Full authority fly-by-wire pedal system

Aeronautics and astronautics – Aircraft control – Pilot operated

Reexamination Certificate

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Details

C244S220000, C074S512000, C074S560000, C074S562000

Reexamination Certificate

active

07874526

ABSTRACT:
A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.

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