摘要
本文提出一种基于初、次级线圈电磁耦合的平衡抛射式火箭弹初速测量方法,给出了软硬件实现方案,射击回收试验验证了该方法的可行性。
This paper presents an implementation method of measuring muzzle velocity for individual equilibrium launch rocket based on inductive coupler between coils. The principle, the key technology and the circuit of the measuring method are described. The experiment results show the method is realizable.
出处
《价值工程》
2016年第14期193-194,共2页
Value Engineering
关键词
测速
火箭弹
平衡抛射
muzzle velocity measurement
rocket
equilibrium launch
