Xinhua Wang

Orcid: 0000-0001-9458-2299

Affiliations:
  • University of Nottingham, Faculty of Engineering, UK
  • Monash University, Department of Mechanical and Aerospace Engineering, Clayton, VIC, Australia (former)
  • Hong Kong University of Science and Technology, Department of Mechanical and Aerospace Engineering, Hong Kong (former)
  • National University of Singapore, Department of Electrical and Computer Engineering, Singapore (former)
  • Beijing University of Aeronautics and Astronautics, National Key Laboratory of Science and Technology on Holistic Control, China (former)
  • Tsinghua University, Department of Automation, Beijing, China (former)
  • Nankai University, Department of Automation, China (PhD 2004)


According to our database1, Xinhua Wang authored at least 21 papers between 2005 and 2023.

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

Timeline

Legend:

Book 
In proceedings 
Article 
PhD thesis 
Dataset
Other 

Links

Online presence:

On csauthors.net:

Bibliography

2023
Output tracking based on extended observer for nonlinear uncertain systems.
CoRR, 2023

2022
Design and analysis of stable differentiator-predictor.
Int. J. Control, 2022

A Highly Customizable and Efficient Hardware Implementation for Parallel Matrix Inversion.
Proceedings of the International Conference on Field-Programmable Technology, 2022

2020
Extended Signal-Correction Observer and Application to Aircraft Navigation.
IEEE Trans. Ind. Electron., 2020

Hardware Implementations with High Throughput, Low-Latency and Low-Area for Matrix Inversion.
Proceedings of the International Conference on Field-Programmable Technology, 2020

2019
Nonlinear Signal-Correction Observer and Application to UAV Navigation.
IEEE Trans. Ind. Electron., 2019

2017
Navigation and Control Based on Integral-Uncertainty Observer for Unmanned Jet Aircraft.
IEEE Trans. Aerosp. Electron. Syst., 2017

2015
Nonlinear Double-Integral Observer and Application to Quadrotor Aircraft.
IEEE Trans. Ind. Electron., 2015

Modeling and control of an agile tail-sitter aircraft.
J. Frankl. Inst., 2015

Mathematical modeling and control of a tilt-rotor aircraft.
CoRR, 2015

2014
Nonlinear Multiple Integrator and Application to Aircraft Navigation.
IEEE Trans. Aerosp. Electron. Syst., 2014

2013
Takeoff/landing control based on acceleration measurements for VTOL aircraft.
J. Frankl. Inst., 2013

2011
Output tracking for nonlinear non-minimum phase systems with output delay and application to an F-16 jet fighter.
Int. J. Syst. Sci., 2011

2010
Tracking control for VTOL aircraft with disabled IMUs.
Int. J. Syst. Sci., 2010

Design and control of a tri-rotor aircraft.
Proceedings of the 8th IEEE International Conference on Control and Automation, 2010

2009
Tracking control for a velocity-sensorless VTOL aircraft with delayed outputs.
Autom., 2009

Output tracking of VTOL aircraft with delayed attitude measurements.
Proceedings of the 48th IEEE Conference on Decision and Control, 2009

Quadrotor aircraft control without velocity measurements.
Proceedings of the 48th IEEE Conference on Decision and Control, 2009

2008
Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft.
Int. J. Syst. Sci., 2008

2007
Finite-Time-Convergent Differentiator Based on Singular Perturbation Technique.
IEEE Trans. Autom. Control., 2007

2005
Centre-manifold-based sliding mode output tracking for non-minimum nonlinear systems.
Int. J. Syst. Sci., 2005


  Loading...