Xinhua Wang

Contact

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

Teaching Summary

Module convenor of MMME2031 - Control of Aerospace Systems;

Module convenor of MMME3077 - Avionic Systems

Research Summary

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

Recent Publications

• WANG, X. and WANG, W, 2020. Extended signal-correction observer and application to aircraft navigation IEEE Transactions on Industrial Electronics. 67(4), 3149-3156
• WANG, X., 2020. Design and analysis of stable differentiator-predictor International Journal of Control. 1-46
• SULTAN ALQAHTANI, YIQUN ZHU, QIZHI SHI, XIAOLIN MENG and XINHUA WANG, 2020. Hardware Implementations with High Throughput, Low-Latency and Low-Area for Matrix Inversion In: IEEE International Conference on Field-Programmable Technology (FPT). 250-255
• WANG, X. and WANG, W., 2019. Nonlinear signal-correction observer and application to UAV navigation IEEE Transactions on Industrial Electronics. 66(6), 4600-4607

• View all publications

Future Research

I welcome enquiries from potential PhD candidates from Home, EU and International countries who are interested in the following research areas: Design, navigation and control of UAVs, Sensor technologies and control of aircraft systems.

• WANG, X. and WANG, W, 2020. Extended signal-correction observer and application to aircraft navigation IEEE Transactions on Industrial Electronics. 67(4), 3149-3156
• WANG, X., 2020. Design and analysis of stable differentiator-predictor International Journal of Control. 1-46
• SULTAN ALQAHTANI, YIQUN ZHU, QIZHI SHI, XIAOLIN MENG and XINHUA WANG, 2020. Hardware Implementations with High Throughput, Low-Latency and Low-Area for Matrix Inversion In: IEEE International Conference on Field-Programmable Technology (FPT). 250-255
• WANG, X. and WANG, W., 2019. Nonlinear signal-correction observer and application to UAV navigation IEEE Transactions on Industrial Electronics. 66(6), 4600-4607
• WANG, X. and CAI, L., 2017. Navigation and control based on integral-uncertainty observer for unmanned jet aircraft IEEE Transactions on Aerospace and Electronic Systems. 53(3), 1230-1249
• WANG, X. and CAI, L., 2017. Aircraft navigation based on differentiation-integration observer Aerospace Science and Technology. 68(9), 109-122
• WANG, X., SHIRINZADEH, B. and ANG JR, M., 2015. Nonlinear double-integral observer and application to quadrotor aircraft IEEE Transactions on Industrial Electronics. 62(2), 1189-1200
• WANG, X. and SHIRINZADEH, B., 2015. Nonlinear augmented observer design and application to quadrotor aircraft Nonlinear Dynamics. 80(3), 1463-1481
• WANG, X., CHEN, Z. and YUAN, Z., 2015. Modeling and control of an agile tail-sitter aircraft Journal of the Franklin Institute. 352(12), 5437-5472
• WANG, X. and CAI, L., 2015. Mathematical modeling and control of a tilt-rotor aircraft Aerospace Science and Technology. 47(12), 473-492
• WANG, X. and SHIRINZADEH, B., 2014. Nonlinear multiple integrator and application to aircraft navigation IEEE Transactions on Aerospace and Electronic Systems. 50(1), 607-622
• WANG, X. and SHIRINZADEH, B., 2014. High-order nonlinear differentiator and application to aircraft control Mechanical Systems and Signal Processing. 46(2), 227-252
• WANG, X. and SHIRINZADEH, B., 2014. Nonlinear continuous integral-derivative observer Nonlinear Dynamics. 77(3), 793-806
• WANG, X., 2013. Takeoff/landing control based on acceleration measurements for VTOL aircraft Journal of the Franklin Institute. 350(10), 3045-3063
• WANG, X. and SHIRINZADEH, B., 2012. Rapid-convergent nonlinear differentiator Mechanical Systems and Signal Processing. 28, 414-431
• WANG, X. and LIN, H., 2012. Design and frequency analysis of continuous finite-time-convergent differentiator Aerospace Science and Technology. 18(1), 69-78
• WANG, X. and LIN, H., 2011. Design and control for rotor-fixed wing hybrid aircraft Proceedings of the IMechE Part G: Journal of Aerospace Engineering. 225(7), 831-847
• WANG, X. and LIN, H., 2011. Design and analysis of a continuous hybrid differentiator. IET Control Theory & Applications. 5(11), 1321-1334
• ZHU, B., WANG, X. and CAI, K., 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
• SU, J., TIE, L., WANG, X. and CAI, K., 2011. State-feedback gain design for a class of relay control systems IET Control Theory & Applications. 5(2), 409-419
• PARTOVI, A, WANG, X., LUM, K.Y and LIN, H., 2011. Modeling and Control of a Small-Scale Hybrid Aircraft In: IFAC 18th World Congress. 10385-10390
• WANG, X., LIU, J. and CAI, K., 2010. Tracking control for VTOL aircraft with disabled IMUs International Journal of Systems Science. 41(10), 1231-1239
• ZHU, B., WANG, X. and CAI, K., 2010. Approximate trajectory tracking of input-disturbed PVTOL aircraft with delayed attitude measurements International Journal of Robust and Nonlinear Control. 20(14), 1610-1621
• ZHU, B., WANG, X. and CAI, K., 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
• FAN, P., WANG, X. and CAI, K., 2010. Design and control of a tri-rotor aircraft In: 2010 8th IEEE International Conference on Control and Automation (ICCA). 1972-1977
• AZZAM, A. and WANG, X., 2010. Quad rotor arial robot dynamic modeling and configuration stabilization In: 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR).
• WANG, X., LIU, J. and CAI, K., 2009. Tracking control for a velocity-sensorless VTOL aircraft with delayed outputs Automatica. 45(12), 2876-2882
• ZHANG, R., WANG, X. and CAI, K., 2009. Quadrotor aircraft control without velocity measurements In: Proceedings of the 48th IEEE on Decision and Control. 5213-5218
• WANG, X., YANG, G. and XU, W., 2008. Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft International Journal of Systems Science. 39(1), 29-42
• WANG, X., CHEN, Z. and YANG, G., 2007. Finite-time-convergent differentiator based on singular perturbation technique IEEE Transactions on Automatic Control. 52(9), 1731-1737
• WANG, X. and YANG, G., 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