Qiu Enpeng,Shen Lin,Li Minmin,Huang Da.A Method for Online Fusion of Terrestrial and Aerospace Data Based on Physics-Informed Neural Net...:2024 Asia-Pacific International Symposium on Aerospace Technology,2024

Cai Wei,Shen Lin.An Ensemble-Reinforcement Learning Approach for Stability Augmentation Control at High Angles of ...:2024 Asia-Pacific International Symposium on Aerospace Technology

邱恩鹏,沈霖,黄达,李民民.基于PINN的试验-飞行气动力数据实时融合建模:第十三届全国流体力学学术会议

蔡微,沈霖.基于集成强化学习的飞机大迎角控制策略研究:第十三届全国流体力学学术会议,2024

Xu Xiaoqiang,Huang Da,Shen Lin,Li Minmin.Research on aerodynamic test at high angle of attack and post-stall reorientation simulation for ...:Lecture Notes in Electrical Engineering,2024,1051:1465–1477

Shen Lin,Huang Da,Wu Genxing.Time delay compensation in lateral directional flight control system at high angles of attack.:Chinese Journal of Aeronautics,2021,34(4):1-18

Shen Lin,hd.战斗机大迎角非定常气动力建模:航空学报,2020,41(3):523440

Shen Lin,Huang Da,Wu Genxing.Effects of yaw roll coupling ratio on lateral directional departure prediction and restraint.:Chinese Journal of Aeronautics, 2019; 32(10): 2239,2019,32(10):2239-2253

Shen Lin,Huang Da,Wu Genxing.Effects of yaw roll coupling ratio on the lateral directional aerodynamic characteristics:Chinese Journal of Aeronautics,2019,32(2):272-280

Shen Lin,Huang Da,Wu Genxing.An investigation of lateral directional departure based on yawing rolling coupled wind tunnel tes...:Proc IMechE Part G: Journal of Aerospace Engineering,2018,232(16):2018; 232(16): 2989 3000.