Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.
AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR
2021-07-22
Patent
Electronic Resource
English
Aircraft pitch control system with electronically geared elevator
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