 KSU-35 INTEGRATED FLIGHT CONTROL SYSTEMThe digital redundant integrated flight control system was developed for equipping the Su-35 aircraft . It performs the following functions:
• Manual fly-by-wire control of the aircraft control surfaces via hydraulic actuators according to pilot commands and flight parameter sensor signals.
• Manual fly-by-wire control of engine thrust and thrust vector via engine nozzle swiveling parts.
• Automatic and flight-director control of the aircraft.
• Object movement control on the ground by means of the nose landing gear wheel (swiveling part) turn and the main landing gear wheels braking with anti-skidding .
• Measuring, calculating and delivering to consumers information about current values of altitude-speed flight parameters.
• Defines the maximum permissible values of flight parameters in accordance with information about current load and fuelling, flight condition and serviceability of interactive systems.
• Generation and delivery of information to external systems in order to report about flight parameters approaching the maximum permissible values and to active automatic prevention of the flight parameters spillover.
• Automatic obstacle collision avoidance (earth surface, other aircraft, armaments, its own air armaments’ fragments and others) by signals from the information management system of an airborne equipment complex.
• Support of aircraft stability and controllability during in-flight refueling.
• Automatic pre-start check of serviceability and continuous in-flight monitoring
with failure localization and results output.
Specifications
Weight, kg no more than 73
Power consumption, W:....750
| 
