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模型驱动的系统设计方法应用研究 被引量:11

Application Research on Model-driven System Design Method
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摘要 本文详细介绍了IBM Rational Harmony系统设计方法在某型飞机IDMS项目中的应用过程。首先,完成IDMS项目的需求分析,输出用户需求与系统需求,采用了DOORS作为需求管理工具,建立了两者的Link关系。然后,完成系统功能分析,输出系统全部用例,采用了RHAPSODY作为系统设计工具,对其中一个用例采用用例图、活动图、顺序图和状态图等进行分析和建模,得到该用例的可执行模型,验证需求。最后,开展系统架构设计,完成系统的初步架构模型。同时,用DOORS和RHAPSODY管理系统设计过程中的知识库。 This paper presents the application of IBM Rational Harmony system design method in IDMS of next generation airplane. It starts with the requirements analysis by DOORS. After the stakeholder requirements and system requirements being produced, the link between them is created. Then, all of the system use cases will be drawn during the system functional analysis. We take one particular use case as an example and draw the use case diagram, activity diagram, sequence diagram and statechart diagram respectively. By doing this the executable model and validation requirements can be derived by RHAPSODY. Finally, the system architecture design and the architecture model are finished. During the development process, the repository database is managed with DOORS and RHAPSODY.
出处 《航空电子技术》 2011年第1期18-23,43,共7页 Avionics Technology
关键词 用例 模型驱动 系统建模 可执行模型 DOORS RHAPSODY use case model-driven system modeling executable model DOORS RHAPSODY
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参考文献4

  • 1Favre L. Foundations for MDA-based forward engineering[J]. Journal of Object Technology, 2005, 4(I): 129-153.
  • 2Hans-Peter Hoffmann. SysML-Based Systems Engineering Using a Model-Driven Development Approach[M]. Proceedings of 1NCOSE 2006 16th International Symposium.
  • 3Hans-Peter Hoffmann. UML 2.0-Based System Engineering Using a Model-Driven Development Approach[J]. November 2005, Cross Talk, Vol. 18 No. 11.
  • 4Hans-Peter Hoffmann. Harmomy/SE-Model-Based Systems Engineering Using SysML[M]. Proceedings of the SDR'08 Technical Conference and Product Exposition, 2008.

同被引文献56

  • 1郭震中,黄伟华,姚有文,陆志肖.直升机机电综合管理系统发展趋势及关键技术分析[J].直升机技术,2011(3):63-68. 被引量:5
  • 2宫谊凡,蒲小勃,刘军,张杰.基于UML语言的航空电子系统快速原型设计[J].系统仿真学报,2007,19(4):749-753. 被引量:14
  • 3孔立中.模型驱动的系统工程设计法研究[J].航天工业管理,2007(3):11-16. 被引量:1
  • 4熊华刚,王中华.先进航空电子综合技术[M].北京:国防工业出版社.2009.
  • 5Estefan J A. Survey of model-based systems engineer- ing (MBSE) methodologies [ R ]. United States: IN- COSE,2008.
  • 6Howells A, Bushell S. Experiences of using model based systems engineering [ Z ]. United Kindom : IBM software, 2010.
  • 7Foster M A. Developing a heavy lift launch vehicle systems architecture using a model based systems engi- neering approach[ C]. AIAA SPACE 2011 Conference & Exposition. Long Beach, California: AIAA, 2011.
  • 8Hoffmann H P. System Engineering Best Practices with the Rational Solution for Systems and Software Engi- neering [ M ]. NY, United States : IBM Corporation, 2011.
  • 9Mangieri M. L. , Vice J. Orion flight software v&v and kedalion engineering lab insight [ C ]. AIAA SPACE2010 Confererce & Exposition Anaheim, California: AIAA,2010.
  • 10Sellers J. J. , Laarson W. J. , Kirkpatrck D. Redefining space system verification & validation [ C ]. U. S. Air Force T&E Days 2009, Albuquerque, New Mexco: AIAA, 2009.

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