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Faculty
SHEN Qiang
Tenured-track Associate Professor
A239, Aerospace Building qiangshen@sjtu.edu.cn https://qiangs.github.io/

Educational Background

  • 2011 - 2012, Nanyang Technological University, Singapore, School of Electrical and Electronic Engineering, Doctor
  • 2006 - 2010, Northwestern Polytechnical University, P.R. China, Bachelor

Work Experience

  • 2019-Present,School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai, P. R. China,Associate Professor
  • 2017-2019,Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ, USA,Postdoctoral Scholar
  • 2015-2017,Temasek Laboratories, National University of Singapore, Singapore,

Research Interests

  • Fault Diagnosis and Tolerant Control
  • Formation flying control
  • Task and trajectory planning

Major Research Projects

  • National Natural Science Foundation of China (No. 62103275)
  • Shanghai Sailing Program (No. 20YF1421600)
  • Natural Science Foundation of Shanghai (No. 20ZR1427000)

Representative Papers And Monographs

  • Z. Y. Kang, Q. Shen, S. F. Wu and C. Damaren, ‘‘Saturated Adaptive Pose Tracking Control of Spacecraft on SE(3) under Attitude Constraints and Obstacle-Avoidance Constraints,” Automatica, 159:111367, Jan. 2024.
  • X. Y. Sun, Q. Shen and S. F. Wu, ‘‘Fuzzy Supervised Learning-Based Model-Free Adaptive Fault-Tolerant Spacecraft Attitude Control with Deferred Asymmetric Constraints,” IEEE Transactions on Aerospace and Electronic Systems, 59(5):8884-8900, 2023.
  • Z. Y. Kang, Q. Shen, S. F. Wu and C. Damaren, ‘‘Prescribed Performance-Based Fixed-Time Adaptive Control Allocation for Over-Actuated Spacecraft,” Journal of Guidance, Control, and Dynamics, 46(2):390-400, 2023.
  • Q. Shen, R. C. Niu and S. Z. Yong, ‘‘Tractable Model Discrimination for Safety-Critical Systems with Disjunctive and Coupled Constraints,” Nonlinear Analysis: Hybrid Systems, 46:101217, 2022.
  • Q. Shen, C. F. 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, 29(1):428-435, 2021.
  • 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):3763-3772, 2019.
  • 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, 90:157-163, 2018.
  • 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):1338-1349, 2018.
  • Q. Shen, D. W. Wang, S. Q. Zhu and E. K. Poh, ‘‘Inertia-Free Fault-Tolerant Spacecraft Attitude Tracking Using Control Allocation,” Automatica, 62:114-121, Dec. 2015.
  • 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):1131-1138, May 2015.

Honorary Information

  • Editorial Board Members, Aerospace Systems, Springer
  • ICGNC FENG Ru Best Paper Award
  • Overseas High-Level Talents Program (Shanghai Specially Recruited Experts)
  • Chinese Government Award for Outstanding Self-Financed Student Abroad
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