远程制导迫弹滑翔增程弹道方案研究  

Research on gliding extended range trajectory scheme of long range guided mortar projectile

作　　者：陈胜政 宋宇航 张意 康博弈 杜青山 CHEN Shengzheng;SONG Yuhang;ZHANG Yi;KANG Boyi;DU Qingshan(Xi’an Institute of Modern Control Technology, Xi’an 710065, China)

机构地区：[1]西安现代控制技术研究所,西安710065

出　　处：《兵器装备工程学报》2022年第1期130-134,169,共6页Journal of Ordnance Equipment Engineering

基　　金：装备预研基金项目。

摘　　要：以满足迫击炮的远程化打击为研究背景,本文提出了以火箭助推+滑翔增程的远程制导迫弹弹道方案,建立了弹道方程组模型,在此基础上对滑翔增程弹道进行研究。理论分析及数字仿真表明,滑翔增程能力主要取决于弹体的升阻比以及最大弹道高。通过提高弹体升阻比和优化最大弹道高设计,远程制导迫弹能够实现较强的弹道增程,满足远程化打击作战需求。In order to meet the long-range attack of mortar,this paper proposed a long-range guided mortar projectile trajectory scheme based on rocket boost and gliding extended range,established the trajectory equations model,and made an in-depth study on gliding extended range trajectory.Theoretical analysis and digital simulation show that the gliding extended range capability mainly depends on the lift drag ratio and the maximum ballistic height of the missile.By improving the lift drag ratio and optimizing the design of maximum ballistic height,the long-range guided mortar projectile can achieve strong ballistic range increasing ability,so as to meet the operational requirements of long-range strike.

关 键 词：远程制导迫弹 滑翔增程 迫击炮 升阻比 

分 类 号：TJ412.1[兵器科学与技术—火炮、自动武器与弹药工程]