摘要
阐述了脉冲控制力实施简易控制的特点,针对某近程单兵火箭建立了其弹道模型,在弹体周向布置两种大小不同的脉冲发动机,采用两种脉冲延时分级控制的控制策略对其实施简易控制,对其控制时刻、转速影响、分档设计等进行了分析证明对该单兵火箭实施简易控制是可行的。
The characteristic of impulse control is explained in the paper. The ballistic model of short range singlesolider rocket is established. Two kinds different impulses are disposed the section of body. The control method, two kinds impulses adopting time-lapse and graded control, is used to carry out simple control. The control time ,effect of rotate speed and control strategy are analyzed, is feasible that the single solider rocket is implemented simple control according to the emulational calculation.
出处
《火力与指挥控制》
CSCD
北大核心
2007年第5期122-124,128,共4页
Fire Control & Command Control
基金
厂校合作型号研发项目
