钟睿

职称\职位：副教授\硕士生导师
出生年月：1984年8月
电子邮箱：zhongruia@163.com
办公地点：北航沙河主楼D座915
办公电话：
http://shi.buaa.edu.cn/09703/zh_CN/index/28311/list/index.htm


基本情况

教育背景：
2006年7月于北京航空航天大学宇航学院获工学学士学位，飞行器设计专业；
2011年7月于北京航空航天大学宇航学院获工学博士学位，飞行器设计专业。

工作经历：
2011年7月至2013年6月于加拿大约克大学地球空间科学与工程，博士后；
2013年9月至今于北京航空航天大学宇航学院，航天飞行器技术系；
现任宇航学院院长助理。

研究方向

1. 绳系卫星动力学与控制；
2. 空间挠性体耦合动力学、参数辨识与智能控制。

主讲课程


本科生课程《坐电梯上太空》、《新概念航天器》；
研究生课程《高等航天动力学与控制》等；
主持教改项目《基于“翻转课堂”的核心通识课程设计实践》。


科研成果

在国内外学术期刊与学术会议上发表论文50余篇，其中一作或唯一通讯作者SCI收录18篇。第九届中国自动化学会空间及运动体控制专业委员会委员；TIS2019国际会议Technical Committee委员，Mario Grossi奖评委；ESCI期刊International Journal of Space Science and Engineering编委。长期担任Acta Astronaut.，IEEE-ASME T. Mech.，Aerosp. Sci. Technol.,《航空学报》等国内外高水平学术期刊审稿人。承担科研项目包括：国家自然科学基金青年项目、面上项目、航天创新基金重点项目及与航天五院和航天八院横向课题等。入选第五批“北航青年拔尖人才”。

代表论文

1. 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.
2 . 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.
3. 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, pp. 2539-2544, 2016.
4. R. Zhong,Y. Wang, “Research on the tether assisted observation of an asteroid,”Acta Astronautica, Vol. 123, pp. 310-319, 2016.
5 . 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, 2014, pp. 1501-1511.
6. R. Zhong, Z. H. Zhu, “Optimal control of nanosatellite fast deorbit using electrodynamic tether,”AIAA Journal of Guidance, Control, and Dynamics, Vol. 37, No. 4, 2014, pp. 1182-1194.
7. 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, 2014. Doi: 10.1061/(ASCE)AS.1943-5525.**, **.
8. 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, 2013, pp. 1530-1544.
9. R. Zhong, Z. H. Zhu, “Libration dynamics and stability of electrodynamic tethers in satellite deorbit,”Celestial Mechanics and Dynamical Astronomy, Vol. 116, No. 3, 2013, pp. 279-298.
10. 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, 2013, pp. 691-700.
11. R. Zhong, S. Xu, “Periodical motion of a tethered satellite system around collinear libration points,”Journal of Aerospace Engineering, Vol. 24, No. 4, 2011, pp. 488-504,.
12. P. Li, R. Zhong, “Optimal control scheme of space tethered system for space debris deorbit” Acta Astronautica, Vol. 165, 2019, pp. 355-364.
13. X. Sun,R. Zhong, “Nutation damping and spin orientation control of tethered space debris,”Acta Astronautica, Vol. 160, 2019, pp.683-693.
14. X. Sun,R. Zhong, “Switched propulsion force libration control for the low-thrust space tug system,”Aerospace Science and Technology, Vol. 80, 2018, pp. 281-287.
15. X. Sun,R. Zhong, “Libration control for the low-thrust space tug systemusing electrodynamic force,”AIAA Journal of Guidance, Control, and Dynamics, Vol. 41, No.7, 2018, pp. 1600-1607
16. Y. Wang,R. Zhong, “Orbital perturbation due to orbit-attitude coupling near asteroids,”Aircraft Engineering and Aerospace Technology, Vol. 90, 2018, pp. 104-113.
17. X. Sun, M. Xu, R. Zhong, “Dynamic analysis of the tether transportation system using absolute nodal coordinate formulation,”Acta Astronautica, Vol. 139, 2017, pp. 266-277.
18. X. Sun, R. Zhong, “Tether attachment point stabilization of noncooperative debris captured by a tethered space system”Acta Astronautica, 2019.
doi:10.1016/j.actaastro.2019.12.012