Yuandong Hu

Nanjing University of Science and Technology — China

Engineering · Physical Sciences

6h-index159citations14works4.02yr avg
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Research Topics

Adaptive Control of Nonlinear Systems(9), Space Satellite Systems and Control(8), Spacecraft Dynamics and Control(5), Inertial Sensor and Navigation(5), Astro and Planetary Science(4)

Publications14 total

A DRL-based handover strategy for ISL-enabled LEO mega-constellation networks under heterogeneous QoS demands
Chinese Journal of Aeronautics·2025· 1 citedOpen Access
Multirate Cascade Spacecraft Attitude-Orbit Integrated State Estimation and Control Framework Based on MHE and PWA-MPC
IEEE Transactions on Aerospace and Electronic Systems·2025
Hybrid Two-Stage Identification-Based Nonlinear MPC Strategy for Satellite Attitude Control
IEEE Transactions on Aerospace and Electronic Systems·2025· 19 cited
Filter Observer-Based Attitude Control for Moving Mass Satellites Under Strong Aerodynamic Torques
Space Science & Technology·2025· 2 citedOpen Access
Constraint tightening-based control for small-satellite formations using differential aerodynamic forces
Advances in Space Research·2024· 2 cited
Adaptive Grey-Box Neural Network Piecewise Affine Multiplexed Mpc for Aerodynamic Force-Actuated Multi-Satellite Formations
SSRN Electronic Journal·2024Open Access
Robust multiplexed piecewise affine MPC-based decentralized control of multi-satellite formations using aerodynamic forces
IEEE Transactions on Aerospace and Electronic Systems·2023· 6 cited
Online Network-Based Identification and its Application in Satellite Attitude Control Systems
IEEE Transactions on Aerospace and Electronic Systems·2022· 84 cited
Multiplexed MPC attitude control of a moving mass satellite using dual-rate piecewise affine model
Aerospace Science and Technology·2022· 25 cited
Attitude control of the low earth orbit CubeSat using a moving mass actuator
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering·2021· 2 cited
Attitude Control of the Low Earth Orbit Satellite with Moving Masses under Strong Aerodynamic Disturbance
2021
Differential Aerodynamic Force-Based Formation Control of Nanosatellites Using Yaw Angle Deviation
Journal of Guidance Control and Dynamics·2021· 7 cited
Modeling and attitude control of CubeSat utilizing moving mass actuators
Advances in Space Research·2020· 5 cited
Speed-adaptive dynamic surface attitude control for a satellite with moving masses under input constraints
Transactions of the Institute of Measurement and Control·2020· 6 cited

Frequent Co-authors

Zhengliang Lu(11), Wenhe Liao(8), Keck Voon Ling(6), Xiang Zhang(5), Yihong Zhou(3), Liao Wen-he(3), Feng Ding(2), Dairu Han(2), Zhen Kan(1), Wenhe Liao(1), Ling Zhao(1), Kan Zheng(1), Xiang Zhang(1), Kan Cheng(1)