摘要: |
针对航天型号技术状态管理中存在的离散式管理状态,系统性、连续性差,控制粗放、精细度不够等现实问题,提出了模型驱动的航天型号技术状态管理方法。该方法立足于对航天型号技术状态管理的内涵和需求的分析,结合模型驱动的系统工程思想,通过建立统一的技术状态全局描述模型,驱动技术状态的演化过程,实现一种精细化、连续可追溯的技术状态管理模式。 |
关键词: 模型驱动;技术状态管理;技术状态模型;技术状态演化 |
基金项目: |
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Research on Model-driven Aerospace Configuration Management Method |
Zhao Han1, Zhang Rongxia2
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1.Beijing Institute of Spacecraft System Engineering, Beijing 100094;2.China Academy of Space Technology, Beijing100094
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Abstract: |
For the lack of adaptation capacity of poor systematic and continuity, and extensive control of discrete configuration management, a new model-driven aerospace configuration management method is proposed. The method establishes a model-driven mechanism based on a unified configuration model that supports the description of both static specification and dynamic evolution of technical states or configuration. Built on the top of this mechanism, a full cycle, traceable and precise configuration management is realized. |
Key words: model-driven;configuration management;configuration model;configuration evolution |