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.
SYSTEMS AND METHODS FOR FLIGHT CONTROL OF EVTOL AIRCRAFT
SYSTEME UND VERFAHREN ZUR FLUGSTEUERUNG EINES EVTOL-FLUGZEUGS
SYSTÈMES ET PROCÉDÉS DE COMMANDE DE VOL D'AÉRONEF ÉLECTRIQUE À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX (EVTOL)
2025-05-28
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR FLIGHT CONTROL OF EVTOL AIRCRAFT
European Patent Office | 2024
|Systems and methods for flight control of EVTOL aircraft
European Patent Office | 2024
|SYSTEMS AND METHODS FOR FLIGHT CONTROL OF EVTOL AIRCRAFT
European Patent Office | 2024
|