TWIN-ENGINED AIRCRAFT CONTROL SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2084375 C1

FIELD: aircraft control systems. SUBSTANCE: control system includes longitudinal and transversal stick position sensors, control surface position sensor, pitch-rate and roll-rate pick-ups, pitch and yaw channels, starboard and port engine electrical adders and electrohydraulic actuators, booster device, electrical mechanisms-adders and manual starboard and port engine thrust control systems. EFFECT: enhanced reliability. 4 dwg

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RU 2 084 375 C1

Authors

Simonov M.P.

Nikitin N.F.

Shenfinkel' Ju.I.

Kalibabchuk O.G.

Moskalev P.B.

Dates

1997-07-20—Published

1995-02-28—Filed