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导弹气动参数的分割法辨识
引用本文:马立元,冯振声,谷宏强.导弹气动参数的分割法辨识[J].军械工程学院学报,1996(4).
作者姓名:马立元  冯振声  谷宏强
作者单位:军械工程学院导弹教研室,军械工程学院导弹教研室,军械工程学院导弹教研室 石家庄 050003,石家庄 050003,石家庄 050003
摘    要:介绍了分割辨识算法及其在导弹气动参数辨识中的应用,并以某导弹为例,采用分割辨识算法对其气动参数进行了估计。仿真计算表明,分割辨识算法计算量小、计算速度快,且精度满足要求。

关 键 词:分割辨识算法  气动参数  估计

PARTITIONING IDENTIFICATION OF THE MISSILE AERODYNAMIC PARAMETERS
Ma Liyuan Feng Zhensheng Gu Hongqiang.PARTITIONING IDENTIFICATION OF THE MISSILE AERODYNAMIC PARAMETERS[J].Journal of Ordnance Engineering College,1996(4).
Authors:Ma Liyuan Feng Zhensheng Gu Hongqiang
Institution:Teaching and Research Section of Missile
Abstract:The partitioning identification algorithm and its application in missile aerodynamic parameter identification are briefly introduced in this paper. The aerodynamic parameters of a certain missile are estimated using the partitioning identification algorithm. The estimated result shows that the partitioning algorithm has the advantage of low calculating time and fastcalculating speed. The accuracy can satisfy our requirement.
Keywords:partitioning identification algorithm  aerodynamic parameter  estimation
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