RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs

In this article, a singularity-free terminal sliding mode (SFTSM) control scheme based on the radial basis function neural network (RBFNN) is proposed for the quadrotor unmanned aerial vehicles (QUAVs) under the presence of inertia uncertainties and external disturbances. Firstly, a singularity-free...

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Main Authors: Meiling Tao, Xiongxiong He, Shuzong Xie, Qiang Chen
Format: Article
Language:English
Published: Hindawi Limited 2021-01-01
Series:Computational Intelligence and Neuroscience
Online Access:http://dx.doi.org/10.1155/2021/3576783
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spelling doaj-5abfb4cb50e24e3c8f67ba5401c9ad822021-08-30T00:00:44ZengHindawi LimitedComputational Intelligence and Neuroscience1687-52732021-01-01202110.1155/2021/3576783RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVsMeiling Tao0Xiongxiong He1Shuzong Xie2Qiang Chen3Data-driven Intelligent Systems LaboratoryData-driven Intelligent Systems LaboratoryKey Laboratory of Advanced Perception and Intelligent Control of High-end EquipmentData-driven Intelligent Systems LaboratoryIn this article, a singularity-free terminal sliding mode (SFTSM) control scheme based on the radial basis function neural network (RBFNN) is proposed for the quadrotor unmanned aerial vehicles (QUAVs) under the presence of inertia uncertainties and external disturbances. Firstly, a singularity-free terminal sliding mode surface (SFTSMS) is constructed to achieve the finite-time convergence without any piecewise continuous function. Then, the adaptive finite-time control is designed with an auxiliary function to avoid the singularity in the error-related inverse matrix. Moreover, the RBFNN and extended state observer (ESO) are introduced to estimate the unknown disturbances, respectively, such that prior knowledge on system model uncertainties is not required for designing attitude controllers. Finally, the attitude and angular velocity errors are finite-time uniformly ultimately bounded (FTUUB), and numerical simulations illustrated the satisfactory performance of the designed control scheme.http://dx.doi.org/10.1155/2021/3576783
collection DOAJ
language English
format Article
sources DOAJ
author Meiling Tao
Xiongxiong He
Shuzong Xie
Qiang Chen
spellingShingle Meiling Tao
Xiongxiong He
Shuzong Xie
Qiang Chen
RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
Computational Intelligence and Neuroscience
author_facet Meiling Tao
Xiongxiong He
Shuzong Xie
Qiang Chen
author_sort Meiling Tao
title RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
title_short RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
title_full RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
title_fullStr RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
title_full_unstemmed RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs
title_sort rbfnn-based singularity-free terminal sliding mode control for uncertain quadrotor uavs
publisher Hindawi Limited
series Computational Intelligence and Neuroscience
issn 1687-5273
publishDate 2021-01-01
description In this article, a singularity-free terminal sliding mode (SFTSM) control scheme based on the radial basis function neural network (RBFNN) is proposed for the quadrotor unmanned aerial vehicles (QUAVs) under the presence of inertia uncertainties and external disturbances. Firstly, a singularity-free terminal sliding mode surface (SFTSMS) is constructed to achieve the finite-time convergence without any piecewise continuous function. Then, the adaptive finite-time control is designed with an auxiliary function to avoid the singularity in the error-related inverse matrix. Moreover, the RBFNN and extended state observer (ESO) are introduced to estimate the unknown disturbances, respectively, such that prior knowledge on system model uncertainties is not required for designing attitude controllers. Finally, the attitude and angular velocity errors are finite-time uniformly ultimately bounded (FTUUB), and numerical simulations illustrated the satisfactory performance of the designed control scheme.
url http://dx.doi.org/10.1155/2021/3576783
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AT shuzongxie rbfnnbasedsingularityfreeterminalslidingmodecontrolforuncertainquadrotoruavs
AT qiangchen rbfnnbasedsingularityfreeterminalslidingmodecontrolforuncertainquadrotoruavs
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