Chatter Free Adaptive Sliding Mode Controller for Plants with Unknown Parameters Using a Varying Boundary Layer Thickness

An adaptive sliding mode controller (ASMC) is presented that can control plants of the n-th order with completely unknown parameters, while using a varying boundary layer thickness for complete chatter prevention. Adaptation laws are derived for parameter estimation and varying boundary layer thickness adaptation. A Lyapunov stability analysis shows that the parameter adaptation laws drive the combined error for the sliding surface to zero while rejecting bounded disturbances. The boundary layer adaptation law automatically grows the boundary layer thickness in the presence of disturbances and reduces it when the disturbances are not present to always keep the sliding surface error trajectory within the boundary layer, which guarantees chatter prevention. Simulations show the superior performance of the proposed ASMC compared to a non-adaptive sliding mode controller with a fixed boundary layer thickness.

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Publication Details

Journal
Automatic Control and Computer Sciences
Published
2025-10-01
DOI
https://doi.org/10.3103/s0146411625701135
Primary Topic
Plasma and Flow Control in Aerodynamics
Type
article
Field-Weighted Citation Impact
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article

Chatter Free Adaptive Sliding Mode Controller for Plants with Unknown Parameters Using a Varying Boundary Layer Thickness

Farbod Fahimi, Josiah Schlabach
Automatic Control and Computer Sciences
Plasma and Flow Control in Aerodynamics
article

Chatter Free Adaptive Sliding Mode Controller for Plants with Unknown Parameters Using a Varying Boundary Layer Thickness

Farbod Fahimi, Josiah Schlabach
article en

Abstract

An adaptive sliding mode controller (ASMC) is presented that can control plants of the n-th order with completely unknown parameters, while using a varying boundary layer thickness for complete chatter prevention. Adaptation laws are derived for parameter estimation and varying boundary layer thickness adaptation. A Lyapunov stability analysis shows that the parameter adaptation laws drive the combined error for the sliding surface to zero while rejecting bounded disturbances. The boundary layer adaptation law automatically grows the boundary layer thickness in the presence of disturbances and reduces it when the disturbances are not present to always keep the sliding surface error trajectory within the boundary layer, which guarantees chatter prevention. Simulations show the superior performance of the proposed ASMC compared to a non-adaptive sliding mode controller with a fixed boundary layer thickness.

Automatic Control and Computer SciencesVol. 59(5)
University of Alabama in Huntsville (US)
Openalex Percentile: Top 18%
Plasma and Flow Control in Aerodynamics
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