[1] 1997.9-2003.5

国防科学技术大学 | 航空宇航科学与技术 | 博士学位 | 博士研究生毕业

[2] 1993.9-1997.7

国防科学技术大学 | 飞行器总体设计与发动机工程 | 学士学位 | 大学本科毕业

[1] 2015.9-至今 航空航天学院 | 中南大学 教授 [2] 2014.12-2015.9 航空航天学院 | 中南大学 副教授 [3] 2010.4-2010.12 School of Engineering Science | University of Southampton 访问学者 [4] 2006.12-2014.11 航天学科与工程学院 | 国防科学技术大学 副教授

目前主要开展多飞行器集群系统技术的研究，重点是多飞行器运动协调控制的理论和实验研究。

[1] Yunhe Meng, Qifeng Chen, Xing Chu, Ahmed Rahmani. Maneuver Guidance and Formation Maintenance for Control of Leaderless Space-robot Teams [J]. 美国: IEEE Transactions on Aerospace and Electronic Syst, 2018,
[2] Yunhe Meng, Qifeng Chen, Ahmed Rahmani. A decentralized cooperative control scheme for a distributed space transportation system [J]. Robotics and Autonomous Systems, 2018, 101: 1–19
[3] Xiang Yu, Kun Liu, Qifeng Chen. Constellation design for responsive visiting based on ground track adjustment [J]. UK: Part G: Journal of Aerospace Engineering, 2017,
[4] Yunhe Meng, Qifeng Chen, Qing Ni. A new geometric guidance approach to spacecraft near-distance rendezvous problem [J]. 英国: Acta Astronautica, 2016, 129: 374–383
[5] Qifeng Chen, Yunhe Meng, Jianjun Xing. Shape control of spacecraft formation using a virtual spring-damper mesh [J]. Chinese Journal of Aeronautics, 2016, 29(6): 1730–1739
[6] Qifeng Chen, Sandor M. Veres, Yaonan Wang, and Yunhe Meng. Virtual Spring-Damper Mesh-Based Formation Control for Spacecraft Swarms in Potential Fields [J]. Journal of Guidance, Control, and Dynamics, 2015, 38(3): 539-546
[7] Qifeng Chen, Yuedong Zhang, Shouyi Liao, and Fanliang Wan. Newton–Kantorovich / Pseudospectral Solution to Perturbed Astrodynamic Two-Point Boundary-Value Problems [J]. Journal of Guidance, Control, and Dynamics, 2013, 36(2): 485-498
[8] Qifeng Chen, and Jinhai Dai. Canonical Solution of Two-Point Boundary-Value Problems [J]. Journal of Guidance, Control, and Dynamics, 2011, 34(1): 287-293
[9] Yunhe Meng, Rui Hao, Qifeng Chen. Attitude stability analysis of a dual-spin spacecraft in halo orbits [J]. 英国: Acta Astronautica, 2014, 99: 318–329
[10] 孟云鹤, 陈琪锋. 地月平动点导航星座的概要设计与性能分析 [J]. 中国: 物理学报, 2014, 63(24): 248402
发表学术论文40余篇，其中SCI检索9篇、EI检索10篇。出版教材1部、学术专著1部。[1]导弹作战应用
[2]平动点航天器动力学与控制

获国防专利授权1项、国家发明专利授权1项。[1]基于虚拟弹簧阻尼网络的卫星编队构形分布式控制方法
[2]×××全球覆盖的星座设计方法