Design and Implementation of Hovering Flapping Wing Micro Air Vehicle

被引：0
|
作者：
Li, Jiaxiang [1 ]
Wang, Chao [1 ,2 ]
Liu, Jin [1 ]
Xie, Peng [1 ]
Zhou, Chaoying [1 ]
机构：
[1] Harbin Inst Technol, Shenzhen 518055, Peoples R China
[2] Dongguan Univ Technol, Dongguan 523000, Peoples R China
来源：
INTELLIGENT ROBOTICS AND APPLICATIONS, ICIRA 2019, PART VI | 2019年 / 11745卷
基金：
中国国家自然科学基金; 中国博士后科学基金;
关键词：
Flapping Wing Micro Air Vehicle; Hovering; Attitude control;
D O I：
10.1007/978-3-030-27529-7_20
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
In this paper, a prototype of a hovering flapping wing micro air vehicle is developed. The aerodynamic force of the prototype at different flapping frequencies and pitch angles is measured, and a hovering flight control scheme for the vehicle is designed based on the measured results. Finally, a flight test of the prototype is carried out. The tail deflection of the prototype is controlled by a micro linear rudder, and the pitch attitude of the prototype is adjusted during flight. The hovering flight within a certain range is realized. The feasibility of the hovering flight control scheme of flapping wing micro air vehicle is verified.
引用
收藏
页码：226 / 233
页数：8
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