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Dong Ye 0005
Person information
- affiliation (PhD 2013): Harbin Institute of Technology, Research Center of Satellite Technology, China
- not to be confused with: Dong Ye 0003
Other persons with the same name
- Dong Ye — disambiguation page
- Dong Ye 0001 — University of Metz, France
- Dong Ye 0002
— Middle Tennessee State University, Murfreesboro, TN, USA
- Dong Ye 0003
- Dong Ye 0004 — Northeastern University, Boston, MA, USA
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2020 – today
- 2024
- [j25]Lixiang Wang
Decentralized Receding Horizon Control for Satellite Cluster Reconfigurations With Successive Convexification Method. IEEE Trans. Aerosp. Electron. Syst. 60(5): 5920-5936 (2024) - [j24]Jiang Shao
Feasibility Analysis and Synchronization Control for Underactuated Spacecraft Formation Hovering. IEEE Trans. Control. Syst. Technol. 32(1): 241-249 (2024) - [j23]Dong Ye
PO-SRPP: A Decentralized Pivoting Path Planning Method for Self-Reconfigurable Satellites. IEEE Trans. Ind. Electron. 71(11): 14318-14327 (2024) - 2023
- [j22]Haoyue Zhang, Peng Xu
A Systematic Approach for Inertial Sensor Calibration of Gravity Recovery Satellites and Its Application to Taiji-1 Mission. Remote. Sens. 15(15): 3817 (2023) - [j21]Yan Xiao
Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds. IEEE Trans. Aerosp. Electron. Syst. 59(2): 1534-1550 (2023) - [j20]Siyuan Li
Collision-Free Flocking Control for Satellite Cluster With Constrained Spanning Tree Topology and Communication Delay. IEEE Trans. Aerosp. Electron. Syst. 59(4): 4134-4146 (2023) - [j19]Dong Ye
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
- [j18]Ruixia Liu, Ming Liu, Dong Ye, Yang Yu:
Event-triggered adaptive fixed-time fuzzy control for uncertain nonlinear systems with unknown actuator faults. Inf. Sci. 612: 344-360 (2022) - [j17]Dong Ye
Predefined-Time Predefined-Bounded Attitude Tracking Control for Rigid Spacecraft. IEEE Trans. Aerosp. Electron. Syst. 58(1): 464-472 (2022) - [j16]Yan Xiao
Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds. IEEE Trans. Aerosp. Electron. Syst. 58(3): 1922-1940 (2022) - [j15]Hongzhu Zhang
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) - [j14]Dong Ye
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) - [c5]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 - 2021
- [j13]Qiliang Song
Autonomous reconfiguration of homogeneous pivoting cube modular satellite by deep reinforcement learning. J. Syst. Control. Eng. 235(10) (2021) - 2020
- [j12]Jianqiao Zhang
Extended-State-Observer-Based Event-Triggered Orbit-Attitude Tracking for Low-Thrust Spacecraft. IEEE Trans. Aerosp. Electron. Syst. 56(4): 2872-2883 (2020)
2010 – 2019
- 2019
- [j11]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) - [j10]Chunbao Wang, Dong Ye, Zhongcheng Mu
Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics. Sensors 19(24): 5568 (2019) - [j9]Dong Ye, Wei Lu, Zhongcheng Mu
Compound control for autonomous docking to a three-axis tumbling target. Trans. Inst. Meas. Control 41(4): 911-924 (2019) - 2018
- [j8]Chuang Liu
Robust Adaptive Variable Structure Tracking Control for Spacecraft Chaotic Attitude Motion. IEEE Access 6: 3851-3857 (2018) - [j7]Dong Ye, Yan Xiao:
Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft. J. Frankl. Inst. 355(18): 9209-9223 (2018) - [j6]Dong Ye, Xiao Zhang, Xucheng Wan, Zhaowei Sun:
Finite time control strategy for satellite attitude maneuver based on hybrid actuator. Trans. Inst. Meas. Control 40(9): 2798-2806 (2018) - [c4]Xiaoyu Yu, Dong Ye:
Performance Comparison of Multiples and Target Detection with Imager-driven Processing Mode for Ultrafast-Imager: (Abstract Only). FPGA 2018: 293 - 2017
- [j5]Ruixia Liu
Adaptive Sliding Mode Control for Spacecraft Autonomous Rendezvous With Elliptical Orbits and Thruster Faults. IEEE Access 5: 24853-24862 (2017) - [j4]Qi Xia, Naiming Qi, Dong Ye, Yubo Guo, Tianye Wang:
Real-time calibration of space zoom cameras based on fixed stars. IET Comput. Vis. 11(5): 342-349 (2017) - [j3]Jianqiao Zhang
Adaptive fuzzy finite-time control for spacecraft formation with communication delays and changing topologies. J. Frankl. Inst. 354(11): 4377-4403 (2017) - [j2]Dong Ye, Yue Zhao, Jianxing Liu
A simple structure robust attitude synchronization with input saturation. J. Frankl. Inst. 354(14): 6062-6077 (2017) - [j1]Lixian Zhang, Xunyuan Yin, Zepeng Ning, Dong Ye:
Robust Filtering for a Class of Networked Nonlinear Systems With Switching Communication Channels. IEEE Trans. Cybern. 47(3): 671-682 (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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