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

研究方向

近5年承担的科研项目

111.高超声速再入滑翔飞行器多约束全局滑模精确制导研究，国家自然科学基金
2.XXX飞行器模糊PID型全局滑模姿态控制，863项目
3.XXX飞行器时变滑模自适应控制方法成果库，国家重大科技工程
4.XXX飞行器PID型滑模制导与控制技术， 863项目
5.XXX飞行器xxx控制方法，国家重大科技工程
6.XXX飞行器多约束制导与强鲁棒控制技术，863项目
7.XXX飞行器时变滑模自适应控制方法研究，国家重大科技工程
8.XXX姿态确定与控制技术研究，航天科技集团横向
9.XXX动力学仿真分析，航天科技集团横向
10.XXX仿真平台软件，航天科技集团横向
11.带大型附件卫星控制与结构一体化仿真平台软件，航天科技集团横向
12.XXX复合控制技术研究，航天科技集团横向
13.XXX最优滑模控制技术研究，航天科技集团横向
14.XXX制导控制技术研究，航天科技集团横向

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.

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