TY - JOUR
T1 - Robust GDI with Extended Differentiator and Observer-Based Fast Terminal Integral Sliding Mode Control for UAV System
AU - Irfan, Saqib
AU - Zhao, Liangyu
AU - Ullah, Safeer
AU - Iqbal, Jamshed
N1 - Publisher Copyright:
© 2027 World Scientific Publishing Company.
PY - 2025
Y1 - 2025
N2 - This study presents advanced robust control strategies for trajectory tracking of a Multiple Input–Multiple Output (MIMO) Unmanned Aerial Vehicle (UAV) system under disturbances and uncertainties. Motivated by the limitations of existing simulation-based studies, this work designs and experimentally validates nonlinear Lyapunov-based control strategies, including Integral Sliding Mode Control (ISMC), Fast Terminal ISMC (FTISMC), and a novel Robust Generalized Dynamic Inversion-based FTISMC (RGDIFTISMC). The proposed methods ensure fast, finite-time convergence and robustness under wind disturbances, incorporating a Uniform Robust Exact Differentiator (URED) and a nonlinear state feedback disturbance observer to accurately recover rotor speed and missing derivatives, while the observer enhances system observability. Experimental validation on a twin rotor system confirms superior performance, with RGDIFTISMC achieving up to 46.7% faster stabilization. The results highlight its efficiency in improving transient response, steady-state accuracy, and robustness against disturbances.
AB - This study presents advanced robust control strategies for trajectory tracking of a Multiple Input–Multiple Output (MIMO) Unmanned Aerial Vehicle (UAV) system under disturbances and uncertainties. Motivated by the limitations of existing simulation-based studies, this work designs and experimentally validates nonlinear Lyapunov-based control strategies, including Integral Sliding Mode Control (ISMC), Fast Terminal ISMC (FTISMC), and a novel Robust Generalized Dynamic Inversion-based FTISMC (RGDIFTISMC). The proposed methods ensure fast, finite-time convergence and robustness under wind disturbances, incorporating a Uniform Robust Exact Differentiator (URED) and a nonlinear state feedback disturbance observer to accurately recover rotor speed and missing derivatives, while the observer enhances system observability. Experimental validation on a twin rotor system confirms superior performance, with RGDIFTISMC achieving up to 46.7% faster stabilization. The results highlight its efficiency in improving transient response, steady-state accuracy, and robustness against disturbances.
KW - disturbance rejection
KW - fast terminal sliding mode control
KW - Robust control
KW - sliding mode control
KW - trajectory tracking
KW - twin rotor MIMO system
UR - https://www.scopus.com/pages/publications/105019677527
U2 - 10.1142/S2301385027500336
DO - 10.1142/S2301385027500336
M3 - Article
AN - SCOPUS:105019677527
SN - 2301-3850
JO - Unmanned Systems
JF - Unmanned Systems
ER -