1989.9-1993.7，东北大学，工业自动化仪表专业，工学学士 1993.9-1996.3，东北大学，检测技术与自动化装置专业，工学硕士 2001.3-2006.3，东北大学，检测技术与自动化装置专业，工学博士

1999.6-2007.12，东北大学信息学院，讲师 2008.3-2010.4，东北大学，计算机科学与应用，博士后 2008.1-至今，东北大学信息学院，副教授

项目 1. 连续加料电弧炉智能炼钢系统，2018021000041，2018.8-2021.8，200万 2. 连续加料电弧炉智能炼钢系统，2018021000072，2018.11-2021.11，200万 3. 精炼炉智能炼钢技术，2019.12-2022.12，201万 4. 连续变姿态角风洞流场精确控制技术研究，2019021000081,2019.9-2022.9,68万

期刊论文 1.Ping Yuan, Bi Zhang, and Zhi-Zhong Mao, A Robust Adaptive Controller for Hammerstein Nonlinear Systems, International Journal of Control, Automation and Systems, 2017,15(2), 656-667 2.Ping Yuan, Bi Zhang,Zhizhong Mao, A self-tuning control method for Wiener nonlinear systems and its application to process control problems, Chinese Journal of Chemical Engineering,2017,15(2), 193-201 3. 袁平, 易凡, 肖宇航, 毛志忠，面向攻角变化的风洞流场模型预测控制器，控制与决策，2018,33(6)：1026-1032 4.Xiaojun Wang,Ping Yuan, Zhizhong Mao, Ensemble Fixed-Size LS-SVMs Applied for the Mach Number Prediction in Transonic Wind Tunnel, IEEE Transactions on Aerospace and Electronic System,2015,51(4),3167-3181. 5. Jian Zhang,Ping Yuan, KWAI-SANG CHIN, Model Predictive Control for the Flow Field in an Intermittent Transonic Wind Tunnel, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS ,2018,54(1):324-338. 6.Xiaojun Wang,Ping Yuan, Zhizhong Mao, Mingshuang You, Molten steel temperature prediction model based on bootstrap Feature Subsets Ensemble Regression Trees, Knowledge-Based Systems,2016,101:48-59. 7. Xiaojun Wang,Ping Yuan, Zhizhong Mao, The Modified Feature Subsets Ensemble Applied for the Mach Number Prediction in Wind Tunnel, IEEE Transactions on Aerospace and Electronic System,2016,52(2):863-874. 8. Xiaojun Wang, Ping Yuan, Zhizhong Mao, Ning Du，Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering，2016， 230(12), 2306-2319. 9. 王晓军，袁平，毛志忠，杜宁, 基于随机森林的风洞马赫数预测模型,航空学报，2016,37(5),1494-1505. 10. Xiaojun Wang,Ping Yuan, Zhizhong Mao, Ensemble Fixed-Size LS-SVMs Applied for the Mach Number Prediction in Transonic Wind Tunnel, IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015,51(4): 3167-3181.

专利 1.一种高精度暂冲型引射式跨声速风洞流场控制结构，2017.6，中国，ZL201510300756.2 2.电炉电极智能控制器，2013.2，中国，ZL200910220049.7