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ORCIDYan Xiao 0003
Person information
- affiliation: Ryerson University, Department of Aerospace Engineering, Toronto, ON, Canada
- affiliation (PhD 2021): Harbin Institute of Technology, Harbin, China
Other persons with the same name
- Yan Xiao — disambiguation page
- Yan Xiao 0001
![[0000-0003-2805-0619]](https://dblp.dagstuhl.de/img/orcid-mark.12x12.png "0000-0003-2805-0619")
— University of Texas at Arlington, College of Nursing and Health Innovation, TX, USA (and 3 more) - Yan Xiao 0002 — Sun Yat-sen University, School of Cyber Science and Technology, China (and 2 more)
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2020 – today
- 2024
[j8]Lixiang Wang, Dong Ye, Xianren Kong, Ming Liu, Yan Xiao:
Decentralized Receding Horizon Control for Satellite Cluster Reconfigurations With Successive Convexification Method. IEEE Trans. Aerosp. Electron. Syst. 60(5): 5920-5936 (2024)- 2023
- [j7]Yan Xiao, Anton H. J. de Ruiter, Dong Ye, Zhaowei Sun:
Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds. IEEE Trans. Aerosp. Electron. Syst. 59(2): 1534-1550 (2023) - [j6]Dong Ye, An-Min Zou, Shengxin Sun, Yan Xiao:
A Predefined-Time Extended-State Observer-Based Approach for Velocity-Free Attitude Control of Spacecraft. IEEE Trans. Aerosp. Electron. Syst. 59(6): 8051-8061 (2023) - 2022
- [j5]Yan Xiao, Anton H. J. de Ruiter, Dong Ye, Zhaowei Sun:
Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds. IEEE Trans. Aerosp. Electron. Syst. 58(3): 1922-1940 (2022) - [j4]Hongzhu Zhang, Dong Ye, Yan Xiao, Zhaowei Sun:
Adaptive Control on SE(3) for Spacecraft Pose Tracking With Harmonic Disturbance and Input Saturation. IEEE Trans. Aerosp. Electron. Syst. 58(5): 4578-4594 (2022) - [j3]Dong Ye, Yan Xiao, Zhaowei Sun, Bing Xiao:
Neural Network Based Finite-Time Attitude Tracking Control of Spacecraft With Angular Velocity Sensor Failures and Actuator Saturation. IEEE Trans. Ind. Electron. 69(4): 4129-4136 (2022) - [c4]Xiaolun Yang, Yvlong Yang, Dong Ye, Yan Xiao, Zhaowei Sun:
Non-Singular and Continuous Back-Stepping Predefined-Time Attitude Tracking Control for Rigid Spacecraft with Predefined Bound. IECON 2022: 1-6
2010 – 2019
- 2019
- [j2]Yan Xiao, Dong Ye, Zhaowei Sun:
Observer-based continuous finite-time attitude control for rigid-flexible coupling satellites. Int. J. Control 92(11): 2667-2680 (2019) - 2018
- [j1]Dong Ye, Yan Xiao:
Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft. J. Frankl. Inst. 355(18): 9209-9223 (2018) - 2017
- [c3]Yan Xiao, Dong Ye, Zhaowei Sun:
Velocity free finite time attitude control for satellites with flexible appendages. IECON 2017: 6596-6600 - 2015
- [c2]Yan Xiao, Dong Ye, Zhengxian Yang, Zhaowei Sun:
Research on Attitude Adjustment Control for Large Angle Maneuver of Rigid-Flexible Coupling Spacecraft. ICIRA (1) 2015: 24-33 - [c1]Lei Chen, Yan Xiao, Dong Ye, Changjun Li:
Quaternion-Based Adaptive Control for Staring-Mode Observation Spacecraft. ICIRA (1) 2015: 632-642
Coauthor Index
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