FIELD: information technology.
SUBSTANCE: system has a module for identifying the base address of a fuel control pump of aircraft engine, a module for generating signals for reading parameters of a valve pair, a module for recording parameters of the valve pair, a module for identifying the base address of ratio of sound speed in the material of the slide valve body to the length of the slide valve, a module for generating signals for reading codes of the ratio of sound speed in the material of the slide valve body to the length of the slide valve, a module for identifying frequency of ultrasonic vibrations of the slide valve body, a module for identifying the base address of the ratio of the mass of the slide valve body to the frequency of ultrasonic vibrations of the slide valve body, a module for generating signals for reading codes of the ratio of the mass of the slide valve body to the frequency of ultrasonic vibrations of the slide valve body, a module for recording codes of the ratio of the mass of the slide valve body to the frequency of ultrasonic vibrations of the slide valve body, a module for identifying the base address of the ratio of frictional force of the slide valve in the body to the mass of the slide valve, a module for generating signals for reading codes of the ratio of frictional force of the slide valve in the body to the mass of the slide valve, a module for recording codes of the ratio of frictional force of the slide valve in the body to the mass of the slide valve, a module for identifying power of the ultrasonic vibrations the slide valve body.
EFFECT: faster operation of the system.
14 dwg
