In the process of unmanned helicopter landing, when gears are touching down, rotation speed of main rotor and collective will both stay at high level, which threatens landing safety severely. This paper proposes a control design aimed at the situation, and then make a proof and simulation.


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    Titel :

    On safe landing control technology of unmanned helicopter


    Beteiligte:
    Wang Lu, (Autor:in) / Yao Weili, (Autor:in) / Zhang Meng, (Autor:in) / Huang Yimin, (Autor:in)


    Erscheinungsdatum :

    2016-08-01


    Format / Umfang :

    370498 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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