控制理论(社会学)
姿态控制
滑模控制
控制工程
模式(计算机接口)
自适应控制
计算机科学
人工神经网络
工程类
控制(管理)
物理
非线性系统
人工智能
量子力学
操作系统
作者
Mati Ullah,Hongbo Gao,Alam Nasir,Yafei Wang,Chengbo Wang
标识
DOI:10.1109/taes.2024.3456760
摘要
Achieving attitude stabilization in quadrotor helicopters (qhs) operating in complex environments, characterized by external disturbances and model uncertainties, presents a significant challenge. This study presents an adaptive-neural finite-time sliding mode control (anft-smc) to effectively address these challenges. The proposed method integrates nonsingular fast terminal sliding mode control (nft-smc) with a radial basis function neural network (rbfnn), which is equipped with a fast auto-tuning law. Consequently, the method transcends qh model constraints and obviates the need for explicit knowledge of external disturbances and model uncertainties. The effectiveness of the proposed approach in stabilizing attitude dynamics is rigorously validated through a comprehensive Lyapunov stability analysis, scrutinizing key stability aspects. Extensive simulations conducted using matlab and Simulink, compared against a nominal nft-smc implementation based on a state observer (so) benchmark, demonstrate the superior performance and robustness of the proposed method in achieving finite-time stabilization of qh attitude dynamics.
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