The invention belongs to the technical field of aero-engine state monitoring and intelligent fault diagnosis, and discloses a multi-
modal information fusion bearing fault diagnosis method based on self-
supervised learning. The method comprises the following steps: firstly, through
mask reconstruction self-supervision pre-training, extracting stable feature representation insensitive to
mask disturbance from an unlabeled multi-
modal signal, and dynamically updating each
modal feature reference point by using an index
moving average algorithm; in a downstream fault diagnosis task, a multi-modal joint
decision model comprising a pre-training
encoder, a single-modal classifier and a fusion classifier is constructed, and adaptive weighted fusion of multi-modal decision is realized through contribution degree calculation based on a cooperative game Shapley value in combination with a deviation degree of modal features and a reference point. According to the method, the dependence of the deep neural
network on fault labeling data is effectively reduced, the accuracy and robustness of the diagnosis
system in a multi-modal
signal diagnosis scene are improved through a dynamic
fusion mechanism, and the method is suitable for industrial scenes with limited
sample label resources.