期刊文献+

Model updating for real time dynamic substructures based on UKF algorithm 被引量:3

在线阅读 下载PDF
导出
摘要 Combining the advantages of numerical simulation with experimental testing,real-time dynamic substructure(RTDS)testing provides a new experimental method for the investigation of engineered structures.However,not all unmodeled parts can be physically tested,as testing is often limited by the capacity of the test facility.Model updating is a good option to improve the modeling accuracy for numerical substructures in RTDS.In this study,a model updating method is introduced,which has great performance in describing this nonlinearity.In order to determine the optimal parameters in this model,an Unscented Kalman Filter(UKF)-based algorithm was applied to extract the knowledge contained in the sensors data.All the parameters that need to be identified are listed as the extended state variables,and the identification was achieved via the step-by-step state prediction and state update process.Effectiveness of the proposed method was verified through a group of experimental data,and results showed good agreement.Furthermore,the proposed method was compared with the Extended Kalman Filter(EKF)-based method,and better accuracy was easily found.The proposed parameter identification method has great applicability for structural objects with nonlinear behaviors and could be extended to research in other engineering fields.
出处 《Earthquake Engineering and Engineering Vibration》 SCIE EI CSCD 2020年第2期413-421,共9页 地震工程与工程振动(英文刊)
基金 National Natural Science Foundation of China under Grant Nos.61903009,51978016 and 61673002 Beijing Municipal Education Commission under Grant No.KM201810011005。
  • 相关文献

参考文献1

二级参考文献18

  • 1潘泉,杨峰,叶亮,梁彦,程咏梅.一类非线性滤波器——UKF综述[J].控制与决策,2005,20(5):481-489. 被引量:236
  • 2Koehl A,Rafaralahy H,Boutayeb M,et al.Aerodynamic modelling and experimental identification of a coaxial-rotor UAV[J].Journal of Intelligent and Robotic Systems,2012,68(1):53-68.
  • 3Kumar R,Ganguli R,Omkar S N,et al.Rotorcraft parameter identification from real time flight data[J].Journal of Aircraft,2008,45(1):333-341.
  • 4WANG Xiaodong,ZHAO Xiaoguang,TAN Min.Modeling,identification and robust control of yaw dynamics of small-scale unmanned helicopters[C]//5th International Conference on Natural Computation.Piscataway,NJ,USA:IEEE,2009:273-276.
  • 5Cheng R,Tischler M,Schulein,G.RMAX helicopter state-space model identification for hover and forward-flight[J].Journal of the American Helicopter Society,2006,51(2):202-210.
  • 6Raptis I,Valavanis K.Linear and nonlinear control of small-scale unmanned helicopters[M].Dordrecht,Netherlands:Springer,2011.
  • 7Pamadi B N.Performance,stability,dynamics,and control of airplanes[M].2nd ed.Hampton,Virginia:AIAA,2003.
  • 8Schafroth D M.Aerodynamics,modeling and control of an autonomous micro helicopter[D].Zürich,Switzerland:Swiss Federal Institute of Technology,2010.
  • 9Schafroth D,Bermes C,Bouabdallah S,et al.Modeling,system identification and robust control of a coaxial micro helicopter[J].Control Engineering Practice,2010,18(7):700-711.
  • 10Jategaonkar R V,Plaetschke E.Algorithms for aircraft parameter estimation accounting for process and measurement noise[J].Journal of Aircraft,1989,26(4):360-372.

共引文献2

同被引文献26

引证文献3

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部