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Derivation of an optimal boundary layer width for the smooth variable structure filter

dc.contributor.authorGadsden SA
dc.contributor.authorSayed ME
dc.contributor.authorHabibi SR
dc.contributor.departmentMechanical Engineering
dc.date.accessioned2025-02-27T19:33:58Z
dc.date.available2025-02-27T19:33:58Z
dc.date.issued2011-06-01
dc.date.updated2025-02-27T19:33:57Z
dc.description.abstractIn this paper, an augmented form of the smooth variable structure filter (SVSF) is proposed. The SVSF is a state estimation strategy based on variable structure and sliding mode concepts. It uses a smoothing boundary to remove chattering (excessive switching along an estimated state trajectory). In its current form, the SVSF defines the boundary layer by an upper-bound on the uncertainties present in the estimation process (i.e., modeling errors, magnitude of noise, etc.). This is a conservative approach as one would be limiting the gain by assuming a larger smoothing boundary subspace than what is necessary. A more well-defined boundary layer will yield more accurate estimates. This paper derives a solution for an optimal boundary layer width by minimizing the trace of the a posteriori covariance matrix. The results of the derivation are simulated on a linear mechanical system for the purposes of control, and compared with the Kalman filter. © 2011 AACC American Automatic Control Council.
dc.identifier.doihttps://doi.org/10.1109/acc.2011.5990970
dc.identifier.issn0743-1619
dc.identifier.issn2378-5861
dc.identifier.urihttp://hdl.handle.net/11375/31201
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)
dc.subject4901 Applied Mathematics
dc.subject40 Engineering
dc.subject49 Mathematical Sciences
dc.subject4001 Aerospace Engineering
dc.titleDerivation of an optimal boundary layer width for the smooth variable structure filter
dc.typeArticle

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