摘要
研究了利用雷达实测数据对沿火箭飞行弹道的大气参数进行辨识和外推落点的方法,进而提出了一个对效力射诸元进行修正的方法。在此基础上,对软件系统进行了设计。最后通过仿真试验,分析了系统的准确性。
Presents an approach using real-time data measured by a tracking-radar for the identification of atmospheric parameters along the trajectory of a missile so as to extrapolate its impact point.A method for correcting the firing data of successive fires in salvo is then suggested.A software system has been designed on the basis of the above methods.The accuracy of the mentioned system is studied through a series of digital simulations.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1994年第2期19-23,共5页
Acta Armamentarii
关键词
火箭弹道
大气参数
辨识系统
long-range MLRS,fire control system,atmosphere parameters,system identification