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低速风洞试验模型振动主动控制技术

  • Lujun Chen
  • , Binghui Che
  • , Yong Huang
  • , Minggang Zhu
  • , Tiejun Yang
  • , Chengwen Zhong
  • Northwestern Polytechnical University Xian
  • China Aerodynamics Research and Development Center
  • Harbin Engineering University

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

In a wind tunnel test, the tail model support system of cantilever beam structure will produce vibration under the wind load, which may threaten test safety and affect test results. In order to suppress the vibration of the model and support system, an active vibration control method is studied and applied. Among them, the actuator of suppression system adopts piezoelectric material, and the control system is based on adaptive internal model control algorithm.This paper analyzes the structure and working principle of the adaptive internal model control algorithm, and introduces the model parameter identification in training mode and the adaptive adjustment process of control parameters in experimental mode. A control system based on the adaptive internal model control algorithm is established. A signal generator is used to simulate the excitation of the system on the ground simulation platform. The control algorithm is verified as the input of the control system. Combined with the wind tunnel test, the control effect of the system is verified under actual conditions. The results show that the active vibration control system based on adaptive internal model control algorithm can reduce the vibration by more than 70%.

投稿的翻译标题Active Vibration Control Method for Test Model in Low Speed Wind Tunnel
源语言繁体中文
页(从-至)591-597
页数7
期刊Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics
53
4
DOI
出版状态已出版 - 8月 2021

关键词

  • Adaptive internal mode control
  • Piezoelectric ceramics
  • Vibration control
  • Wind tunnel

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