Aspects of this present disclosure relate to flight control of electric aircrafts and other vehicles. In one embodiment, an aircraft is disclosed comprising: a fuselage; one or more flight control computers configured to provide control signals; four sets of electrically powered propellers, wherein a first set is disposed forward of a second set both on one side of the fuselage, and wherein a third set is disposed forward of a fourth set both on another side of the fuselage; and a plurality of electrical buses; wherein the one or more flight control computers are configured to provide control signals via one electrical bus of the plurality of electrical buses to: at least one of the first set of propellers and at least one of the fourth set of propellers; and to at least one of the third set of propellers and at least one of the second set of propellers.


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    Title :

    SYSTEMS AND METHODS FOR FLIGHT CONTROL OF EVTOL AIRCRAFT


    Additional title:

    SYSTEME UND VERFAHREN ZUR FLUGSTEUERUNG EINES EVTOL-FLUGZEUGS
    SYSTÈMES ET PROCÉDÉS DE COMMANDE DE VOL D'AÉRONEF ÉLECTRIQUE À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX (EVTOL)



    Publication date :

    2025-05-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64U



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