FIELD: aviation instrumentation engineering. SUBSTANCE: proposed complex includes digital computer system, information exchange with three multiplex channels, aircraft complex control system, armament control system, complex electronic display, control and aiming system, general aircraft equipment control system, on-board monitoring system, power supply system and power plant control system. Complex is also provided with means for preliminary processing of signals of sensors for forming single information field. In case of failure of computer control system, control is shifted to general aircraft equipment control system. Multi-functional colored displays are interchangeable; they furnish complete pilotage and navigational information in case of failure of one of them. In case of failure of two digital computers of computer system and general aircraft equipment control system, complex is shifted to manual control. EFFECT: enhanced operational reliability. 3 cl, 1 dwg
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Authors
Dates
2003-11-10—Published
2002-11-11—Filed