Reliability Evaluation of a Hexacopter-Based Flight Module of a Tethered Unmanned High-Altitude Platform

This article discusses a model on the basis of a multidimensional Markov process applied for evaluation of the reliability characteristics of a tethered multirotor high-altitude platform based on a hexacopter. The proposed model takes into account the increase in the functional load after the failure of an element on the remaining operating ones, and also takes into account the location of the failed elements. © 2019, Springer Nature Switzerland AG.

Авторы
Kozyrev D.V. 1, 2 , Phuong N.D.3 , Houankpo H.G.K. 2 , Sokolov A.1
Издательство
Springer Verlag
Язык
Английский
Страницы
646-656
Статус
Опубликовано
Том
1141 CCIS
Год
2019
Организации
  • 1 V. A. Trapeznikov Institute of Control Sciences of Russian Academy of Sciences, 65 Profsoyuznaya street, Moscow, 117997, Russian Federation
  • 2 Department of Applied Probability and Informatics, Peoples’ Friendship University of Russia (RUDN University), 6 Miklukho-Maklaya Street, Moscow, 117198, Russian Federation
  • 3 Moscow Institute of Physics and Technology (National Research University), 9 Institutskiy per., Moscow Region, Dolgoprudny, 141701, Russian Federation
Ключевые слова
Hexacopter; High-altitude platform; k-out-of-n system; Reliability; UAV
Дата создания
10.02.2020
Дата изменения
10.02.2020
Постоянная ссылка
https://repository.rudn.ru/ru/records/article/record/56414/
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