航空宇航信息与控制系
沈强

沈强

职务:航空宇航信息与控制系副主任、长聘教轨副教授

电子邮件:qiangshen@sjtu.edu.cn

办公地址:bob综合体育app下载手机版

        个人主页:https://qiangs.github.io/

 

工作经历

时间 任职单位 职务
2019年-至今 bob综合体育app下载手机版 长聘教轨副教授
2017年-2019年 亚利桑那州立大学机械工程系 博士后
2015年-2017年 新加坡国立大学淡马锡实验室 研究科学家

教育背景

时间 毕业院校 学历
2011年-2016年 新加坡南洋理工大学 博士
2006年-2010年 西北工业大学 本科

研究方向

(1)航天器动力学和控制;

(2)故障诊断和容错控制;

(3)模型区分和验证。

代表性论文专著

(1)Q. Shen, C. F. Yue, C. H. Goh, B. L. Wu and D. W. Wang, “Rigid-Body Attitude Stabilization with Attitude and Angular Rate Constraints,” Automatica, 90, pp. 157-163, 2018.  

(2)Q. Shen, D. W. Wang, S. Q. Zhu and E. K. Poh, “Inertia-Free Fault-Tolerant Spacecraft Attitude Tracking Using Control Allocation,” Automatica, 62, pp. 114-121, 2015. 

(3)Q. Shen, C. Yue, X. Yu and C. H. Goh, “Fault Modeling, Estimation and Fault-Tolerant Steering Logic Design for Single Gimbal Control Moment Gyro,” IEEE Transactions on Control Systems Technology, 2020, DOI: 10.1109/TCST.2020.2971959.

(4)Q. Shen, D. W. Wang, S. Q. Zhu and E. K. Poh, “Robust Control Allocation for Spacecraft Attitude Tracking under Actuator Faults,” IEEE Transactions on control systems Technology, 25(3), pp. 1068-1075, 2017.  

(5)Q. Shen, D. W. Wang, S. Q. Zhu and E. K. Poh, “Integral-Type Sliding Mode Fault-Tolerant Control for Attitude Stabilization of Spacecraft,” IEEE Transactions on Control Systems Technology, 23(3), pp. 1131-1138, 2015. 

(6)Q. Shen, C. F. Yue, C. H. Goh and D. W. Wang, “Active Fault-Tolerant Control System Design for Spacecraft Attitude Maneuvers with Actuator Saturation and Faults,” IEEE Transactions on Industrial Electronics, 66(5), pp. 3763-3772, 2019. 

(7)Q. Shen, C. F. Yue, C. H. Goh, B. L. Wu and D. W. Wang, “Rigid-Body Attitude Tracking Control under Actuator Faults and Angular Velocity Constraints,” IEEE/ASME Transactions on Mechatronics, 23(3), pp. 1338-1349, 2018. 

(8)Q. Shen, D. W. Wang, S. Q. Zhu and E. K. Poh, “Finite-Time Fault-Tolerant Attitude Stabilization for Spacecraft with Actuator Saturation,” IEEE Transactions on Aerospace and Electronic Systems, 51(3), pp. 2390-2405, Jul. 2015.

(9)Q. Shen, C. F. Yue and C. H. Goh, “Velocity-Free Attitude Reorientation of a Flexible Spacecraft with Attitude Constraints,” Journal of Guidance, Control, and Dynamics, 40(5), pp. 1293-1299, 2017.

(10)C. F. Yue, F. Wu, F. Wang, X. B. Cao, Q. Shen and K. D. Kumar, “Two Parallel Single Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver,” IEEE Transactions on Aerospace and Electronic Systems, 2020, DOI:10.1109/TAES.2020.2974053.

(11)C. F. Yue, K. D. Kumar, Q. Shen, C. H. Goh and T. H. Lee, “Attitude Stabilization Using Two Parallel Single Gimbal Control Moment Gyros,” Journal of Guidance, Control, and Dynamics, 42(6), pp.1353-1364, 2019.  

(12)S. Q. Zhu, D. W. Wang, Q. Shen and E. K. Poh, “Satellite Attitude Stabilization Control with Actuator Faults,” Journal of Guidance, Control, and Dynamics, 40(5), pp. 1304-1313, 2017.  

(13)B. L. Wu, Q. Shen and X. B. Cao, “Event-Triggered Attitude Control of Spacecraft,” Advances in Space Research, 61(3), pp. 927-934, 2018.  

(14)C. F. Yue, F. Wang, X. B. Cao, Q. Shen, X. Q. Chen, “Robust Fault-Tolerant Attitude Tracking with Guaranteed Prescribed Performance,” Journal of The Franklin Institute, 357(1), pp.229-253, 2020.   

 

学术兼职

(1)IEEE Member;

(2)包括Automatica, IEEE TCST, IEEE TIE, IEEE/ASME TMech等30多个期刊和会议审稿人。

 

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