The invention belongs to the technical field of aircraft airborne testing, and particularly relates to a rapid fault diagnosis method for an airborne
vibration sensor. Comprising the following steps that 1,
flight test sensor
record data are obtained, data of a
vibration sensor are separated according to parameter names, and the data of the sensor comprise a fault sample data sequence and a normal sample data sequence; 2, respectively forming a
training set, a
verification set and a
test set according to a random selection mode; 3, respectively constructing normal sampling training subsets for the
training set, and constructing an unbalanced sampling training subset by diluting normal samples; 4,
wavelet transformation is carried out on the normal sampling training subset data sequence and the unbalanced sampling training subset data sequence respectively, and a normal sampling training subset input matrix and an unbalanced sampling training subset input matrix based on
wavelet transformation
modulus maxima are constructed respectively; 5, inputting the normal sampling training subset input matrix and the unbalanced sampling training subset input matrix into the bilateral
branch network model for training, and obtaining prediction output through different weight accumulation learning of two sample sets; step 6, using a
cross entropy loss function to realize convergence of the
network model, and completing
network model training; and 7, performing sensor fault judgment on output of the sensor and prediction output of the network model by adopting a majority consistent voting principle. The problem of sensor abnormal phenomenon detection or abnormal missing in a
flight test is solved.