INFORMATION AND AERONAUTICAL EQUIPMENT CONTROL COMPLEX SYSTEM Russian patent published in 2013 - IPC G06F11/00 

FIELD: aircraft engineering.

SUBSTANCE: proposed device comprises health sensors with their three outputs connected to complex warning information system connected with parameters registration magnetic system, and indication unit. Besides, device comprises pulse counter, channel number selector, register unit and logical function computation unit. Note here that channel and frame pulses from parameters registration magnetic system are connected to pulse counter. Third output of said system is connected via data bus to four inputs of register unit. Four other inputs of said register unit are connected to channel number selector outputs. Six inputs of said selector are connected to appropriate pulse counter outputs. Four data inputs of logical function computation unit are connected via data bus to appropriate outputs of register unit. Fifth data input is connected via bus to second data output of health sensors while four outputs of logical function computation unit are connected to appropriate inputs of indication unit.

EFFECT: minimising crew faults.

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