泮斌峰


的个人主页 http://teacher.nwpu.edu.cn/panbinfeng

  被浏览次数:23316

基本信息 The basic information

泮斌峰

航天学院

博士研究生毕业

博士

教授

航空宇航科学与技术

panbinfeng@nwpu.edu.cn

工作经历 Work Experience

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


教育经历 Education Experience

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


教育教学 Education And Teaching

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

招生信息 Admission Information

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)。

科学研究 Scientific Research

研究方向:面向导弹武器系统、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、国防基础科研重点项目、国防科技重点实验室基金、863项目及军兵种/科研院所项目等多项课题。

学术成果 Academic Achievements

以第一/第二作者所发表的SCI论文:

1) 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.(SCI)

2) Yangyang Ma, Binfeng Pan, Shuo Tang. Improved Parallel-Structured Newton-Type Guidance for Launch Vehicles Under Thrust Drop Fault[J], Journal of Spacecraft and Rockets, 2021.(SCI)

3) Yangyang Ma, Binfeng Pan, Parallel-Structured Newton-Type Guidance by Using Modified Chebyshev–Picard Iteration[J], Journal of Spacecraft and Rockets, 58(3),2021.(SCI:000672531200013)

4) 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.   (SCI:000539191600002) 

5) 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.  (SCI:000524679300011) 

6) Binfeng Pan, Yangyang Ma, Yang Ni,A New Fractional Homotopy Method for Solving Nonlinear Optimal Control Problems[J], Acta Astronautica, 2019. (SCI) (航空宇航领域顶级期刊)

7) 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. (SCI:000501655900009) 

8) 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. (SCI) (JCR分区: Q1) (航空宇航领域顶级期刊)

9) Binfeng Pan, Yangyang Ma, Rui Yan,Newton-Type Methods in Computational Guidance[J], Journal of Guidance, Control and Dynamics, 2019,42 (2): 377-383. (SCI:000457386900012) (JCR分区: Q1) (航空宇航领域顶级期刊)

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(SCI:000457390100025) 

11) 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(SCI:000462094000015) 

12) 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. (SCI:000443211800002)

13) Binfeng Pan, Yang Wang, Shaohua Tian, A High-Precision Single Shooting Method for Solving Hypersensitive Optimal Control Problems [J], Mathematical Problems in Engineering,2018. (SCI: 000431237700001 ) 

14) 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. (SCI: 000424057800003 )

15) 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. (SCI: 000416642100004 ) 

16) 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. (SCI:000382502500002 )(航空宇航领域顶级期刊)

17) 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. (SCI:000324155000005)(航空宇航领域顶级期刊)

18) 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. (SCI:000301631100010) (航空宇航领域顶级期刊)

19) Binfeng Pan, Ping Lu, Zheng Chen. Three-Dimensional Closed-Form Costate Solutions in Optimal Coast[J]. Acta Astronautica , 2012. 77(0): 156-166.(SCI:000305303700017 ) (航空宇航领域顶级期刊)

20) Ping Lu, Binfeng Pan. Highly Constrained Optimal Launch Ascent Guidance[J]. Journal of Guidance Control and Dynamics, 2010,33(2): 404-414.(SCI:000275802200010) (航空宇航领域顶级期刊)


其它及最新论文可浏览个人Researchgage主页: https://www.researchgate.net/profile/Binfeng_Pan2

最后更新时间: 2021-11


社会兼职 Social Appointments

1. 国际航天领域著名期刊Acta Astronautica(SCI二区)编委

2. 国际学术期刊Astrodynamics编委

3. AIAA高级会员

4.中国宇航学会深空探测技术专业委员会委员

5.中国人工智能学会智能空天系统专业委员会委员

6.西北工业大学-美国圣迭戈州立大学飞行力学与计算制导控制联合创新实验室主任

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

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,依托于西北工业大学-美国圣迭戈州立大学飞行力学与计算制导控制联合创新实验室,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。

目前实验室有博士后、博士生、硕士生10余名。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。