Basic Information
Telephone: 0755-26915894
Address： Room 719, Research Building, Harbin Institute of Technology Shenzhen
Email address: yuechengfei@hit.edu.cn
Personal Profile
Yue Chengfei, male, born in 1989, associate professor. He has published more than 20 papers.
The Research Direction
1. Conceptual design of spacecraft
2. Attitude control of spacecraft
3. Space robot system
Education Experience
2009 -- 2013, Harbin Institute of Technology, Spacecraft Design, Bachelor
2015-2019, National University of Singapore, Electrical and Computer Engineering, Doctor.
2020 Shenzhen peacock plan talents (Class C)
Postgraduate Courses:
"Spacecraft Design and Optimization" Fall semester.
" Dynamic and Control of satellites" Fall semester.
（Selected Journal Publications:）
1. Yue C. F., Shen Q., Cao X.B., Wang F., Goh C.H., Lee T.H. Fault Modeling of General Momentum Exchange Devices in Spacecraft Attitude Control Systems. Journal of the Franklin Institute. 2020 Apr 10. (JCR Q1)
2. Yue C. F., Wu F., Wang F., Cao X.B., Shen Q., Kumar K.D. Two Parallel Single Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver. IEEE Transactions on Aerospace and Electronic Systems. 2020 Feb 14. (JCR Q1)
3. Yue C. F. Wang F, Cao X, Shen Q, Chen X. Robust fault-tolerant attitude tracking with guaranteed prescribed performance. Journal of the Franklin Institute. 2020 Jan 1;357(1):229-53. (JCR Q1)
4. Yue C. F., Kumar KD, Shen Q, Goh CH, Lee TH. Attitude stabilization using two parallel single-gimbal control moment gyroscopes. Journal of Guidance, Control, and Dynamics. 2019 Jun;42(6):1353-64. (JCR Q1)
5. Cao X. B., Yue C. F., Liu M., Wu B.L. Time efficient spacecraft maneuver using constrained torque distribution. Acta Astronautica，2016， 123:320-329. (JCR Q1)
6. Shen Q, Yue C. F.*, Yu X, Goh CH. Fault Modeling, Estimation, and Fault-Tolerant Steering Logic Design for Single-Gimbal Control Moment Gyro. IEEE Transactions on Control Systems Technology. 2020 Feb 18. (JCR Q1)
7. Yao, W.R., Qi N.M,, Yue C.F., Wan N. Curvature-Bounded Lengthening and Shortening for Restricted Vehicle Path Planning. IEEE Transactions on Automation Science and Engineering. 2020,17(1):15-28. (JCR Q1)
8. Shen Q, Yue C. F., Goh C. H., Wang D. W., Active fault-tolerant control system design for spacecraft attitude maneuvers with actuator saturation and faults." IEEE Transactions on Industrial Electronics，2019,66(5): 3763-3772. (JCR Q1)
9. Shen Q., Yue C. F., Goh C. H., Wu B. L., Wang D. W. Rigid-body attitude stabilization with attitude and angular rate constraints. Automatica. 2018, 90: 157-163.(JCR Q1)
10. Cao X. B., Yue C. F., Liu M. Flexible satellite attitude maneuver via constrained torque distribution and active vibration suppression. Aerospace Science and Technology. 2017, 67(August): 387-397.(JCR Q1)
Overview
