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作 者:唐甜[1] 葛洋洋 梁欣颖 TANG Tian;GE Yang-yang;LIANG Xin-ying(Xi′an Aeronautics Computing Technique Research Institute,AVIC,Xi′an 710000,China)
机构地区:[1]航空工业西安航空计算技术研究所,陕西西安710000
出 处:《航空计算技术》2021年第4期101-104,共4页Aeronautical Computing Technique
基 金:航空科学基金项目资助(MJ-2017-D-28)。
摘 要:摒弃传统的“基于代码的开发流程”研发方式,将MBSE引入了航空动力控制系统进排气门组件,通过模型的方式完成需求分析、软件设计和验证等活动,不再使用自然语言或手工编码,而是一个相互依赖、反复迭代和递归的过程,引入“基于模型的开发流程”代替传统的“基于代码的开发流程”研发流程,将软件研发工作的重点从编码阶段提升至设计阶段,具有知识点表达无二义性、沟通交流效率高、系统设计一体化、系统内容可重用性高以及知识获取再利用率高等特点,极大地改善了软件的可靠性,具有较强的实用价值。Instead of the traditional code based development process,MBSE is introduced into the IEU components of the APU,and the requirements analysis,software design and verification are completed by model.Instead of using natural language or manual coding,it is an interdependent,iterative and recursive process.It introduces the model-based development process instead of the traditional code based development process,which promotes the focusing of software research and development from stage of software development to the design stage.It has the characteristics of unambiguous knowledge point expression,high communication efficiency,system design integration,high reusability of system content and high reuse rate of knowledge acquisition.No longer through the test or can not measure the quantitative evaluation to ensure the high reliability of the software,but through the effective management of the whole development process to ensure the high reliability of the software,greatly improve the reliability of the software,which has a strong practical value.
分 类 号:V243[航空宇航科学与技术—飞行器设计]
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