Recently, R/C helicopter is used in fields of aerial photography and aerial investigation. But helicopter rotor blades are not covered, and the thrust is generated by high rotational speed. Thus R/C helicopter has a high risk of damage. In this study, we developed a new flying object using ducted fans instead of rotor blades. At first, PD control was employed for pitch and roll attitude control, but it caused steady-state error. Moreover PI-D control was used instead of PD control, and it reduced the steady-state error. We succeeded to achieve stable hovering by three-axes (roll, pitch, and yaw axes) attitude control.


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    Titel :

    Control of Ducted Fan Flying Object Using Thrust Vectoring


    Weitere Titelangaben:

    Intelligent Systems, Cont. (formerly: Microprocessor)


    Beteiligte:
    Nonami, Kenzo (Herausgeber:in) / Kartidjo, Muljowidodo (Herausgeber:in) / Yoon, Kwang-Joon (Herausgeber:in) / Budiyono, Agus (Herausgeber:in) / Miwa, Masafumi (Autor:in) / Shigematsu, Yuki (Autor:in) / Yamashita, Takashi (Autor:in)


    Erscheinungsdatum :

    16.03.2013


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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