A flight control system of an aircraft and a flight control method of the aircraft are provided in which the overrunning an operation limitation on a flight condition can be prevented even when a pilot operates a flight control device fast. The flight control system of the aircraft includes a flight control device; a sensor configured to detect a first parameter changed based on a flight condition of the aircraft; a limitation flight control position calculating section configured to calculate a limitation flight control position of the flight control device when the first parameter reaches a limitation value, based on the first parameter; a reaction force generating actuator configured to change a reaction force which the pilot receives when carrying out a flight control input to the flight control device, in response to a reaction force generating command generated based on the flight control position of the flight control device and the limitation flight control position; an inner loop command calculating section configured to generate an inner loop command based on the flight control position; and a control surface actuator configured to drive a control surface of the aircraft based on the flight control position and the inner loop command.
AIRCRAFT FLIGHT CONTROL SYSTEM
FLUGZEUGFLUGSTEUERUNGSSYSTEM
SYSTÈME DE COMMANDE DE VOL D'AÉRONEF
30.05.2018
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2022
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British Library Conference Proceedings | 2021
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