泮斌峰科研成果

个人经历 personal experience 工作经历 教育经历 2019.7-至今，西北工业大学航天学院，教授，博士生导师2013.5-2019.6，西北工业大学航天学院，副教授，硕士生导师2011.1-2013.4，西北工业大学航天学院，讲师 博士，西北工业大学，2006.9-2010.12联合培养博士生，美国爱荷华州立大学，2007.9-2009.9硕士，西北工业大学，2004.9-2007.4本科，西北工业大学，2000.9-2004.7 内容来自集群智慧云企服 发明专利4999元代写全部资料全国受理

教育教学

教育教学 Education and teaching 教育教学 招生信息 讲授本科生/研究生课程：1.航天器制导理论 2.飞行力学最优控制与估计理论3.轨道力学 招收航空宇航科学与技术、导航制导与控制、数学、力学、人工智能等相关专业硕士、博士研究生及博士后。欢迎相关方向青年学者加入团队（具体可Email联系）。

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荣誉获奖

科学研究 Scientific Research 研究方向：面向运载器、近地航天器及深空探测器的飞行器自主制导控制技术、飞行器智能技术、飞行动力学与轨迹优化技术等。主持承担国家自然科学基金青年基金/面上项目等40余项课题。

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科学研究

学术成果 Academic Achievements 部分SCI论文（*为唯一通讯作者）：26) Mengxin Zhao, Binfeng Pan*, et al. NURBS-based Sequential Convex Programming for Onboard Trajectory Optimization[J]. IEEE Transactions on Aerospace and Electronic Systems, 2024. (中科院SCI二区)(航空宇航领域顶刊)25) Wenjie Qing, Binfeng Pan*. Modified fractional homotopy method for solving nonlinear optimal control problems[J]. Nonlinear Dynamics, 2024.(中科院SCI二区)24) Yang Ni, Binfeng Pan*, et al. Accelerating Deep Neural Network training for autonomous landing guidance via homotopy[J]. Acta Astronautica, 2023.(中科院SCI二区)23) Binfeng Pan*, et al. Smoothing Homotopy Methods for Solving Nonlinear Optimal Control Problems[J]. Journal of Guidance Control and Dynamics, 2023.(中科院SCI二区)(航空宇航领域顶刊)22) Yangyang Ma, Binfeng Pan*, et al. Feasible Sequential Convex Programming With Inexact Restoration for Multistage Ascent Trajectory Optimizatio [J]. IEEE Transactions on Aerospace and Electronic Systems, 2022. (中科院SCI二区)(航空宇航领域顶刊)21)Yangyang Ma, Binfeng Pan*, et al. Picard Iteration-Based Convexification for Fuel-Optimal Rocket Descent Inside Atmosphere[J]. Journal of Guidance Control and Dynamics, 2022.(中科院SCI二区)(航空宇航领域顶刊)20)Wenjie Qing, Binfeng Pan*, et al. Fractional-Order Sliding Mode Control Method for a Class of Integer-Order Nonlinear Systems[J], Aerospace , 2022.(中科院SCI二区)19)Yangyang Ma, Binfeng Pan*, et al. Improved sequential convex programming using modified Chebyshev-Picard iteration for ascent trajectory optimization[J], Aerospace Science and Technology, 2021.(中科院SCI一区)18) Yangyang Ma, Binfeng Pan*, et al. Improved Parallel-Structured Newton-Type Guidance for Launch Vehicles Under Thrust Drop Fault[J], Journal of Spacecraft and Rockets, 2021.(中科院SCI三区)17) Yangyang Ma, Binfeng Pan*, Parallel-Structured Newton-Type Guidance by Using Modified Chebyshev–Picard Iteration[J], Journal of Spacecraft and Rockets, 58(3)，2021.(中科院SCI三区)16) Xun Pan, Binfeng Pan*, Zenghao Li . Bounding Homotopy Method for Minimum-Time Low-Thrust Transfer in the Circular Restricted Three-Body Problem[J], Journal of the Astronautical Sciences, Vol. 167, 2020, pp. 1220-1248.  (中科院SCI四区)15) Xun Pan, Binfeng Pan*, Practical Homotopy Methods for Finding the Best Minimum-Fuel Transfer in the Circular Restricted Three-Body Problem[J],  IEEE Access, Vol. 8, 2020, pp. 47845-47862. (中科院SCI三区)14) Binfeng Pan*, Yangyang Ma, Yang Ni,A New Fractional Homotopy Method for Solving Nonlinear Optimal Control Problems[J], Acta Astronautica, 2019. (中科院SCI二区)13) Binfeng Pan*, Usman Fareed, Wenjie Qing, Shaohua Tian, A Nnovel Fractional Order PID Navigation Guidance Law by Finite Time Stability Approach[J], ISA Transactions, 2019. (中科院SCI二区)12) Yue Zheng, Binfeng Pan, Shuo Tang,A Hybrid Method Based on Invariant Manifold and Chaos Control for Earth-Moon Low-Energy Transfer[J], Acta Astronautica, 2019. (中科院SCI二区) 11) Binfeng Pan*, Yangyang Ma, Rui Yan,Newton-Type Methods in Computational Guidance[J], Journal of Guidance, Control and Dynamics, 2019，42 (2): 377-383. (中科院SCI二区)(航空宇航领域顶刊)10) Binfeng Pan*, Xun Pan, Ping Lu, Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy[J], Journal of Spacecraft and Rockets, 2019，56(6)：283-291. (中科院SCI三区)9) Binfeng Pan*, Xun Pan, Yangyang Ma, A Quadratic Homotopy Method for Fuel-Optimal Low-Thrust Trajectory Design [J], Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 2019，232(5)：1741-1757. (中科院SCI四区)8) Binfeng Pan*, Xun Pan, Siqi Zhang, A New Probability-one Homotopy Method for Solving Minimum-Time Low-Thrust Orbital Transfer Problems[J], Astrophysics and Space Science, 2018，363(9)：198-210. (中科院SCI四区)7) Binfeng Pan, Yangyang Ma, Lambert's Problem and Solution by Non-Rational Bezier Functions [J], Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 2018, 232(2) : 227-245.(中科院SCI四区)6) Yang Wang, Binfeng Pan*, Yue Zheng, Xiang Lu, ETLBO Based Optimal Targeting to the Moon in the PCR3BP Chaotic System[J], Chaos Solitons & Fractals, 2017,105 : 21-28. (中科院SCI一区)5) Binfeng Pan*, Ping Lu, Xun Pan, Yangyang Ma, Double-Homotopy Method for Solving Optimal Control Problems [J], Journal of Guidance, Control and Dynamics , 2016, 39(8): 1706-1720. (中科院SCI二区) (航空宇航领域顶刊)4) Binfeng Pan*, Zheng Chen, Ping Lu, Reduced Transversality Conditions in Optimal Space Trajectories[J], Journal of Guidance, Control and Dynamics, 2013, 36(5): 1289-1300. (中科院SCI二区) (航空宇航领域顶刊)3) Binfeng Pan*, Ping Lu, Zheng Chen. Coast Arcs in Optimal Multiburn Orbital Transfers[J]. Journal of Guidance, Control and Dynamics, 2012, 35(2): 451-461. (中科院SCI二区) (航空宇航领域顶刊)2) Binfeng Pan, Ping Lu, Zheng Chen. Three-Dimensional Closed-Form Costate Solutions in Optimal Coast[J]. Acta Astronautica , 2012. 77(0): 156-166. (中科院SCI二区) 1) Ping Lu, Binfeng Pan. Highly Constrained Optimal Launch Ascent Guidance[J]. Journal of Guidance Control and Dynamics, 2010,33(2): 404-414.(中科院SCI二区) (航空宇航领域顶刊)其它及最新论文可浏览个人Researchgage主页: https://www.researchgate.net/profile/Binfeng_Pan2 内容来自集群智慧云企服 软件产品登记测试全国受理

学术成果

社会兼职 Social Appointments 1.  美国航空航天学会(AIAA)，Associate Fellow2.  国际宇航科学院(IAA)，Corresponding Member3. Acta Astronautica（SCI二区），副主编4. Astrodynamics，副主编5. 中国宇航学会深空探测技术专业委员会，委员6.中国人工智能学会智能空天系统专业委员会，委员7.西北工业大学航天学院深空探测与智能技术交叉研究中心，主任 内容来自集群智慧云企服 软件产品登记测试全国受理

综合介绍

团队信息 Team Information 西北工业大学航天学院航天器计算制导控制与人工智能实验室，主要开展考虑机载计算机有限计算和存储能力的实时自主制导控制技术、面向高动态/复杂任务的飞行器人工智能技术及近地/深空探测轨道动力学与控制技术等研究。毕业学生去向：国内相关高校、航空航天/兵工等科研院所、科技公司工作及国外知名高校继续深造。 内容来自集群智慧云企服