AIRCRAFT ONBOARD HARDWARE EXPERT-CONTROL SYSTEM Russian patent published in 2014 - IPC G05B23/00 G06F11/26 

FIELD: aircraft engineering.

SUBSTANCE: proposed system comprises tolerance unit (TU), output completeness unit (OCU) and aircraft hardware control system with data transducer subsystem. Said units and system are connected with network of local computation circuit (LCC) connected via cell systems with network of nuclei 9. Outputs of the latter are connected with input of input unit 12, inputs of training unit 11 and tolerance unit 13. Second input of TU 13 is connected with the input of processor 16. Output of said TU 13 is connected with second input of input unit 12. Input of OCU 21 is connected with output of MLV 20. First output of OCU 21 is connected with first input of decision-making unit 17. Second output is connected with interpretation unit 22 connected in series with communication unit 18 and user's terminal 14.

EFFECT: higher efficiency of diagnostics for logical conclusion making.

1 dwg