南京航空航天大学学报（英文版）2025，Vol.42Issue(2)：250-260,11.DOI:10.16356/j.1005-1120.2025.02.009
基于卡尔曼滤波的连续系统结构动响应重构方法
A Structural Dynamic Response Reconstruction Method for Continuous System Based on Kalman Filter
摘要
Abstract
The structural dynamic response reconstruction technology can extract unmeasured information from limited measured data,significantly impacting vibration control,load identification,parameter identification,fault diagnosis,and related fields.This paper proposes a dynamic response reconstruction method based on the Kalman filter,which simultaneously identifies external excitation and reconstructs dynamic responses at unmeasured positions.The weighted least squares method determines the load weighting matrix for excitation identification,while the minimum variance unbiased estimation determines the Kalman filter gain.The excitation prediction Kalman filter is constructed through time,excitation,and measurement updates.Subsequently,the response at the target point is reconstructed using the state vector,observation matrix,and excitation influence matrix obtained through the excitation prediction Kalman filter algorithm.An algorithm for reconstructing responses in continuous system using the excitation prediction Kalman filtering algorithm in modal space is derived.The proposed structural dynamic response reconstruction method evaluates the response reconstruction and the load identification performance under various load types and errors through simulation examples.Results demonstrate the accurate excitation identification under different load conditions and simultaneous reconstruction of target point responses,verifying the feasibility and reliability of the proposed method.关键词
动载荷识别/结构响应重建/激励识别/卡尔曼滤波器/连续系统Key words
dynamic load identification/structural response reconstruction/excitation identification/Kalman filter/continuous system引用本文复制引用
李鸿秋,姜金辉,MOHAMED M Shadi..基于卡尔曼滤波的连续系统结构动响应重构方法[J].南京航空航天大学学报（英文版）,2025,42(2):250-260,11.基金项目
This work was supported by the Na-tional Natural Science Foundation of China(Nos.12372066,U23B6009,52171261),the Aeronautical Sci-ence Fund(No.20240013052002),and the Qing Lan Project. （Nos.12372066,U23B6009,52171261）
