A system for piloting an aircraft includes a throttle, a flight parameter sensor system, and an engine calculator controlling thrust parameters of an engine of the aircraft. The piloting system includes a flight control unit connected to the engine calculator, the sensors and the throttle. The flight control unit generates a thrust control vector from a flight control law and sends a digital signal including the generated thrust control vector to the engine calculator. The engine calculator controlling said thrust parameters of the engine depending on the generated thrust control vector received.
SYSTÈME DE PILOTAGE D AÉRONEF, AÉRONEF ET PROCÉDÉ ASSOCIÉS
DEVICE FOR PILOTING AN AIRCRAFT, ASSOCIATED AIRCRAFT AND METHOD
VORRICHTUNG ZUM STEUERN EINES LUFTFAHRZEUGS, ENTSPRECHENDES LUFTFAHRZEUG UND VERFAHREN
2024-03-13
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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