基于PCA-ELM的弹载组合导航智能故障检测算法
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  • 英文篇名:Intelligent Fault Detection Method of Missile Borne Integrated Navigation System Based on PCA-ELM
  • 作者:王进达 ; 鲁浩 ; 程海彬 ; 李群生 ; 徐剑芸 ; 何海洋
  • 英文作者:Wang Jinda;Lu Hao;Cheng Haibin;Li Qunsheng;Xu Jianyun;He Haiyang;China Airborne Missile Academy;
  • 关键词:神经网络 ; PCA-ELM ; 卡尔曼滤波 ; 组合导航 ; 故障检测 ; 智能化
  • 英文关键词:neural network;;PCA-ELM;;Kalman filter;;integrated navigation;;fault detection;;intelligentization
  • 中文刊名:HKBQ
  • 英文刊名:Aero Weaponry
  • 机构:中国空空导弹研究院;
  • 出版日期:2019-02-01 12:59
  • 出版单位:航空兵器
  • 年:2019
  • 期:v.26;No.309
  • 语种:中文;
  • 页:HKBQ201901014
  • 页数:6
  • CN:01
  • ISSN:41-1228/TJ
  • 分类号:93-98
摘要
针对传统PCA-ELM(主元分析-极限学习机)算法分类效果稳定性差和准确率不高等问题,结合弹载组合导航系统卡尔曼滤波器,提出一种改进PCA-ELM故障检测方法。首先,分析了PCA算法负载矩阵与卡尔曼滤波新息协方差矩阵的关系,构造新的权系数矩阵,并引入极限学习机对权系数矩阵进行参数优化,将参数优化后的负载矩阵进行故障分析。最后,将该算法首次应用于弹载组合导航系统。仿真实验表明,在检测斜坡型故障方面,检测速度和检测正确率均优于传统PCA,MSS(多子集分离法)及AIME(自主完好性外推法)算法。
        In view of the problem of poor stability and low accuracy in the traditional PCA-ELM (principal component analysis-extreme learning machine) algorithm,an improved PCA-ELM fault detection method is proposed by combining the Kalman filter of the missile borne integrated navigation system.Firstly,the relationship between the load matrix of the PCA algorithm and the covariance matrix of the Kalman filter is analyzed. Then,the new weight coefficient matrix is introduced,and the extreme learning machine is introduced to optimize the weight coefficient matrix,and the load matrix is optimized for fault analysis. Finally,the algorithm is applied to the missile borne integrated navigation system for the first time. The simulation experiment shows that the method proposed in this paper is superior to the traditional PCA,MSS and AIME algorithms in the detection speed and detection accuracy.
引文
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