Fault-Tolerant Actuation Architectures for Unmanned Aerial Vehicles

M. A.A. Ismail*, C. Bosch, S. Wiedemann, A. Bierig

*Corresponding author for this work

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

10 Scopus citations

Abstract

Rising civilian applications that make use of unmanned aerial vehicles (UAVs) demand crucial precautions to minimize safety hazards. Future UAVs are expected to incorporate fault-tolerant architectures for critical on-board systems to ensure compliance with airworthiness certification. Reliability reports of in-service UAVs showed that flight control actuators are among the highest root-causes of UAVs mishaps. In this paper, the current state-of-the-art actuation architectures for UAVs are reviewed to identify technical requirements for certification. This work is part of a TEMA-UAV research project aimed at developing certifiable fault-Tolerant Electro-Mechanical Actuators for future UAVs.

Original languageEnglish
Title of host publicationWCCM 2019
EditorsLen Gelman, Nadine Martin, Andrew A. Malcolm, Chin Kian (Edmund) Liew
PublisherSpringer Science and Business Media Deutschland GmbH
Pages345-354
Number of pages10
ISBN (Print)9789811591983
DOIs
StatePublished - 2021
Externally publishedYes
Event2nd World Congress on Condition Monitoring, WCCM 2019 - Singapore, Singapore
Duration: 2 Dec 20195 Dec 2019

Publication series

NameLecture Notes in Mechanical Engineering
ISSN (Print)2195-4356
ISSN (Electronic)2195-4364

Conference

Conference2nd World Congress on Condition Monitoring, WCCM 2019
Country/TerritorySingapore
CitySingapore
Period2/12/195/12/19

Bibliographical note

Publisher Copyright:
© 2021, Springer Nature Singapore Pte Ltd.

Keywords

  • Airworthiness certification for UAVs
  • Electro-mechanical actuators
  • Fault-tolerant control

ASJC Scopus subject areas

  • Automotive Engineering
  • Aerospace Engineering
  • Mechanical Engineering
  • Fluid Flow and Transfer Processes

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