Quaternion-Based Adaptive Control for Staring-Mode Observation Spacecraft. - Lei Chen; Yan Xiao 003; Dong Ye 005; Changjun Li (ICIRA (1), 2015)

Research on Attitude Adjustment Control for Large Angle Maneuver of Rigid-Flexible Coupling Spacecraft. - Yan Xiao 003; Dong Ye 005; Zhengxian Yang; Zhaowei Sun (ICIRA (1), 2015)

Velocity free finite time attitude control for satellites with flexible appendages. - Yan Xiao 003; Dong Ye 005; Zhaowei Sun (IECON, 2017)

Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft. - Dong Ye 005; Yan Xiao 003 (J. Frankl. Inst., 2018)

Observer-based continuous finite-time attitude control for rigid-flexible coupling satellites. - Yan Xiao 003; Dong Ye 005; Zhaowei Sun (Int. J. Control, 2019)

Non-Singular and Continuous Back-Stepping Predefined-Time Attitude Tracking Control for Rigid Spacecraft with Predefined Bound. - Xiaolun Yang; Yulong Yang; Dong Ye 005; Yan Xiao 003; Zhaowei Sun (IECON, 2022)

Adaptive Fault-Tolerant Attitude Tracking Control for Flexible Spacecraft With Guaranteed Performance Bounds. - Yan Xiao 003; Anton H. J. de Ruiter; Dong Ye 005; Zhaowei Sun (IEEE Trans. Aerosp. Electron. Syst., 2022)

Adaptive Control on SE(3) for Spacecraft Pose Tracking With Harmonic Disturbance and Input Saturation. - Hongzhu Zhang; Dong Ye 005; Yan Xiao 003; Zhaowei Sun (IEEE Trans. Aerosp. Electron. Syst., 2022)

Neural Network Based Finite-Time Attitude Tracking Control of Spacecraft With Angular Velocity Sensor Failures and Actuator Saturation. - Dong Ye 005; Yan Xiao 003; Zhaowei Sun; Bing Xiao 001 (IEEE Trans. Ind. Electron., 2022)

Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds. - Yan Xiao 003; Anton H. J. de Ruiter; Dong Ye 005; Zhaowei Sun (IEEE Trans. Aerosp. Electron. Syst., 2023)

A Predefined-Time Extended-State Observer-Based Approach for Velocity-Free Attitude Control of Spacecraft. - Dong Ye 005; An-Min Zou; Shengxin Sun; Yan Xiao 003 (IEEE Trans. Aerosp. Electron. Syst., 2023)

Decentralized Receding Horizon Control for Satellite Cluster Reconfigurations With Successive Convexification Method. - Lixiang Wang; Dong Ye 005; Xianren Kong; Ming Liu 014; Yan Xiao 003 (IEEE Trans. Aerosp. Electron. Syst., 2024)

Scaling-Transformation-Based Attitude Tracking Control for Rigid Spacecraft With Prescribed Time and Prescribed Bound. - Yan Xiao 003; Yulong Yang; Dong Ye 005; Yu Zhao (IEEE Trans. Aerosp. Electron. Syst., 2025)

Quantitative Precision Second-Order Temporal Transformation-Based Pose Control for Spacecraft Proximity Operations. - Yan Xiao 003; Yulong Yang; Dong Ye 005; Jianqiao Zhang 001 (IEEE Trans. Aerosp. Electron. Syst., 2025)

Approximate Analytical Approach for Spacecraft Pursuit-Evasion Game With Reachability Analysis. - Zhen Jia; Dong Ye 005; Yan Xiao 003; Zhaowei Sun (IEEE Trans. Aerosp. Electron. Syst., 2025)

Closed-Loop Strategy Synthesis for Real-Time Spacecraft Pursuit-Evasion Games in Elliptical Orbits. - Zhen Jia; Dong Ye 005; Yan Xiao 003; Zhaowei Sun (IEEE Trans. Aerosp. Electron. Syst., 2025)