摘要
通过建立末段修正迫弹在俯仰平面的简化弹道模型,对末段修正迫弹主要参数的确定方法进行了研究,分别对脉冲力值、修正阈值和脉冲发动机个数对脱靶量的影响进行了仿真计算和分析,研究成果可为末段修正迫弹总体方案设计提供重要的参考依据。
This paper established the simplified pitch plane trajectory model of terminal correction mortar projectile(TCMP), and researched the primary parameters determination methods of TCMP, simulated and analyzed the miss distance influenced by impulse force value, correction threshold and numbers of impulse rocket respectively, the research results can provide important information for TCMP overall scheme design.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第2期80-82,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
国家部委预研基金资助项目