火力与指挥控制2025，Vol.50Issue(4)：107-111,5.DOI:10.3969/j.issn.1002-0640.2025.04.015
舰载火箭炮双发射装置点火控制设计
Design of Ignition Control for Double-launcher of Shipborne Rocket Launcher
赵彦龙 1朱建峰 2齐蕾 1姚宗 1李晓光 1朱锐1
作者信息
- 1. 北方自动控制技术研究所,太原 030006
- 2. 陆装驻太原地区第二军代室,太原 030006
- 折叠
摘要
Abstract
Traditional land-based rocket artillery weapon systems employ a"one-to-one"control mode,where a single control terminal operates a launcher.To enhance operational efficiency,shipborne rocket artillery weapon systems adopt a"one-to-many"approach,allowing a single operational terminal to simultaneously control multiple shipborne rocket launchers.Additionally,due to the limited deck space on ships,shipborne rocket artillery is typically deployed in a concentrated manner,side by side on the port and starboard sides,with a relatively short horizontal distance between two launchers.When two shipborne rocket launchers conduct simultaneous firing,their trajectories can easily interfere with each other,leading to deviations and even the risk of missile collisions,posing significant safety hazards.The dual-launcher coordinated alternating ignition control method designed in this paper ensures both the firepower density of simultaneous salvo fire and the shooting safety.关键词
舰载火箭炮/双发射装置/交替点火/火力控制/武器系统Key words
shipborne rocket launcher/dual launcher/alternating ignition/fire control/weapon system分类
军事科技引用本文复制引用
赵彦龙,朱建峰,齐蕾,姚宗,李晓光,朱锐..舰载火箭炮双发射装置点火控制设计[J].火力与指挥控制,2025,50(4):107-111,5.
