Xiaodong Liu

Orcid: 0000-0002-5286-6717

Affiliations:
  • Beijing Aerospace Automatic Control Institute, China
  • Beihang University, School of Automation Science and Electrical Engineering, Beijing, China (PhD 2013)


According to our database1, Xiaodong Liu authored at least 13 papers between 2012 and 2024.

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

Timeline

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Bibliography

2024
Decentralized Multiagent Reinforcement Learning Based State-of-Charge Balancing Strategy for Distributed Energy Storage System.
IEEE Trans. Ind. Informatics, October, 2024

2023
Decentralized Multi-agent Reinforcement Learning based State-of-Charge Balancing Strategy for Distributed Energy Storage System.
CoRR, 2023

2021
Fixed-Time Disturbance Observer-Based Adaptive Finite-Time Guidance Law Design considering Impact Angle Constraint and Autopilot Dynamics.
Complex., 2021

2020
Lines cluster approaching mode control for air-breathing hypersonic vehicle under disturbances and uncertainties.
Int. J. Model. Simul. Sci. Comput., 2020

Super Twisting Disturbance Observer-Based Fixed-Time Sliding Mode Backstepping Control for Air-Breathing Hypersonic Vehicle.
IEEE Access, 2020

Adaptive Sliding Mode Guidance With Impact Time and Angle Constraints.
IEEE Access, 2020

Adaptive sliding mode back-stepping control for hypersonic flight vehicle with state constraints and unmodeled disturbances.
Proceedings of the 16th IEEE International Conference on Control & Automation, 2020

2015
A dual-loop robust controller for DC electro-mechanical servo system.
Int. J. Model. Simul. Sci. Comput., 2015

2014
Backstepping attitude control for hypersonic gliding vehicle based on a robust dynamic inversion approach.
J. Syst. Control. Eng., 2014

Sliding mode controller design based on reaching law for hypersonic flight vehicle.
Int. J. Model. Simul. Sci. Comput., 2014

2013
Adaptive backstepping sliding mode controller for Flight Simulator based on RBFNN.
Int. J. Model. Simul. Sci. Comput., 2013

Simulation Research of Active vibration control for elastic missile with swing nozzle thrust Vector control.
Int. J. Model. Simul. Sci. Comput., 2013

2012
Application of STM32 Microcomputer in the Design of Pressure Sensor Compensation.
Proceedings of the AsiaSim 2012, 2012


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