基于工作流的液体火箭发动机虚拟试验流程管理  

Workflow-based process management in virtual test of liquid rocket engine

作　　者：段娜[1] 朱子环[1] 于海磊[1] 张黎辉[2] 

机构地区：[1]北京航天试验技术研究所,北京100074 [2]北京航空航天大学宇航学院,北京100191

出　　处：《火箭推进》2012年第3期74-79,共6页Journal of Rocket Propulsion

摘　　要：以液体火箭发动机虚拟试验为对象,研究了数字化试验流程管理的解决方案。通过分析发动机虚拟试验流程,建立了基于工作流的试验管理系统过程仿真模型,提出了一个支撑整个试验管理系统的层次化体系架构。该架构为整个虚拟试验过程提供了统一的试验信息集成平台和应用服务环境。最后,以试验准备阶段为例,给出了该系统的一个集成应用,介绍了基于图形管理系统的实现过程,得到了过程中资源消耗优化的结论。所提出的液体火箭发动机虚拟试验流程管理体系为真实试验的资源优化提供了理论依据,在航天领域的数字化试验方面进行了探索性研究。The digitalized test process management in the virtual test of liquid rocket engines is studied. By analyzing the virtual test process of such engines, the workflow-based process simulation model of test management system is established, and a hierarchical architecture is proposed to support the test process management system. The architecture provides a unified test information integrated platform and an application service environment for the entire virtual test process. Taking preparatory stage of the test as an example, the integrated application of the the management system is shown, and the implementation process based on graphics management system is introduced. A conclusion of optimized consumption of resources is achieved. The test process management system presented in this paper for the virtual test of liquid rocket engines can provide a theoretic foundation for resource utilization in real test. It conduces to farther research in digitalized test process management in the field of space technology.

关 键 词：液体火箭发动机 虚拟试验 试验流程管理 离散事件 工作流 

分 类 号：V434-34[航空宇航科学与技术—航空宇航推进理论与工程]