A method of assisting a pilot (26) in controlling an aircraft (20) having a plurality of lift-generating propulsion devices (21), the method comprising the following method steps, calculation of momentary control limitations (3, 4) for each control of the aircraft around its roll axis (x), control of the aircraft around its pitch axis (y), control of the aircraft around its yaw axis (z) and a control of the total thrust T of all the propulsion devices (21), and display of the calculated control limitations (3, 4) by a display device (29).
METHOD FOR ASSISTING A PILOT IN CONTROLLING AN AIRCRAFT, ASSISTANCE SYSTEM FOR AN AIRCRAFT PILOT, AND AIRCRAFT
VERFAHREN ZUR UNTERSTÜTZUNG EINES PILOTEN BEI DER STEUERUNG EINES FLUGZEUGS, ASSISTENZSYSTEM FÜR EINEN PILOTEN EINES FLUGZEUGS UND FLUGZEUG
PROCÉDÉ D'ASSISTANCE D'UN PILOTE POUR COMMANDER UN AÉRONEF, SYSTÈME D'ASSISTANCE POUR UN PILOTE D'AÉRONEF ET AÉRONEF
2025-05-14
Patent
Electronic Resource
English
European Patent Office | 2025
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