触发式远程制导火箭弹对单目标射击效率评定  

Firing Efficiency Evaluation for Triggered Long-range Satellite Guided Rockets on Single Target

作　　者：于远鹏 李臣明 YU Yuanpeng;LI Chenming(Nanjing Campus of PLA Army Academy of Artillery and Air Defense Nanjing,211132,China)

机构地区：[1]陆军炮兵防空兵学院南京校区,南京211132

出　　处：《火力与指挥控制》2023年第8期190-194,共5页Fire Control & Command Control

基　　金：国防科技卓越青年科学基金会资助项目(2021-JCJQ-ZQ-001)。

摘　　要：针对卫星制导触发式远程制导火箭弹技术特点,对误差源因素和基于射击相关性的两组误差型进行分析,推导了对单个目标射击的命中毁伤律、射击效率的积分表达式和简化计算表达式。数值计算结果表明:触发式远程制导火箭弹的射击效率与目标性质、圆概率误差精度(CEP)和用弹量等因素密切相关。在不考虑电磁干扰情况下对同一目标射击时,射击效率随CEP的增加而减小,随用弹量的增加而增大。CEP值越大,射击独立性越强。研究的结果可用于远程制导火箭弹的射击效率评定。Aiming at the technical characteristics of triggered long-range satellite guided rockets,the error source factors and two sets of errors based firing correlation are analyzed,the integral expression and simplified calculation expression of hit damage law and firing efficiency are derived too.The simulation results show that the firing efficiency of triggered long-range satellite guided rocket is closely related with the nature of targets,circular error probable(CEP),the consumption of rockets and other factors.As for firing the same target without consideration of the case of the electromagnetic interference,the firing efficiency decreases with the increase of CEP and increases with the increase of consumption of rockets.The CEP value is larger,the firing independence is stronger.The researched results can be applied in firing efficiency evaluation for long-range guided rockets.

关 键 词：炮兵射击学 卫星制导 远程火箭 射击效率 两组误差型 毁伤律 

分 类 号：TJ7[兵器科学与技术—武器系统与运用工程]