Salman Ijaz

Orcid: 0000-0002-6964-5179

Affiliations:
  • Nanjing University of Aeronautics and Astronautics, College of Automation Engineering, China
  • Beihang University, School of Automation and Electrical Engineering, China (PhD 2018)
  • COMSATS Institute of Information Technology, Lahore, Pakistan (2014 - 2015)


According to our database1, Salman Ijaz authored at least 12 papers between 2018 and 2024.

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

Timeline

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Bibliography

2024
Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults.
Appl. Math. Comput., March, 2024

Output Feedback Fault Tolerant Control for Linear Parameter Varying Plants Considering Imperfect Fault Information.
IEEE Access, 2024

Fault Tolerant Control Allocation Scheme for LPV system.
Proceedings of the Australian & New Zealand Control Conference, 2024

Spacecraft Attitude Stabilization Control Under Actuator Faults and Input Saturation.
Proceedings of the 18th IEEE International Conference on Advanced Motion Control, 2024

2022
High-Performance Adaptive Attitude Control of Spacecraft With Sliding Mode Disturbance Observer.
IEEE Access, 2022

A Robust Sensor and Actuator Fault Tolerant Control Scheme for Nonlinear System.
IEEE Access, 2022

2021
Model identification and real-time implementation of a linear parameter-varying control scheme on lab-based inverted pendulum system.
J. Syst. Control. Eng., 2021

Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty.
Appl. Math. Comput., 2021

2019
Adaptive fault tolerant control of dissimilar redundant actuation system of civil aircraft based on integral sliding mode control strategy.
Trans. Inst. Meas. Control, 2019

Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure.
J. Frankl. Inst., 2019

An adaptive integral sliding mode FTC scheme for dissimilar redundant actuation system of civil aircraft.
Int. J. Syst. Sci., 2019

2018
An Adaptive LPV Integral Sliding Mode FTC of Dissimilar Redundant Actuation System for Civil Aircraft.
IEEE Access, 2018


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