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基于数据融合的某型导弹智能温度测量控制系统
引用本文:郭利,张锡恩,马彦恒.基于数据融合的某型导弹智能温度测量控制系统[J].军械工程学院学报,2003,15(4):27-30.
作者姓名:郭利  张锡恩  马彦恒
作者单位:军械工程学院导弹工程系,军械工程学院导弹工程系,军械工程学院光学与电子工程系 河北石家庄 050003,河北石家庄 050003,河北石家庄 050003
摘    要:介绍了应用于某型导弹的温度测量控制系统的硬件组成和工作过程。为了消除测量干扰,提出一种一致性加权融合估计算法,给出了多传感器一致性检验的准则,并利用多元统计理论推导出了最优权值的计算公式。最后将该算法应用于导弹温度测量控制系统。实验证明:该算法具有较好的稳定性,可有效降低噪声干扰,提高测量精度。

关 键 词:数据融合  温度测量控制  一致性加权  导弹
文章编号:1008-2956(2003)04-0027-04
修稿时间:2003年6月10日

Intelligent Temperature Measuring and Control Systemof a Certain Missile Basing on Data Fusion
GUO LiZHANG Xi-enMA Yan-heng.Intelligent Temperature Measuring and Control Systemof a Certain Missile Basing on Data Fusion[J].Journal of Ordnance Engineering College,2003,15(4):27-30.
Authors:GUO LiZHANG Xi-enMA Yan-heng
Institution:GUO Li~1ZHANG Xi-en~1MA Yan-heng~2
Abstract:This paper introduces the hardware and working process of the intelligent temperature measuring and control system applied in a certain missile.In order to eliminate measuring interference, a consensus weighting fusion estimate algorithm and the rule of consensus multi-sensor testing are brought forward,and the optimal weight calculation formula is derived by using the multivariate numerical theory. At last, this algorithm is used in the temperature measuring and control system for missile. The experiment proves that this algorithm is stable, and is able to reduce the noise interference and improve the measuring accuracy.
Keywords:data fusion  temperature measuring and control  consensus weighting  missile
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