A method converts an aircraft takeoff trim setting that would be a function of several parameters to a value that is a function of CG position only. In this way, it is possible to create a direct simple equivalence between Stabilizer angle and CG. The equivalent CG can be presented in real time to the pilot.
ENHANCED TAKEOFF TRIM INDICATION
2019-02-14
Patent
Electronic Resource
English
LONGITUDINAL TRIM CONTROL MOVEMENT DURING TAKEOFF ROTATION
European Patent Office | 2023
|LONGITUDINAL TRIM CONTROL MOVEMENT DURING TAKEOFF ROTATION
European Patent Office | 2021
|