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某型导弹发射内弹道数值仿真
引用本文:陈庆贵,齐强,朱保义.某型导弹发射内弹道数值仿真[J].海军航空工程学院学报,2010,25(5):501-504.
作者姓名:陈庆贵  齐强  朱保义
作者单位:[1]海军航空工程学院研究生管理大队,山东烟台264001 [2]海军航空工程学院七系,山东烟台264001 [3]海装驻郑州地区军事代表室,郑州450000
基金项目:国防科工委"十一五"预研项目
摘    要:建立某型潜射导弹的内弹道方程组,对内弹道方程组进行了仿真计算,研究了变深度发射内弹道参数的变化规律及发射深度变化对导弹离筒参数的影响。

关 键 词:内弹道方程  仿真计算  变深度发射

Numerical Simulation of Launching Inner Trajectory of one Missile
CHEN Qing-gui,QI Qiang and ZHU Bao-yi.Numerical Simulation of Launching Inner Trajectory of one Missile[J].Journal of Naval Aeronautical Engineering Institute,2010,25(5):501-504.
Authors:CHEN Qing-gui  QI Qiang and ZHU Bao-yi
Institution:1.Naval Aeronautical and Astronautical University a. Graduate Students’ Brigade;b. №7 Department,Yantai Shandong 264001,China;2.Military Representatives Bureau of NED in Zhengzhou,Zhengzhou 450000,China)
Abstract:The inner trajectory equations of one kind of missile launched by submarine were established, simulated and computed, and the changing law of inner trajectory parameters as well as the effect of changing launch depth on parameters of leaving canister were studied.
Keywords:inner trajectory equations  simulation and computation  launch in changing depth
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