Design of a High-Performance Biomimetic Butterfly Flyer

To achieve miniaturization and lightweight design of a flapping-wing aircraft, a high-performance biomimetic butterfly flyer was designed based on an analysis of the butterfly’s body structure and flight principles. The aircraft has a mass of 20.6 g and a wingspan of 0.295 m. To validate the rationality of the design, sensitivity analysis of the flapping-wing drive mechanism was first conducted using MATLAB 2022B software, and the length of the driving rod was optimized. Subsequently, a dynamic model was established to calculate the aerodynamic performance of the flapping wing. Then, the aerodynamic performance of the aircraft was verified using simulation software (XFLOW 2022). Finally, the flight stability of the aircraft was validated using the SIMULINK toolbox. Flight test results show that the biomimetic butterfly flyer achieves a maximum flight speed of 0.9 m/s, a climb rate of 0.12 m/s, and a flight endurance of up to 3 min, with good flight stability. This design provides a new approach for the development of small and lightweight flapping-wing aircraft.

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Publication Details

Journal
Machines
Published
2025-09-08
DOI
https://doi.org/10.3390/machines13090829
Primary Topic
Biomimetic flight and propulsion mechanisms
Type
article
Field-Weighted Citation Impact
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article

Design of a High-Performance Biomimetic Butterfly Flyer

Daqian Zhang, Hongshuang Li, Zhihan Li, G. Qiu
Machines
Biomimetic flight and propulsion mechanisms
article

Design of a High-Performance Biomimetic Butterfly Flyer

Daqian Zhang, Hongshuang Li, Zhihan Li, G. Qiu
article en

Abstract

To achieve miniaturization and lightweight design of a flapping-wing aircraft, a high-performance biomimetic butterfly flyer was designed based on an analysis of the butterfly’s body structure and flight principles. The aircraft has a mass of 20.6 g and a wingspan of 0.295 m. To validate the rationality of the design, sensitivity analysis of the flapping-wing drive mechanism was first conducted using MATLAB 2022B software, and the length of the driving rod was optimized. Subsequently, a dynamic model was established to calculate the aerodynamic performance of the flapping wing. Then, the aerodynamic performance of the aircraft was verified using simulation software (XFLOW 2022). Finally, the flight stability of the aircraft was validated using the SIMULINK toolbox. Flight test results show that the biomimetic butterfly flyer achieves a maximum flight speed of 0.9 m/s, a climb rate of 0.12 m/s, and a flight endurance of up to 3 min, with good flight stability. This design provides a new approach for the development of small and lightweight flapping-wing aircraft.

MachinesVol. 13(9)
Shenyang Aerospace University (CN)
Openalex Percentile: Top 67%
Biomimetic flight and propulsion mechanisms
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Design of a High-Performance Biomimetic Butterfly Flyer — Daqian Zhang, Hongshuang Li, et al. · Machines (2025) | TGRS Research Map | TGRS