So as to deal with the poor static stability, strong nonlinear aerodynamic parameters and serious coupling of control rudder surface of flying-wing UAV. On the basis of the theory of active disturbance rejection control (ADRC), this attitude controller consists of two parts, which are outer angle controller and inner angle velocity controller. The simulation displays that this attitude controller shows advantageous control effect and strong robustness.


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    Title :

    Attitude Control for Flying-Wing UAV Based on Active Disturbance Rejection Control


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Shen, Boyuan (author) / Huang, Xi (author) / Li, Qingxian (author) / Qi, Pengyuan (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Publication date :

    2025-03-04


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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