Provided is a control method of a drone with a multiple DOF flight mode according to the present invention. The drone may include a fuselage in which a battery is mounted and a forward direction is set in an x-axis, a plurality of rotors disposed about the fuselage in four or more, each rotational axis of which is aligned in a z-axis direction, an x-axis tilting mechanism unit formed to tilt the plurality of rotors about an axis parallel to the x-axis, a y-axis tilting mechanism unit formed to tilt the plurality of rotors about an axis parallel to the y-axis, a first drive motor unit driving the y-axis tilting mechanism unit, a second drive motor unit guiding the x-axis tilting mechanism unit, and a control unit configured to implement a plurality of flight modes by controlling the first rotor, the second rotor, the third rotor, the fourth rotor, the first drive motor unit, and the second drive motor unit.


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    Titel :

    METHOD FOR CONTROLLING DRONE HAVING MULTI-DEGREE-OF-FREEDOM FLIGHT MODE


    Weitere Titelangaben:

    VERFAHREN ZUR STEUERUNG EINER DROHNE MIT FLUGMODUS MIT MEHREREN FREIHEITSGRADEN
    PROCÉDÉ DE COMMANDE D'UN DRONE DOTÉ D'UN MODE DE VOL À DEGRÉS DE LIBERTÉ MULTIPLES


    Beteiligte:
    LEE SANG HYUN (Autor:in)

    Erscheinungsdatum :

    10.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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