大型火箭发动机地面试验系统测控软件架构设计  

Software architecture design of measurement and control system in ground testing system for large-scale rocket engine

作　　者：许广柱[1] 吴锦凤[1] 

机构地区：[1]西安航天动力试验技术研究所,陕西西安710100

出　　处：《火箭推进》2012年第2期68-74,共7页Journal of Rocket Propulsion

基　　金：国家高技术项目(2006AA705311)

摘　　要：通过对国内大型火箭发动机地面试验测控系统软件开发模式现状的分析,提出采用Rational统一过程"4+1"视图法,结合面向对象设计思想对测控系统软件进行建模,构建出一整套有针对性的面向对象测控系统软件设计模型,为解决现在大型火箭发动机地面试验测控系统软件开发普遍低效、问题反复和难维护等问题奠定良好的基础。Through the status analysis of software development modes of ground testing and control system for the domestic large-scale rocket engines,the Rational Unified Process＂4＋1＂view method is proposed.The modeling of measurement and control system software was carried out in combination with object-oriented design idea.A set of targeted object-oriented model of measurement and control system software design was build.It laid a good foundation for solving the problems（low efficiency,high failure repeatability,difficult maintenance） generally existing in the software development of ground testing and monitoring system for large-scale rocket engines.

关 键 词：地面试验系统 测控系统 软件架构 建模 

分 类 号：V434.3[航空宇航科学与技术—航空宇航推进理论与工程]