FIELD: measurement technology.
SUBSTANCE: invention relates to measuring circuit (3) monitoring method and system intended for collection of measurements relating to aircraft turbojet engine (13) during period of time, wherein system comprises means of processing (21), made with possibility of constructing of said measuring circuit state indicator, based on counting transitions between successive state words, defining index of correctness of corresponding successive measurements.
EFFECT: disclosed is turbojet engine measuring circuit monitoring system.
7 cl, 6 dwg
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