FIELD: physics; control.
SUBSTANCE: invention relates to aerospace instrument making and specifically to systems for controlling and indicating the state of an aircraft. The aircraft information-control system has an information-control field, an onboard digital computer system, an input-output and exchange control unit, a unit for setting pilot-navigation parametres and a flight mission database. The system also has a signal concentrator unit, a unit for generating and integrating display data and receiving control input, a unit for controlling and monitoring general aircraft equipment, an electronic countermeasure control unit, a unit for enabling low-altitude flying, a unit for enabling group aircraft navigation, a unit for controlling recording on objective control apparatus and a mode control unit.
EFFECT: broader functional capabilities.
4 cl, 1 dwg
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