基于MEMS技术的扑翼式微飞行器的研究  

Study of Flapping-wing MAV Based on MEMS Technology

作　　者：左德参[1] 陈文元[1] 彭松林[1] 李智军[1] 张卫平[1] 

机构地区：[1]上海交通大学微纳科学技术研究院

出　　处：《系统仿真学报》2005年第6期1505-1508,1527,共5页Journal of System Simulation

基　　金：国家自然科学基金(60375033)

摘　　要：在低雷诺数环境下对长度大约15cm,重量在20～60g的直翅类昆虫的飞行进行了空气动力学的建模研究,对扑翼式微飞行器的系统结构进行了详细的分析论述;通过仿真软件建立了所需要的扑翼飞行机器人的数学模型,并对其进行了仿真研究,从而为扑翼飞行器的研制提供理论依据。The aerodynamic modeling of the orthoptera insect with wing length about fifteen centimeters and weight about twenty to sixty gram under low Reynolds number was studied, the system structure of flapping-wing Micro Aerial Vehicle was detailedly analyzed and discussed, the mathematics modeling of flapping-wing MAV was established through simulation software, and simulation studying was performed, so it offers the academic warrant for the study of flapping-wing Micro Aerial Vehicle.

关 键 词：低雷诺数 MEMS 扑翼式微飞行器 仿真 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]