The quadcopter is an unmanned aerial vehicle (UAV) suitable for various applications (environmental monitoring, aerial photography, search and rescue, and surveillance, etc.) due to its adaptable mobility. This paper discusses the mathematical modeling and controlling of the quadcopter. The Proportional-Integral-Derivative (PID) controller is used for stabilizing and controlling quadcopters in the presence of external disturbances, including aerodynamic effects, external interference, and wind disturbance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Dynamic Modeling and Control of the Quadcopter Under External Disturbances


    Beteiligte:
    Saif, Md (Autor:in) / Kumar, Sanjay (Autor:in) / Dewan, Lillie (Autor:in)


    Erscheinungsdatum :

    03.05.2024


    Format / Umfang :

    449593 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Lifting-Wing Quadcopter Modeling and Unified Control

    Quan, Quan / Wang, Shuai / Gao, Wenhan | AIAA | 2025


    Modeling and Control of a Tilting Quadcopter

    Ji, Ruihang / Ma, Jie / Sam Ge, Shuzhi | IEEE | 2020


    Lifting-wing Quadcopter Modeling and Unified Control

    Quan, Quan / Shuai, Wang / Wenhan, Gao | ArXiv | 2023

    Freier Zugriff

    QUADCOPTER

    KORNILOV VLADIMIR ALEKSANDROVICH / TUGAENKO VYACHESLAV YUREVICH | Europäisches Patentamt | 2020

    Freier Zugriff

    Modeling, control, and simulation of a quadcopter

    Atthota, Ravi Teja | BASE | 2016

    Freier Zugriff