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Salman Ijaz 0002
Person information
- affiliation: Nanjing University of Aeronautics and Astronautics, College of Automation Engineering, China
- affiliation (PhD 2018): Beihang University, School of Automation and Electrical Engineering, China
- affiliation (2014 - 2015): COMSATS Institute of Information Technology, Lahore, Pakistan
Other persons with the same name
- Salman Ijaz 0001 — NUST, Military College of signals, Pakistan
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2020 – today
- 2024
- [j11]Omar Azeem
, Mirza Tariq Hamayun
Output Feedback Fault Tolerant Control for Linear Parameter Varying Plants Considering Imperfect Fault Information. IEEE Access 12: 12257-12270 (2024) - [j10]Umair Javaid
Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults. Appl. Math. Comput. 465: 128406 (2024) - [j9]Salman Ijaz
A New Output Integral Sliding Mode Fault-Tolerant Control and Fault Estimation Scheme for Uncertain Systems. IEEE Trans Autom. Sci. Eng. 21(3): 4214-4225 (2024) - [c3]Umair Javaid, Michael V. Basin, Salman Ijaz:
Spacecraft Attitude Stabilization Control Under Actuator Faults and Input Saturation. AMC 2024: 1-6 - [c2]Salman Ijaz, Umair Javaid, Ahmed Nasr
Fault-Tolerant Control of Hybrid UAV Using Weighted Control Allocation Scheme. ACC 2024: 4687-4692 - [c1]Salman Ijaz, Ahmed Nasr
Fault Tolerant Control Allocation Scheme for LPV system. ANZCC 2024: 78-83 - 2022
- [j8]Muhammad Ammar Ashraf
A Robust Sensor and Actuator Fault Tolerant Control Scheme for Nonlinear System. IEEE Access 10: 626-637 (2022) - [j7]Umair Javaid, Hongyang Dong
High-Performance Adaptive Attitude Control of Spacecraft With Sliding Mode Disturbance Observer. IEEE Access 10: 41990-41999 (2022) - 2021
- [j6]Salman Ijaz
Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty. Appl. Math. Comput. 402: 126053 (2021) - [j5]Anila Barkat, Mirza Tariq Hamayun, Salman Ijaz
Model identification and real-time implementation of a linear parameter-varying control scheme on lab-based inverted pendulum system. J. Syst. Control. Eng. 235(1) (2021)
2010 – 2019
- 2019
- [j4]Salman Ijaz
An adaptive integral sliding mode FTC scheme for dissimilar redundant actuation system of civil aircraft. Int. J. Syst. Sci. 50(14): 2687-2702 (2019) - [j3]Salman Ijaz
Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure. J. Frankl. Inst. 356(3): 1302-1332 (2019) - [j2]Salman Ijaz
Adaptive fault tolerant control of dissimilar redundant actuation system of civil aircraft based on integral sliding mode control strategy. Trans. Inst. Meas. Control 41(13): 3756-3768 (2019) - 2018
- [j1]Salman Ijaz
An Adaptive LPV Integral Sliding Mode FTC of Dissimilar Redundant Actuation System for Civil Aircraft. IEEE Access 6: 65960-65973 (2018)
Coauthor Index
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last updated on 2024-10-07 21:15 CEST by the dblp team
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