A Fault-Tolerant Control System for Hexacopters with a Changeable Structure in Rotor Arrangement Angle

Keigo Watanabe, Taisei Endo, Xiongshi Xu, Shilin Yi, Isaku Nagai

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this study, an airframe structure is proposed to be able to effectively utilize all remaining normal rotors even in the case of a single rotor failure by making the rotor arrangement angle of a hexacopter variable. Furthermore, position and attitude control is achieved by setting the control allocation problem under failure as a nonlinear optimization problem, while satisfying the rotor constraints such as a maximum thrust, etc. The effectiveness of the present method is demonstrated by using comparative numerical simulations with a normal hexacopter or a special structure possessing a tiltable rotor mechanism.

Original languageEnglish
Title of host publication2022 IEEE International Conference on Mechatronics and Automation, ICMA 2022
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1719-1726
Number of pages8
ISBN (Electronic)9781665408523
DOIs
Publication statusPublished - 2022
Event19th IEEE International Conference on Mechatronics and Automation, ICMA 2022 - Guilin, Guangxi, China
Duration: Aug 7 2022Aug 10 2022

Publication series

Name2022 IEEE International Conference on Mechatronics and Automation, ICMA 2022

Conference

Conference19th IEEE International Conference on Mechatronics and Automation, ICMA 2022
Country/TerritoryChina
CityGuilin, Guangxi
Period8/7/228/10/22

Keywords

  • Fault-tolerant control
  • Hexacopter
  • Variable rotor-arrangement angle

ASJC Scopus subject areas

  • Artificial Intelligence
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Control and Optimization

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