本硕毕业于西北工业大学航空学院，博士毕业于复旦大学航空航天系。2016-2017加拿大Concordia大学机械工程系航空宇航创新中心访问学者。现为复旦大学航空航天系副教授，复旦大学飞行器设计研究所副所长。长期从事航空航天飞行器飞行控制，控制理论与应用研究，电子数据证据技术等交叉学科研究工作。主持、参与了多项航天创新基金，国家中长期重大专项等科研项目。

1. Jing Wan*, Guangshan Chen，Prescribed Performance Control of Air-breathing Hypersonic Vehicle with Propulsion System Constraint, The 5th International Symposium on Autonomous Systems, Hangzhou, China, 2021-12-17至2021-12-19.

2. Chao Tao, Jing Wan*, Jianliang Ai, A nonlinear control approach for a hypersonic vehicle, Aircraft Engineering and Aerospace Technology, 2017, 89(2): 320-329.

3. Jing Wan*, Model for evaluation the design patterns of the micro-air vehicle under interval-valued intuitionistic uncertain linguistic environment, Intelligent and Fuzzy Systems. 2016, 30(5): 2963-2969.

4. Jing Wan*, Jianliang Ai, Lag synchronization of a class of time-delayed chaotic neural networks by impulsive control, Telkomnika-Indonesian Journal of Electrical Engineering, 2013, 11(6):3341-3348.

5. Jing Wan*, Qian Wang, Jianliang Ai, Dynamic inversion-based control system of a hypersonic vehicle with model uncertainty, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 2012.9.24-9.28.

6. Qi Chen, Jing Wan, Jianliang Ai*, L1 adaptive control of a generic hypersonic vehicle model with a blended pneumatic and thrust vectoring control strategy. Science China-information Sciences. 2017.3.

7. Chen Li, Jiong-Ran Wen, Jing Wan, Osman Taylan, Cheng-Wei Fei, Adaptive directed support vector machine method for the reliability evaluation of aeroengine structure, Reliability Engineering & System Safety, 2024, 246: 1-12.