Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV

This paper deals with the design of a novel modified supertwisting fast nonlinear sliding mode controller (MSTFNSMC) to stabilize a quadrotor system under time-varying disturbances. The suggested control strategy is based on a modified supertwisting controller with a fast nonlinear sliding surface t...

Full description

Saved in:
Bibliographic Details
Main Authors: Yassine El Houm, Ahmed Abbou, Moussa Labbadi, Mohamed Cherkaoui
Format: Article
Language:English
Published: Wiley 2020-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2020/9753870
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1832567934573084672
author Yassine El Houm
Ahmed Abbou
Moussa Labbadi
Mohamed Cherkaoui
author_facet Yassine El Houm
Ahmed Abbou
Moussa Labbadi
Mohamed Cherkaoui
author_sort Yassine El Houm
collection DOAJ
description This paper deals with the design of a novel modified supertwisting fast nonlinear sliding mode controller (MSTFNSMC) to stabilize a quadrotor system under time-varying disturbances. The suggested control strategy is based on a modified supertwisting controller with a fast nonlinear sliding surface to improve the tracking performance. The paper suggests a simple optimization tool built-in MATLAB/Simulink to tune the proposed controller parameters. Fast convergence of state variables is established by using a nonlinear sliding surface for rotational and translational subsystems. The modified supertwisting controller is developed to suppress the effect of chattering, reject disturbances, and ensure robustness against external disturbance effect. The stability of the proposed controller (MSTFNSMC) is proved using the Lyapunov theory. The performance of the proposed MSTFNSMC approach is compared with the supertwisting sliding mode controller (STSMC) by numerical simulations to verify its effectiveness.
format Article
id doaj-art-4d101d193791480cbc7e8c728720b75c
institution Kabale University
issn 1687-5966
1687-5974
language English
publishDate 2020-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-4d101d193791480cbc7e8c728720b75c2025-02-03T01:00:13ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742020-01-01202010.1155/2020/97538709753870Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAVYassine El Houm0Ahmed Abbou1Moussa Labbadi2Mohamed Cherkaoui3Engineering for Smart and Sustainable Systems Research Center, Mohammadia School of Engineers, Mohammed V University in Rabat, MoroccoEngineering for Smart and Sustainable Systems Research Center, Mohammadia School of Engineers, Mohammed V University in Rabat, MoroccoEngineering for Smart and Sustainable Systems Research Center, Mohammadia School of Engineers, Mohammed V University in Rabat, MoroccoEngineering for Smart and Sustainable Systems Research Center, Mohammadia School of Engineers, Mohammed V University in Rabat, MoroccoThis paper deals with the design of a novel modified supertwisting fast nonlinear sliding mode controller (MSTFNSMC) to stabilize a quadrotor system under time-varying disturbances. The suggested control strategy is based on a modified supertwisting controller with a fast nonlinear sliding surface to improve the tracking performance. The paper suggests a simple optimization tool built-in MATLAB/Simulink to tune the proposed controller parameters. Fast convergence of state variables is established by using a nonlinear sliding surface for rotational and translational subsystems. The modified supertwisting controller is developed to suppress the effect of chattering, reject disturbances, and ensure robustness against external disturbance effect. The stability of the proposed controller (MSTFNSMC) is proved using the Lyapunov theory. The performance of the proposed MSTFNSMC approach is compared with the supertwisting sliding mode controller (STSMC) by numerical simulations to verify its effectiveness.http://dx.doi.org/10.1155/2020/9753870
spellingShingle Yassine El Houm
Ahmed Abbou
Moussa Labbadi
Mohamed Cherkaoui
Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
International Journal of Aerospace Engineering
title Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
title_full Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
title_fullStr Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
title_full_unstemmed Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
title_short Optimal New Sliding Mode Controller Combined with Modified Supertwisting Algorithm for a Perturbed Quadrotor UAV
title_sort optimal new sliding mode controller combined with modified supertwisting algorithm for a perturbed quadrotor uav
url http://dx.doi.org/10.1155/2020/9753870
work_keys_str_mv AT yassineelhoum optimalnewslidingmodecontrollercombinedwithmodifiedsupertwistingalgorithmforaperturbedquadrotoruav
AT ahmedabbou optimalnewslidingmodecontrollercombinedwithmodifiedsupertwistingalgorithmforaperturbedquadrotoruav
AT moussalabbadi optimalnewslidingmodecontrollercombinedwithmodifiedsupertwistingalgorithmforaperturbedquadrotoruav
AT mohamedcherkaoui optimalnewslidingmodecontrollercombinedwithmodifiedsupertwistingalgorithmforaperturbedquadrotoruav