微型飞行器
拍打
翼
空气动力学
工程类
航空学
飞行操纵面
弹道
航空航天工程
电梯
飞机飞行力学
电传电报
控制(管理)
计算机科学
控制工程
飞行模拟器
人工智能
物理
天文
作者
Fang Xiao-qing,Yian Wen,Zhida Gao,Kai Gao,Qi Luo,Hui Peng,Ronghua Du
出处
期刊:Micromachines
[Multidisciplinary Digital Publishing Institute]
日期:2023-07-31
卷期号:14 (8): 1547-1547
被引量:6
摘要
The Bird-like Flapping-wing Air Vehicle (BFAV) is a robotic innovation that emulates the flight patterns of birds. In comparison to fixed-wing and rotary-wing air vehicles, the BFAV offers superior attributes such as stealth, enhanced maneuverability, strong adaptability, and low noise, which render the BFAV a promising prospect for numerous applications. Consequently, it represents a crucial direction of research in the field of air vehicles for the foreseeable future. However, the flapping-wing vehicle is a nonlinear and unsteady system, posing significant challenges for BFAV to achieve autonomous flying since it is difficult to analyze and characterize using traditional methods and aerodynamics. Hence, flight control as a major key for flapping-wing air vehicles to achieve autonomous flight garners considerable attention from scholars. This paper presents an exposition of the flight principles of BFAV, followed by a comprehensive analysis of various significant factors that impact bird flight. Subsequently, a review of the existing literature on flight control in BFAV is conducted, and the flight control of BFAV is categorized into three distinct components: position control, trajectory tracking control, and formation control. Additionally, the latest advancements in control algorithms for each component are deliberated and analyzed. Ultimately, a projection on forthcoming directions of research is presented.
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