With Power Amplification TRIZ Cases

Shared consolidation of flight parameters lets redundant flight control computers compute one flight order for both command and monitor roles.

Buffered detent-state sensing uses trim data to detect pilot override in rotorcraft FBW control and prevent rapid state cycling.

Redundant inner and outer control loops with electromechanical braking stabilize helicopter flight and reduce pilot workload without hydraulics.

A stick-mounted attitude hold button and fine tracking quickener help large aircraft capture trim quickly and track tanker drogues more precisely.