{"title":"带脉宽换能器的直流电动机建模","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":"{\"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}","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}
Modeling of DC motor with pulse-duration transducer
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.