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反坦克导弹的气动参数辨识
引用本文:马立元.反坦克导弹的气动参数辨识[J].军械工程学院学报,1991(1).
作者姓名:马立元
作者单位:军械工程学院导弹教研室
摘    要:本文运用极大似然法进行激光驾束制导反坦克导弹气动参数的辨识。在辨识的迭代寻优过程中,采用变步长搜索提高辨识准度;在辨识算法的具体计算处理上,采用了模型分解法,大大减少了计算时间,保证了气动参数的辨识精度。同时给出辨识仿真验证结果.

关 键 词:辨识  气动参数  极大似然  模型分解

IDENTIFICATION OF AERODYNAMIC PARAMETERS OF ANTI-TANK MISSILES
Ma Liyuan.IDENTIFICATION OF AERODYNAMIC PARAMETERS OF ANTI-TANK MISSILES[J].Journal of Ordnance Engineering College,1991(1).
Authors:Ma Liyuan
Institution:Teaching and Research Section of Missilery
Abstract:In this paper,the aerodynamic parameters of laser beem-rider guide anti-tank mis- siles are identified using maximum likelihood algorithms.In the course of iterative optimization of maximum likelihood algorithms,variable searching step is used to improve the identification criterion.As for a specific identification,the model decomposition is used, which considerably reduces the time of calculation and ensures the accuracy of the paramete.The estimated and simulated results are also given in this paper.
Keywords:identification  aerodynamic parameter  maximum likelihood  model decomposition
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