一种多弹协同制导策略  

Multi-Missile Cooperative Attacking Strategy

作　　者：花文涛[1] 刘沛文 贾晓洪[1] 梁晓庚[1] HUA Wentao;LIU Peiwen;JIA Xiaohong;LIANG Xiaogeng(Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons, China Airborne Missile Academy, Luoyang 471009, China)

机构地区：[1]中国空空导弹研究院航空制导武器航空科技重点实验室,河南洛阳471009

出　　处：《兵器装备工程学报》2021年第2期180-183,228,共5页Journal of Ordnance Equipment Engineering

基　　金：航空科学基金项目(2018ZC12006)。

摘　　要：在角度约束最优导引律分析的基础上,设计了一种多弹协同制导律,将其应用到对空运动目标攻击过程中,分析了导弹剩余飞行时间估计方法和领弹与从弹选择策略,通过仿真,验证了对运动目标协同攻击的可行性。Based on the analysis of angular constraint optimal guidance law,a multi-missile cooperative guidance law was designed,which was applied to the process of moving target attack.This paper analyzed the method of estimating remaining flight time of missile and the selection strategy of lead and subordinate missile.The feasibility of cooperative attack on moving target was verified by digital simulation.

关 键 词：协同制导 剩余飞行时间 运动目标 角度时间约束 最优控制 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]