机械制造与自动化Issue(2)：183-186,4.DOI:10.19344/j.cnki.issn1671-5276.2018.02.050
基于LabVIEW的微扑翼机实验台测控系统设计
Design of Test System for Flapping-wing Micro Air Vehicles Test Bench Based on LabVIEW
摘要
Abstract
To be inconvenient to do the aerodynamic experimental tests for flapping-wing micro air vehicles, this paper presents a kind of test system for micro ornithopter test bench based on LabVIEW software. Through reasonable design of the hardware and software,test system can be used to achieve the aerodynamic characteristics test for the ornithopter and the observation of the flap-ping-wing flow field. It mainly consists of the aerodynamic testing devices,the three-dimensional particle image velocimetry devices (3D-PIV) and micro ornithopter prototype.The aerodynamic data,the twist angle of the wings,flapping frequency,vorticity diagram of the flapping-wing flow field can be obtained through this test.These experimental datum can reflect the aerodynamic performance of the ornithopter,which are agreat help to the design of the ornithopter and its research.关键词
微型扑翼机/测控系统/气动力测试/三维粒子图像测速Key words
micro ornithopter/test system/faerodynamic testing/3D particle image velocimetry分类
机械制造引用本文复制引用
田培培,金晓怡,黄立新,邢亚飞,朱建柳..基于LabVIEW的微扑翼机实验台测控系统设计[J].机械制造与自动化,2018,(2):183-186,4.基金项目
上海工程技术大学高水平项目(2012gp05) （2012gp05）
上海工程技术大学研究生科研创新项目(E109031501016) （E109031501016）
