刘闯


的个人主页 http://teacher.nwpu.edu.cn/cliu

  被浏览次数:7151

基本信息 The basic information

刘闯

航天学院

博士研究生毕业

工学博士

副教授

航空宇航科学-飞行器设计

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

l  2009.08-2013.07,哈尔滨工业大学,飞行器设计,学士

l  2013.09-2015.07,哈尔滨工业大学,飞行器设计,硕士

l  2015.09-2019.04,哈尔滨工业大学,航空宇航科学与技术,博士

l  2017.10-2018.10,加拿大约克大学,航天工程,访学

招生信息 Admission Information

硕士招生专业:飞行器设计、航天工程、控制工程 硕士生 2-3 名


联系方式:liuchuangforever@msn.com

荣誉获奖 Awards Information

l 2021年,陕西省自然科学一等奖(R2)

l 2021年,陕西省科协青年人才托举计划

l 2020年,国际空间研究委员会青年科学家杰出论文奖(COSPAR Outstanding Paper Award for Young Scientists)

l 2019年,春晖创新成果奖

l 2018年,博士研究生国家奖学金

科学研究 Scientific Research

l  航天器姿态动力学与控制

l  航天器轨道交会控制

l  大规模星群协同控制

l  鲁棒控制、容错控制

学术成果 Academic Achievements

l   以第一/通信作者在IJRNC(封面论文1篇)、JGCD、AST等国际著名航天动力学与控制期刊上发表高水平论文20余篇

l   主持国家自然科学基金、陕西省自然科学基金、中国博士后面上资助、陕西省科协青年人才托举计划项目等

l   出版学术著作1部


发表论文:

[1] Chuang Liu, Xiaokui Yue, Jianqiao Zhang, Keke Shi. Active Disturbance Rejection Control for Delayed Electromagnetic Docking of Spacecraft in Elliptical Orbits. IEEE Transactions on Aerospace and Electronic Systems, 2021, doi: 10.1109/TAES.2021.3130830.

[2] Chuang Liu, Xiaokui Yue, Ziyu Yang. Are nonfragile controllers always better than fragile controllers in attitude control performance of post-capture flexible spacecraft?. Aerospace Science and Technology, 2021, 118: 107053.

[3] 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.

[4] 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.

[5] 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.

[6] 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.

[7] 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.

[8] 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.

[9] 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.

[10] 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.

[11] 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.

[12] 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.

[13] Keke Shi, Chuang Liu*, Zhaowei Sun. Constrained fuel-free control for spacecraft electromagnetic docking in elliptical orbits. Acta Astronautica, 2019, 162: 14-24.

[14] Keke Shi, Chuang Liu*, Zhaowei Sun, Xiaokui Yue. Coupled Orbit-Attitude Dynamics and Trajectory Tracking Control for Spacecraft Electromagnetic Docking. Applied Mathematical Modelling, 2022, 101: 553-572.

[15] 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.

[16] 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.

[17] Siyuan Li, Chuang Liu*, Zhaowei Sun. Finite-time distributed hierarchical control for satellite cluster with collision avoidance. Aerospace Science and Technology, 2021, 114: 106750.

[18] Lei Xing, Jianqiao Zhang, Chuang Liu*, Xiao Zhang. Fuzzy-logic-based adaptive event-triggered sliding mode control for spacecraft attitude tracking. Aerospace Science and Technology, 2021, 108: 106394.

[19] Jianqiao Zhang, Xianglong Kong, Chuang Liu*, Qing Deng, Keke Shi. Agile attitude maneuver with active vibration-suppression for flexible spacecraft. Journal of the Franklin Institute, 2022, 359(3): 1172-1195.

[20] Zhiwei Hao, Xiaokui Yue, Haowei Wen, Chuang Liu*. Full-state-constrained non-certainty-equivalent adaptive control for satellite swarm subject to input fault. IEEE/CAA Journal of Automatica Sinica, 2022, 9(3): 482-495.

[21] 刘闯,岳晓奎.空间非合作航天器抓捕后姿态抗干扰控制.航空学报,2021, 42(11): 524289.


出版著作:

[1] Chuang Liu, Xiaokui Yue, Keke Shi, Zhaowei Sun. Spacecraft Attitude Control: A Linear Matrix Inequality Approach. Science/Elsevier Press, 2022, ISBN: 978-0-323-99005-9.


申请/授权发明专利:

[1] 孙兆伟,刘闯,石珂珂,王雪峰,叶东,张剑桥,邢雷.一种部分执行机构故障下航天器混沌姿态控制方法,2018-9-11,ZL201610494493.8. 

[2] 刘闯,杨子煜,岳晓奎,王时玉.一种非合作柔性组合体航天器姿态稳定混合非脆弱控制方法,2021-3-31,CN202110350727.2.

[3] 刘闯,吕佰梁,岳晓奎,代洪华.一种航天器姿态/故障/干扰协同观测与容错抗干扰控制方法,2021-9-30,CN202111173687.5.