火箭炮倾斜调炮修正数学模型研究  

The Mathematical Model Study on Launch Precision Rectification of Gradient Rocket Launcher

作　　者：方安国 邵炜 

机构地区：[1]湖北江山重工有限责任公司研发中心,湖北襄樊441813

出　　处：《弹箭与制导学报》2008年第4期165-167,171,共4页Journal of Projectiles,Rockets,Missiles and Guidance

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.

关 键 词：校正精度 数学模型 自动操瞄 火箭炮 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]