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不同导引模式下的末修弹脉冲参数优化研究
引用本文:曹营军,郎玉飞,邵毅,朱宗平,李立春.不同导引模式下的末修弹脉冲参数优化研究[J].军械工程学院学报,2013(1):23-28.
作者姓名:曹营军  郎玉飞  邵毅  朱宗平  李立春
作者单位:北京特种车辆研究所,北京100072
摘    要:在总脉冲量确定的情形下,在启控时间、总脉冲数、最小点火时间间隔及点火阈值等脉冲参数对末修弹落点散布的影响进行详细分析的基础上,利用数值仿真的方法,对比例导引模式、抛物线导引模式、落点预测导引模式、弹道追踪导引模式和zx导引模式等常用导引模式下的脉冲参数优化进行深入分析研究.

关 键 词:末修弹  脉冲参数  导引模式  优化

Research on Pulse Parameters Correction Projectile Based Optimization of Terminal Trajectory on Different Guidance Law Mode
CAO Ying-jun,LANG Yu-fei,SHAO Yi,ZHU Zong-ping,LI Li-chun.Research on Pulse Parameters Correction Projectile Based Optimization of Terminal Trajectory on Different Guidance Law Mode[J].Journal of Ordnance Engineering College,2013(1):23-28.
Authors:CAO Ying-jun  LANG Yu-fei  SHAO Yi  ZHU Zong-ping  LI Li-chun
Institution:(Beijing Special Vehicle Institute, Beijing 100072, China)
Abstract:In the case of invariable whole pulse energy, after analysing the effect of the main pulse parameters including starting control time, pulse number, minimum igniting interval and igniting pulse threshold on the terminal trajectory correction projectile impact point correction in detail, the optimization between the impulse parameters and guidance law mode including proportion guidance mode,parabolic guidance mode,impact point prediction guidance mode,trajectory track- ing guidance mode and xz guidance mode is researched by numerical simulation method.
Keywords:terminal trajectory correction projectile  impulse parameters  guidance law mode  optimization
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