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Xu Huang

Orcid: 0000-0002-5777-9313

Affiliations:
  • National University of Defense Technology, College of Aerospace Science and Engineering, Changsha, China


According to our database1, Xu Huang authored at least 7 papers between 2015 and 2024.

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

Timeline

Legend:

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Links

Online presence:

On csauthors.net:

Bibliography

2024
Neural-Network-Based Nonlinear Optimal Terminal Guidance With Impact Angle Constraints.
[BibTeX]
[DOI]
Lin Cheng
,
Han Wang
,
Shengping Gong
,
Xu Huang
IEEE Trans. Aerosp. Electron. Syst., February, 2024

Real-Time Multiconstrained Polynomial Guidance Based on Analytical Gradient Derivation.
[BibTeX]
[DOI]
Peng Shi
,
Siyue Guan
,
Lin Cheng
,
Wenlong Li
,
Xu Huang
IEEE Trans. Aerosp. Electron. Syst., 2024

2017
Saturated Backstepping Control of Underactuated Spacecraft Hovering for Formation Flights.
[BibTeX]
[DOI]
Xu Huang
,
Ye Yan
IEEE Trans. Aerosp. Electron. Syst., 2017

Neural network-based adaptive second order sliding mode control of Lorentz-augmented spacecraft formation.
[BibTeX]
[DOI]
Xu Huang
,
Ye Yan
,
Yang Zhou
Neurocomputing, 2017

2016
Output Feedback Control of Underactuated Spacecraft Hovering in Circular Orbit With Radial or In-Track Controller Failure.
[BibTeX]
[DOI]
Xu Huang
,
Ye Yan
IEEE Trans. Ind. Electron., 2016

2015
Multi-objective robust controller design for spacecraft hovering around elliptical orbital target.
[BibTeX]
[DOI]
Yang Zhou
,
Ye Yan
,
Xu Huang
J. Syst. Control. Eng., 2015

Output feedback sliding mode control of Lorentz-augmented spacecraft hovering using neural networks.
[BibTeX]
[DOI]
Xu Huang
,
Ye Yan
,
Yang Zhou
,
Hai Xu
J. Syst. Control. Eng., 2015


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