摘要
为全面评估某型制导火箭子母弹弹道性能,采用飞行试验与理论计算结合的方法,建立弹道仿真模型,设计关键弹道参数的精确化确定方法,通过准确弹道仿真实现了型号边界条件下的最大射程评估。该方法已经应用到实际型号鉴定中,解决了0 m发射阵地高度的弹道性能评估问题。
In order to evaluate the trajectory performance of x-type guided rocket submunition,the ballistic model was established,and the precision method of key ballistic parameters was designed,the maximum range assessment under the boundary condition is achieved through accurate trajectory simulation.The method has been applied to the actual model PET and solved the ballistic performance evaluation problem where the altitude of launching position is zero meters.
作者
王海峰
王广伟
贾波
邵庆新
WANG Haifeng;WANG Guangwei;JIA Bo;SHAO Qingxin(No.63850 Unit,Jilin Baicheng 137000,China)
出处
《弹箭与制导学报》
北大核心
2019年第6期21-24,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
制导火箭弹
弹道仿真
弹道性能评估
guided rocket
trajectory simulation
ballistic performance evaluation
