The invention discloses a no-load state monitoring method and
system for an aircraft power supply
system, and relates to the technical field of electrical parameter measurement and aircraft power supply
system monitoring. Initializing a
monitoring system, calibrating a
voltage sensor, a
current sensor, a frequency sensor and an
impedance sensor, setting a no-load state judgment threshold system, and importing historical no-load data as a comparison reference; no-load
voltage, current, frequency and impedance signals are synchronously acquired through sampling frequency of the sensor group, and the signals are transmitted to the
data processing unit through the shielding cable; median filtering and low-pass filtering are adopted to remove
noise interference, normalization
processing is carried out on the signals, and basic electrical parameters are calculated; calculating core characteristic values of the
voltage stability, the frequency fluctuation coefficient, the impedance stability and the
harmonic distortion rate; comparing the characteristic value with a preset threshold value, judging whether the state is normal or not by combining historical data, and identifying an abnormal type; and outputting a judgment result in real time, and starting acousto-optic early warning in case of
abnormality. Abnormal
traceability and
trend prediction are realized, and safe and stable operation of an aircraft power supply system is guaranteed.