The invention discloses a method for predicting the remaining service life of a
control moment gyroscope based on parameter fusion, and relates to the technical field of health management of
spacecraft attitude control systems. According to the method, optimal fusion of measurement parameters and implicit parameters is realized through adversarial learning
feature extraction and a channel attention mechanism, and the method is particularly suitable for high-precision residual life prediction of the
spacecraft control moment gyroscope under variable working conditions. The method comprises four main steps of
data preparation and multi-source input, adversarial learning
feature extraction, SE-Attention
feature fusion and three-stage training optimization. In the
data preparation step, original time sequences of
voltage and current of a rotor motor are collected through a built-in electrical sensor of a CMG, and key physical parameters of a full-film
lubrication friction coefficient, lubricating
oil viscosity, a bearing clearance and contact stiffness are inverted based on an
electromechanical coupling model; in the adversarial learning step, a game framework of a feature extractor and a working condition
discriminator is constructed, and working condition-independent robust
feature extraction is realized through a gradient inversion layer; in the SE-Attention
feature fusion step, importance weights are adaptively distributed to different feature channels through an
extrusion-excitation mechanism; and the three-stage training optimization step adopts a preheating-confrontation-
fine tuning strategy to ensure the
network convergence. The method solves the problem of
domain adaptation, has the technical advantages of strong robustness, high precision, strong generalization,
interpretability and self-
adaptation, and can realize high-precision RUL prediction under variable working conditions.