虫型FWMAV串型扑翼机构及模块化尾缘控制系统

IF 1.5 4区工程技术 Q2 ENGINEERING, AEROSPACE

International Journal of Micro Air Vehicles Pub Date : 2019-04-01 DOI:10.1177/1756829319842547

DuHyun Gong, Dawoon Lee, Sang-Joon Shin, Sangyong Kim

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引用次数: 11

摘要

本文介绍了一种新型扑翼微型飞行器扑翼后缘控制机构的设计过程和实验结果。提出了以串为主要部件的扑动机构，并采用改进的模式搜索法对扑动机构进行了优化。后缘俯仰力矩和滚转力矩控制机构被设计成以模块化的方式附加在当前的扑动机构上。为了检验设计的可行性，制作了两种机构的原型并进行了实验测试。预计目前的扑翼机构将产生足够的升力，以满足车辆的总重量。发现现有的控制机构能够提供足够的控制力矩。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

String-based flapping mechanism and modularized trailing edge control system for insect-type FWMAV

This paper presents the design process and experimental results of a brand new flapping and trailing edge control mechanism for a flapping wing micro air vehicle. The flapping mechanism, whose main components are fabricated from string, is suggested and optimized further by a modified pattern search method. The trailing edge control mechanisms for pitching and rolling moments are designed to be attached onto the present flapping mechanism in a modularized fashion. Prototypes of both mechanisms are fabricated and experimentally tested in order to examine the feasibility of the designs. It is expected that the present flapping mechanism will generate enough lift for the total weight of the vehicle. The present control mechanism is found to be able to supply sufficient control moment.

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来源期刊

International Journal of Micro Air Vehicles ENGINEERING, AEROSPACE-

CiteScore

3.00

自引率

7.10%

发文量

审稿时长

>12 weeks

期刊介绍： The role of the International Journal of Micro Air Vehicles is to provide the scientific and engineering community with a peer-reviewed open access journal dedicated to publishing high-quality technical articles summarizing both fundamental and applied research in the area of micro air vehicles.