Abstract
Reusable spacecraft electronic components experience multiple, complex shock damage during their operational life, which is a primary contributor to mission failure. This study proposes a data-assisted physics-informed neural network (DA-PINN) model to assess fatigue damage in electronic components under complex shock loads. Unlike traditional PINN that solves partial differential equations, DA-PINN combines experimental with physics equations to enhance prediction accuracy. An autoregressive (AR) model was used to improve the shock fatigue life model, which was then integrated as a physical constraint into the loss function of DA-PINN. Subsequently, using ball grid array (BGA) solder joints as the research subject, complex shock fatigue experiments were conducted to train and validate the DA-PINN model. The results demonstrate the outstanding performance of the DA-PINN model, with all predicted shock fatigue life values falling within a scatter band of 1.5 times, surpassing the traditional shock fatigue life model and artificial neural networks. Notably, the physics-informed constraints embedded in DA-PINN enable it to maintain strong prediction accuracy and stability even when trained on small datasets. The proposed model can provide a reference for predicting the shock fatigue life of electronic components in reusable spacecraft.
| Original language | English |
|---|---|
| Article number | 108933 |
| Journal | International Journal of Fatigue |
| Volume | 197 |
| DOIs | |
| State | Published - Aug 2025 |
Keywords
- Aerospace
- Autoregressive model
- Physics-informed neural network
- Shock fatigue life
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