Aero-engine fault diagnosis method based on transferable neural network
An aero-engine and fault diagnosis technology, applied in neural learning methods, biological neural network models, neural architectures, etc., can solve the problems of not landing, staying, unrealistic, etc., to reduce distribution differences and improve fault diagnosis accuracy. Effect
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[0079] In the case of multi-fault diagnosis of aeroengines, firstly, the objective function of the original RVFL model is established based on all collected engine operating data (including normal data sample information and fault data sample information)
[0080]
[0081] in is the sample, N is the total number of samples, and d is the number of features. For the i-th instance, x i is a d-dimensional feature vector. is the output weight, is the jth row of β. w j and b j The weights and biases of the input to the enhancement layer are randomly set. T=[t i ,...t N ] T is the label set of the sample, if x i belongs to class j, then t ij is 1, and the rest are 0. h j (·) is the activation function of the jth enhanced node, for x i , which is defined as:
[0082]
[0083] Furthermore, formula (1) can be further expressed as a matrix, and its objective function is:
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[0085] where matrix The definition of is shown in the following formula
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