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 |
| 卷 | 57 |
| 期 | 6 |
| DOI | |
| 出版状态 | 已出版 - 12月 2025 |
| 已对外发布 | 是 |
关键词
- control methods
- flapping wing
- flapping-wing rotor
- micro air vehicle
- system modeling
指纹
探究 '扑 翼 /扑 旋 翼 微 型 飞 行 器 系 统 建 模 与 控 制 方 法 研 究 进 展' 的科研主题。它们共同构成独一无二的指纹。引用此
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