摘要
长延时火箭弹同步起爆控制技术以远程破障作战为背景,文中根据火箭弹的最大延时时间和同步起爆误差,论述了炮口感应装定系统的组成和工作原则,并分析了装定数据传输原理、校频二进制编码原理和解码原理。长延时火箭弹同步起爆控制技术对提高远程破障能力具有重要的意义。
Taking the long-distance broken-barrier warfare as background,according to the maximum delay time and the error of synchronous detonation of rocket,this paper discusses the makeup and working principle of the muzzle inductive set system,analyzes the transmission principle of the set data,the coding principle of the verifying- frequency binary and the decoding principle.The study has important significance for improving the long-distance broken-barrier ability of rocket.
出处
《弹箭与制导学报》
CSCD
北大核心
2004年第S1期155-156,159,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
火箭弹
同步起爆
编码原理
解码原理
rocket
synchronous detonation
coding principle
decoding principle
