Attitude control of a quadrotor unmanned aerial vehicle is still a hot research topic. Active disturbance rejection control attracts more attention recently. This paper takes into account the dynamics of the propulsion system and designs a higher-order active disturbance rejection controller with compensation of partial model information. Simulation and experiment demonstrate that the proposed controller presents better performance and robustness compared with the traditional active disturbance rej ection controller.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Quadrotor Attitude Control Based on Modified Linear Active Disturbance Rejection Control


    Contributors:
    Wang, Biao (author) / Tang, Chaoying (author) / Yao, Zhennan (author) / Yang, Feng (author)


    Publication date :

    2024-06-18


    Size :

    928144 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Error-Based Active Disturbance Rejection Altitude/Attitude Control of a Quadrotor UAV

    Stankovic, Momir / Madonski, Rafal / Manojlovic, Stojadin et al. | TIBKAT | 2020



    Disturbance Rejection Attitude Control for a Quadrotor: Theory and Experiment

    Li Ding / Qing He / Chengjun Wang et al. | DOAJ | 2021

    Free access