A control method for controlling a yaw angle γz and a roll angle γx of a vertical take-off aircraft comprising at least two drive groups arranged in opposite side regions of the aircraft so as to be spaced apart from a fuselage of the aircraft is presented. Each drive group comprises at least one first drive unit. The first drive unit is arranged so as to be spaced apart from the fuselage to pivot about a pivot angle α into a horizontal flight position and a vertical flight position.


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    Titel :

    Control method for controlling a yaw angle and a roll angle of a vertical take-off aircraft


    Beteiligte:

    Erscheinungsdatum :

    2024-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    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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    HESSELBARTH JONATHAN | Europäisches Patentamt | 2022

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    Control method for controlling a yaw angle and a roll angle of a vertical take-off aircraft

    HESSELBARTH JONATHAN | Europäisches Patentamt | 2021

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    Control method for controlling a yaw angle and a roll angle of a vertical take-off aircraft

    HESSELBARTH JONATHAN | Europäisches Patentamt | 2020

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    Control method for controlling a yaw angle and a roll angle of a vertical take-off aircraft

    HESSELBARTH JONATHAN | Europäisches Patentamt | 2022

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    CONTROL METHOD FOR CONTROLLING A YAW ANGLE AND A ROLL ANGLE OF A VERTICAL TAKE-OFF AIRCRAFT

    HESSELBARTH JONATHAN | Europäisches Patentamt | 2018

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