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Full Gradient Solution to Adaptive Hybrid Control
- 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 :
- Acoustics
Subjects
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