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
LUFTFAHRZEUGPITCHREGELUNGSSYSTEM MIT ELEKTRONISCH ÜBERSETZTEM HÖHENRUDER
SYSTÈME DE CONTRÔLE D'AÉRONEF EN TANGAGE COMPRENANT UN ÉLÉVATEUR AGENCÉ PAR UN MOTORÉDUCTEUR ÉLECTRONIQUE
01.07.2020
Patent
Elektronische Ressource
Englisch
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