摘要
针对火箭炮武器在野外进行自动操瞄时,由于车体倾斜而导致调炮精度降低的现象,文中在结合对火箭炮车体倾斜时定向管的射向、射角计算的基础上提出了火箭炮调炮精度修正方法。从理论上证明了该方法在消除调炮精度偏差上的可行性。同时,文中建立的数学模型也适用于其它武器发射系统。
Aimed at the phenomenon of rocket launcher vehicle obliqueness and this leads to the reduction of rocket launcher rectification precision when auto-operating and aiming to the rocket launcher in fields, the rocket launcher obliqueness rectification mathematical model was developed via calculating the horizontal and rotated angles about rocket launch barrels of oblique vehicle. The feasibility of improving rocket launcher rectification precision in theory was testified by the mathematical model and the mathematical model can also be applicable to other gun launch system.
出处
《弹箭与制导学报》
CSCD
北大核心
2008年第4期165-167,171,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
校正精度
数学模型
自动操瞄
火箭炮
rectification precision
mathematical model
auto aiming
rocket launcher
作者简介
方安国（1962-），男，湖北汉川人，研究员，研究方向：火箭炮总体技术研究。
