远程多管火箭射击精度折合方法研究  

Study of Shot Accuracy Reduced Computation Method for Long Range MLRS

作　　者：姚志军[1] 芮筱亭[1] 王执铨[1] 王广伟[1] 

机构地区：[1]南京理工大学,南京210094

出　　处：《弹箭与制导学报》2006年第4期197-200,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中根据发射动力学和多体系统动力学最新理论,利用建立的可以精细刻画远程多管火箭运动规律的仿真系统,确定了远程多管火箭中、小射程射击精度与最大射程射击精度的定量关系,从而可以实现不同射程射击精度的折算。According to the up-to-date theories from the launching dynamics and the multi-body system dynamics and utilizing the established simulation system which can precisely depict the motion law of the long range MLRS, The relationship of the shot accuracy between short, middle and maximum range can be quantitatively defined, so an it can be used to realize the reduced computation of different range.

关 键 词：远程多管火箭 射击精度 折算 发射动力学 仿真系统 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]