A novel RNN terminal sliding mode controller design based on barrier function for uncertain quad-rotor UAV systems

A new triple-loop recurrent neural network (TLRNN) super-twisting terminal sliding mode control (TSMC) scheme based on the barrier function is proposed for the attitude tracking control of flight systems with unknown disturbances and parameter uncertainties. Compared with the traditional recurrent neural network (RNN), the newly designed TLRNN incorporates three different feedback loops, which improves the performance of approximation and enhances the capacity to save information. Additionally, the barrier function-based variable gain super-twisting algorithm is used to reduce chattering and dynamically adjust control gain. The finite-time convergence of a quad-rotor UAV system is derived using the Lyapunov function technique. The experiments, compared with existing methods, demonstrate the effectiveness of the proposed control strategy.

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Publication Details

Journal
Advances in Mechanical Engineering
Published
2025-12-01
DOI
https://doi.org/10.1177/16878132251396728
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
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article

A novel RNN terminal sliding mode controller design based on barrier function for uncertain quad-rotor UAV systems

Qing Li
Advances in Mechanical Engineering
Adaptive Control of Nonlinear Systems
article

A novel RNN terminal sliding mode controller design based on barrier function for uncertain quad-rotor UAV systems

Qing Li
article en

Abstract

A new triple-loop recurrent neural network (TLRNN) super-twisting terminal sliding mode control (TSMC) scheme based on the barrier function is proposed for the attitude tracking control of flight systems with unknown disturbances and parameter uncertainties. Compared with the traditional recurrent neural network (RNN), the newly designed TLRNN incorporates three different feedback loops, which improves the performance of approximation and enhances the capacity to save information. Additionally, the barrier function-based variable gain super-twisting algorithm is used to reduce chattering and dynamically adjust control gain. The finite-time convergence of a quad-rotor UAV system is derived using the Lyapunov function technique. The experiments, compared with existing methods, demonstrate the effectiveness of the proposed control strategy.

Advances in Mechanical EngineeringVol. 17(12)
First Affiliated Hospital of Henan University (CN)
Affordable and clean energy
Openalex Percentile: Top 37%
Adaptive Control of Nonlinear Systems
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