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Full Gradient Solution to Adaptive Hybrid Control

Authors :
Bean, Jacob
Schiller, Noah H
Fuller, Chris
Source :
Proceedings of Meetings on Acoustics. 29
Publication Year :
2016
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2016.

Abstract

This paper focuses on the adaptation mechanisms in adaptive hybrid controllers. Most adaptive hybrid controllers update two filters individually according to the filtered-reference least mean squares (FxLMS) algorithm. Because this algorithm was derived for feedforward control, it does not take into account the presence of a feedback loop in the gradient calculation. This paper provides a derivation of the proper weight vector gradient for hybrid (or feedback) controllers that takes into account the presence of feedback. In this formulation, a single weight vector is updated rather than two individually. An internal model structure is assumed for the feedback part of the controller. The full gradient is equivalent to that used in the standard FxLMS algorithm with the addition of a recursive term that is a function of the modeling error. Some simulations are provided to highlight the advantages of using the full gradient in the weight vector update rather than the approximation.

Subjects

Subjects :
Acoustics

Details

Language :
English
Volume :
29
Database :
NASA Technical Reports
Journal :
Proceedings of Meetings on Acoustics
Notes :
WBS 664817.02.07.03.02.02
Publication Type :
Report
Accession number :
edsnas.20170003219
Document Type :
Report