TY - JOUR
T1 - URED Observer-Based Feedback Linearized Neuro Adaptive SMC for a Twin Rotor MIMO System
T2 - Design and Experimental Study
AU - Irfan, Saqib
AU - Zhao, Liangyu
AU - Javaid, Usman
AU - Iqbal, Jamshed
N1 - Publisher Copyright:
© 2025 Technical Committee on Guidance, Navigation and Control, CSAA.
PY - 2025/11/30
Y1 - 2025/11/30
N2 - Unmanned Aerial Vehicles (UAVs) are highly nonlinear and sophisticated systems that demand precise trajectory tracking in environments with uncertainties and disturbances. This research presents advanced nonlinear, adaptive, and artificial intelligence-based control strategies for UAVs. Beyond simulation, the strategies are experimentally evaluated on a coupled Two Degree of Freedom (2-DOF) Twin-rotor MIMO System (TRMS). The proposed strategies include Sliding Mode Control (SMC), Super Twisting (ST), BackStepping (BS), and Neuro-Adaptive SMC (NNSMC), all designed using a feedback linearized mathematical model of the system. System performance is enhanced by decoupling the TRMS into horizontal and vertical subsystems through Lie derivatives and diffeomorphism principles. A Uniform Robust Exact Differentiator (URED) estimates rotor speeds and recovers missing derivatives, while a nonlinear state feedback observer improves system observability and mitigates uncertainties and external wind gusts. Furthermore, ST and NNSMC-based laws reduce high-frequency oscillations in the control input of the first-order SMC law, resulting in improved transient response. The experimental results reveal that NNSMC significantly outperforms ST and BS in terms of trajectory tracking accuracy, transient performance, and integral performance indices for both pitch and yaw angles. These findings underscore the superior convergence performance and robustness of NNSMC, establishing it as a promising solution for precise TRMS control in real real-world environment.
AB - Unmanned Aerial Vehicles (UAVs) are highly nonlinear and sophisticated systems that demand precise trajectory tracking in environments with uncertainties and disturbances. This research presents advanced nonlinear, adaptive, and artificial intelligence-based control strategies for UAVs. Beyond simulation, the strategies are experimentally evaluated on a coupled Two Degree of Freedom (2-DOF) Twin-rotor MIMO System (TRMS). The proposed strategies include Sliding Mode Control (SMC), Super Twisting (ST), BackStepping (BS), and Neuro-Adaptive SMC (NNSMC), all designed using a feedback linearized mathematical model of the system. System performance is enhanced by decoupling the TRMS into horizontal and vertical subsystems through Lie derivatives and diffeomorphism principles. A Uniform Robust Exact Differentiator (URED) estimates rotor speeds and recovers missing derivatives, while a nonlinear state feedback observer improves system observability and mitigates uncertainties and external wind gusts. Furthermore, ST and NNSMC-based laws reduce high-frequency oscillations in the control input of the first-order SMC law, resulting in improved transient response. The experimental results reveal that NNSMC significantly outperforms ST and BS in terms of trajectory tracking accuracy, transient performance, and integral performance indices for both pitch and yaw angles. These findings underscore the superior convergence performance and robustness of NNSMC, establishing it as a promising solution for precise TRMS control in real real-world environment.
KW - Lyapunov stability
KW - Twin rotor MIMO system
KW - back stepping
KW - disturbances
KW - neural network
KW - sliding mode control
KW - super twisting
KW - uniform robust exact differentiator
UR - https://www.scopus.com/pages/publications/105010137139
U2 - 10.1142/S2737480725500281
DO - 10.1142/S2737480725500281
M3 - Article
AN - SCOPUS:105010137139
SN - 2737-4807
VL - 5
SP - 559
EP - 583
JO - Guidance, Navigation and Control
JF - Guidance, Navigation and Control
IS - 4
ER -