摘要
动能拦截弹脱靶量要求为零,其杀伤目标为近地轨道运行的弹道导弹和低轨卫星等,目标运行速度极快,与其它类型导弹相比,动能拦截弹的弹道计算精度要求更高。针对这一问题,介绍了动能拦截弹的拦截段弹道数学模型,分析了弹道数据计算流程,将诸元解算转化为方位角和程序角的计算问题,采用计算精度较高的积分算法,得到了导弹拦截过程的弹道数据,仿真表明,导弹数据计算精度满足作战仿真要求。
Kinetic energy interceptor missile which destroys the target by the way of a direct hit needs zero effort miss. The target is ballistic missiles and low-orbit satellites in low earth orbit,which has fast velocity. Compared with other types of missiles,the calculation of kinetic energy interceptor missile ballistic data needs higher accuracy and different ballistic mathematical model. The ballistic mathematical model is introduced and the data calculation process is analyzed. The moroto solver is transformed into the calculation of the angle of azimuth and procedures. Simulation results show that the accuracy of the ballistic data meets the requirements of combat simulation.
出处
《战术导弹技术》
北大核心
2015年第1期53-57,共5页
Tactical Missile Technology
关键词
动能拦截弹
弹道计算
仿真
kinetic energy interceptor missile
ballistic calculation
simulation
