沈强 - 上海交通大学 - 航空航天学院

个人简介

沈强工作经历时间任职单位职务 2019年-至今上海交通大学航空航天学院长聘教轨副教授 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

研究领域

（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。

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

（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。