摘要
对防空导弹战斗部有效起爆区、引信实际引爆区和引战配合度概念进行了分析 ,提出引战配合模型 ,应用Simulink仿真工具 ,绘出了某型防空导弹在尾追和迎击情况下的引战配合度曲线 。
The concepts about the effective detonating area of warhead in air defense missile, the real detonating area of the fuze and the cooperation degree for fuze and warhead are analyzed.The cooperation degree model is established with simulation tool Simulink.The lines of cooperation degree of some air defense missile under condition of stern chase and head on attack are drawn and analyzed.
出处
《战术导弹技术》
2003年第4期31-36,共6页
Tactical Missile Technology
关键词
防空导弹
引战配合
配合度
air defense missile
cooperation degree of fuze and warhead
cooperation degree
