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Research on insect-like long endurance hovering double-wing FMAV prototype

Yichen Zhang (National Key Laboratory of Advanced Micro and Nano Manufacture Technology, Shanghai Jiao Tong University, Shanghai, China and Department of Micro/Nano Electronics, School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University, Shanghai, China)
Feng Cui (National Key Laboratory of Advanced Micro and Nano Manufacture Technology, Shanghai Jiao Tong University, Shanghai, China)
Wu Liu (National Key Laboratory of Advanced Micro and Nano Manufacture Technology, Shanghai Jiao Tong University, Shanghai, China)
Wenhao Zhu (National Key Laboratory of Advanced Micro and Nano Manufacture Technology, Shanghai Jiao Tong University, Shanghai, China and Department of Micro/Nano Electronics, School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University, Shanghai, China)
Yiming Xiao (National Key Laboratory of Advanced Micro and Nano Manufacture Technology, Shanghai Jiao Tong University, Shanghai, China and Department of Micro/Nano Electronics, School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University, Shanghai, China)
Qingcheng Guo (Department of Micro/Nano Electronics, School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University, Shanghai, China)
Jiawang Mou (Designing Institute of Hubei Space Technology Academy, Wuhan, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 25 July 2024

Issue publication date: 7 August 2024

107

Abstract

Purpose

Endurance time is an important factor limiting the progress of flapping-wing aircraft. In this study, this paper developed a prototype of a double-wing flapping-wing micro air vehicle (FMAV) that mimics insect-scale flapping wing for flight. Besides, novel methods for optimal selection of motor, wing length and battery to achieve prolonged endurance are proposed. The purpose of this study is increasing the flight time of double-wing FMAV by optimizing the flapping mechanism, wings, power sources, and energy sources.

Design/methodology/approach

The 20.4 g FMAV prototype with wingspan of 21.5 cm used an incomplete gear flapping wing mechanism. The motor parameters related to the lift-to-power ratio of the prototype were first identified and analyzed, then theoretical analysis was conducted to analyze the impact of wing length and flapping frequency on the lift-to-power ratio, followed by practical testing to validate the theoretical findings. After that, analysis and testing examined the impact of battery energy density and efficiency on endurance. Finally, the prototype’s endurance duration was calculated and tested.

Findings

The incomplete gear facilitated 180° symmetric flapping. The motor torque constant showed a positive correlation with the prototype’s lift-to-power ratio. It was also found that the prototype achieved the best lift-to-power ratio when using 100 mm wings.

Originality/value

A gear-driven flapping mechanism was designed, capable of smoothly achieving 180° symmetric flapping. Besides, factors affecting long-duration flight – motor, wings and battery – were identified and a theoretical flight duration analysis method was developed. The experimental result proves that the FMAV could achieve the longest hovering time of 705 s, outperforming other existing research on double-wing FMAV for improving endurance.

Keywords

Acknowledgements

The authors acknowledge financial support by the Natural Science Foundation of China under Grant 61871266 and the Professional technical service platform of Shanghai under Grant 19DZ2291103.

Citation

Zhang, Y., Cui, F., Liu, W., Zhu, W., Xiao, Y., Guo, Q. and Mou, J. (2024), "Research on insect-like long endurance hovering double-wing FMAV prototype", Aircraft Engineering and Aerospace Technology, Vol. 96 No. 6, pp. 769-779. https://doi.org/10.1108/AEAT-09-2023-0239

Publisher

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Emerald Publishing Limited

Copyright © 2024, Emerald Publishing Limited

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