Выдержка

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.

Язык оригиналаанглийский
Название основной публикацииIntelligent Distributed Computing XIII, IDC 2019
РедакторыIgor Kotenko, Vasily Desnitsky, Costin Badica, Didier El Baz, Mirjana Ivanovic
ИздательSpringer
Страницы13-22
ISBN (печатное издание)9783030322571
DOI
СостояниеОпубликовано - янв 2020
Событие13th International Symposium on Intelligent Distributed Computing, IDC 2019 - St. Petersburg, Российская Федерация
Продолжительность: 7 окт 20199 окт 2019

Серия публикаций

НазваниеStudies in Computational Intelligence
Том868
ISSN (печатное издание)1860-949X
ISSN (электронное издание)1860-9503

Конференция

Конференция13th International Symposium on Intelligent Distributed Computing, IDC 2019
СтранаРоссийская Федерация
ГородSt. Petersburg
Период7/10/199/10/19

Отпечаток

Unmanned aerial vehicles (UAV)
Landing
MATLAB
Mathematical models
Experiments

Предметные области Scopus

  • Искусственный интеллект

Цитировать

Baranov, O. V., Smirnov, N. V., Smirnova, T. E., & Zholobov, Y. V. (2020). Design of Fail-Safe Quadrocopter Configuration. В I. Kotenko, V. Desnitsky, C. Badica, D. El Baz, & M. Ivanovic (Ред.), Intelligent Distributed Computing XIII, IDC 2019 (стр. 13-22). (Studies in Computational Intelligence; Том 868). Springer. https://doi.org/10.1007/978-3-030-32258-8_2
Baranov, Oleg V. ; Smirnov, Nikolay V. ; Smirnova, Tatiana E. ; Zholobov, Yefim V. / Design of Fail-Safe Quadrocopter Configuration. Intelligent Distributed Computing XIII, IDC 2019. редактор / Igor Kotenko ; Vasily Desnitsky ; Costin Badica ; Didier El Baz ; Mirjana Ivanovic. Springer, 2020. стр. 13-22 (Studies in Computational Intelligence).
@inproceedings{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 = "1",
doi = "10.1007/978-3-030-32258-8_2",
language = "English",
isbn = "9783030322571",
series = "Studies in Computational Intelligence",
publisher = "Springer",
pages = "13--22",
editor = "Igor Kotenko and Vasily Desnitsky and Costin Badica and {El Baz}, Didier and Mirjana Ivanovic",
booktitle = "Intelligent Distributed Computing XIII, IDC 2019",
address = "Germany",

}

Baranov, OV, Smirnov, NV, Smirnova, TE & Zholobov, YV 2020, Design of Fail-Safe Quadrocopter Configuration. в I Kotenko, V Desnitsky, C Badica, D El Baz & M Ivanovic (ред.), Intelligent Distributed Computing XIII, IDC 2019. Studies in Computational Intelligence, том. 868, Springer, стр. 13-22, St. Petersburg, Российская Федерация, 7/10/19. https://doi.org/10.1007/978-3-030-32258-8_2

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

Intelligent Distributed Computing XIII, IDC 2019. ред. / Igor Kotenko; Vasily Desnitsky; Costin Badica; Didier El Baz; Mirjana Ivanovic. Springer, 2020. стр. 13-22 (Studies in Computational Intelligence; Том 868).

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференции

TY - GEN

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

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

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

M3 - Conference contribution

AN - SCOPUS:85075549675

SN - 9783030322571

T3 - Studies in Computational Intelligence

SP - 13

EP - 22

BT - Intelligent Distributed Computing XIII, IDC 2019

A2 - Kotenko, Igor

A2 - Desnitsky, Vasily

A2 - Badica, Costin

A2 - El Baz, Didier

A2 - Ivanovic, Mirjana

PB - Springer

ER -

Baranov OV, Smirnov NV, Smirnova TE, Zholobov YV. Design of Fail-Safe Quadrocopter Configuration. В Kotenko I, Desnitsky V, Badica C, El Baz D, Ivanovic M, редакторы, Intelligent Distributed Computing XIII, IDC 2019. Springer. 2020. стр. 13-22. (Studies in Computational Intelligence). https://doi.org/10.1007/978-3-030-32258-8_2