Saleh Mobayen

Prof. Saleh Mobayen

National Yunlin University of Science and Technology, Taiwan
+2
orcid

Research Focus & Metrics

Academic Career Length

20Years (2007-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 January 2018 in ISA Transactions
Verified
Journal Article
Closed access
OMOmid Mofid
Omid Mofid
Saleh MobayenSaleh Mobayen
Saleh Mobayen

1 April 2022 in ISA Transactions
Verified
Journal Article
Closed access
OMOmid Mofid
Omid Mofid
Saleh MobayenSaleh Mobayen
Saleh Mobayen
CZChunwei Zhang
Chunwei Zhang
BEBalasubramanian Esakki
Balasubramanian Esakki

28 December 2022 in Aerospace Science and Technology
Verified
Journal Article
Closed access
JWJianghua Wang
Jianghua Wang
KAKhalid A. Alattas
Khalid A. Alattas
YBYassine Bouteraa
Yassine Bouteraa
OMOmid Mofid
Omid Mofid
Saleh MobayenSaleh Mobayen
Saleh Mobayen

2 March 2017 in International Journal of Systems Science
Verified
Journal Article
Closed access
Saleh MobayenSaleh Mobayen
Saleh Mobayen
FTFairouz Tchier
Fairouz Tchier
LRLakhdar Ragoub
Lakhdar Ragoub
This paper develops an adaptive super-twisting global nonlinear sliding mode control technique for n-link rigid robotic manipulators. A novel control law is designed to guarantee elimination of the reaching phase and existence of the sliding mode around the surface right from the initial time. Furthermore, the adaptive tuning law eliminates requirement of the knowledge about the upper bounds of external disturbances. By using the proposed method, a robust controller is designed so that the tracking error of rigid manipulator is convergent to the global nonlinear sliding surface in a finite time, and strong robustness with respect to large uncertainties and disturbances is guaranteed. Illustrative simulations on a two-link elbow robot manipulator and a three degree of freedom rigid manipulator are presented to show the robustness and effectiveness of the suggested design compared to other method. Moreover, a simulation as well as experimental study of a rotary inverted pendulum system demonstrates the applicability of the proposed method.

7 October 2021 in Mathematical Methods in the Applied Sciences
Verified
Journal Article
Closed access
PDF file
AJAmin Jajarmi
Amin Jajarmi
Dumitru BaleanuDumitru Baleanu
Dumitru Baleanu
KVKianoush Zarghami Vahid
Kianoush Zarghami Vahid
Saleh MobayenSaleh Mobayen
Saleh Mobayen

28 December 2020 in IEEE Access
Verified
Journal Article
Open access
OMOmid Mofid
Omid Mofid
Saleh MobayenSaleh Mobayen
Saleh Mobayen
WWWing-Kwong Wong
Wing-Kwong Wong
In this paper, a 6-Degrees-of-Freedom (6-DOF) Unmanned Aerial Vehicle (UAV) system with external disturbance corresponding to sensor failure is considered. The control method is presented in two parts. In the first part, the upper bound of external disturbance is known and a Proportional-Integral-Derivative (PID) Sliding Mode Control (SMC) technique is planned for maintaining the desired position in the finite time. Whereas, the upper bound of the external disturbance is considered unknown in the second part and the adaptive PID-SMC method is offered for stability and position tracking control of UAV systems. Using the Lyapunov stability notion, the offered control method proves that the quadrotor’s states can be tracked and stabilized in the finite time. Moreover, for the approximation of unknown bound of the external disturbances which are entered in the quadrotor dynamic model at any moment, adaptive control laws have been applied. Finally, simulation outcomes are provided to display the efficiency of the recommended technique.