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Hamid Reza Karimi

Researcher at Polytechnic University of Milan

Publications -  981
Citations -  31217

Hamid Reza Karimi is an academic researcher from Polytechnic University of Milan. The author has contributed to research in topics: Control theory & Nonlinear system. The author has an hindex of 83, co-authored 874 publications receiving 24361 citations. Previous affiliations of Hamid Reza Karimi include University of Wollongong & University of Bremen.

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Robust Dynamic Output Feedback Control Synthesis with Pole Placement Constraints for Offshore Wind Turbine Systems

TL;DR: In this paper, the problem of robust dynamic output feedback control with pole placement constraints is studied for a linear parameter-varying model of a floating wind turbine, and the control problem is formulated in terms of linear matrix inequalities (LMIs).
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Robust H∞ reliable control for delta operator switched systems with time-varying delays under asynchronous switching

TL;DR: In this paper, a state feedback controller is designed such that the closed-loop system is exponentially stable with H∞ performance in the presence of actuator faults, and the obtained results are formulated in the form of linear matrix inequalities (LMIs).
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Stability of genetic regulatory networks with time-varying delay

TL;DR: This paper investigates the stability problem for a class of uncertain genetic regulatory networks with time-varying delay via delta operator approach with an appropriate Lyapunov-Krasovskii functional.
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Robust control for a class of uncertain state‐delayed singularly perturbed systems

TL;DR: In this paper, the authors considered the problem of robust control for a class of uncertain state-delayed singularly perturbed systems with norm-bounded nonlinear uncertainties and showed that the state feedback gain matrices can guarantee the stability of the closed-loop system for all ), 0 ( ∞ ∈ e and independently of the time delay.
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Adaptive Finite-Time Control for a Flexible Hypersonic Vehicle with Actuator Fault

TL;DR: In this article, an adaptive fault-tolerant control strategy for a flexible air-breathing hypersonic vehicle (FAHV) with actuator faults and uncertainties is presented.