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.

Authors
Kozyrev D.V. 1, 2 , Phuong N.D.3 , Houankpo H.G.K. 2 , Sokolov A.1
Publisher
Springer Verlag
Language
English
Pages
646-656
Status
Published
Volume
1141 CCIS
Year
2019
Organizations
  • 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
Keywords
Hexacopter; High-altitude platform; k-out-of-n system; Reliability; UAV
Date of creation
10.02.2020
Date of change
10.02.2020
Short link
https://repository.rudn.ru/en/records/article/record/56414/
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