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基本信息 The basic information
姓名: 郭永

学院: 自动化学院


学历: 博士研究生毕业

学位: 工学博士


职称: 副教授

职务:


学科: 控制科学与工程





工作经历 Work Experience
2019/12 – 至今，西北工业大学，自动化学院， 副教授/硕士生导师
2019/07 – 至今，西北工业大学，自动化学院，硕士生导师
2016/08 – 2019/12，西北工业大学，自动化学院， 助理教授





教育经历 Education Experience
2012/03-2016/06，哈尔滨工业大学，航天学院控制科学与工程系，博士
2008/08-2010/07，哈尔滨工业大学，航天学院控制科学与工程系，硕士
2004/08-2008/07，哈尔滨工业大学，航天学院控制科学与工程系，本科



招生信息 Admission Information
硕士研究生，每年2-3名


联系方式 guoyong@nwpu.edu.cn



荣誉获奖 Awards Information
西北工业大学2018-2019学年校级优秀教学成果奖二等奖

2019年陕西省学位与研究生教育学会“研究生教育成果奖”二等奖



科学研究 Scientific Research
研究方向：
飞行器制导控制与仿真、航天器控制与仿真、编队飞行控制、智能控制


主持的科研项目：

1.国家自然科学基金国际(地区)合作与交流项目，绳系微小卫星编队飞行动力学分析与协同控制，2021/01-2022/12
2.海军装备部装备项目管理中心国防预先研究课题子课题，反舰导弹与蜂群无人机仿真建模技术研究2020/05-2021/04
3.陕西省自然科学基金青年项目，基于预设性能的微小卫星编队姿态饱和协同控制算法研究，2020/01-2021/12
4.中央高校基本科研业务费资助项目，具有安全约束的微小卫星编队飞行协同控制，2020/01-2021/12
5.航空科学基金项目，基于预设性能控制的空天飞行器直接力/气动力复合控制 2019/10-2021/09
6.中国博士后科学基金面上项目，基于预设性能控制的卫星编队飞行协同控制算法研究，2019/09-2021/08
7.国家自然科学基金青年项目，微小卫星编队飞行饱和有限时间协同控制算法研究，2019/01-2021/12
8.中央高校基本科研业务费资助项目，经管安环约束的复杂制造环境的“人机物”自主智能控制和决策的理论方法，2019/01-2019/12
9.中央高校基本科研业务费资助项目，航天器编队飞行有限时间协同控制方法研究，2017/01-2018/12
10.航空科学基金项目，空空导弹直接力/气动力复合控制技术研究，2016/10-2018/09



学术成果 Academic Achievements



(1)Guo Yong＃, Zhang Dawei, Li Ai-jun, Song Shenmin, Wang Chang-qing, Liu Zongming*，Finite-time control for autonomous rendezvous and docking under safe constraint[J]. Aerospace Science and Technology. 2021, 109: 106390.
(2)Guo Yong＃*, Guo Jin-hua, Liu Xiang, Li Ai-jun, and Wang Chang-qing. Finite-time blended control for air-to-air missile with lateral thrusters and aerodynamic surfaces[J]. Aerospace Science and Technology. 2020, 97: 105638.
(3)Sun Jing-Guang, Li Chuan-Ming, Guo Yong*, Wang Chang-qing, Li Peng. Adaptive fault tolerant control for hypersonic vehicle with input saturation and state constraints[J]. Acta Astronautica. 2020, 167: 302-313.
(4)Liu Chenguang, Wang Wei, Guo Yong*, Chen Shumin, Li Aijun, and Wang Changqing. Neural network based adaptive terminal sliding mode control for the deployment process of dual-body tethered satellite system. Proceedings of the Institution of Mechanical Engineers Part G- Journal of aerospace engineering. 2020,234(6):1157-1171.
(5) Guo Yong＃*, Huang Bing, Li Ai-jun, Wang Chang-qing. Integral sliding mode control for Euler‐Lagrange systems with input saturation. International Journal of Robust and Nonlinear Control. 2019, 29(4): 1088-1100.
(6) Guo Yong＃*, Huang Bing, Guo Jin-hua, Li Ai-jun, Wang Chang-qing. Velocity-free sliding mode control for spacecraft with input saturation. Acta Astronautica, 2019, 154: 1-8.
(7) Guo Yong＃*, Huang Bing, Song Shen-min, Li Ai-jun, Wang Chang-qing. Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode. Journal of Guidance, Control, and Dynamics, 2019, 42(2): 440-446.
(8) Guo Yong＃*, Huang bing, Wang Shuo, Li Ai-jun,Wang, Wang Chang-qing, Adaptive finite-time control for attitude tracking of the spacecraft under input saturation. Journal of Aerospace Engineering, 2018, 31(2).
(9) Guo Yong＃, Song Shen-min*, Li Xue-Hui, Zhu Zhibin, Finite-time output feedback control for the attitude of the spacecraft without unwinding. Proceedings of the Institution of Mechanical Engineers Part G- Journal of aerospace engineering, 2018, 232(8): 1421-1433.
(10) Guo Yong＃, Song Shen-min*, Li Xue-Hui. Backstepping sliding mode control for formation flying spacecraft. Aircraft Engineering and Aerospace Technology, 2018, 90(1):56–64.
(11) Guo Yong＃, Guo Jinhua, Song Shen-min*, Backstepping control for attitude tracking of the spacecraft under input saturation. Acta Astronautica, 2017, 138:318–325.
(12) Guo Yong＃, Song Shen-min*, Li Xue-Hui, Li Peng, Terminal sliding mode control for attitude tracking of spacecraft under input saturation. Journal of Aerospace Engineering, 2017, 30(3).
(13) Guo Yong＃*, Guo Jin-hua, Li Ai-jun, Wang Chang-qing, Attitude Coordination Control for Formation Flying Spacecraft Based on the Rotation Matrix. Journal of Aerospace Engineering, 2017, 30(5).
(14) Guo Yong＃, Song Shen-min*, Li Xue-Hui, Finite-time output feedback attitude coordination control for formation flying spacecraft without unwinding. Acta Astronautica, 2016, 122:159–174.
(15) Guo Yong＃, Song Shen-min*, Yan Zhibin, Finite-time coordination control for formation flying spacecraft without unwinding. Proceedings of the Institution of Mechanical Engineers Part G- Journal of aerospace engineering, 2016, 230(1):172–188.
(16) Guo Yong＃, Song Shen-min*, Li Xue-Hui, Quaternion-based finite time control for attitude tracking of spacecraft without unwinding. International Journal of Control, Automation, and Systems, 2015, 13(6):1351–1359.
(17) Guo Yong＃, Song Shen-min*, Li Xue-Hui. Terminal sliding mode control for attitude tracking of spacecraft based on the rotation matrix. Mathematical Problems in Engineering, 2015.
(18) Guo Yong＃, Song Shen-min*, Adaptive finite-time backstepping control for attitude tracking of spacecraft based on rotation matrix. Chinese Journal of Aeronautics, 2014, 27(2): 375–382.
(19) Guo Yong＃, Song Shen-min*, Deng Li-wei, Finite-time Coordination Control for Formation Flying Spacecraft. Journal of Systems Engineering and Electronics, 2014, 25(5): 859–867.
(20)郭永、宋申民、李学辉. 非合作交会对接的姿态和轨道耦合控制. 控制理论与应用. 2016, 33(5): 638-644.
(21)宋申民, 郭永, 李学辉. 航天器姿态跟踪有限时间饱和控制. 控制与决策, 2015, 30(11): 2004-2008.







社会兼职 Social Appointments
Automatica, IEEE Transactions on Automatic Control, IEEE Transactions on Industrial Informatics, Aerospace Science and Technology, Acta Astronautica, Journal of Aerospace Engineering, IET Control Theory & Applications,等期刊审稿人



团队信息 Team Information
团队负责人：李爱军教授（博导）
团队骨干教师：王长青教授（博导）、郭永副教授、杨庶助理教授