An efficient and safe landing procedure for an aircraft holds significance across economic, operational, and strategic considerations. Achieving the shortest possible landing distance without skidding necessitates a variable braking force that consistently matches the friction force. Thus, the control strategy of the Anti-skid Braking System (ABS) must encompass the ability to address pronounced nonlinearity and substantial unpredictable disturbances, while also regulating the wheel slip ratio to ensure a stable braking process. This study introduces the application of the Active Disturbance Rejection Control Technique to the anti-skid braking system. The proposed control algorithm guarantees that the closed-loop system operates within the vicinity of the peak point of the stable region on the friction curve. This optimization significantly enhances both braking performance and overall safety.


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    Title :

    Aircraft Anti-Skid Braking Nonlinear Control Based on ADRC


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Jing, Xingjian (editor) / Ding, Hu (editor) / Ji, Jinchen (editor) / Yurchenko, Daniil (editor) / Yu, FengRui (author) / Zou, Jingting (author) / Chen, Xinmin (author) / Lin, Yue (author) / Yu, Feifan (author)

    Conference:

    The International Conference on Applied Nonlinear Dynamics, Vibration and Control ; 2023 ; Kowloon, Hong Kong December 04, 2023 - December 06, 2023



    Publication date :

    2024-02-11


    Size :

    12 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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