FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises the following extra units: control board as mixer of audio signals from first and second astatic radio range mikes for transmission and registration in front and rear onboard multipurpose protected integrators and as Ethernet network commutator. Whereto connected are front and rear multipurpose protected onboard integrators, video camera, combined flight data acquisition unit and wireless data transfer unit. It has at least one high-speed data exchange channel to transmit video signal from multipurpose indicators to combined flight data acquisition unit and, further, to front and rear onboard multipurpose protected integrators via onboard circuit.
EFFECT: higher reliability and perfected control.
6 cl, 1 dwg
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