File Download

  • Find it @ UNIST can give you direct access to the published full text of this article. (UNISTARs only)
Related Researcher

손흥선

Son, Hungsun
Electromechanical System and control Lab.
Read More

Views & Downloads

Detailed Information

Cited time in webofscience Cited time in scopus
Metadata Downloads

Full metadata record

DC Field Value Language
dc.citation.endPage 41020 -
dc.citation.number 24 -
dc.citation.startPage 41010 -
dc.citation.title IEEE Sensors Journal -
dc.citation.volume 24 -
dc.contributor.author Shin, Minho -
dc.contributor.author Cho, Yonghyun -
dc.contributor.author Son, Hungsun -
dc.date.accessioned 2026-02-19T09:18:42Z -
dc.date.available 2026-02-19T09:18:42Z -
dc.date.created 2026-02-13 -
dc.date.issued 2024-12 -
dc.description.abstract This article presents a fault-tolerant estimator using a probabilistic voting algorithm (PVA) for the safe maneuvering of multirotor unmanned aerial vehicles (UAVs). UAVs are widely utilized in numerous applications, but any malfunction can lead to secondary accidents. The safety and robustness of the UAV component should be guaranteed to minimize fatal accidents during flight. A flight control computer (FCC) with various sensors is one of the most important components, the robustness of which should be guaranteed. In this article, a hybrid FCC including both hardware and software is developed to improve the robustness and safety of the FCC by both hardware and analytical redundancy. Triple modular FCCs for hardware redundancy are utilized to deal with various faults. The PVA is designed to estimate the reference state of the UAV and make the consensus to select the fault-free FCC by the fault probabilities of each state measurement from the FCC estimators. Moreover, multiplexers (MUXs) switch the FCC channel based on the consensus result to compensate for faults. Then, the fault identification algorithm identifies the source of the estimator faults by information on the residual signals between the estimated states and the sensor measurements. The PVA is validated through numerical simulations and experiments. This method achieves approximately a 93% correct detection rate and a fault detection time of less than 1 s, which is sufficient to maintain the dynamic responses of the UAV. These results show that the PVA improves and ensures the safe maneuvering of the UAV in various fault situations. © 2001-2012 IEEE. -
dc.identifier.bibliographicCitation IEEE Sensors Journal, v.24, no.24, pp.41010 - 41020 -
dc.identifier.doi 10.1109/JSEN.2024.3483220 -
dc.identifier.issn 1530-437X -
dc.identifier.scopusid 2-s2.0-85208096699 -
dc.identifier.uri https://scholarworks.unist.ac.kr/handle/201301/90496 -
dc.identifier.url https://ieeexplore.ieee.org/document/10735101 -
dc.identifier.wosid 001380730100013 -
dc.language 영어 -
dc.publisher Institute of Electrical and Electronics Engineers Inc. -
dc.title Robust Estimation and Sensor Fault Management Using Probabilistic Voting Algorithm in UAVs -
dc.type Article -
dc.description.isOpenAccess TRUE -
dc.type.docType Article -
dc.description.journalRegisteredClass scie -
dc.description.journalRegisteredClass scopus -
dc.subject.keywordAuthor probabilistic voting algorithm (PVA) -
dc.subject.keywordAuthor sensor fault-tolerant system -
dc.subject.keywordAuthor triple modular redundancy (TMR) -
dc.subject.keywordAuthor unmanned aerial vehicle (UAV) -
dc.subject.keywordAuthor Data fusion -
dc.subject.keywordAuthor flight control computer (FCC) -

qrcode

Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.