{"title":"Design of a portable drone for educational purposes","authors":"Maximilian Hell, R. Bolam, Y. Vagapov, A. Anuchin","doi":"10.1109/IWED.2018.8321377","DOIUrl":null,"url":null,"abstract":"This paper discusses the design of a portable drone to be used by students for practical investigations of drone operating principles. The drone design is based on a Y6 frame module concept and takes into account the affordability and combinability of components which are widely available via the hobbyist drone manufacturing market. It is a foldable device and is protected against water ingress according standard DIN EN 60529 (IP01). The drone generates high thrust for a Maximum Take-off Mass (MTOM) of 5 kg and the propeller design has been investigated and analysed in detail to determine the optimum location required to provide maximum thrust.","PeriodicalId":132863,"journal":{"name":"2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED)","volume":"57 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-01-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/IWED.2018.8321377","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5
Abstract
This paper discusses the design of a portable drone to be used by students for practical investigations of drone operating principles. The drone design is based on a Y6 frame module concept and takes into account the affordability and combinability of components which are widely available via the hobbyist drone manufacturing market. It is a foldable device and is protected against water ingress according standard DIN EN 60529 (IP01). The drone generates high thrust for a Maximum Take-off Mass (MTOM) of 5 kg and the propeller design has been investigated and analysed in detail to determine the optimum location required to provide maximum thrust.
本文讨论了一种便携式无人机的设计,供学生用于无人机工作原理的实际调查。无人机设计基于Y6框架模块概念,并考虑到通过业余爱好者无人机制造市场广泛可用的组件的可负担性和可组合性。它是一个可折叠的设备,并按照标准DIN EN 60529 (IP01)防水。无人机产生5公斤最大起飞质量(MTOM)的高推力,螺旋桨设计已经进行了详细的调查和分析,以确定提供最大推力所需的最佳位置。