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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2019, Vol. 40 ›› Issue (8): 222931-222931.doi: 10.7527/S1000-6893.2019.22931

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

Online identification of time-varying structural modal parameters combined with offline knowledge

YUE Zhenjiang1, LIU Li1,2, YU Lei1, KANG Jie1   

  1. 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;
    2. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing Institute of Technology, Beijing 100081, China
  • Received:2019-01-22 Revised:2019-02-25 Online:2019-08-15 Published:2019-04-17

Abstract: The online acquisition of modal parameters of aircraft structures is of great significance for efficient and reliable operation of the aircraft. The traditional modal parameter identification methods for time-varying structures have problems such as more false results and the poor ability to resist extreme outliers in measured data, becoming difficult to effectively apply to online processes. To solve these problems, an online identification model of time-varying structural modal parameters based on long short-term memory networks is established. For a given time-varying structures, prior information is introduced offline through the data set construction process, and the characteristics of the model are utilized to effectively improve the reliability of the online identification application. The experimental results show that compared with the traditional identification method, the proposed online identification model can effectively alleviate the problem of false results and ensure the continuity of identification results. The α stable distribution model is used to model the impulse noise, verifying the robustness of the online identification model that contains extreme outliers in measured data due to accidental factors.

Key words: time varying structure, modal identification, online, deep learning, spurious modes, impulse noise

CLC Number: