余文斌 - 北京航空航天大学

个人简介

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，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

高超声速飞行器动力学高超声速飞行器滑翔弹道解析解与解析弹道规划方法高超声速飞行器制导与控制

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Wenbin Yu,Wanchun Chen.Entry Guidance Based on Analytical Trajectory Solutions.[期刊]:IEEE Transactions on Aerospace and Electronic Systems,2021 Wenbin Yu,Jin Yang,Bo Liao,Hengwei Zhu.Analytical trajectory prediction for near-first-cosmic-velocity atmospheric gliding using a perturbation method.[期刊]:Acta Astronautica,2021,187:79–88 Wenbin Yu.High-Accuracy Approximate Solutions for Hypersonic Gliding Trajectory with Large Lateral Maneuvering Range.[期刊]:IEEE Transactions on Aerospace and Electronic Systems,2021,57(3):1498-1512 Wanqing Zhang,Wanchun Chen.Analytical solutions to three-dimensional hypersonic gliding trajectory over rotating Earth.[期刊]:Acta Astronautica,2021,179:702-716 Wenbin Yu,Penglei Zhao,Wanchun Chen.Analytical Solutions to Aeroassisted Orbital Transfer Problem.[期刊]:IEEE Transactions on Aerospace and Electronic Systems,2020,56(5):3502-3515 Wenbin Yu.Analytical Cooperative Entry Guidance for Rendezvous and Formation Flight.[期刊]:ACTA Astronautica,2020,171:118-138 Penglei Zhao,Wanchun Chen.Analytical solutions for longitudinal-plane motion of hypersonic skip-glide trajectory.[期刊]:Nonlinear Dynamics,2019,96(3):1947-1969 Wenbin Yu.Analytical entry guidance for coordinated flight with multiple no-fly-zone constraints.[期刊]:Aerospace Science and Technology,2018,84:273–290 Wenbin Yu,Wanchun Chen,Zhiguo Jiang.Analytical Entry Guidance for No-Fly-Zone Avoidance.[期刊]:Aerospace Science and Technology,2018,72:426–442 Wenbin Yu.Analytical Entry Guidance based on Pseudo-Aerodynamic Profiles.[期刊]:Aerospace Science and Technology,2017,66:315–331 Wanqing Zhang,Wanchun Chen.Entry guidance for high-L/D hypersonic vehicle based on drag-vs-energy profile.[期刊]:ISA Transactions,2018,83:176–188 Penglei Zhao,Wanchun Chen.Optimal perturbation guidance with constraints on terminal flight-path angle and angle of attack.[期刊]:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2019,233(12):4436-4446 Penglei Zhao,Wanchun Chen.Guidance law for intercepting target with multiple no-fly zone constraints.[期刊]:The Aeronautical Journal,2017,121(1244):1479-1501 Wenbin Yu,Wanchun Chen.Optimal Terminal Guidance for Exoatmospheric Interception.[期刊]:Chinese Journal of Aeronautics,2016,29(4):1052–1064 Wenbin Yu,Wanchun Chen,Zhiguo Jiang.Omnidirectional Autonomous Entry Guidance based on 3-D Analytical Glide Formulas.[期刊]:ISA Transactions,2016,65:487-503 Wenbin Yu,Wanchun Chen.Entry guidance with real-time planning of reference based on analytical solutions.[期刊]:Advances in Space Research,2015,55(9):2325 – 2345 Wenbin Yu,Wanchun Chen.Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.[期刊]:ISA Transactions,2015,56:42 – 52 Wenbin Yu,Wanchun Chen.Guidance Law with Circular No Fly Zone Constraint.[期刊]:Nonlinear Dynamics,2014,78(3):1953–1971 Mengya Gao,Wanchun Chen.Research of modeling and decoupling on cruise aircraft with parachute.[会议录].Weihai City, China:2020 International Conference on Aviation Safety and Information Technology,2020 Penglei Zhao,Wanchun Chen.Autopilot for Near-space Hypersonic Vehicle Controlled by Aerodynamics Lift and Divert Thrusters with Off-Centered Seeker Window.[会议录].Hawaii, USA:29th AAS/AIAA Space Flight Mechanics Meeting,2019 Jingwei Meng,Wanchun Chen.Sub-optimal Ground-Strike Guidance based on Perturbation Method.[会议录].Harbin, China:Proceedings of 2016 IEEE International Conference on Mechatronics and Automation,2016 余文斌.用于显式制导的LTV系统谱分解法解析求解及其稳定域研究.[会议录].哈尔滨:2014年飞行器轨迹优化与制导学术研讨会,2014 Wenbin Yu.Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle.[会议录].Portland, USA:AIAA Guidance, Navigation, and Control Conference,2011