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Performance of active feedforward control systems in non-ideal, synthesized diffuse sound fields

Misol, Malte und Bloch, Christian und Monner, Hans Peter und Sinapius, Michael (2014) Performance of active feedforward control systems in non-ideal, synthesized diffuse sound fields. Journal of the Acoustical Society of America, 135 (4), Seiten 1887-1897. Acoustical Society of America. doi: 10.1121/1.4865578. ISSN 0001-4966.

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Offizielle URL: http://scitation.aip.org/content/asa/journal/jasa/135/4/10.1121/1.4865578

Kurzfassung

The acoustic performance of passive or active panel structures is usually tested in sound transmission loss facilities. A reverberant sending room, equipped with one or a number of independent sound sources, is used to generate a diffuse sound field excitation which acts as a disturbance source on the structure under investigation. The spatial correlation and coherence of such a synthesized non-ideal diffuse-sound-field excitation, however, might deviate significantly from the ideal case. This has consequences for the operation of an active feedforward control system which heavily relies on the acquisition of coherent disturbance source information. This work, therefore, evaluates the spatial correlation and coherence of ideal and non-ideal diffuse sound fields and considers the implications on the performance of a feedforward control system. The system under consideration is an aircraft-typical double panel system, equipped with an active sidewall panel (lining), which is realized in a transmission loss facility. Experimental results for different numbers of sound sources in the reverberation room are compared to simulation results of a comparable generic double panel system excited by an ideal diffuse sound field. It is shown that the number of statistically independent noise sources acting on the primary structure of the double panel system depends not only on the type of diffuse sound field but also on the sample lengths of the processed signals. The experimental results show that the number of reference sensors required for a defined control performance exhibits an inverse relationship to control filter length.

elib-URL des Eintrags:https://elib.dlr.de/89851/
Dokumentart:Zeitschriftenbeitrag
Zusätzliche Informationen:Copyright (2014) Acoustical Society of America. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the Acoustical Society of America. The following article appeared in The Journal of the Acoustical Society of America, Vol. 135, No. 4 and may be found at (http://scitation.aip.org/content/asa/journal/jasa/135/4/10.1121/1.4865578)
Titel:Performance of active feedforward control systems in non-ideal, synthesized diffuse sound fields
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Misol, MalteInstitut für Faserverbundleichtbau und AdaptronikNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Bloch, ChristianNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Monner, Hans PeterInstitut für Faserverbundleichtbau und AdaptronikNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Sinapius, MichaelInstitut für Faseverbundleichtbau und AdaptronikNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:April 2014
Erschienen in:Journal of the Acoustical Society of America
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:135
DOI:10.1121/1.4865578
Seitenbereich:Seiten 1887-1897
Verlag:Acoustical Society of America
ISSN:0001-4966
Status:veröffentlicht
Stichwörter:Active feedforward control, diffuse sound field, double panel, spatial coherence, experiment
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Systeme und Kabine (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Adaptronik
Hinterlegt von: Stanitzek, Silke
Hinterlegt am:21 Jul 2014 08:24
Letzte Änderung:29 Nov 2023 08:48

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