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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2021-01-01
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Series: | Computational Intelligence and Neuroscience |
Online Access: | http://dx.doi.org/10.1155/2021/3576783 |
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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 |
work_keys_str_mv |
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1721186094577352704 |