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Sliding mode control for non-linear systems with adaptive sliding surfaces
Date
2012-02-01
Author
Durmaz, Burak
Özgören, Mustafa Kemal
SALAMCİ, METİN UYMAZ
Metadata
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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This study covers the sliding mode control design with adaptive sliding surfaces for a class of affine non-linear systems, which can be described by (x) over dot = A(x)x + B(x)u + f(x) + d(x, t). The main streamline of the study is the sliding surface design for such systems. The sliding surfaces are designed to be moving with varying slopes and offsets. The varying sliding surface parameters are determined by solving the state-dependent Riccati equations online during the control process. Thus, the sliding surfaces are updated in an adaptive manner to cope with the non-linearities of the system. The adaptive sliding mode control method developed in this study is used to design a longitudinal controller based on the mathematical model of a generic hypersonic aircraft. Then, the successful performance of this controller is demonstrated by means of a simulated manoeuvre of the aircraft.
Subject Keywords
Adaptive control
,
Sliding mode control
,
State-dependent Riccati equations
,
Variable structure control systems
URI
https://hdl.handle.net/11511/30315
Journal
TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL
DOI
https://doi.org/10.1177/0142331210384648
Collections
Graduate School of Natural and Applied Sciences, Article