Abstract:To address the mass-loading effect, limited measurement points, and complicated multi-point deployment of conventional contact sensors in wing modal tests, a wing vibration measurement method combining improved You Only Look Once (YOLO) with predictive optical flow, termed YK-WingVib, was proposed. A quadrant-cross-target detection model, QCT-YOLO, was developed by introducing edge-enhanced re-parameterized convolution (EdgeRepConv), a cross-stage partial edge dual-level aggregation network (CSP-EDLAN), and an efficient upsampling convolution block (EUCB) to improve detection accuracy under complex conditions. To reduce mismatching under large displacement and tracking drift during long-duration tests, a predictive robust adaptive Kanade–Lucas–Tomasi method, PRA-KLT, was proposed for stable and continuous measurement-point tracking. Ablation experiments, algorithm comparisons, and scaled-wing model tests showed that QCT-YOLO achieved a mean average precision (mAP)@0.5:0.95 of 0.904, while the root mean square error (RMSE) of PRA-KLT remained within 0.67 px across multiple frequency bands. In scaled-wing model tests under real experimental conditions, the average displacement RMSE was 0.35 mm, and the mean correlation coefficient with fiber-optic sensor measurements was 0.989. The mean relative error of the first natural frequency was 0.126%. The method meets the requirements for high-precision non-contact measurement in wing ground vibration tests and structural health monitoring.