Four rotor unmanned aerial vehicle (UAV) control of the bottom of society, this article is based on the cascade PID algorithm with the improved design and double closed-loop position controller and attitude controller, the outer ring of position and attitude controller adopts hyperbolic tangent function as the position loop, position controller of the PID as the inner ring speed ring, inner ring USES the intelligent PID control algorithm as angular velocity loop. In this paper, detailed steps of UAV modelling are given, and experiments are carried out on ROS, PX4 and Prometheus. In the experiments, the algorithm is verified and compared with traditional PID and cascade PID control algorithms. The experimental results show that the double closed-loop intelligent controller designed in this paper can ensure the flight stability of the quadrotor UAV and the accuracy of the trajectory tracking, and has a certain anti-interference ability.


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    Titel :

    Trajectory tracking control of quadrotor UAV based on T265 positioning


    Beteiligte:
    Bai, Lvzhao (Autor:in) / Liang, Jianshu (Autor:in) / Zhang, LinLin (Autor:in)

    Kongress:

    International Conference on Algorithms, Microchips and Network Applications ; 2022 ; Zhuhai,China


    Erschienen in:

    Proc. SPIE ; 12176


    Erscheinungsdatum :

    06.05.2022





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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