Name: SUN Liang

Title: Assistant Professor

School: School of Astronautics

Email: sunliang@buaa.edu.cn

Tel: +86(10)82339194

EDUCATION:

2009.9-2014.1: PhD in Beihang University, China; Specialty: Aerospace Science and Technology.

2007.9-2009.8: Master Degree in Harbin Institute of Technology, China; Specialty: Mechanics.

2001.9-2005.8: Bachelor Degree in Harbin Institute of Technology, China. Specialty: Automation.

PROFESSORNAL EXPERIENCE:

2014.7-now: working as an assistant professor at Beihang University, China.

2011.10-2012.10: working as a visiting scholar at Michigan State University, USA.

2005.8-2007.8: working as an assistant engineer at China Academy of Space Technology (CAST).

RESEARCH INTERESTS:

1. Satellite Attitude Determination and Control; 2. Nonlinear Dynamics; 3. Robot Control; 4. Spacecraft Design.

PUBLICATIONS:

[1] Liang Sun, Guowei Zhao, Hai Huang. Stability and control of tethered satellite with chemical propulsion in orbital plane [J]. Nonlinear dynamics. 2013, 74(4): 1113-1131.

[2] Guowei Zhao, Liang Sun, Shuping Tan, Hai Huang. Librational characteristics of a dumbbell modeled tethered satellite under small, continuous, constant thrust [J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering. 2013, 227(5): 857-872.

[2] Guowei Zhao, Liang Sun, Hai Huang. Thrust control of tethered satellite with a short constant tether in orbital maneuvering [J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering. 2014, 228(14): 2569-2586.                          

[4] Jianguo Zhao, Bo Song, Ning Xi, Liang Sun, et al. Non-vector space approach for nanoscale motion control [J]. Automatica, 2014, 50(7): 1835-1842

[5] Kaixin Zhou, Hai Huang, Xinsheng Wang, Liang Sun. Magnetic attitude control for Earth-pointing satellites in the presence of gravity gradient [J]. Aerospace Science & Technology. 2017(60): 115-123.

[6] Liang Sun, Guowei Zhao, Hai Huang, Ming Chen. Optimal Control Scheme of the Tethered System for Orbital Transfer under a Constant Thrust [J]. International Journal of Aerospace Engineering. 2018(2):1-12

[7] Liang Sun, Guowei Zhao, Hai Huang. Effect of mass variation on dynamics of tethered system in orbital maneuvering [J]. 2018, 146: 15-23.