This study presents an adaptive sliding mode control approach for trajectory tracking of a quadrotor unmanned aerial vehicle functioning under external interference and kinematic unpredictability. Linear and rotational motion equations formulated in inactive local coordinate system frames are developed with the aid of a nonlinear six-degrees-of-freedom quadrotor dynamic model. Through mitigating excessive switching activity, reliability is improved. Here, the proposed controller integrates sliding mode control with bounded adaptive switching gain factors and boundary-layer smoothing. The operational design is applied within a sequential outer-loop/inner-loop structure for linear and orientation control. The conventional sliding mode control, alongside the proportional derivative control, which employs MATLAB/Simulink R2024a simulations while being interference-affected with an unknown performance set-up, is deployed in this work to relatively appraise the proposed ASM controller. The assessment involves three-dimensional trajectory, control input characteristics, tracking error analysis, adaptive gain growth, and chattering analysis with quantitative performance metrics. The computational output revealed that the proposed ASMC attained superior tracking performance with limited oscillation and level control action. The controller achieves a total RMSE of approximately 0.38 m and a lower aggregate tracking error when using the conventional SMC and PD controllers under equivalent conditions. Furthermore, the adaptive gain mechanism successfully lowers chattering while maintaining robustness against interferences, a large amount of ambiguity, and inertial imbalance with signal noise. The results validate that the proposed ASMC delivers a functional balance between robustness, control smoothness, and tracking accuracy alongside execution homogeneity for autonomous quadrotor UAV trajectory tracking in unsettled and unstable environments.
A robust control framework integrating the integral sliding mode controller (ISMC) with a momentum-based estimator (MBE) to ensure accurate trajectory tracking under uncertainty and maintains stability under up to 50% mass uncertainty is proposed.
Abdelkrim Kherkhar, B. Babes, Muath Odeh et al.· Scientific Reports· 0 citations
Numerical simulations demonstrate superior tracking accuracy and disturbance rejection capability compared to conventional adaptive neural DSC without disturbance observers, validating the effectiveness and robustness of the proposed scheme.
Xian Pan, Dong-Xue Wang, You-Wu Liu et al.· PLoS ONE· 0 citations
In this study, we have developed a novel robust fixed-time control framework that integrates a fractional-order sliding mode control with a disturbance observer for a quadrotor UAV. The overall system dynamics are represented in a cascaded structure with two major loops: position and orientation (attitude). To facilita...
Nasser Firouzi, Younis K. Khdir· Journal of Vibration and Con...· 0 citations
This paper presents the design, stability analysis, and validation of a neural adaptive sliding mode controller with an optimized fast logarithmic-tanh sliding surface (NASMC-OFLTS) for the attitude and altitude control of quadrotor unmanned aerial vehicles (UAVs) under parametric uncertainties and external disturban...
Azmat Saeed, H. Desa· Engineering Research Express· 0 citations
This paper investigates a disturbance observer combined with model predictive control (MPC) for trajectory tracking of quadrotor UAVs against model parameter perturbations, unmolded dynamics and external wind disturbances in complex low-altitude scenarios. Based on the small attitude angle assumption, the nonlinear dyn...
Hui Jia, Xiao-Wei Wei, Wei-Chao Li et al.· International Symposium on S...· 0 citations
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