个人简历

基本情况

教育背景：
2010.09-2016.01，北京航空航天大学，宇航学院，飞行器设计专业，直接攻读博士学位；
2006.09-2010.06，北京航空航天大学，宇航学院，飞行器设计与工程(航天)专业，学士学位。
工作经历：
2018.07-至今，北京航空航天大学，宇航学院，“卓越百人”特别副研究员，硕士生导师；
2016.03-2018.05，北京航空航天大学，宇航学院，博士后。


科研成果

长期从事精确制导与控制技术研究，主要承担来自航天院所的科研项目，其中多数属于国家重大专项工程。针对某新型飞行器弹道规划难的问题，提出了弹道阻尼控制技术和高精度三维弹道解析解，大幅改善飞行过程中的力热环境与控制品质，将弹道规划效率和制导精度提高数个量级，为我国多种飞行器的研制作出重要贡献。目前以第一作者/通讯作者发表SCI论文10篇，其中Q1区8篇，申请专利9项。

研究领域

飞行动力学、弹道规划技术、精确制导与控制技术

近期论文

[1]Yu Wenbin, Chen Wanchun*, Jiang Zhiguo, Zhang Wanqing, Zhao Penglei. Analytical entry guidance for coordinated flight with multiple no-fly-zone constraints [J]. Aerospace Science and Technology, 84(2019): 273–290.
[2]Zhang Wanqing, Chen Wanchun, Yu Wenbin*. Entry guidance for high-L/D hypersonic vehicle based on drag-vs-energy profile. ISA Transactions (2018).
[3]Yu Wenbin*, Chen Wanchun, Jiang Zhiguo, Liu Ming, Yang Ding, Yang Ming, Ge Yajie. Analytical entry guidance for no-fly-zone avoidance, Aerospace Science and Technology, 72(2018), 426–442.
[4]Zhao Penglei, Chen Wanchun, Yu Wenbin*. Guidance law for intercepting target with multiple no-fly zone constraints[J]. The Aeronautical Journal, 2017, 121(1244): 1479-1501
[5]Yu Wenbin, Chen Wanchun, Jiang Zhiguo, Zhou Hao*, Liu Xiaoming, Liu Ming. Analytical entry guidance based on pseudo-aerodynamic profiles, Aerospace Science and Technology. 66 (2017), 315–331.
[6]Yu Wenbin, Chen Wanchun, Jiang Zhiguo, LiuXiaoming*, Zhou Hao. Omnidirectional autonomous entry guidance based on 3-D analytical glide formulas. ISA Transactions, 65 (2016), 487–503.
[7]Meng Jingwei, Chen Wanchun, Yu Wenbin*. Sub-optimal Ground-Strike Guidance based on Perturbation Method [C]. Harbin, China: Proceedings of 2016 IEEE International Conference on Mechatronics and Automation, August 7 - 10, 2016.
[8]Yu Wenbin, Chen Wanchun, Yang Liang *, Liu Xiaoming, Zhou Hao. Optimal Terminal Guidance for Exoatmospheric Interception. Chinese Journal of Aeronautics, 2016, V29 (4): 1052–1064.
[9]Yu Wenbin*, Chen Wanchun. Entry guidance with real-time planning of reference based on analytical solutions. Advances in Space Research. 55 (2015), 2325–2345.
[10]Yu Wenbin*, Chen Wanchun. Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints. ISA Transactions, 2015, V56: 42 – 52.
[11]Yu Wenbin*, Chen Wanchun. Guidance Law with Circular No Fly Zone Constraint. Nonlinear Dynamics, 2014, V78 (3): 1953–1971.
[12]Yu Wenbin*, Chen Wanchun. Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle. Portland, USA: AIAA Guidance, Navigation, and Control Conference, 2011.