总线型导弹控制系统状态监测与故障诊断技术  

The Technique of the Monitor and Fault Diagnosis of Missile Control System Based on the Bus

作　　者：曾庆华[1] 杜明波[1] 杜诚谦 刘道平[1] 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073 [2]北京航天自动控制研究所,北京100854

出　　处：《国防科技大学学报》2007年第1期7-11,共5页Journal of National University of Defense Technology

基　　金：航空科学基金资助项目(20060112126)

摘　　要：分析了总线型导弹控制系统的地面测控体系及其特点,阐述了系统中单机部件的组成结构及其BIT技术;提出了新的测控体系下导弹控制系统状态监测和故障诊断方法,重点针对总线数据接口格式、系统知识表示和状态监测与故障诊断流程进行了讨论。This paper first analyzed the ground test and control system architecture and its characteristics of the missile control system based on the bus. Then it made an explanation to the structure and BIT technique of a single component. Furthermore, it put forward the method of the monitor and fault diagnosis of missile control system based on the bus, in which the formats of bus data interface, the expression of system knowledge and the process of monitor and fault diagnosis were mainly discussed.

关 键 词：导弹 故障诊断 1553总线 控制系统 

分 类 号：V448.11[航空宇航科学与技术—飞行器设计]