In order to enhance the safety of the aircraft’s take-off and landing process, it is necessary to control the shimmy phenomenon of the aircraft wheel. In this situation, the magnetor-rheological damper is used to reduce the wheel shimmy, several years. This paper, firstly, builds the model of the aircraft landing gear and magneto-rheological damper is established. Then the linear active disturbance rejection control technique (LADRC) method is used to control the shimmy and compared with the PID method. The simulation results show that LADRC can control the wheel shimmy well. And when the aircraft speed is high, the stabilization time and the amplitude are smaller than PID.


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    Title :

    Study on Magneto-rheological Damper Control of Aircraft Landing Gear Based on LADRC


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Jia, Yingmin (editor) / Zhang, Weicun (editor) / Fu, Yongling (editor) / Yu, Zhiyuan (editor) / Zheng, Song (editor) / Dong, Lei (author) / Chen, Zengqiang (author) / Sun, Mingwei (author) / Sun, Qinglin (author) / Yu, ZhenPing (author)


    Publication date :

    2021-10-07


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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