Modeling and simulation study of an insect-like flapping-wing micro aerial vehicle

被引:12
|
作者
Zuo, Decan [1 ]
Chen, Wenyuan [1 ]
Peng, Songlin [1 ]
Zhang, Weiping [1 ]
机构
[1] Shanghai Jiao Tong Univ, Natl Key Lab Nano Micro Fabricat Technol, Key Lab Thin Film & Microfabricat Minist Educ, Inst Micro & Nano Sci & Technol, Shanghai 200030, Peoples R China
基金
中国国家自然科学基金;
关键词
flapping-wing micro aerial vehicle; low Reynolds number; simulation model; kinematics equations; aerodynamics model;
D O I
10.1163/156855306777681393
中图分类号
TP24 [机器人技术];
学科分类号
080202 ; 1405 ;
摘要
The goal of this paper is to show some of the most important features of flying insects from a control point of view, describe in details the kinematics of insects during flapping flight, establish the corresponding kinematics equations of flying insects, analyze the force and moment acting on the flying insects, and establish the corresponding aerodynamic equations. Through the kinematics equations and aerodynamic equations of flying insects, the trajectory equations and attitude equations have also been established. A detailed mathematical model of flying insects is presented in this paper, which including 3 d.o.f. of wings kinematics, i.e., flapping, lagging and feathering, and 6 d.o.f. of insects body, i.e., yaw, roll, up-down flight, left-right flight and fore-back flight. All these motions of flying insects are interrelated by the kinematics equations, attitude equations, aerodynamics model and dynamics equations of the insects' centroid. In the findal part of this paper, the mathematical simulation model of flapping-wing insects is set up and the corresponding simulation curve created.
引用
收藏
页码:807 / 824
页数:18
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