Today's World is getting more addicted of robot's applications and autonomous vehicles due to their improved performance and higher accuracy. A quad copter belongs to the same family due to flight stability, light weight, durability in flight, and accurate maneuverability. This research is based on design of dynamics controller of a quadcopter during hovering manuever using PID and SMC (sliding mode control) control techniques. The simulation results show improved response as compared to the previous studies under the same input conditions.


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    Title :

    Control and stability analysis of quadcopter


    Contributors:
    Katiar, Asma (author) / Rashdi, Rabbia (author) / Ali, Zeeshan (author) / Baig, Urooj (author)


    Publication date :

    2018-03-01


    Size :

    280530 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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