CS for Helicopter

KSU-A integrated flight control system

Thе digital redundant integrated flight control system was developed for equipping the Ansat helicopter. It provides automatic and manual helicopter control by means of control levers and electrohydraulic actuators, as well as replaces the mechanical control linkage with an electrical (fly-by-wire) one and realizes following functions:

VTU Trajectory Control Computers

The VTU-123 trajectory control computer is an additional device that together with the director-control system computer, autopilot and trim mechanisms provides the automatic trajectory control of the Mi-172 helicopter and its modifications by roll, pitch, yaw and collective channels during the flight on heading, landing approach, vertical and horizontal maneuvers, which essentially reduces the crew work load.