A method and control system for controlling the thrust of an aircraft. A thrust request is input into a controller and the controller determines throttle, governor, and RPM setpoints to meet the input thrust request. The controller can determine minimum and maximum available thrust limits of the engine and can modify any of the setpoints if any setpoint violates the available thrust limit.
Direct Thrust Control Method for Aircraft Thruster
13.03.2025
Patent
Elektronische Ressource
Englisch