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Article

Design and Experimental Validation of an Adaptive Multi-Layer Neural Network Observer-Based Fast Terminal Sliding Mode Control for Quadrotor System

by
Zainab Akhtar
1,
Syed Abbas Zilqurnain Naqvi
1,
Yasir Ali Khan
2,
Mirza Tariq Hamayun
3 and
Salman Ijaz
2,*
1
Mechatronics and Control Engineering Department, University of Engineering and Technology, Lahore 54000, Pakistan
2
Member of Control System Laboratory, University of Nottingham, Ningbo 315104, China
3
Department of Electrical and Computer Engineering, COMSATS University Islamabad (CUI), Lahore 54000, Pakistan
*
Author to whom correspondence should be addressed.
Aerospace 2024, 11(10), 788; https://doi.org/10.3390/aerospace11100788
Submission received: 19 July 2024 / Revised: 12 September 2024 / Accepted: 13 September 2024 / Published: 24 September 2024
(This article belongs to the Special Issue Challenges and Innovations in Aircraft Flight Control)

Abstract

This study considers the numerical design and practical implementation of a new multi-layer neural network observer-based control design technique for unmanned aerial vehicles systems. Initially, an adaptive multi-layer neural network-based Luenberger observer is designed for state estimation by employing a modified back-propagation algorithm. The proposed observer’s adaptive nature aids in mitigating the impact of noise, disturbance, and parameter variations, which are usually not considered by conventional observers. Based on the observed states, a nonlinear dynamic inversion-based fast terminal sliding mode controller is designed to attain the desired attitude and position tracking control. This is done by employing a two-loop control structure. Numerical simulations are conducted to demonstrate the effectiveness of the proposed scheme in the presence of disturbance, parameter uncertainty, and noise. The numerical results are compared with current approaches, demonstrating the superiority of the proposed method. In order to assess the practical effectiveness of the proposed method, hardware-in-loop simulations are conducted by utilizing a Pixhawk 6X flight controller that interfaces with the mission planner software. Finally, experiments are conducted on a real F450 quadrotor in a secured laboratory environment, demonstrating stability and good tracking performance of the proposed MLNN observer-based SMC control scheme.
Keywords: unmanned aerial vehicles; multi-layer neural network; fast terminal sliding mode controller; flight controller unmanned aerial vehicles; multi-layer neural network; fast terminal sliding mode controller; flight controller

Share and Cite

MDPI and ACS Style

Akhtar, Z.; Naqvi, S.A.Z.; Khan, Y.A.; Hamayun, M.T.; Ijaz, S. Design and Experimental Validation of an Adaptive Multi-Layer Neural Network Observer-Based Fast Terminal Sliding Mode Control for Quadrotor System. Aerospace 2024, 11, 788. https://doi.org/10.3390/aerospace11100788

AMA Style

Akhtar Z, Naqvi SAZ, Khan YA, Hamayun MT, Ijaz S. Design and Experimental Validation of an Adaptive Multi-Layer Neural Network Observer-Based Fast Terminal Sliding Mode Control for Quadrotor System. Aerospace. 2024; 11(10):788. https://doi.org/10.3390/aerospace11100788

Chicago/Turabian Style

Akhtar, Zainab, Syed Abbas Zilqurnain Naqvi, Yasir Ali Khan, Mirza Tariq Hamayun, and Salman Ijaz. 2024. "Design and Experimental Validation of an Adaptive Multi-Layer Neural Network Observer-Based Fast Terminal Sliding Mode Control for Quadrotor System" Aerospace 11, no. 10: 788. https://doi.org/10.3390/aerospace11100788

APA Style

Akhtar, Z., Naqvi, S. A. Z., Khan, Y. A., Hamayun, M. T., & Ijaz, S. (2024). Design and Experimental Validation of an Adaptive Multi-Layer Neural Network Observer-Based Fast Terminal Sliding Mode Control for Quadrotor System. Aerospace, 11(10), 788. https://doi.org/10.3390/aerospace11100788

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