This paper presents the results of the first stage of creating a multi-rotor unmanned aerial vehicle (UAV) simulation model in MATLAB Simulink. A quadcopter mechanical model based on Simscape Multibody library elements was developed. In addition, an angular position and flight altitude control model based on proportional-integral derivative (PID) controllers was designed using the standard Simulink libraries.


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    Title :

    Simulink-based Quadcopter Control System Model




    Publication date :

    2020-12-10


    Size :

    1017981 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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