FIELD: electrical engineering.
SUBSTANCE: invention is used for detection of intermittent contacts on probes forming sensors of an aviation turbine engine. The first measurement value is obtained, an increment is compared with an increment threshold, and the measurement to be processed is transmitted to a processing interface, wherein the mentioned measurement is selected equal to a value of an assessment model of the obtained measurement, if the increment is more than the increment threshold, or equal to the first obtained measurement value, if the increment is less than the increment threshold, then, additional processing stages are performed.
EFFECT: provision of a possibility of implementation of a method for checking measurements obtained by a probe forming a sensor of a turbine engine, which has a better reaction to intermittent circuit breaking.
8 cl, 7 dwg
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