仿鸟扑翼飞行器关键技术综述
收稿日期: 2023-12-15
修回日期: 2024-01-24
录用日期: 2024-01-30
网络出版日期: 2024-02-07
基金资助
国家自然科学基金(12272318);特色学科基础研究项目(G2022WD)
Key technologies of bird inspired flapping-wing micro aerial vehicles: Review
Received date: 2023-12-15
Revised date: 2024-01-24
Accepted date: 2024-01-30
Online published: 2024-02-07
Supported by
National Natural Science Foundation of China(12272318);ND Basic Research Funds(G2022WD)
仿鸟扑翼飞行器（BIFMAVs）在飞行效率、隐身性和机动性上有巨大发展潜力，是一种具有较高研究价值和应用前景的微型飞行器。本文主要回顾了近20年来BIFMAVs的研究发展历程，对其总体设计方法、气动分析方法、驱动系统关键技术和飞行动力学与控制关键技术的研究现状进行了总结与分析，并指出了各项技术的特点、发展趋势和面临的挑战，最后提出了对BIFMAVs未来发展方向的展望。对仿鸟扑翼飞行器关键技术研究现状和发展方向的综合评述可为后续从事该方面的研究人员提供参考和借鉴。
关键词： 仿鸟扑翼飞行器（BIFMAVs）; 总体设计; 驱动系统; 多体动力学; 控制系统
薛栋 , 朱紫文 , 宋笔锋 . 仿鸟扑翼飞行器关键技术综述[J]. 航空学报, 2024 , 45(17) : 529984 -529984 . DOI: 10.7527/S1000-6893.2024.29984
Bird Inspired Flapping-wing Micro Aerial Vehicles （BIFMAVs） have great development potential in terms of flight efficiency， stealth， and maneuverability， exhibiting high research value and application prospects. This article mainly reviews the research and development progress of BIFMAVs over the past 20 years， summarizing and analyzing the current state of research on their overall design methods， aerodynamic analysis methods， and key technologies of the driven system and the flight dynamics and control. The characteristics and developmental trends of， and the challenges faced by each technology are presented， and the prospects for the future development direction of BIFMAVs are ultimately proposed. By providing a comprehensive review of the current state of research and development direction of key technologies for BIFMAVs， it can serve as a reference for subsequent researchers working in this field.
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