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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    Title :

    STEUERUNGSVERFAHREN ZUR STEUERUNG EINES GIER- UND EINES ROLLWINKELS EINES SENKRECHT STARTENDEN FLUGZEUGS


    Additional title:

    CONTROL METHOD FOR CONTROLLING A YAW ANGLE AND A ROLL ANGLE OF AN AIRCRAFT THAT TAKES OFF VERTICALLY
    PROCÉDÉ DE COMMANDE POUR LA COMMANDE D'UN ANGLE DE LACET ET DE ROULIS D'UN AVION À DÉMARRAGE VERTICAL


    Contributors:

    Publication date :

    2021-11-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    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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