基本介紹
- 中文名：盛永智
- 學位/學歷：博士
- 職業：教師
- 任職院校：北京理工大學
個人經歷,學術成果,
個人經歷
1999/09 – 2003/09，北京航空航天大學，宇航學院，學士
2003/09 – 2006/06，北京航空航天大學，宇航學院，碩士
2006/06 – 2009/06，中國航天二院研究生院，飛行器設計系，博士
2009/07 – 2011/09，北京航空航天大學，宇航學院，博士後
2011/09 – ，北京理工大學，自動化學院
學術成果
科研項目
111.高超聲速再入滑翔飛行器多約束全局滑模精確制導研究，國家自然科學基金
2.XXX飛行器模糊PID型全局滑模姿態控制，863項目
3.XXX飛行器時變滑模自適應控制方法成果庫，國家重大科技工程
4.XXX飛行器PID型滑模製導與控制技術， 863項目
5.XXX飛行器xxx控制方法，國家重大科技工程
6.XXX飛行器多約束制導與強魯棒控制技術，863項目
7.XXX飛行器時變滑模自適應控制方法研究，國家重大科技工程
8.XXX姿態確定與控制技術研究，航天科技集團橫向
9.XXX動力學仿真分析，航天科技集團橫向
10.XXX仿真平台軟體，航天科技集團橫向
11.帶大型附屬檔案衛星控制與結構一體化仿真平台軟體，航天科技集團橫向
12.XXX複合控制技術研究，航天科技集團橫向
13.XXX最優滑模控制技術研究，航天科技集團橫向
14.XXX制導控制技術研究，航天科技集團橫向
代表性學術論文
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 頁: 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 頁: 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 頁: 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 文獻號: 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 頁: 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，劉向東，盛永智, 基於高階滑模觀測器的自適應時變滑模再入姿態控制, 控制與決策, 第29卷, 第2期, 281-286頁, 2014.
17.王亮，劉向東，盛永智, 叢炳龍, 基於擾動觀測器的巡航飛行器指數時變滑模控制, 宇航學報, 第34卷, 第8期, 1091-1099頁, 2013.
18.耿潔, 劉向東, 盛永智, 叢炳龍, 飛行器再入段最優自適應積分滑模姿態控制，宇航學報，第34卷, 第9期, 1215-1223頁, 2013.
19.王亮，劉向東，盛永智, 叢炳龍, 再入飛行器基於擾動觀測器的指數時變滑模姿態控制系統設計, 中國空間科學技術, 第33卷, 第4期, 31-39頁, 2013.
20.王亮，劉向東，盛永智, 叢炳龍, 基於指數時變滑模的再入飛行器控制系統設計,飛行力學, 第30卷, 第6期, 532-536頁, 2012.
