Design and flight testing of the ducted-fan UAV flight array system

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dc.contributor.authorKim, Taegyun
dc.contributor.authorJeaong, Hoijo
dc.contributor.authorKim, Seongyoung
dc.contributor.authorKim, Inrae
dc.contributor.authorKim, Seungkeun
dc.contributor.authorSuk, Jinyoung
dc.contributor.authorShin, Hyosang
dc.date.accessioned2023-03-16T19:08:21Z
dc.date.available2023-03-16T19:08:21Z
dc.date.issued2023-02-24
dc.description.abstractThis study proposes a ducted-fan flight array (DFA) system that can change the array based on the mission environment and validate the feasibility through ground and flight tests. This DFA can carry out normal formation flight as separated UAV members and can also cooperate as a single entity by physical connection. The ducted-fan unmanned aerial vehicle (UAV) is manufactured in-house and equipped with a connected surface and an assembly device on the side to perform connection and separation tasks. Moreover, the control system was designed using an open-source autopilot environment, and the communication environment for multi-UAV flight was constructed using the Robot Operating System (ROS). Then, ground and preliminary experimental tests verified the feasibility and performance of the DFA system for connected and separated flight.en_UK
dc.identifier.citationKim T, Jeaong H, Kim S, et al., (2023) Design and flight testing of the ducted-fan UAV flight array system. Journal of Intelligent and Robotic Systems, Volume 107, February 2023, Article number 32en_UK
dc.identifier.issn0921-0296
dc.identifier.urihttps://doi.org/10.1007/s10846-023-01821-6
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/19325
dc.language.isoenen_UK
dc.publisherSpringeren_UK
dc.subjectducted-fan flight array systemen_UK
dc.subjectunmanned aerial vehicleen_UK
dc.subjectformation flighten_UK
dc.subjectflight testen_UK
dc.titleDesign and flight testing of the ducted-fan UAV flight array systemen_UK
dc.typeArticleen_UK

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