Xu Huang
Orcid: 0000-0002-5777-9313Affiliations:
- National University of Defense Technology, College of Aerospace Science and Engineering, Changsha, China
According to our database1,
Xu Huang
authored at least 11 papers
between 2015 and 2025.
Collaborative distances:
Collaborative distances:
Timeline
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Bibliography
2025
Robust Incremental Learning of Approximate Dynamic Programming for Nonlinear Optimal Guidance.
IEEE Trans. Aerosp. Electron. Syst., June, 2025
Learning-Based Stable Optimal Control for Infinite-Time Nonlinear Regulation Problems.
CoRR, June, 2025
Real-Time Lateral Predictor-Corrector Entry Guidance With Terminal Heading Angle Constraint.
IEEE Trans. Aerosp. Electron. Syst., April, 2025
2024
Neural-Network-Based Nonlinear Optimal Terminal Guidance With Impact Angle Constraints.
IEEE Trans. Aerosp. Electron. Syst., February, 2024
Real-Time Multiconstrained Polynomial Guidance Based on Analytical Gradient Derivation.
IEEE Trans. Aerosp. Electron. Syst., 2024
2017
Saturated Backstepping Control of Underactuated Spacecraft Hovering for Formation Flights.
IEEE Trans. Aerosp. Electron. Syst., 2017
Neural network-based adaptive second order sliding mode control of Lorentz-augmented spacecraft formation.
Neurocomputing, 2017
2016
Output Feedback Control of Underactuated Spacecraft Hovering in Circular Orbit With Radial or In-Track Controller Failure.
IEEE Trans. Ind. Electron., 2016
2015
Multi-objective robust controller design for spacecraft hovering around elliptical orbital target.
J. Syst. Control. Eng., 2015
Output feedback sliding mode control of Lorentz-augmented spacecraft hovering using neural networks.
J. Syst. Control. Eng., 2015