Modeling of DC motor with pulse-duration transducer

N. Rustam, Y. Anastasia
{"title":"Modeling of DC motor with pulse-duration transducer","authors":"N. Rustam, Y. Anastasia","doi":"10.1109/DYNAMICS.2014.7005658","DOIUrl":null,"url":null,"abstract":"To study the possibilities of UAV electrification simulation modeling was conducted of controlled electric drive of engine-propeller combination of low power with non-linear load in the software package MATLAB, using a library of SimPowerSystems with batch expansion Simulink. As the power machine there is used a DC motor. The characteristics of the electric drive system from the study model show the possibility of its use as a drive-rotor of UAV group up to 3 kW.","PeriodicalId":248001,"journal":{"name":"2014 Dynamics of Systems, Mechanisms and Machines (Dynamics)","volume":"31 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2014-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2014 Dynamics of Systems, Mechanisms and Machines (Dynamics)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DYNAMICS.2014.7005658","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

To study the possibilities of UAV electrification simulation modeling was conducted of controlled electric drive of engine-propeller combination of low power with non-linear load in the software package MATLAB, using a library of SimPowerSystems with batch expansion Simulink. As the power machine there is used a DC motor. The characteristics of the electric drive system from the study model show the possibility of its use as a drive-rotor of UAV group up to 3 kW.
带脉宽换能器的直流电动机建模
为了研究无人机电气化的可能性,利用SimPowerSystems库与Simulink批量扩展,在MATLAB软件包中对低功率、非线性载荷的发动机-螺旋桨组合可控电驱动进行了仿真建模。作为动力机,使用直流电机。从研究模型中得出的电驱动系统的特性显示了其作为无人机群驱动旋翼的可能性,最大功率为3kw。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信