopter Configuration. / Baranov, Oleg V.; Smirnov, Nikolay V.; Smirnova, Tatiana E.; Zholobov, Yefim V.

In: Studies in Computational Intelligence, Vol. 868, 01.2020, p. 13-22.

Research output: Contribution to journal › Article › peer-review

Harvard

Baranov, OV, Smirnov, NV, Smirnova, TE & Zholobov, YV 2020, 'Design of Fail-Safe Quadrocopter Configuration', Studies in Computational Intelligence, vol. 868, pp. 13-22. https://doi.org/10.1007/978-3-030-32258-8_2

APA

Baranov, O. V., Smirnov, N. V., Smirnova, T. E., & Zholobov, Y. V. (2020). Design of Fail-Safe Quadrocopter Configuration. Studies in Computational Intelligence, 868, 13-22. https://doi.org/10.1007/978-3-030-32258-8_2

Vancouver

Baranov OV, Smirnov NV, Smirnova TE, Zholobov YV. Design of Fail-Safe Quadrocopter Configuration. Studies in Computational Intelligence. 2020 Jan;868:13-22. https://doi.org/10.1007/978-3-030-32258-8_2

Author

Baranov, Oleg V. ; Smirnov, Nikolay V. ; Smirnova, Tatiana E. ; Zholobov, Yefim V. / Design of Fail-Safe Quadrocopter Configuration. In: Studies in Computational Intelligence. 2020 ; Vol. 868. pp. 13-22.

BibTeX

@article{e6940e12433747deb15ec0fbd93f7fdb,
title = "Design of Fail-Safe Quadrocopter Configuration",
abstract = "Unmanned aerial vehicles have become widespread in various fields of activity. In this article, we propose an approach to choosing performance characteristics of a quadrocopter, which provide a possibility to solve emergency landing problems. The key target characteristics for such a device are substantiated. The calculation methodology assumes the selection of commercially available components with the appropriate characteristics. For this purpose, the eCalc software was used. In the second part of the work, we propose a mathematical model describing the quadrocopter movement in emergency situations. This model allows us to create algorithms for solving control problems in various emergency situations. For implementation the possibilities of MATLAB package were used. Numerical experiment is carried out to prove the efficiency of this approach.",
keywords = "Control, Fail-safe landing, Quadrocopter, UAV",
author = "Baranov, {Oleg V.} and Smirnov, {Nikolay V.} and Smirnova, {Tatiana E.} and Zholobov, {Yefim V.}",
year = "2020",
month = jan,
doi = "10.1007/978-3-030-32258-8_2",
language = "English",
volume = "868",
pages = "13--22",
journal = "Studies in Computational Intelligence",
issn = "1860-949X",
publisher = "Springer Nature",

}

RIS

TY - JOUR

T1 - Design of Fail-Safe Quadrocopter Configuration

AU - Baranov, Oleg V.

AU - Smirnov, Nikolay V.

AU - Smirnova, Tatiana E.

AU - Zholobov, Yefim V.

PY - 2020/1

Y1 - 2020/1

N2 - Unmanned aerial vehicles have become widespread in various fields of activity. In this article, we propose an approach to choosing performance characteristics of a quadrocopter, which provide a possibility to solve emergency landing problems. The key target characteristics for such a device are substantiated. The calculation methodology assumes the selection of commercially available components with the appropriate characteristics. For this purpose, the eCalc software was used. In the second part of the work, we propose a mathematical model describing the quadrocopter movement in emergency situations. This model allows us to create algorithms for solving control problems in various emergency situations. For implementation the possibilities of MATLAB package were used. Numerical experiment is carried out to prove the efficiency of this approach.

AB - Unmanned aerial vehicles have become widespread in various fields of activity. In this article, we propose an approach to choosing performance characteristics of a quadrocopter, which provide a possibility to solve emergency landing problems. The key target characteristics for such a device are substantiated. The calculation methodology assumes the selection of commercially available components with the appropriate characteristics. For this purpose, the eCalc software was used. In the second part of the work, we propose a mathematical model describing the quadrocopter movement in emergency situations. This model allows us to create algorithms for solving control problems in various emergency situations. For implementation the possibilities of MATLAB package were used. Numerical experiment is carried out to prove the efficiency of this approach.

KW - Control

KW - Fail-safe landing

KW - Quadrocopter

KW - UAV

UR - http://www.scopus.com/inward/record.url?scp=85075549675&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/8aa34bd8-0992-337e-8641-02f431e60e47/

U2 - 10.1007/978-3-030-32258-8_2

DO - 10.1007/978-3-030-32258-8_2

M3 - Article

AN - SCOPUS:85075549675

VL - 868

SP - 13

EP - 22

JO - Studies in Computational Intelligence

JF - Studies in Computational Intelligence

SN - 1860-949X

ER -

ID: 76389990