IJAPM 2024 Vol.14(3): 92-98
DOI: 10.17706/ijapm.2024.14.3.92-98
DOI: 10.17706/ijapm.2024.14.3.92-98
3D Simulation for TRMS Flight Control
Malika Yaici1,*, Amine Ouchene2, Mohand-Akli Kacimi3
1. Computer Department, University of Bejaia, Algeria.
2. Electronics Department, University of Bejaia, Algeria.
3. LTII Laboratory, University of Bejaia, Algeria.
Email: yaicimalika@gmail.com (M.Y.); aminersline@gmail.com (A.O.); mohandakli.kacimi@univ-bejaia.dz (M.A.K.)
*Corresponding author
2. Electronics Department, University of Bejaia, Algeria.
3. LTII Laboratory, University of Bejaia, Algeria.
Email: yaicimalika@gmail.com (M.Y.); aminersline@gmail.com (A.O.); mohandakli.kacimi@univ-bejaia.dz (M.A.K.)
*Corresponding author
Manuscript submitted March 11, 2024; revised May 8, 2024; accepted June 10, 2024; published August 23, 2024.
Abstract—The nonlinear nature of helicopters, and their operation in the presence of several defects and imperfection, causes a drop in performance. The main objective of this work is to use and to create a simulator of a Twin Rotor Mimo System (TRMS) helicopter flight using SlidWorks and Simscape, and use anLinear Quadratic Regulator (LQR) and Link Quality Indication (LQI) control to assure a tracking of a setpoint, in spite of the presence of different disturbances. The simulation results obtained using MATLAB/Simulink show the effectiveness of this control strategy and our simulated TRMS.
Keywords—Helicopter, Linear Quadratic Regulator (LQR) and Link Quality Indication (LQI) control, Twin Rotor Mimo System (TRMS), simulation
Cite: Malika Yaici, Amine Ouchene, Mohand-Akli Kacimi, "3D Simulation for TRMS Flight Control," International Journal of Applied Physics and Mathematics, vol. 14, no. 3, pp. 92-98, 2024.
Copyright © 2024 by the authors. This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited (CC BY 4.0).
Keywords—Helicopter, Linear Quadratic Regulator (LQR) and Link Quality Indication (LQI) control, Twin Rotor Mimo System (TRMS), simulation
Cite: Malika Yaici, Amine Ouchene, Mohand-Akli Kacimi, "3D Simulation for TRMS Flight Control," International Journal of Applied Physics and Mathematics, vol. 14, no. 3, pp. 92-98, 2024.
Copyright © 2024 by the authors. This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited (CC BY 4.0).
General Information
ISSN: 2010-362X (Online)
Abbreviated Title: Int. J. Appl. Phys. Math.
Frequency: Quarterly
APC: 500USD
DOI: 10.17706/IJAPM
Editor-in-Chief: Prof. Haydar Akca
Abstracting/ Indexing: INSPEC(IET), CNKI, Google Scholar, EBSCO, Chemical Abstracts Services (CAS), etc.
E-mail: ijapm@iap.org
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