The mathematical model of the miniature unmanned helicopter was established, the parameters involved in the dynamics model were identified by the prediction-error method. The H∞ loop shaping robust control approach was utilized for the attitude control of the miniature unmanned helicopter. The results of the frequency analysis showed that the control system had good shape and ideal bandwidth. The simulation results showed the strong robustness. The flight test verified the feasibility and the effectiveness of the modeling and the control methods.


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    Titel :

    Modeling and attitude control of the miniature unmanned helicopter


    Beteiligte:
    Chen, Xianxiang (Autor:in) / Liu, Ying (Autor:in) / Hu, Xiongwen (Autor:in) / Qian, Yi (Autor:in) / Wang, Jinhua (Autor:in)


    Erscheinungsdatum :

    01.07.2013


    Format / Umfang :

    173756 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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