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扑 翼 /扑 旋 翼 微 型 飞 行 器 系 统 建 模 与 控 制 方 法 研 究 进 展

  • Yuanyuan He*
  • , Jinfeng Huo
  • , Ao Li
  • , Qiaoya Yang
  • , Haixu Liu
  • *此作品的通讯作者
  • Beijing Institute of Technology

科研成果: 期刊稿件文献综述同行评审

摘要

Flapping-wing vehicles,inspired by the wing kinematics of insects and birds,exhibit remarkable aerodynamic efficiency and maneuverability under low-Reynolds-number regimes. In contrast,flapping-wing rotor vehicles,an emerging research frontier in recent years,integrate passive rotational motion with flapping actuation,enabling enhanced hovering and vertical take-off/landing capabilities. It presents a systematic review of recent advancements in system modeling and control methodologies for flapping-wing micro air vehicles(FWMAVs)and flapping-wing rotor micro air vehicles(FWRMAVs). It delves into the unsteady aerodynamic theories underlying the insect-inspired flapping-wing flight mechanism,and further explores the existing system modeling and control approaches tailored to insect-inspired FWMAVs and FWRMAVs. Finally, this review addresses current challenges in FWMAVs dynamics and control methodologies, including aerodynamic modeling of flexible wings and suppression of unsteady disturbances. It further highlights the insufficient research on flight dynamic characteristics and active attitude control of FWRMAVs, thereby outlining prospects for future investigations.

投稿的翻译标题Research Progress on Modeling and Control Methods of Flapping-Wing/Flapping-Wing Rotor Micro Air Vehicle Systems
源语言繁体中文
页(从-至)1046-1060
页数15
期刊Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics
57
6
DOI
出版状态已出版 - 12月 2025
已对外发布

关键词

  • control methods
  • flapping wing
  • flapping-wing rotor
  • micro air vehicle
  • system modeling

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