Xinhua Wang

Contact

• workRoom B113 Coates Building
  University Park
  Nottingham
  NG7 2RD
  UK
• work0115 74 83080
• Xinhua.Wang1@nottingham.ac.uk

Teaching Summary

[1] Control of Aerospace Systems; [2] Avionics

Research Summary

[1] Design, navigation and Control for UAVs; [2] Sensor technologies and control for aircrafts; [3] Design and control of new conceptual aircrafts.

Research detail:

https://scholar.google.co.uk/citations?hl=en&user=BS9qXi4AAAAJ

Selected Publications

• XINHUA WANG and LILONG CAI, 2017. Navigation and control based on integral-uncertainty observer for unmanned jet aircraft IEEE Transactions on Aerospace and Electronic Systems. 53(3), 1230-1249
• XINHUA WANG, BIJAN SHIRINZADEH and MARCELO H ANG JR, 2015. Nonlinear double-integral observer and application to quadrotor aircraft IEEE Transactions on Industrial Electronics. 62(2), 1189-1200
• XINHUA WANG and BIJAN SHIRINZADEH, 2014. Nonlinear multiple integrator and application to aircraft navigation IEEE Transactions on Aerospace and Electronic Systems. 50(1), 607-622
• XINHUA WANG, ZENGQIANG CHEN and GENG YANG, 2007. Finite-time-convergent differentiator based on singular perturbation technique IEEE Transactions on Automatic Control. 52(9), 1731-1737

• View all publications

Past Research

https://scholar.google.co.uk/citations?hl=en&user=BS9qXi4AAAAJ

• XINHUA WANG and LILONG CAI, 2017. Navigation and control based on integral-uncertainty observer for unmanned jet aircraft IEEE Transactions on Aerospace and Electronic Systems. 53(3), 1230-1249
• XINHUA WANG and LILONG CAI, 2017. Aircraft navigation based on differentiation-integration observer Aerospace Science and Technology. 68(9), 109-122
• XINHUA WANG, BIJAN SHIRINZADEH and MARCELO H ANG JR, 2015. Nonlinear double-integral observer and application to quadrotor aircraft IEEE Transactions on Industrial Electronics. 62(2), 1189-1200
• XINHUA WANG and BIJAN SHIRINZADEH, 2015. Nonlinear augmented observer design and application to quadrotor aircraft Nonlinear Dynamics. 80(3), 1463-1481
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2015. Modeling and control of an agile tail-sitter aircraft Journal of the Franklin Institute. 352(12), 5437-5472
• XINHUA WANG and LILONG CAI, 2015. Mathematical modeling and control of a tilt-rotor aircraft Aerospace Science and Technology. 47(12), 473-492
• XINHUA WANG and BIJAN SHIRINZADEH, 2014. Nonlinear multiple integrator and application to aircraft navigation IEEE Transactions on Aerospace and Electronic Systems. 50(1), 607-622
• XINHUA WANG and BIJAN SHIRINZADEH, 2014. High-order nonlinear differentiator and application to aircraft control Mechanical Systems and Signal Processing. 46(2), 227-252
• XINHUA WANG and BIJAN SHIRINZADEH, 2014. Nonlinear continuous integral-derivative observer Nonlinear Dynamics. 77(3), 793-806
• XINHUA WANG, 2013. Takeoff/landing control based on acceleration measurements for VTOL aircraft Journal of the Franklin Institute. 350(10), 3045-3063
• XINHUA WANG and BIJAN SHIRINZADEH, 2012. Rapid-convergent nonlinear differentiator Mechanical Systems and Signal Processing. 28, 414-431
• XINHUA WANG and HAI LIN, 2012. Design and frequency analysis of continuous finite-time-convergent differentiator Aerospace Science and Technology. 18(1), 69-78
• XINHUA WANG and HAI LIN, 2011. Design and control for rotor-fixed wing hybrid aircraft Proceedings of the IMechE Part G: Journal of Aerospace Engineering. 225(7), 831-847
• XINHUA WANG and HAI LIN, 2011. Design and analysis of a continuous hybrid differentiator. IET Control Theory & Applications. 5(11), 1321-1334
• BO ZHU, XINHUA WANG and KAIYUAN CAI, 2011. Output tracking for nonlinear non-minimum phase systems with output delay and application to an F-16 jet fighter International Journal of Systems Science. 42(3), 529-538
• JINGYA SU, LIN TIE, XINHUA WANG and KAIYUAN CAI, 2011. State-feedback gain design for a class of relay control systems IET Control Theory & Applications. 5(2), 409-419
• ALIREZA PARTOVI, XINHUA WANG, KAI-YEW LUM and HAI LIN, 2011. Modeling and Control of a Small-Scale Hybrid Aircraft In: IFAC 18th World Congress. 10385-10390
• XINHUA WANG, JINKUN LIU and KAIYUAN CAI, 2010. Tracking control for VTOL aircraft with disabled IMUs International Journal of Systems Science. 41(10), 1231-1239
• BO ZHU, XINHUA WANG and KAIYUAN CAI, 2010. Approximate trajectory tracking of input-disturbed PVTOL aircraft with delayed attitude measurements International Journal of Robust and Nonlinear Control. 20(14), 1610-1621
• BO ZHU, XINHUA WANG and KAIYUAN CAI, 2010. Tracking control for angular-rate-sensorless VTOL aircraft in the presence of angular-position measurement delay IET Control Theory & Applications. 4(6), 957-969
• PENGHUI FAN, XINHUA WANG and KAIYUAN CAI, 2010. Design and control of a tri-rotor aircraft In: 2010 8th IEEE International Conference on Control and Automation (ICCA). 1972-1977
• A. AZZAM and XINHUA WANG, 2010. Quad rotor arial robot dynamic modeling and configuration stabilization In: 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR).
• PENGHUI FAN, XINHUA WANG and KAIYUAN CAI, 2010. Design and control of aircraft of vertical take-off-and-landing and high-speed forward flight Journal of Control Theory and Applications. 26(9), 1171-1177
• XINHUA WANG, JINKUN LIU and KAIYUAN CAI, 2009. Tracking control for a velocity-sensorless VTOL aircraft with delayed outputs Automatica. 45(12), 2876-2882
• RUIFENG ZHANG, XINHUA WANG and KAIYUAN CAI, 2009. Quadrotor aircraft control without velocity measurements In: Proceedings of the 48th IEEE on Decision and Control. 5213-5218
• BO ZHU, XINHUA WANG and KAIYUAN CAI, 2009. Fast and nonovershooting control for a double-integral system with step input: nonlinear PD control based on gain-switching Journal of Control Theory and Applications. 26(10), 1111-1117
• JINGYA SU, RUIFENG ZHANG, XINHUA WANG and KAIYUAN CAI, 2009. Controlling a four-rotor aircraft based on noise-attenuation differentiator Journal of Control Theory and Applications. 26(8), 827-832
• BO ZHU, XINHUA WANG and KAIYUAN CAI, 2009. Output tracking of VTOL aircraft with delayed attitude measurements In: 48th IEEE Conference on Decision and Control. 2528-2533
• XINHUA WANG, GENG YANG and WENLI XU, 2008. Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft International Journal of Systems Science. 39(1), 29-42
• XINHUA WANG, ZENGQIANG CHEN and GENG YANG, 2007. Finite-time-convergent differentiator based on singular perturbation technique IEEE Transactions on Automatic Control. 52(9), 1731-1737
• XINHUA WANG and GENG YANG, 2007. Equivalent sliding mode control based on nonlinear observer for nonlinear non-minimum-phase systems Journal of Dynamical and Control Systems. 13(1), 25-36
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2005. Centre-manifold-based sliding mode output tracking for non-minimum nonlinear systems International Journal of Systems Science. 36(4), 191-199
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2004. Output tracking based on extend observer for nonlinear uncertain systems Control and Decision. 19(10), 1113-1116
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2004. Lyapunov-energy based stability control for inverted pendulums Journal of Control Theory and Applications. 21(5), 699-702
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2003. Design and analysis for new discrete tracking-differentiators Applied Mathematics-A Journal of Chinese Universities. 18(2), 214–222
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2003. Nonlinear tracking-differentiator with high speed in whole course Journal of Control Theory and Applications. 20(6), 875-878
• XINHUA WANG, ZENGQIANG CHEN and ZHUZHI YUAN, 2002. Analyse and improvement for nonlinear tracking-differentiator Control and Decision. 17, 752-754