According to one embodiment, a rotorcraft includes rotors (3), a fuselage (2), at least three rods (4), at least one load sensor (5) and a control device (6). The rotors (3) obtain lift. The fuselage (2) is coupled to the rotors (3). The at least three rods (4) support the fuselage (2). The at least one load sensor (5) detects loads (F1, F2, F3, F4) applied on the at least three rods (4). The control device (6) automatically controls the rotors (3) so that measured values of the loads (F1, F2, F3, F4) detected by the at least one load sensor (5) are brought to targeted values of the loads (F1, F2, F3, F4).


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    Title :

    ROTORCRAFT AND METHOD OF CONTROLLING ROTORCRAFT


    Additional title:

    DREHFLÜGLER UND VERFAHREN ZUR STEUERUNG DES DREHFLÜGLERS
    GIRAVION ET PROCÉDÉ DE COMMANDE D'UN GIRAVION


    Contributors:

    Publication date :

    2023-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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