小型战术导弹动态测试技术研究  

Investigation on Small Tactical Missile Dynamic Test Technology

作　　者：徐宝连 周玉清 

机构地区：[1]中国兵器工业第203研究所,西安710065

出　　处：《弹箭与制导学报》2015年第4期159-161,166,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：提出一种新颖的小型战术导弹动态测试技术,该技术提供一个非破坏的并且行之有效的手段来判断导弹各个部件是否处于良好的工作状态或性能是否退化。文中首先阐述了导弹动态测试的含义以及国内外发展现状,深入研究了总体、接口选择、测试态、电源、安全等设计原则以及导引头、弹上计算机、惯导装置、舵机等制导控制部件测试方法,并对导弹动态测试装置进行了初步的设计。实际应用表明了设计方法的可行性和有效性。One novel kind of small dynamic tactical missile test technology was proposed. A non-destructive and effective method was presented to estimate performance of the missile units. In this paper,the meaning of missile dynamic performance detection technology and technological advances were introduced. Then,the rules of total design testing,interface selection,test state,power,safety and the test methods to guidance and control units such as seeker,missile-borne computer,INS,actuator were investigated. Furthermore,a kind of dynamic missile test equipment was simply designed. The result of application demonstrates reliability and validity of the proposed technology for dynamic missile test.

关 键 词：小型战术导弹 动态测试 直升机载 制导控制部件 

分 类 号：TP302[自动化与计算机技术—计算机系统结构]