Feature-Driven Specification of VTOL Air-Taxis with the Use of the Model-Based System Engineering (MBSE) Methodology CUBE

Nicolas Jäckel, J. Andert, Abdulsamed Karaduman, C. Granrath, Bernhard Rumpe, L. Wachtmeister
{"title":"Feature-Driven Specification of VTOL Air-Taxis with the Use of the Model-Based System Engineering (MBSE) Methodology CUBE","authors":"Nicolas Jäckel, J. Andert, Abdulsamed Karaduman, C. Granrath, Bernhard Rumpe, L. Wachtmeister","doi":"10.4050/f-0077-2021-16881","DOIUrl":null,"url":null,"abstract":"\n Ground-bound transport systems in major cities are increasingly encountering their limits. Vertical Take-Off and Landing systems, in short VTOL systems, possibly autonomous and electrified, are a promising way to utilize urban space for public transportation. In this context, the application of the Compositional Unified system-Based Engineering (CUBE) methodology, enables the use of Model-Based Systems Engineering (MBSE) to develop suitable VTOLs. This methodology can be used to move from abstract artifacts to concrete architecture and from system to subsystem development. In this paper, the CUBE methodology is presented using a feature-driven specification to demonstrate its general applicability. The model-based description of the System of Interest (SoI, i.e., the VTOL system) from an abstract use case to a technical architecture is exemplified using three features. This methodology approaches the creation of system- and feature-based models with a tailored level of abstraction to better manage complexity.\n","PeriodicalId":273020,"journal":{"name":"Proceedings of the Vertical Flight Society 77th Annual Forum","volume":"46 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-05-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Vertical Flight Society 77th Annual Forum","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4050/f-0077-2021-16881","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

Abstract

Ground-bound transport systems in major cities are increasingly encountering their limits. Vertical Take-Off and Landing systems, in short VTOL systems, possibly autonomous and electrified, are a promising way to utilize urban space for public transportation. In this context, the application of the Compositional Unified system-Based Engineering (CUBE) methodology, enables the use of Model-Based Systems Engineering (MBSE) to develop suitable VTOLs. This methodology can be used to move from abstract artifacts to concrete architecture and from system to subsystem development. In this paper, the CUBE methodology is presented using a feature-driven specification to demonstrate its general applicability. The model-based description of the System of Interest (SoI, i.e., the VTOL system) from an abstract use case to a technical architecture is exemplified using three features. This methodology approaches the creation of system- and feature-based models with a tailored level of abstraction to better manage complexity.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
基于模型系统工程(MBSE)方法论CUBE的垂直起降空中出租车特征驱动规范
大城市的地面交通系统正日益面临极限。垂直起降系统,简称VTOL系统,可能是自动的和电气化的,是利用城市空间进行公共交通的一种很有前途的方式。在这种情况下,基于组合的统一系统工程(CUBE)方法的应用,使得基于模型的系统工程(MBSE)能够开发合适的垂直起降工具。该方法可用于从抽象工件转移到具体架构,从系统转移到子系统开发。在本文中,使用功能驱动的规范来展示CUBE方法的一般适用性。感兴趣的系统(SoI,即垂直起降系统)从抽象用例到技术体系结构的基于模型的描述使用三个特征来举例说明。这种方法通过定制的抽象层次来创建基于系统和特征的模型,从而更好地管理复杂性。
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 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Hover Performance in Ground Effect Prediction Using a Dual Solver Computational Methodology AW609 Civil Tiltrotor Drive Train Torsional Stability Analysis and Certification Test Campaign  Boiling Down Aviation Data: Development of the Aviation Data Distillery Reliability-Driven Analysis, Design and Characterization of Rotorcraft Structures: Decision-Making Framework High-Speed Rotorcraft Pitch Axis Response Type Investigation
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1