This paper investigates the problem of the position and attitude control of quad-rotor UAV. A new simplified model which is more reasonable for some actual cases is derived. Based on the simplified model, a T-S fuzzy state feedback controller to stabilize the attitude of quad-rotor UAV is designed. Proposed control strategy can steer quad-rotor UAV flight with a desired acceleration. In addition, it can guarantee the assumption for simplifying quad-rotor model is reasonable during the flight. Finally, numerical simulations are provided to illustrate the effectiveness of the obtained theoretical results.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    T-S fuzzy control for a quad-rotor UAV


    Beteiligte:
    Mao, Xiang (Autor:in) / Zhang, Hongbin (Autor:in) / Han, Dongfei (Autor:in)


    Erscheinungsdatum :

    2015-07-01


    Format / Umfang :

    250641 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Fuzzy control of quad-rotor in nondeterministic environments

    Sokolov, O. / Hussein, W. / Ushan, V. | Tema Archiv | 2010


    Retractable folding quad rotor

    LI BOCHEN / WANG HONGZHOU / XU XINGGUO et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    The Quad-rotor Rotorcraft

    Castillo, Pedro / Lozano, Rogelio / Dzul, Alejandro E. | Springer Verlag | 2005


    Robust formation control of quad-rotor helicopters

    Pilz, Ulf / Popov, Andrey / Werner, Herbert | Tema Archiv | 2009


    Quad-rotor unmanned aerial vehicle

    XIE XINLIN / LUO WEIBIN / CHEN YUANZHOU et al. | Europäisches Patentamt | 2020

    Freier Zugriff