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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    Titel :

    Control and stability analysis of quadcopter


    Beteiligte:
    Katiar, Asma (Autor:in) / Rashdi, Rabbia (Autor:in) / Ali, Zeeshan (Autor:in) / Baig, Urooj (Autor:in)


    Erscheinungsdatum :

    01.03.2018


    Format / Umfang :

    280530 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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