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Dr Salman Ijaz
Staff

Dr Salman Ijaz

Assistant Professor (Lecturer) in Control of Aerospace Systems

Research Focus

Fault tolerant control of aircraftLinear parameter varying control of nonlinear systemsFractional order modeling and control of aircraft systemControl allocation SchemeIntegral sliding mode controlRobust controlAircraft actuation system (dissimilar redundant actuation system)Aircraft dynamics and controlUnmanned aerial vehicle systemMore Electric Aircrafts

About

Salman Ijaz received the PhD Degree in Control Sciences and Control Engineering from Beihang University (BUAA) Beijing in 2018. He then joined Nanjing University of Aeronautics and Astronautics (NUAA) to pursue his post-doctoral studies where he worked for two years. He is currently serving as Assistant Professor in University of Nottingham Ningbo China. His area of interest includes modeling and fault tolerant control of aircraft system, sliding mode control, robust control, and unmanned aerial vehicles. He has six years of teaching experience in different public and private sector universities.

Publications

6-DOF Parallel Robot under Partial Observation: Modelling, Control and Trajectory Planning

Xiao, Junlin et al.

2025

Aerodynamic optimization for stability improvement of a centrifugal compressor using arbitrary-shape volute design

Adjei, Richard Amankwa et al.

Case Studies in Thermal Engineering2025

Design of a UV with Adjustable Thruster Orientations and SA-SQP-Based Thruster Orientation Optimization

Wang, Hao et al.

2025

A multilayer neural‐network‐based fault estimation and fault tolerant control scheme for uncertain system

Akhtar, Zainab et al.

International Journal of Robust and Nonlinear Control2024

Adaptive Backstepping Integral Sliding Mode Control of Multirotor UAV System Used for Smart Agriculture

Shi, Yuhao et al.

2024

Fault Tolerant Control Allocation Scheme for LPV system

Ijaz, Salman et al.

2024

Fault-Tolerant Control of Hybrid UAV Using Weighted Control Allocation Scheme

Ijaz, Salman et al.

2024

Design and Validation of Flexible Aerial Robotics for Safe Human-Robot Interaction

Jia, Fuhua et al.

IROS 20242024

Optimal Endurance Prediction for a Battery-Powered Unmanned Aerial Vehicle with High Aspect Ratio Wings

Yu, Xia et al.

2024

Predictor-based constrained fixed-time sliding mode control of multi-UAV formation flight

Khodaverdian, Maria et al.

Aerospace Science and Technology2024

Robust adaptive control law design for enhanced stability of agriculture UAV used for pesticide spraying

Ijaz, Salman et al.

Aerospace Science and Technology2024

Composite anti-unwinding attitude control of spacecraft under actuator saturation and angular velocity limits

Javaid, Umair et al.

Advances in Space Research2023

Observer-based attitude control of spacecraft under actuator dead zone and misalignment faults

Javaid, Umair et al.

Applied Mathematics and Computation2023

Output feedback attitude control of flexible spacecraft under actuator misalignment and input nonlinearities

Javaid, Umair et al.

Journal of Vibration and Control2023

Active and passive fault tolerant control allocation strategy for nonlinear systems

Ijaz, Salman et al.

Journal of Vibration and Control2022

Passive Fault Tolerant Control Allocations for Nonlinear Systems

Ijaz, Salman et al.

2022 34th Chinese Control and Decision Conference (CCDC)2022

Robust adaptive attitude control of flexible spacecraft using a sliding mode disturbance observer

Javaid, Umair et al.

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering2022

Sequential Finite-Element-based Model Predictive Torque and Flux Control Method for IPMSM

Nasr, Ahmed et al.

2022 5th International Conference on Energy, Electrical and Power Engineering (CEEPE)2022

A new actuator fault‐tolerant control for Lipschitz nonlinear system using adaptive sliding mode control strategy

Ijaz, Salman et al.

International Journal of Robust and Nonlinear Control2021

A Robust Sensor and Actuator Fault Tolerant Control Scheme for Nonlinear System

Ashraf, Muhammad Ammar et al.

IEEE Access2021

Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty

Ijaz, Salman et al.

Applied Mathematics and Computation2021

Tracking Control of Vertical Tail Damaged Aircraft with dissimilar Actuator Configuration

Ashraf, Muhammad Ammar et al.

2021 IEEE International IOT, Electronics and Mechatronics Conference (IEMTRONICS)2021

An integral sliding mode fault tolerant control for a class of non‐linear Lipschitz systems

Ashraf, Muhammad Ammar et al.

IET Control Theory and Applications2020