Aircraft pitch control systems and methods are disclosed. In one exemplary embodiment, an aircraft pitch control system comprises a movable horizontal stabilizer and an elevator movably coupled to the horizontal stabilizer. The elevator is electronically geared to the horizontal stabilizer.
AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR
2022-03-31
Patent
Electronic Resource
English
AIRCRAFT PITCH CONTROL SYSTEM WITH ELECTRONICALLY GEARED ELEVATOR
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