This paper aims to present data analysis of quadcopter dynamic attitude on a circular trajectory, specifically by comparing the modeling results of conventional Proportional Integral Derivative (PID) and Fuzzy-PID controllers. Simulations of attitude stability with both control systems were done using Simulink toolbox from Matlab so the identification of each control system is clearly seen. Each control system algorithm related to roll and pitch angles which affects the horizontal movement on a circular trajectory is explained in detail. The outcome of each tuning variable of both control systems on the output movement is observable while the error magnitude can be compared with the reference angles. To obtain a deeper analysis, wind disturbance on each axis was added to the model, thus differences between each control system are more recognizable. According to simulation results, the Fuzzy-PID controller has relatively smaller errors than the PID controller and has a better capability to reject disturbances. The scaling factors of gain values of the two controllers also play a vital role in their design.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PID and Fuzzy-PID Control Model for Quadcopter Attitude with Disturbance Parameter


    Beteiligte:

    Erscheinungsdatum :

    29.06.2017


    Anmerkungen:

    doi:10.15837/ijccc.2017.4.2962
    INTERNATIONAL JOURNAL OF COMPUTERS COMMUNICATIONS & CONTROL; Vol 12 No 4 (2017): International Journal of Computers Communications & Control (August); 519-532 ; 1841-9844 ; 1841-9836 ; 10.15837/ijccc.2017.4



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Klassifikation :

    DDC:    629





    Bounded Gradient Attitude Control of a Quadcopter

    G, Jesse Kyle G. / Diaz-Tellez, J. / Estevez-Carreon, J. et al. | IEEE | 2022


    Quadcopter UAV attitude control based on DDPG

    HUANG Xijie | DOAJ | 2024

    Freier Zugriff

    Control System for Quadcopter UAV based SMC-RBFNN with External Disturbance

    Sari Delima Palwa / Darwito Purwadi Agus | DOAJ | 2024

    Freier Zugriff

    Attitude Free Position Control of a Quadcopter using Dynamic Inversion

    Wang, Jian / Bierling, Thomas / Achtelik, Michael et al. | AIAA | 2011