Output feedback sliding mode control of Lorentz-augmented spacecraft hovering using neural networks. - Xu Huang 003; Ye Yan; Yang Zhou; Hai Xu (J. Syst. Control. Eng., 2015)

Multi-objective robust controller design for spacecraft hovering around elliptical orbital target. - Yang Zhou; Ye Yan; Xu Huang 003 (J. Syst. Control. Eng., 2015)

Output Feedback Control of Underactuated Spacecraft Hovering in Circular Orbit With Radial or In-Track Controller Failure. - Xu Huang 003; Ye Yan (IEEE Trans. Ind. Electron., 2016)

Neural network-based adaptive second order sliding mode control of Lorentz-augmented spacecraft formation. - Xu Huang 003; Ye Yan; Yang Zhou (Neurocomputing, 2017)

Saturated Backstepping Control of Underactuated Spacecraft Hovering for Formation Flights. - Xu Huang 003; Ye Yan (IEEE Trans. Aerosp. Electron. Syst., 2017)

Recursive Gaussian Process State Space Model. - Tengjie Zheng; Lin Cheng; Shengping Gong; Xu Huang 003 (CoRR, 2024)

Real-Time Multiconstrained Polynomial Guidance Based on Analytical Gradient Derivation. - Peng Shi 011; Siyue Guan; Lin Cheng; Wenlong Li; Xu Huang 003 (IEEE Trans. Aerosp. Electron. Syst., 2024)

Neural-Network-Based Nonlinear Optimal Terminal Guidance With Impact Angle Constraints. - Lin Cheng; Han Wang 046; Shengping Gong; Xu Huang 003 (IEEE Trans. Aerosp. Electron. Syst., 2024)

Real-Time Lateral Predictor-Corrector Entry Guidance With Terminal Heading Angle Constraint. - Peng Shi 011; Jingjing Xu; Lin Cheng; Changhong Dong; Xu Huang 003 (IEEE Trans. Aerosp. Electron. Syst., 2025)

Learning-Based Stable Optimal Control for Infinite-Time Nonlinear Regulation Problems. - Han Wang 046; Di Wu; Lin Cheng; Shengping Gong; Xu Huang 003 (CoRR, 2025)

Robust Incremental Learning of Approximate Dynamic Programming for Nonlinear Optimal Guidance. - Han Wang 046; Lin Cheng; Shengping Gong; Xu Huang 003 (IEEE Trans. Aerosp. Electron. Syst., 2025)