Fault-tolerant Control Law for Unmanned Aerial Vehicle Array Based on Sliding Mode Control

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

Unmanned aerial vehicle array(UAV array) has become the focus of many researchers as a feasible solution to solve the problem of short endurance and weak load capacity. After investigating the research status and key problems of UAV array at home and abroad, this paper establishes the array dynamics model composed of a new configuration of the quadrotor flying array with the main and auxiliary rotor structure under the triangular prism frame. Based on this model, a sliding mode control method is designed to solve the fault-tolerant control problem of UAV array. In order to further verify the control performance of the proposed control algorithm, typical topology structures were selected as experimental representatives to complete the control simulation design and experiment of the system. The results show that this algorithm can achieve good control effect.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control and Decision Conference, CCDC 2022
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1769-1774
Number of pages6
ISBN (Electronic)9781665478960
DOIs
Publication statusPublished - 2022
Event34th Chinese Control and Decision Conference, CCDC 2022 - Hefei, China
Duration: 15 Aug 202217 Aug 2022

Publication series

NameProceedings of the 34th Chinese Control and Decision Conference, CCDC 2022

Conference

Conference34th Chinese Control and Decision Conference, CCDC 2022
Country/TerritoryChina
CityHefei
Period15/08/2217/08/22

Keywords

  • Sliding Mode Control and Fault-tolerant Control
  • UAV array

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