摘要
利用ＷｏｒｋｉｎｇＭｏｄｅｌ仿真软件对导弹安全系统用双转子驱动的无返回力矩钟表机构进行了计算机综合仿真，研究结果表明。
The computer synthesis simulation of a missile safety system is made by using a working model simulating software and an untuned runaway escapement driven by two rotors. The research results have shown that the safety system can deteromnine lateral accelerating effect.
出处
《探测与控制学报》
CSCD
1999年第1期23-28,共6页
Journal of Detection & Control
关键词
安全系统
横向过载
空空导弹
地空导弹
自动定距
Safety system
untuned runaway escapement
lateral acceleration, automatical determination safety distance.
