zouaoui satla

@univ-tissemsilt.dz

Department of Civil, Mechanical, and Transport engineering; Faculty of Science and Technology
Tissemsilt university; Tissemsilt, Algeria

zouaoui satla


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https://researchid.co/zouaoui85
Dr. Zouaoui is a researcher in mechanical engineering with expertise in drones, control systems, active vibration, and mechanical dynamics. He earned an Engineering Diploma (2010), a Magister degree (2012), and a Doctorate in Mechanical Engineering (2019) from Djilali Liabes University in Sidi Bel Abbès, Algeria. He is currently a professor at the University of Tissemsilt, where his work focuses on UAV design, intelligent control algorithms, vibration mitigation, and the integration of AI in mechanical systems. His research combines modeling, simulation, and experimental validation to develop innovative solutions for advanced engineering applications.

EDUCATION

Dr. Zouaoui is a mechanical engineer and researcher specializing in drones, control systems, active vibration, and mechanical dynamics. He earned his Engineering Diploma in Mechanical Engineering in 2010, followed by a Magister degree in the same specialty in 2012, and later completed his Doctorate in Mechanical Engineering in 2019 at Djilali Liabes University in Sidi Bel Abbès, Algeria

RESEARCH, TEACHING, or OTHER INTERESTS

Mechanical Engineering, Engineering, Mechanics of Materials, Control and Systems Engineering
7

Scopus Publications

162

Scholar Citations

6

Scholar h-index

4

Scholar i10-index

Scopus Publications

  • A new optimization framework for piezoelectric actuators location identification
    Kouider Bendine, Abdeddaim Mahdi, Amine Smahat, Satla Zouaoui, Abdeljelil Mankour
    Mechanics of Advanced Materials and Structures, 2025
  • Vibration control of FGM plate using optimally placed piezoelectric patches
    Zouaoui SATLA, Lakhdar Boumia, Mohamed Kherrab
    Revista Mexicana De Fisica, 2024
    The aim of this study is to propose a methodology to actively control the vibration of functionally graded plates, with the help of piezoelectric actuators and sensors. The study relays on the classical plate theory to analytically formulate the governing equation of motion, which is then expanded to derive a space state equation of the model. The material properties of the FG plate are assumed to vary along the thickness direction. In order to improve the damping effectiveness, the location of the piezoelectric sensors and actuators is optimally determined using the H2 norm. The necessary control voltage was determined based on optimal LQR and LQG controllers.
  • Drone control using the coupling of the pid controller and genetic algorithm
    Mohamed Elajrami, Zouaoui Satla, Kouider Bendine
    Communications Scientific Letters of the University of Zilina, 2021
    Due to their strong abilities and easy usage, unmanned aerial vehicles (UAVs) commonly named drones have found a place and merged in the different industrial sectors. These varieties of applications encourage researchers to search for new control algorithms that make drones operate smoothly. In this regard, the present study mains to design a PID controller for four motors drones (quadcopter). For this purpose, a state-space representation of the drone is proposed based on Newton Euler's formularies for a rigid body. For better performance of the control algorithm (PID) the parameters Kp, Ki, and Kd for the controller are established using an optimization search schema based on a genetic algorithm. Various simulations were performed to test the proposed idea.
  • Easy tracking of UAV using PID controller
    Satla Zouaoui, Elajrami Mohamed, Bendine Kouider
    Periodica Polytechnica Transportation Engineering, 2019
    The main objective of the present paper is to design a mathematical model to estimate the behavior of flying robots with four motors (quadcopters) controlled by three algorithms; P depends on the present errors; I on the accumulation of past errors, and D a prediction of future errors (PID controller design) with simple strategy. In this regard, a governing equation of motion based on Newton Euler’s formularies for rigid body dynamics is presented. In order to design the control algorithm some assumptions are made such as the ignorance of the blade flapping, surrounding fluid velocities. This exclusion of parameters makes the model flexible, simple, and allows the control to be more efficiency and easy to designed without the need of expensive computation. The simulation studies are carried out using MATLAB program.
  • Active Vibration damping of Smart composite beams based on system identification technique
    Kouider Bendine, Zouaoui Satla, Farouk Benallel Boukhoulda, Mohammed Nouari
    Curved and Layered Structures, 2018
    In the present paper, the active vibration control of a composite beam using piezoelectric actuator is investigated. The space state equation is determined using system identification technique based on the structure input output response provided by ANSYS APDL finite element package. The Linear Quadratic (LQG) control law is designed and integrated into ANSYS APDL to perform closed loop simulations. Numerical examples for different types of excitation loads are presented to test the efficiency and the accuracy of the proposed model.
  • Structural modeling and active vibration control of smart FGM plate through ANSYS
    Kouider Bendine, Benallel Farouk Boukhoulda, Mohammed Nouari, Zouaoui Satla
    International Journal of Computational Methods, 2017
    This paper presents a methodology to use the software ANSYS in modeling and active vibration control of a functionally graded (FGM) plate with upper and lower surface-bonded piezoelectric layers. First a FGM plate with piezoelectric layers is designed using APDL ANSYS. Then a modal analysis has been carried out to get the first five rank frequencies and mode shapes. A proportional–integral–derivative (PID) and a linear-quadratic-based output feedback controller are introduced to realize the vibration control through a closed loop. Results for various volume fraction indexes are presented.
  • Active vibration control of functionally graded beams with piezoelectric layers based on higher order shear deformation theory
    K. Bendine, F. B. Boukhoulda, M. Nouari, Z. Satla
    Earthquake Engineering and Engineering Vibration, 2016

RECENT SCHOLAR PUBLICATIONS

  • A new optimization framework for piezoelectric actuators location identification
    K Bendine, A Mahdi, A Smahat, S Zouaoui, A Mankour
    Mechanics of Advanced Materials and Structures 32 (20), 4959-4970 , 2025
    2025
  • Effect of porosity and power law index on the actuation properties of functionally graded piezoelectric plates
    S Zouaoui, A Smahat
    HCMCOU Journal of Science-Advances in Computational Structures, 3-16 , 2025
    2025
  • The geometry uniformity parameters effect on the dynamic behaviour of trapezoidal beam
    M Bouamama, Z Satla, A Belaziz, L Boumia
    Studies in Engineering and Exact Sciences 5 (1), 1530-1547 , 2024
    2024
    Citations: 1
  • Vibration control of FGM plate using optimally placed piezoelectric patches
    Z Satla, L Boumia, M Kherrab
    Revista mexicana de física 70 (1) , 2024
    2024
    Citations: 7
  • NEW DESIGN FOR AN ORNITHOPTER DRONE USING SIMPLE MECHANISM BASED ON PID CONTROLLER
    Z Satla, K Bendine, M Elajrami, L Boumia
    INTERNATIONAL ISTANBUL CURRENT SCIENTIFIC RESEARCH CONGRESS, 729-737 , 2023
    2023
  • A NEW DRONE DESIGN USING SIMPLE MECHANISMS BASED ON PD CONTROLLER
    S Zouaoui, B Kouider, E Mohamed, L Boumia
    INTERNATIONAL ANTALYA SCIENTIFIC RESEARCH AND INNOVATIVE STUDIES CONGRESS … , 2023
    2023
  • Drone control using the coupling of the PID controller and genetic algorithm
    M Elajrami, Z Satla, K Bendine
    Communications-Scientific letters of the University of Zilina 23 (3), C75-C82 , 2021
    2021
    Citations: 8
  • Contribution à la modélisatio et à la commande d'un drone miniature
    Z SATLA
    Université de Sidi Bel Abbès-Djillali Liabes , 2019
    2019
    Citations: 1
  • Contributiona la Modélisation eta La Commande d’un Drone Miniature
    Z Satla
    PhD diss., PhD thesis, Djillali Liabes-Sidi Bel Abbes , 2019
    2019
    Citations: 3
  • Easy tracking of UAV using PID controller
    S Zouaoui, E Mohamed, B Kouider
    Periodica Polytechnica Transportation Engineering 47 (3), 171-177 , 2019
    2019
    Citations: 42
  • Active Vibration damping of Smart composite beams based on system identification technique
    K Bendine, Z Satla, FB Boukhoulda, M Nouari
    Curved and Layered Structures 5 (1), 43-48 , 2018
    2018
    Citations: 11
  • P, PI, PID controller designed for UAV Quadrotors trajectory
    S Zouaoui, E Mohamed, B Kouider, P Alper
    International Conference on Innovative Engineering ApplicationsAt: Sivas, Turkey , 2018
    2018
  • Vibration Analysis Of New Type Uav Drone Wing
    M Salah, S Zouaoui, B Kouider, P Alper
    International Conference on Innovative Engineering ApplicationsAt: sicas, Turkey , 2018
    2018
  • Active Vibration damping of Smart composite beams based on system identification technique. Curved and Layered Structures, 5 (1): 43-48
    K Bendine, Z Satla, FB Boukhoulda, M Nouari
    2018
    Citations: 3
  • Structural modeling and active vibration control of smart FGM plate through ANSYS
    K Bendine, BF Boukhoulda, M Nouari, Z Satla
    International Journal of Computational Methods 14 (04), 1750042 , 2017
    2017
    Citations: 41
  • Vibration damping of cantilever beam by means piezoelectric actuator
    S Mostefa, S Zouaoui
    2017
  • Active vibration control of functionally graded beams with piezoelectric layers based on higher order shear deformation theory
    K Bendine, FB Boukhoulda, M Nouari, Z Satla
    Earthquake Engineering and Engineering Vibration 15 (4), 611-620 , 2016
    2016
    Citations: 43
  • Simulation des vibrations mécaniques d’une aile d’avion.
    Z SATLA
    2012
  • Simulation numériques des vibrations mécaniques d'une aile d'avion sous MATLAB
    Z SATLA
    Université de Sidi Bel Abbès-Djillali Liabes , 2012
    2012
    Citations: 1
  • Simulation numériques des vibrations d’une aile d’avion
    M ELAJRAMI, Z SATLA, BB FAROUK
    2012
    Citations: 1

MOST CITED SCHOLAR PUBLICATIONS

  • Active vibration control of functionally graded beams with piezoelectric layers based on higher order shear deformation theory
    K Bendine, FB Boukhoulda, M Nouari, Z Satla
    Earthquake Engineering and Engineering Vibration 15 (4), 611-620 , 2016
    2016
    Citations: 43
  • Easy tracking of UAV using PID controller
    S Zouaoui, E Mohamed, B Kouider
    Periodica Polytechnica Transportation Engineering 47 (3), 171-177 , 2019
    2019
    Citations: 42
  • Structural modeling and active vibration control of smart FGM plate through ANSYS
    K Bendine, BF Boukhoulda, M Nouari, Z Satla
    International Journal of Computational Methods 14 (04), 1750042 , 2017
    2017
    Citations: 41
  • Active Vibration damping of Smart composite beams based on system identification technique
    K Bendine, Z Satla, FB Boukhoulda, M Nouari
    Curved and Layered Structures 5 (1), 43-48 , 2018
    2018
    Citations: 11
  • Drone control using the coupling of the PID controller and genetic algorithm
    M Elajrami, Z Satla, K Bendine
    Communications-Scientific letters of the University of Zilina 23 (3), C75-C82 , 2021
    2021
    Citations: 8
  • Vibration control of FGM plate using optimally placed piezoelectric patches
    Z Satla, L Boumia, M Kherrab
    Revista mexicana de física 70 (1) , 2024
    2024
    Citations: 7
  • Contributiona la Modélisation eta La Commande d’un Drone Miniature
    Z Satla
    PhD diss., PhD thesis, Djillali Liabes-Sidi Bel Abbes , 2019
    2019
    Citations: 3
  • Active Vibration damping of Smart composite beams based on system identification technique. Curved and Layered Structures, 5 (1): 43-48
    K Bendine, Z Satla, FB Boukhoulda, M Nouari
    2018
    Citations: 3
  • The geometry uniformity parameters effect on the dynamic behaviour of trapezoidal beam
    M Bouamama, Z Satla, A Belaziz, L Boumia
    Studies in Engineering and Exact Sciences 5 (1), 1530-1547 , 2024
    2024
    Citations: 1
  • Contribution à la modélisatio et à la commande d'un drone miniature
    Z SATLA
    Université de Sidi Bel Abbès-Djillali Liabes , 2019
    2019
    Citations: 1
  • Simulation numériques des vibrations mécaniques d'une aile d'avion sous MATLAB
    Z SATLA
    Université de Sidi Bel Abbès-Djillali Liabes , 2012
    2012
    Citations: 1
  • Simulation numériques des vibrations d’une aile d’avion
    M ELAJRAMI, Z SATLA, BB FAROUK
    2012
    Citations: 1
  • A new optimization framework for piezoelectric actuators location identification
    K Bendine, A Mahdi, A Smahat, S Zouaoui, A Mankour
    Mechanics of Advanced Materials and Structures 32 (20), 4959-4970 , 2025
    2025
  • Effect of porosity and power law index on the actuation properties of functionally graded piezoelectric plates
    S Zouaoui, A Smahat
    HCMCOU Journal of Science-Advances in Computational Structures, 3-16 , 2025
    2025
  • NEW DESIGN FOR AN ORNITHOPTER DRONE USING SIMPLE MECHANISM BASED ON PID CONTROLLER
    Z Satla, K Bendine, M Elajrami, L Boumia
    INTERNATIONAL ISTANBUL CURRENT SCIENTIFIC RESEARCH CONGRESS, 729-737 , 2023
    2023
  • A NEW DRONE DESIGN USING SIMPLE MECHANISMS BASED ON PD CONTROLLER
    S Zouaoui, B Kouider, E Mohamed, L Boumia
    INTERNATIONAL ANTALYA SCIENTIFIC RESEARCH AND INNOVATIVE STUDIES CONGRESS … , 2023
    2023
  • P, PI, PID controller designed for UAV Quadrotors trajectory
    S Zouaoui, E Mohamed, B Kouider, P Alper
    International Conference on Innovative Engineering ApplicationsAt: Sivas, Turkey , 2018
    2018
  • Vibration Analysis Of New Type Uav Drone Wing
    M Salah, S Zouaoui, B Kouider, P Alper
    International Conference on Innovative Engineering ApplicationsAt: sicas, Turkey , 2018
    2018
  • Vibration damping of cantilever beam by means piezoelectric actuator
    S Mostefa, S Zouaoui
    2017
  • Simulation des vibrations mécaniques d’une aile d’avion.
    Z SATLA
    2012