Drone fault tolerance strategy by allowing remaining rotor to pan and tilt

Quadcopter drones rely on their four rotors to control altitude and attitude. If one rotor fails, the drone loses its ability to maintain control. This paper proposes a solution to improve attitude control in such a scenario by minimising roll, pitch, and yaw deviations when a single rotor has stopp...

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Main Author: Zaludin, Zairil
Format: Article
Published: Inderscience Publishers 2024
Online Access:http://psasir.upm.edu.my/id/eprint/113718/
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author Zaludin, Zairil
author_facet Zaludin, Zairil
author_sort Zaludin, Zairil
building UPM Institutional Repository
collection Online Access
description Quadcopter drones rely on their four rotors to control altitude and attitude. If one rotor fails, the drone loses its ability to maintain control. This paper proposes a solution to improve attitude control in such a scenario by minimising roll, pitch, and yaw deviations when a single rotor has stopped. By enabling opposing motors to pan and tilt independently, the study demonstrates the feasibility of landing the drone safely. The concept explores the idea of thrust vectoring by the individual rotor, which better manages the drone’s roll, pitch, and yaw angles, along with their respective rates. The paper includes simulation results and a summary of the performance improvements achieved through this approach. Copyright © 2024 Inderscience Enterprises Ltd.
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format Article
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institution Universiti Putra Malaysia
institution_category Local University
last_indexed 2025-11-15T14:18:27Z
publishDate 2024
publisher Inderscience Publishers
recordtype eprints
repository_type Digital Repository
spelling upm-1137182025-01-20T01:02:05Z http://psasir.upm.edu.my/id/eprint/113718/ Drone fault tolerance strategy by allowing remaining rotor to pan and tilt Zaludin, Zairil Quadcopter drones rely on their four rotors to control altitude and attitude. If one rotor fails, the drone loses its ability to maintain control. This paper proposes a solution to improve attitude control in such a scenario by minimising roll, pitch, and yaw deviations when a single rotor has stopped. By enabling opposing motors to pan and tilt independently, the study demonstrates the feasibility of landing the drone safely. The concept explores the idea of thrust vectoring by the individual rotor, which better manages the drone’s roll, pitch, and yaw angles, along with their respective rates. The paper includes simulation results and a summary of the performance improvements achieved through this approach. Copyright © 2024 Inderscience Enterprises Ltd. Inderscience Publishers 2024 Article PeerReviewed Zaludin, Zairil (2024) Drone fault tolerance strategy by allowing remaining rotor to pan and tilt. International Journal of Advanced Mechatronic Systems, 11 (2). pp. 102-110. ISSN 1756-8412; eISSN: 1756-8420 https://www.inderscienceonline.com/doi/abs/10.1504/IJAMECHS.2024.139180 10.1504/IJAMECHS.2024.139180
spellingShingle Zaludin, Zairil
Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title_full Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title_fullStr Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title_full_unstemmed Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title_short Drone fault tolerance strategy by allowing remaining rotor to pan and tilt
title_sort drone fault tolerance strategy by allowing remaining rotor to pan and tilt
url http://psasir.upm.edu.my/id/eprint/113718/
http://psasir.upm.edu.my/id/eprint/113718/
http://psasir.upm.edu.my/id/eprint/113718/