摘要
以某火箭弹惯性开关为研究背景,介绍一种基于计算机仿真的设计和调整引信零件结构参数的方法,并对该方法进行了验模试验,验模结果表明该设计方法的计算结果与试验结果十分接近。
This paper introduces a design method about a inertia switch of rocket fuze. The method dependents on computer models and simulation computation, The structure of the inertia switch was finished with computer. We had experimented. The experiment result approximates to the calculation result.
出处
《探测与控制学报》
CSCD
北大核心
2004年第2期44-46,50,共4页
Journal of Detection & Control
关键词
引信惯性开关
虚拟样机
验模
inertia switch of fuze
simulation models
experimented model.
