A flight control system for controlling an aircraft during a variable engine thrust takeoff operation operative to perform a method including calculating a calculated acceleration in response to a takeoff distance and a selection of a variable engine thrust takeoff mode, generating an initial thrust control signal in response to the calculated acceleration, controlling a thrust of an aircraft engine in response to the initial thrust control signal, measuring a measured acceleration of the aircraft, generating an updated thrust control signal in response to a difference between the calculated acceleration and the measured acceleration, and controlling the thrust of the aircraft engine in response to the updated thrust control signal.
CONTROLLERS AND AIRCRAFT WITH VARIABLE ENGINE THRUST TAKEOFF SYSTEM
REGLER UND FLUGZEUG MIT VARIABLEM MOTORSCHUBSTARTSYSTEM
ORGANES DE COMMANDE ET AÉRONEF DOTÉ D'UN SYSTÈME DE DÉCOLLAGE À POUSSÉE MOTEUR VARIABLE
2024-04-03
Patent
Elektronische Ressource
Englisch
CONTROLLERS AND AIRCRAFT WITH VARIABLE ENGINE THRUST TAKEOFF SYSTEM
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