The method of forming a fault-tolerant integrated control system (KSU) and fault-tolerant KSU

摘要

FIELD: aviation.SUBSTANCE: in each pilot's control station the system contains a stick with quadruplex-redundant stick position sensors (SPS) in the number of control channels (roll, pitch, yaw), a control panel, redundant computers (RC) of robot-control system, quadruplex-redundant RC of remote control systems, quadruplex-redundant integrated sensor unit, quadruplex-redundant backup navigation unit, three quadruplex-redundant drive control unit, drives, the number of which is determined by the number of the aircraft control surfaces and the required redundancy level.EFFECT: increase of survivability, reliability and fail-safety of the system.18 cl, 6 dwg