沈强
职务：航空宇航信息与控制系主任、长聘教轨副教授
电子邮件：qiangshen@sjtu.edu.cn
办公地址：诸侯快讯导航ok1188诸侯快讯官方
个人主页：https://qiangs.github.io/
工作经历
| 时间 | 任职单位 | 职务 |
|---|---|---|
| 2019年-至今 | 诸侯快讯导航ok1188诸侯快讯官方 | 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。
