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基本信息 The basic information
姓名: 刘闯

学院: 航天学院


学历: 博士研究生毕业

学位: 工学博士


职称: 副教授

职务:


学科: 航空宇航科学-飞行器设计


邮箱: cliu@nwpu.edu.cn




工作经历 Work Experience
2019.07-至今，西北工业大学，航天学院，副教授/硕导



教育经历 Education Experience
2009.08-2013.07，哈尔滨工业大学，飞行器设计，学士
2013.09-2015.07，哈尔滨工业大学，飞行器设计，硕士
2015.09-2019.04，哈尔滨工业大学，航空宇航科学与技术，博士
2017.10-2018.10，加拿大约克大学，航天工程，访学



荣誉获奖 Awards Information
2018年，博士研究生国家奖学金
2019年，春晖创新成果奖
2020年，COSPAR青年科学家杰出论文奖（COSPAR Outstanding Paper Award for Young Scientists）



科学研究 Scientific Research
航天器姿态动力学与控制
航天器轨道交会控制



学术成果 Academic Achievements
[1] Chuang Liu, Keke Shi, Xiaokui Yue, Zhaowei Sun. Inertia-Free Saturated Output Feedback Attitude Stabilization for Uncertain Spacecraft. International Journal of Robust and Nonlinear Control, 2020, 30(13): 5101-5121.
[2] Chuang Liu, Xiaokui Yue, Keke Shi, Zhaowei Sun. Inertia-Free Attitude Stabilization for Flexible Spacecraft with Active Vibration Suppression. International Journal of Robust and Nonlinear Control, 2019, 29(18): 6311-6336.
[3] Chuang Liu, George Vukovich, Zhaowei Sun, Keke Shi. Observer-Based Fault Tolerant Attitude Control for Spacecraft with Input Delay. Journal of Guidance, Control and Dynamics, 2018, 41(9): 2041-2053.
[4] Chuang Liu, Zhaowei Sun, Keke Shi, Feng Wang. Robust dynamic output feedback control for attitude stabilization of spacecraft with nonlinear perturbations. Aerospace Science and Technology, 2017, 64: 102-121.
[5] Chuang Liu, Dong Ye, Keke Shi, Zhaowei Sun. Robust high-precision attitude control for flexible spacecraft with improved mixed H₂/H_∞ control strategy under poles assignment constraint. Acta Astronautica, 2017, 136: 166-175.
[6] Chuang Liu, George Vukovich, Keke Shi, Zhaowei Sun. Robust fault tolerant non-fragile H_∞ attitude control for spacecraft via stochastically intermediate observer. Advances in Space Research, 2018, 62(9): 2631-2648.
[7] Chuang Liu, Keke Shi, Zhaowei Sun. Robust H_∞ controller design for attitude stabilization of flexible spacecraft with input constraints. Advances in Space Research, 2019, 63(5): 1498-1522.
[8] Chuang Liu, Zhaowei Sun, Keke Shi, Feng Wang. Robust non-fragile state feedback attitude control for uncertain spacecraft with input saturation. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(2): 246-259.
[9] Chuang Liu, Zhaowei Sun, Dong Ye, Keke Shi. Robust Adaptive Variable Structure Tracking Control for Spacecraft Chaotic Attitude Motion. IEEE Access, 2018, 6: 3851-3857.
[10] Chuang Liu, Keke Shi, Zhaowei Sun. Spacecraft chaotic attitude control with certain actuator failure based on integral sliding mode. Journal of Engineering Research, 2018, 6(1): 153-169.
[11] Keke Shi, Chuang Liu^*, James D. Biggs, Zhaowei Sun, Xiaokui Yue. Observer-based control for spacecraft electromagnetic docking. Aerospace Science and Technology, 2020, 99: 105759.
[12] Keke Shi, Chuang Liu^*, Zhaowei Sun. Constrained fuel-free control for spacecraft electromagnetic docking in elliptical orbits. Acta Astronautica, 2019, 162: 14-24.
[13] Keke Shi, Chuang Liu^*, Zhaowei Sun, Xiaokui Yue. Disturbance Observer-Based Attitude Stabilization for Rigid Spacecraft with Input MRCs. Advances in Space Research, 2020, 66(3): 689-701.
[14] Keke Shi, Chuang Liu^*, Zhaowei Sun, George Vukovich. A Novel Robust Non-fragile Control Approach for a Class of Uncertain Linear Systems with Input Constraints. Transactions of the Institute of Measurement and Control, 2019, 41(8): 2365-2373.
[15] LeiXing, Jianqiao Zhang*, Chuang Liu*, et al. Fuzzy-logic-based adaptive event-triggered sliding mode control for spacecraft attitude tracking. Aerospace Science and Technology, 2020: 106394.
[16] Chuang Liu, Zhaowei Sun, Keke Shi, Feng Wang. Mixed H₂/H_∞ Control Approach and its Application in Satellite Attitude Control System. International Journal of Engineering Research in Africa, 2016, 25: 89-97.
[17] Zhaowei Sun, Chuang Liu, Keke Shi, Jianqiao Zhang. Underactuated Spacecraft Chaotic Attitude Control Based on Exponential Reaching Law// 2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE). IEEE, 2017: 615-619.



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