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Issue:ISSN 2095-1353
           CN 11-6020/Q
Director:Chinese Academy of Sciences
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Your Position :Home->Past Journals Catalog->2025年62 No.6

Flight characteristics of two stalk-eyed fruit flies during takeoff
Author of the article:CHEN Xiao-Lin1** SU Guan-Ting2 ZHENG Meng-Zong2 ZENG Yu3 WANG Yong1 HAO Jia-Min2 HUANGFU Ning
Author's Workplace:1. Institute of Zoology, Chinese Academy of Sciences, Beijing 100101, China; 2. Beihang University, Beijing 100191, China; 3. University of South Florida, Tampa, FL 33620, America; 4. National Natural History Museum of China, Beijing 100050, China
Key Words: stalk-eyed fruit flies; eye-stalk; takeoff; flight; kinematics parameters
Abstract:

 [Aim]  To investigate the flight characteristics of Pelmatops ichneumoneus and Pseudopelmatops angustifasciatus (Diptera: Tephritidae), rare stalk-eyed fruit flies with large body sizes, and determine whether variations in eye-stalk length correlate with differences in flight behavior and flight mode. [Methods]  High-speed videography was used to record and analyze the takeoff and forward flight of both species, and compare their flight characteristics and kinematic parameters. [Results]  After takeoff, both species exhibited level flight, gradually increasing speed to a maximum of 0.48 m/s (Pe. ichneumoneus) and 0.46 m/s (Ps. angustifasciatus). Pe. ichneumoneus had a higher maximum speed and greater yaw rotation during turning compared to Ps. angustifasciatus. During stable flight, wingbeat frequency reached 77 Hz in Pe. ichneumoneus and 88 Hz in Ps. angustifasciatus. Furthermore, Ps. angustifasciatus had a smaller wing stroke amplitude than Pe. ichneumoneus, potentially contributing to differences in body rotation behavior. There was a positive correlation between eye stalk-to-body size ratio and flight velocity, yaw and pitch angles, wing stroke duration, and amplitude, and a negative correlation to wingbeat frequency. [Conclusion]  These results provide insights into the biomechanics and evolution of flight in stalk-eyed fruit flies and potential inspiration for the design of micro air vehicles.

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