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航天器推进系统故障的面向时态检测和诊断
引用本文:王日新,徐敏强,宋政吉.航天器推进系统故障的面向时态检测和诊断[J].推进技术,2002,23(1):11-14.
作者姓名:王日新  徐敏强  宋政吉
作者单位:哈尔滨工业大学,航天学院,黑龙江,哈尔滨,150001
基金项目:国家“八六三”基金资助项目 (86 3 2 4 8 1)
摘    要:根据航天器推进系统的时变性特点,在规则的专家系统方法基础上,提出了推进系统面向时态的故障检测和诊断方法,在对知识表示方法和推理诊断策略进行改进后,在Windows NT环境与实现了一个基于知识的故障诊断原型系统,介绍了原型系统的结构、功能及网络实时数据通信方法,经过仿真数据测试验证了方法的有效性。

关 键 词:航天器  推进系统  故障诊断专家系统  故障检测  系统故障  面向时态检测
文章编号:1001-4055(2002)01-0011-04
修稿时间:2001年1月31日

Fault detection and diagnosis system based on the rule and time variation for spacecraft propulsion system
WANG Ri xin,XU Min qiang and SONG Zheng ji.Fault detection and diagnosis system based on the rule and time variation for spacecraft propulsion system[J].Journal of Propulsion Technology,2002,23(1):11-14.
Authors:WANG Ri xin  XU Min qiang and SONG Zheng ji
Institution:School of Astronautics,Harbin Inst. of Technology,Harbin 150001, China;School of Astronautics,Harbin Inst. of Technology,Harbin 150001, China;School of Astronautics,Harbin Inst. of Technology,Harbin 150001, China
Abstract:A fault detection and diagnosis method based on the rule and time variation was presented based on the normal diagnostic expert system. The knowledge representation method and diagnostic reasoning strategies were described. A fault diagnostic prototype system was developed in Windows NT. The architecture and function of the prototype system were introduced.
Keywords:Spacecraft propulsion  Engine failure  Time  varying system  Fault diagnosis expert system  Fault detection
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