Helicopters are theoretically unstable aircraft, but they are widely used in many fields, because of their high maneuverability. The goal of this paper is to build two different real-time control systems for vehicle stabilization and for control to track the desired points or paths. This control system was designed in Matlab/Simulink to control a single RC coaxial helicopter. In the system, four pilot inputs (the desired thrust and the desired roll, pitch, and yaw rates) were calculated from LQR and H∞ control system, and those signals were sent to the RC helicopter's microcontroller using the RC transmitter and receiver.


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    Title :

    Modeling of real-time flight control system for small coaxial helicopter


    Contributors:


    Publication date :

    2014-03-01


    Size :

    1641858 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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