FIELD: aircraft engineering.
SUBSTANCE: proposed multi-task control data system comprises the following components. TV signal converter unit, external memory, data control field, signal concentrator unit, onboard computer system, data exchange channel, I/O and exchange control unit, indication data generation unit, general-aircraft control unit, navigation computation unit, electronic countermeasure control unit, mission data base, low-altitude flight support unit, team flight support unit, aircraft control unit, recorder control unit, fighting capability control unit, mode control unit, terrain digital map control unit, electromagnetic compatibility control unit, TV signal conversion control unit, maintenance unit, serviceability indication and control unit, mating equipment, switching unit, data exchange network channel.
EFFECT: higher fault tolerance, expanded operating capabilities.
4 cl, 1 dwg
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