Dong Ye

Orcid: 0000-0002-7400-7104

Affiliations:
  • Harbin Institute of Technology, Research Center of Satellite Technology, China (PhD 2013)


According to our database1, Dong Ye authored at least 30 papers between 2015 and 2024.

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

Timeline

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Bibliography

2024
PO-SRPP: A Decentralized Pivoting Path Planning Method for Self-Reconfigurable Satellites.
IEEE Trans. Ind. Electron., November, 2024

Decentralized Receding Horizon Control for Satellite Cluster Reconfigurations With Successive Convexification Method.
IEEE Trans. Aerosp. Electron. Syst., October, 2024

Feasibility Analysis and Synchronization Control for Underactuated Spacecraft Formation Hovering.
IEEE Trans. Control. Syst. Technol., January, 2024

2023
A Predefined-Time Extended-State Observer-Based Approach for Velocity-Free Attitude Control of Spacecraft.
IEEE Trans. Aerosp. Electron. Syst., December, 2023

Collision-Free Flocking Control for Satellite Cluster With Constrained Spanning Tree Topology and Communication Delay.
IEEE Trans. Aerosp. Electron. Syst., August, 2023

A Systematic Approach for Inertial Sensor Calibration of Gravity Recovery Satellites and Its Application to Taiji-1 Mission.
Remote. Sens., August, 2023

Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds.
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.
IEEE Trans. Ind. Electron., 2022

Adaptive Control on SE(3) for Spacecraft Pose Tracking With Harmonic Disturbance and Input Saturation.
IEEE Trans. Aerosp. Electron. Syst., 2022

Predefined-Time Predefined-Bounded Attitude Tracking Control for Rigid Spacecraft.
IEEE Trans. Aerosp. Electron. Syst., 2022

Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds.
IEEE Trans. Aerosp. Electron. Syst., 2022

Event-triggered adaptive fixed-time fuzzy control for uncertain nonlinear systems with unknown actuator faults.
Inf. Sci., 2022

Non-Singular and Continuous Back-Stepping Predefined-Time Attitude Tracking Control for Rigid Spacecraft with Predefined Bound.
Proceedings of the IECON 2022, 2022

2021
Autonomous reconfiguration of homogeneous pivoting cube modular satellite by deep reinforcement learning.
J. Syst. Control. Eng., 2021

2020
Extended-State-Observer-Based Event-Triggered Orbit-Attitude Tracking for Low-Thrust Spacecraft.
IEEE Trans. Aerosp. Electron. Syst., 2020

2019
Compound control for autonomous docking to a three-axis tumbling target.
Trans. Inst. Meas. Control, 2019

Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics.
Sensors, 2019

Observer-based continuous finite-time attitude control for rigid-flexible coupling satellites.
Int. J. Control, 2019

2018
Finite time control strategy for satellite attitude maneuver based on hybrid actuator.
Trans. Inst. Meas. Control, 2018

Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft.
J. Frankl. Inst., 2018

Robust Adaptive Variable Structure Tracking Control for Spacecraft Chaotic Attitude Motion.
IEEE Access, 2018

Performance Comparison of Multiples and Target Detection with Imager-driven Processing Mode for Ultrafast-Imager: (Abstract Only).
Proceedings of the 2018 ACM/SIGDA International Symposium on Field-Programmable Gate Arrays, 2018

2017
Robust Filtering for a Class of Networked Nonlinear Systems With Switching Communication Channels.
IEEE Trans. Cybern., 2017

Adaptive fuzzy finite-time control for spacecraft formation with communication delays and changing topologies.
J. Frankl. Inst., 2017

A simple structure robust attitude synchronization with input saturation.
J. Frankl. Inst., 2017

Real-time calibration of space zoom cameras based on fixed stars.
IET Comput. Vis., 2017

Adaptive Sliding Mode Control for Spacecraft Autonomous Rendezvous With Elliptical Orbits and Thruster Faults.
IEEE Access, 2017

Velocity free finite time attitude control for satellites with flexible appendages.
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.
Proceedings of the Intelligent Robotics and Applications - 8th International Conference, 2015

Quaternion-Based Adaptive Control for Staring-Mode Observation Spacecraft.
Proceedings of the Intelligent Robotics and Applications - 8th International Conference, 2015


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