VORRICHTUNG ZUR STEUERKRAFTSTABILISIERUNG BEI EINEM DREHFLUEGELFLUGZEUG.

摘要

The method and system allows a sional to oass to a servo drive (3) acting on a spring (2) engaging the control column roughly opposite the control rod (4) linked to the control column. The signal depends on flight speed and increases at least above a given threshold with increasing flight speed. A feedback signal (R) is added to the flight-speed signal (S) and varies in the same sense as the servo drive's measured travel.