We stand with Ukraine  

Yan Xiao

Orcid: 0000-0002-1655-4695

Affiliations:
  • Ryerson University, Department of Aerospace Engineering, Toronto, ON, Canada
  • Harbin Institute of Technology, Harbin, China (PhD 2021)


According to our database1, Yan Xiao authored at least 11 papers between 2015 and 2023.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of five.

Timeline

Legend:

Book 
In proceedings 
Article 
PhD thesis 
Dataset
Other 

Links

Online presence:

On csauthors.net:

Bibliography

2023
A Predefined-Time Extended-State Observer-Based Approach for Velocity-Free Attitude Control of Spacecraft.
[BibTeX]
[DOI]
Dong Ye
,
An-Min Zou
,
Shengxin Sun
,
Yan Xiao
IEEE Trans. Aerosp. Electron. Syst., December, 2023

Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds.
[BibTeX]
[DOI]
Yan Xiao
,
Anton H. J. de Ruiter
,
Dong Ye
,
Zhaowei Sun
IEEE Trans. Aerosp. Electron. Syst., April, 2023

2022
Neural Network Based Finite-Time Attitude Tracking Control of Spacecraft With Angular Velocity Sensor Failures and Actuator Saturation.
[BibTeX]
[DOI]
Dong Ye
,
Yan Xiao
,
Zhaowei Sun
,
Bing Xiao
IEEE Trans. Ind. Electron., 2022

Adaptive Control on SE(3) for Spacecraft Pose Tracking With Harmonic Disturbance and Input Saturation.
[BibTeX]
[DOI]
Hongzhu Zhang
,
Dong Ye
,
Yan Xiao
,
Zhaowei Sun
IEEE Trans. Aerosp. Electron. Syst., 2022

Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds.
[BibTeX]
[DOI]
Yan Xiao
,
Anton H. J. de Ruiter
,
Dong Ye
,
Zhaowei Sun
IEEE Trans. Aerosp. Electron. Syst., 2022

Non-Singular and Continuous Back-Stepping Predefined-Time Attitude Tracking Control for Rigid Spacecraft with Predefined Bound.
[BibTeX]
[DOI]
Xiaolun Yang
,
Yvlong Yang
,
Dong Ye
,
Yan Xiao
,
Zhaowei Sun
Proceedings of the IECON 2022, 2022

2019
Observer-based continuous finite-time attitude control for rigid-flexible coupling satellites.
[BibTeX]
[DOI]
Yan Xiao
,
Dong Ye
,
Zhaowei Sun
Int. J. Control, 2019

2018
Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft.
[BibTeX]
[DOI]
Dong Ye
,
Yan Xiao
J. Frankl. Inst., 2018

2017
Velocity free finite time attitude control for satellites with flexible appendages.
[BibTeX]
[DOI]
Yan Xiao
,
Dong Ye
,
Zhaowei Sun
Proceedings of the IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society, Beijing, China, October 29, 2017

2015
Research on Attitude Adjustment Control for Large Angle Maneuver of Rigid-Flexible Coupling Spacecraft.
[BibTeX]
[DOI]
Yan Xiao
,
Dong Ye
,
Zhengxian Yang
,
Zhaowei Sun
Proceedings of the Intelligent Robotics and Applications - 8th International Conference, 2015

Quaternion-Based Adaptive Control for Staring-Mode Observation Spacecraft.
[BibTeX]
[DOI]
Lei Chen
,
Yan Xiao
,
Dong Ye
,
Changjun Li
Proceedings of the Intelligent Robotics and Applications - 8th International Conference, 2015


  Loading...