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：

中国博士后科学基金; 中国国家自然科学基金;

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

页码：226 / 233

页数：8

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