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Lookup NU author(s): Dr Leo ChenORCiD
This work is licensed under a Creative Commons Attribution 4.0 International License (CC BY 4.0).
The stability of flying of a hummingbird-like flapping-wing micro air vehicle (MAV) has been challenging. In this paper, experimental studies are reported on the tail shapes of hummingbird-like flapping-wing MAVs, since tails play an important role in-flight stability. Dynamics parameters of hummingbird tails are firstly studied and evaluated. Then man-made tails inspired by the natural hummingbirds are designed, manufactured and optimized for experimental tests. The results show that lift generated by the tail is independent of a fan angle, whereas the pitch moment is related to the fan angle. Further, the~tail can be applied to stabilising hovering twin-wing flapping wing MAVs.
Author(s): Nan Y-H, Chen Y, McGlinchey D, Li Y
Publication type: Article
Publication status: Published
Journal: IEEE Access
Year: 2020
Volume: 8
Pages: 52622-52630
Online publication date: 16/03/2020
Acceptance date: 01/03/2020
Date deposited: 17/03/2020
ISSN (electronic): 2169-3536
Publisher: IEEE
URL: https://doi.org/10.1109/ACCESS.2020.2981190
DOI: 10.1109/ACCESS.2020.2981190
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