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防空多管火箭武器跟踪发射模型研究
引用本文:任杰,马大为,朱忠领,朱孙科.防空多管火箭武器跟踪发射模型研究[J].火炮发射与控制学报,2012(2):79-83.
作者姓名:任杰  马大为  朱忠领  朱孙科
作者单位:南京理工大学机械工程学院,江苏南京,210094
摘    要:立足于火箭武器发展的需求,研究了防空多管火箭炮的跟踪运动对火箭弹离轨参数的影响,给出了跟踪发射时火箭弹运动参数的计算方法,确定了火箭弹脱离定向器瞬时的运动参数,获得了空间弹道计算的初始条件,同时研究了两种特殊跟踪运动下火箭弹的离轨参数,为火箭弹飞行性能优化和发射装置的设计提供了参考。

关 键 词:基础力学  多管火箭  跟踪  发射模型  离轨参数

Study on Launch Model of Multiple Launch Rocket System for Air Defense While Tracking Target
REN Jie , MA Da-wei , ZHU Zhong-ling , ZHU Sun-ke.Study on Launch Model of Multiple Launch Rocket System for Air Defense While Tracking Target[J].Gun Launch & Control Journal,2012(2):79-83.
Authors:REN Jie  MA Da-wei  ZHU Zhong-ling  ZHU Sun-ke
Affiliation:(School of Mechanical Engineering,NUST,Nanjing 210094,Jiangsu,China)
Abstract:To face the development of rocket weapons,this article was focused on the rocket lift-off parameters of multiple launch rocket system for air defense while tracking target.The formulas of lift-off parameters were developed when the rocket was launched in the tracking mode,and the run-off the track parameters of rocket were determined,then the initial trajectory parameter of the rocket which is the initial condition of rocket exterior ballistics can be calculated.Also the rocket lift-off parameters of two special tracking movement were studied.It can be used as a reference for the design and optimization of ro-cket flying performance and rocket launcher.
Keywords:basic mechanics  multiple launch rocket  track  Launch model  initial trajectory parameter
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