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.
出处
《系统仿真学报》
EI
CAS
CSCD
北大核心
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)
