A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV

This paper proposes a robust algorithm based on a fixed-time sliding mode controller (FTSMC) for a Quadrotor aircraft. This approach is based on Lyapunov theory, which guarantees system stability. Nonlinear error dynamics techniques are used to achieve accurate trajectory tracking in the presence of...

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Main Authors: Jairo Olguin-Roque, Sergio Salazar, Iván González-Hernandez, Rogelio Lozano
Format: Article
Language:English
Published: MDPI AG 2023-04-01
Series:Algorithms
Subjects:
Online Access:https://www.mdpi.com/1999-4893/16/5/229
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author Jairo Olguin-Roque
Sergio Salazar
Iván González-Hernandez
Rogelio Lozano
author_facet Jairo Olguin-Roque
Sergio Salazar
Iván González-Hernandez
Rogelio Lozano
author_sort Jairo Olguin-Roque
collection DOAJ
description This paper proposes a robust algorithm based on a fixed-time sliding mode controller (FTSMC) for a Quadrotor aircraft. This approach is based on Lyapunov theory, which guarantees system stability. Nonlinear error dynamics techniques are used to achieve accurate trajectory tracking in the presence of disturbances. The performance of the FTSMC is compared with the typical non-singular terminal sliding mode controller (NTSMC) to evaluate its effectiveness. The numerical results show that FTSMC is more efficient than the typical NTSMC in disturbance reduction.
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spelling doaj.art-f3cb624a9dc143688c85010f2ea9a8d82023-11-18T00:08:31ZengMDPI AGAlgorithms1999-48932023-04-0116522910.3390/a16050229A Robust Fixed-Time Sliding Mode Control for Quadrotor UAVJairo Olguin-Roque0Sergio Salazar1Iván González-Hernandez2Rogelio Lozano3UMI-LAFMIA, CINVESTAV, Ciudad de Mexico 07360, MexicoUMI-LAFMIA, CINVESTAV, Ciudad de Mexico 07360, MexicoUMI-LAFMIA, CINVESTAV, Ciudad de Mexico 07360, MexicoUMI-LAFMIA, CINVESTAV, Ciudad de Mexico 07360, MexicoThis paper proposes a robust algorithm based on a fixed-time sliding mode controller (FTSMC) for a Quadrotor aircraft. This approach is based on Lyapunov theory, which guarantees system stability. Nonlinear error dynamics techniques are used to achieve accurate trajectory tracking in the presence of disturbances. The performance of the FTSMC is compared with the typical non-singular terminal sliding mode controller (NTSMC) to evaluate its effectiveness. The numerical results show that FTSMC is more efficient than the typical NTSMC in disturbance reduction.https://www.mdpi.com/1999-4893/16/5/229Quadrotor aircraftFTSMCNTSMCrobust controltrajectory tracking control
spellingShingle Jairo Olguin-Roque
Sergio Salazar
Iván González-Hernandez
Rogelio Lozano
A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
Algorithms
Quadrotor aircraft
FTSMC
NTSMC
robust control
trajectory tracking control
title A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
title_full A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
title_fullStr A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
title_full_unstemmed A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
title_short A Robust Fixed-Time Sliding Mode Control for Quadrotor UAV
title_sort robust fixed time sliding mode control for quadrotor uav
topic Quadrotor aircraft
FTSMC
NTSMC
robust control
trajectory tracking control
url https://www.mdpi.com/1999-4893/16/5/229
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