Aiming at the problem that the stability of a quadrotor with a suspension system is affected by the swing of the slung-load due to the wind and so on, a nonlinear control method is proposed to reduce the influence of the slung-load on the flight of the quadrotor. Firstly, the mathematical model of the suspension system of the quadrotor is established by using Hamilton principle and Lagrange formula; secondly, the adaptive backstepping controller is designed to control the position and attitude of the quadrotor, and eliminate the steady-state error of the system and enhance the robustness of the system; thirdly, the integral backstepping controller is designed to reduce the swing of the slung-load; finally, the simulation experiment system of the quadrotor with a slung-load suspension is built. The simulation experiment results verify the validity and accuracy of mathematical model and designed controller.


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    Titel :

    Adaptive Integral Backstepping Control for a Quadrotor with Suspended Flight


    Beteiligte:
    Xinyu, Chen (Autor:in) / Yongsheng, Zhao (Autor:in) / Yunsheng, Fan (Autor:in)


    Erscheinungsdatum :

    01.09.2020


    Format / Umfang :

    251747 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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