个人简历

教育与工作经历
1999/09 – 2003/09，北京航空航天大学，宇航学院，学士
2003/09 – 2006/06，北京航空航天大学，宇航学院，硕士
2006/06 – 2009/06，中国航天二院研究生院，飞行器设计系，博士
2009/07 – 2011/09，北京航空航天大学，宇航学院，博士后
2011/09 – 至今，北京理工大学，自动化学院

近期论文

代表性学术论文
1.1.Zhao Yao, Sheng Yongzhi*, Liu Xiangdong, Sliding mode control based guidance law with impact angle constraint, Chinese Journal of Aeronautics, Vol. 27, No. 1, pp.145-152, 2014.
2.Wang Liang, Sheng Yongzhi*, Liu Xiangdong, Continuous time-varying sliding mode based attitude control for reentry vehicle, Proceedings of the Institution of Mechanical Engineers, Part G Journal of Aerospace Engineering,
3.Wang Liang, Sheng Yongzhi*, Liu Xiangdong, A novel adaptive higher-order sliding mode control based on integral sliding mode, International Journal of Control, Automation, and Systems,
4.Geng Jie, Sheng Yongzhi*, Liu Xiangdong, Finite-time sliding mode attitude control for reentry vehicle with blended aerodynamic surfaces and reaction control system, Chinese Journal of Aeronautics,
5.Geng Jie, Sheng Yongzhi*, Liu Xiangdong, Time-varying nonsingular terminal sliding mode control for robot manipulators, Transactions of the Institute of Measurement and Control,
6.Wang, Liang; Sheng, Yongzhi; Lu, Xiangdong. High-order sliding mode attitude controller design for reentry flight. JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS 卷: 25 期: 5 页: 848-858 出版年: OCT 2014
7.Sheng, Yong-Zhi; Geng, Jie; Liu, Xiang-Dong. Nonsingular Finite-time Second Order Sliding Mode Attitude Control for Reentry Vehicle. INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS 卷: 13 期: 4 页: 853-866 出版年: AUG 2015
8.Zhao, Yao; Sheng, Yongzhi; Liu, Xiangdong. Impact angle constrained guidance for all-aspect interception with function-based finite-time sliding mode control. NONLINEAR DYNAMICS 卷: 85 期: 3 页: 1791-1804 出版年: AUG 2016
9.Zhao, Yao; Sheng, Yongzhi; Liu, Xiangdong; 等. Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method. JOURNAL OF AEROSPACE ENGINEERING 卷: 29 期: 4 文献号: 04016008 出版年: JUL 2016
10.Zhao, Yao; Sheng, Yongzhi; Liu, Xiangdong. Analytical impact time and angle guidance via time-varying sliding mode technique. ISA TRANSACTIONS 卷: 62 特刊: SI 页: 164-176 出版年: MAY 2016
11.Yongzhi Sheng, Liang Wang and Xiangdong Liu. A Novel Sliding Mode Control for a Class of Second-order Mechanical Systems. Asian Journal of Control. Volume 18, Issue 5
12.Zhao Yao, Sheng Yongzhi, Liu Xiangdong. Trajectory reshaping based guidance with impact time and angle constraints. CHINESE JOURNAL OF AERONAUTICS，2016 Vol. 29 (4): 984-994
13.Wang Liang, Sheng Yongzhi, Liu Xiangdong, A new higher order sliding mode control for a class of SISO systems, ICIC Express Letters, Part B: Applications, Vol. 5, No. 3, pp. 865-870, 2014.
14.Geng Jie, Sheng Yongzhi, Liu Xiangdong, Second-order time-varying sliding mode tracking control for uncertain systems, ICIC Express Letters Part B: applications, Vol. 4, No. 6, pp. 1683-1690, 2013.
15.Geng Jie, Sheng Yongzhi, Liu Xiangdong, Second-order time varying sliding mode control for reentry flight vehicle, International Journal of Intelligent Computing and Cybernetics, Vol. 6, No.3, pp.272-295, 2013.
16.王亮，刘向东，盛永智, 基于高阶滑模观测器的自适应时变滑模再入姿态控制, 控制与决策, 第29卷, 第2期, 281-286页, 2014.
17.王亮，刘向东，盛永智, 丛炳龙, 基于扰动观测器的巡航飞行器指数时变滑模控制, 宇航学报, 第34卷, 第8期, 1091-1099页, 2013.
18.耿洁, 刘向东, 盛永智, 丛炳龙, 飞行器再入段最优自适应积分滑模姿态控制，宇航学报，第34卷, 第9期, 1215-1223页, 2013.
19.王亮，刘向东，盛永智, 丛炳龙, 再入飞行器基于扰动观测器的指数时变滑模姿态控制系统设计, 中国空间科学技术, 第33卷, 第4期, 31-39页, 2013.
20.王亮，刘向东，盛永智, 丛炳龙, 基于指数时变滑模的再入飞行器控制系统设计,飞行力学, 第30卷, 第6期, 532-536页, 2012.