个人简介
钟睿，男，中共党员，江西赣州人，1984年8月生。现为北京航空航天大学宇航学院副教授，博士生导师，飞行器设计系教学主任。2006年7月和2011年7月分别获北京航空航天大学飞行器设计专业学士和博士学位。2011年7月至2013年6月在加拿大约克大学从事博士后研究。研究方向为空间绳系体动力学与控制、空间挠性结构耦合非线性动力学与控制。近期研究：空间挠性多体动力学与控制；绳系系统动力学与控制；空间碎片处理、空间拖船；基于摄影测量的模态参数辨识及姿态控制；基于智能算法的航天器控制。作为负责人主持多项纵、横向课题，包括国家自然科学基金青年科学基金项目、面上项目，航天创新基金重点项目，国防科技重点实验室创新基金，航天五院和八院合作课题等。以（唯一）第一作者或通讯作者身份发表和录用学术论文50余篇，其中SCI检索21篇，5篇发表在航天领域顶级期刊AIAA Journal of Guidance Control and Dynamics上，另有6项国家发明专利授权。受邀担任国际学术会议TIS2019技术委员会委员，参加国际小卫星任务设计大赛获得优秀奖（The 2nd Mission Idea Contest for Micro/Nano Satellite Utilization），担任Acta Astronautica，Transactions on Mechatronics，Aerospace Science and Technology，Astrodynamics，《航空学报》等国内外高水平学术期刊审稿人。教学方面，主讲《坐电梯上太空》核心通识课、《新概念飞行器》本科生选修课和《高等航天动力学与控制》研究生选修课，参与讲授《飞行动力学》本科必修课等。所培养的硕士大多数进入我国航天工业重要部门工作，学生张宇靖获得2018“校级工程硕士实习实践优秀成果”，实际指导的博士生孙鑫，获得博士创新基金。
教育经历
2006.9 -- 2011.6 北京航空航天大学 飞行器设计 博士研究生毕业 博士学位
2002.9 -- 2006.6 北京航空航天大学 飞行器设计与工程 大学本科毕业 学士学位
工作经历
2011.7 -- 2013.6 加拿大约克大学 地球空间科学与工程系 博士后
2013.9 -- 至今 北京航空航天大学 宇航学院 院长助理 副教授
社会兼职
受邀担任国际学术会议TIS2019技术委员会委员，参加国际小卫星任务设计大赛获得入围奖（The 2nd Mission Idea Contest for Micro/Nano Satellite Utilization），担任Acta Astronautica，Transactions on Mechatronics，Aerospace Science and Technology，Astrodynamics，《航空学报》等国内外高水平学术期刊审稿人
近期论文
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H. Rao, R. Zhong, P. Li, “Fuel-optimal deorbit scheme of space debris using tethered spacetug based on pseudospectral method”, Chinese Journal of Aeronautics, accepted.
R. Zhong, Z. H. Zhu, “Attitude Stabilization of Tug–Towed Space Target by Thrust Regulation in Orbital Transfer,” IEEE/ASME Transactions On Mechatronics, Vol. 24, No. 1, 2019, pp.373-383.
X. Sun, R. Zhong, “Nutation damping and spin orientation control of tethered space debris,” Acta Astronautica, Vol. 160, p. 683-693, 2019.
P. Li, R. Zhong, “Optimal control scheme of space tethered system for space debris deorbit” Acta Astronautica, Vol. 165, p. 355-364, 2019.
X. Sun, R. Zhong, “Tether attachment point stabilization of noncooperative debris captured by a tethered space system” Acta Astronautica, Vol. 177, p. 784-797 2020.
X. Sun, R. Zhong*, “Libration control for the low-thrust space tug system using electrodynamic force,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 41, No.7, 2018, 1600-1607. (SCI index)
Y. Wang, R. Zhong*, “Orbital perturbation due to orbit-attitude coupling near asteroids,” Aircraft Engineering and Aerospace Technology, Vol. 90, p. 104-113, 2018. (SCI index)
X. Sun, R. Zhong*, “Switched propulsion force libration control for the low-thrust space tug system,” Aerospace Science and Technology, Vol. 80, 2018, 281-287. (SCI index)
R. Zhong, Y. Wang, “Dynamics and control of a probe tethered to an asteroid,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 41, No. 7, 2018, pp. 1583-1588. (SCI index)
X. Sun, M. Xu, R. Zhong*, “Dynamic analysis of the tether transportation system using absolute nodal coordinate formulation,” Acta Astronautica, Vol. 139, p. 266-277, 2017 (SCI index)
R. Zhong, Z. H. Zhu, “Timescale Separate Optimal Control of Tethered Space-Tug Systems for Space-Debris Removal,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 39, No. 11, p. 2539-2544, 2016. (SCI index)
R. Zhong, Y. Wang, “Research on the tether assisted observation of an asteroid,” Acta Astronautica, Vol. 123, p. 310-319, 2016. (SCI index)
R. Zhong, Z. H. Zhu, “Optimal Control of Satellite Fast Deorbit using Electrodynamic Tether,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, p. 1182-1194, 2014. (SCI index)
R. Zhong, Z. H. Zhu, “Optimal current switching control of electrodynamic tethers for fast deorbit,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 37, No. 5, p. 1501-1511, 2014. (SCI index)
R. Zhong, Z. H. Zhu, “Libration Dynamics and Stability of Electrodynamic Tethers in Satellite Deorbit,” Celestial Mechanics and Dynamical Astronomy, Vol. 116, No. 3, p. 279-298, 2013. (SCI index)
R. Zhong, Z. H. Zhu, "Long Term Dynamics and Optimal Control of Nano-Satellite Deorbit Using a Short Electrodynamic Tether", Advances in Space Research, Vol. 52, No. 8, p. 1530-1544, 2013. (SCI index)
R. Zhong, Z. H. Zhu, “Dynamics of Nano-Satellite Deorbit by Bare Electrodynamic Tether in Low Earth Orbit,” Journal of Spacecraft and Rockets, Vol. 50, No.3, p. 691-700, 2013. (SCI index)
R. Zhong, Z. H. Zhu, “Long-Term Libration Dynamics and Stability Analysis of Electrodynamic Tethers in Spacecraft Deorbit,” Journal of Aerospace Engineering, accepted in November, 2012. Doi: 10.1061/(ASCE)AS.1943-5525.0000310, 04014020. (SCI index)
Zhong Rui, Xu Shijie, “Periodical Motion of a Tethered Satellite System around Collinear Libration Points,” Journal of Aerospace Engineering, Vol. 24, No. 4, p. 488-504, 2011. (SCI index)
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