Disclosed are a quad-rotor control system and a control method thereof. The present invention uses a nine axis inertial navigation device based on a quad-rotor with four motors to measure the posture and motion of a flying object, and controls a modularized controller to improve the performance and efficiency of a system. Thereby, the stability of quad-rotor is increased. The adjustment/control of the quad-rotor can be easily carried out. Especially, the performance of a hovering can be improved.


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    Titel :

    QUAD-ROTOR POSITION CONTROL SYSTEM AND CONTROL METHOD THEREOF


    Beteiligte:
    HA YOUNG GUK (Autor:in) / JEONG HYEOK JUNE (Autor:in)

    Erscheinungsdatum :

    23.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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