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Conference Paper: HALO: A Safe, Coaxial, and Dual-Ducted UAV Without Servo

TitleHALO: A Safe, Coaxial, and Dual-Ducted UAV Without Servo
Authors
Issue Date2023
Citation
IEEE International Conference on Intelligent Robots and Systems, 2023, p. 6935-6941 How to Cite?
AbstractThis paper presents a novel uncrewed aerial vehicle (UAV) design named HALO, which stands for 'harmless aerial limber robot'. HALO uses a swashplateless mechanism to generate a moment for pitch and roll control without requiring additional actuators such as servo, reducing the number of components needed for control and enhancing reliability. Its reduced weight and number of actuators improve payload capacity and maneuverability. Meanwhile, HALO's coaxial duct design improves safety and aerodynamic efficiency. Experimental tests, including figure-of-eight trajectory tracking, wind gust and stick poking disturbances, hover efficiency comparison, and actual flight with collision is conducted to confirm HALO's robustness and exceptional safety characteristics, suggesting it as a promising design for various applications.
Persistent Identifierhttp://hdl.handle.net/10722/368104
ISSN
2023 SCImago Journal Rankings: 1.094

 

DC FieldValueLanguage
dc.contributor.authorLi, Haotian-
dc.contributor.authorChen, Nan-
dc.contributor.authorKong, Fanze-
dc.contributor.authorZou, Yuying-
dc.contributor.authorZhou, Shenji-
dc.contributor.authorHe, Dongjiao-
dc.contributor.authorZhang, Fu-
dc.date.accessioned2025-12-19T08:01:49Z-
dc.date.available2025-12-19T08:01:49Z-
dc.date.issued2023-
dc.identifier.citationIEEE International Conference on Intelligent Robots and Systems, 2023, p. 6935-6941-
dc.identifier.issn2153-0858-
dc.identifier.urihttp://hdl.handle.net/10722/368104-
dc.description.abstractThis paper presents a novel uncrewed aerial vehicle (UAV) design named HALO, which stands for 'harmless aerial limber robot'. HALO uses a swashplateless mechanism to generate a moment for pitch and roll control without requiring additional actuators such as servo, reducing the number of components needed for control and enhancing reliability. Its reduced weight and number of actuators improve payload capacity and maneuverability. Meanwhile, HALO's coaxial duct design improves safety and aerodynamic efficiency. Experimental tests, including figure-of-eight trajectory tracking, wind gust and stick poking disturbances, hover efficiency comparison, and actual flight with collision is conducted to confirm HALO's robustness and exceptional safety characteristics, suggesting it as a promising design for various applications.-
dc.languageeng-
dc.relation.ispartofIEEE International Conference on Intelligent Robots and Systems-
dc.titleHALO: A Safe, Coaxial, and Dual-Ducted UAV Without Servo-
dc.typeConference_Paper-
dc.description.naturelink_to_subscribed_fulltext-
dc.identifier.doi10.1109/IROS55552.2023.10341923-
dc.identifier.scopuseid_2-s2.0-85182524432-
dc.identifier.spage6935-
dc.identifier.epage6941-
dc.identifier.eissn2153-0866-

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