教师简介

机器人工程课程组成员——Umair Javaid

浏览次数:    2023-11-06

姓名:Umair Javaid

性别:

学历:博士研究生

学位:博士

教育经历:

2015-2019,北京航空航天大学,控制系统与控制理论,博士

2012-2015,巴基斯坦拉合尔工程与技术大学,控制系统,硕士

职称:讲师

研究方向:

航空航天系统的控制,非线性系统;

容错控制,鲁棒控制,滑模控制,控制分配方案,非线性系统的线性参数变化控制;

太空飞行器姿态动力学和控制,飞行器动力学和控制,无人飞行器系统。


代表性成果:

·U. Javaid, Z. Zhen, S. Shahid, DS Ibrahim, S. Ijaz, Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults,Applied Mathematics and Computation, Volume 465, 2024,128406.https://doi.org/10.1016/j.amc.2023.128406.(SCI)

·U. Javaid, Z. Zhen, S. Shahid, DS. Ibrahim, S. Ijaz. Output feedback attitude control of flexible spacecraft under actuator misalignment and input nonlinearities.Journal of Vibration and Control. 2023;0(0). doi:10.1177/10775463231171386.(SCI)

·S. Ijaz, M. Galea, M. T. Hamayun, H. Ijaz and U. Javaid, "A New Output Integral Sliding Mode Fault-Tolerant Control and Fault Estimation Scheme for Uncertain Systems," inIEEE Transactions on Automation Science and Engineering, doi: 10.1109/TASE.2023.3293318.(SCI)

·U. Javaid,Z. Zhen, S. Shahid, S. Ijaz, and D. Sh Ibrahim, “Composite anti-unwinding attitude control of spacecraft under actuator saturation and angular velocity limits,”Advances in Space Research., vol. 72, no. 2, pp. 552-564, 2023, doi: 10.1016/j.asr.2023.03.007. (SCI)

·M. A. Ashraf, S. Ijaz, U. Javaid, S. Hussain, H. Anwaar, and M. Marey, “A Robust Sensor and Actuator Fault Tolerant Control Scheme for Nonlinear System,” IEEE Access, vol. 10, pp. 626–637, 2022, doi: 10.1109/ACCESS.2021.3137388. (SCI)

·S. Shahid, Z. Zhen, U. Javaid, and L. Wen, “Offense-Defense Distributed Decision Making for Swarm vs. Swarm Confrontation While Attacking the Aircraft Carriers,” Drones, vol. 6, no. 10, 2022, doi: 10.3390/drones6100271. (SCI)

·U. Javaid,Z. Zhen, Y. Xue, and S. Ijaz, “Robust adaptive attitude control of flexible spacecraft using a sliding mode disturbance observer,” Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., no. 29, 2022, doi: 10.1177/09544100211055318. (SCI)

·U. Javaid,H. Dong, S. Ijaz, T. Alkarkhi, and M. Haque, “High-Performance Adaptive Attitude Control of Spacecraft With Sliding Mode Disturbance Observer,” IEEE Access, vol. 10, pp. 41990–41999, 2022, doi: 10.1109/ACCESS.2022.3168600. (SCI)

·S. Ijaz, H. Ijaz, M. T. Hamayun, and U. Javaid, “Active and passive fault tolerant control allocation strategy for nonlinear systems,”JVC/Journal Vib. Control, no. April, 2022, doi: 10.1177/10775463221097763. (SCI)

·U. Javaidand H. Dong, “Disturbance-observer-based attitude control under input nonlinearity,” Trans. Inst. Meas. Control, vol. 43, no. 10, pp. 2358–2367, 2021, doi: 10.1177/0142331221997204. (SCI)

·U. Javaid,M. J. Razzaq, and S. F. Rafique, “PD Integrated Sliding Mode Controller Design for Attitude Tracking Control of Rigid Body Spacecraft,” Proc. 2019 16th Int. Bhurban Conf. Appl. Sci. Technol. IBCAST 2019, pp. 537–542, 2019, doi: 10.1109/IBCAST.2019.8666964. (EI)

·U. Javaidand Q. L. Hu, “Composite back stepping anti-unwinding control of spacecraft with finite time convergence,”Int. Conf. Control. Autom. Syst., vol. 2018-Octob, no. Iccas, pp. 1360–1365, 2018.https://ieeexplore.ieee.org/document/8572001(EI)

·U. Javaid,“Anti-unwinding Attitude Control of Spacecraft using Back-Stepping Technique with Finite Time Convergence,”2018 15th Int. Conf. Control. Autom. Robot. Vision, ICARCV 2018, pp. 692–697, 2018, doi: 10.1109/ICARCV.2018.8581317. (EI)

·S. Ijaz, U. Javaid, Linyan, M. A. Ashraf, and Y. A. Khan, “Mixed sensitivity ∞ controller design for force tracking control of electro-hydraulic servo system,” Proc. 2018 15th Int. Bhurban Conf. Appl. Sci. Technol. IBCAST 2018, vol. 2018-January, pp. 291–297, 2018, doi: 10.1109/IBCAST.2018.8312238. (EI)

·S. F. Rafique et al., “Global power grid interconnection for sustainable growth: concept, project and research direction,” IET Gener. Transm. Distrib., vol. 12, no. 13, pp. 3114–3123, Jul. 2018, doi: 10.1049/iet-gtd.2017.1536. (SCI)

·S. Ijaz, L. Yan, N. Shahzad, M. T. Humayun, and U. Javaid, “Fractional order control of dissimilar redundant actuating system used in large aircraft,” in 2017 29th Chinese Control and Decision Conference (CCDC), May 2017, vol. 31, no. 5, pp. 3686–3691, doi: 10.1109/CCDC.2017.7979145. (EI)