Return to search

Active control of sound in a small single engine aircraft cabin with virtual error sensors

Bibliography: p. 199-207. Electronic publication; full text available in PDF format; abstract in HTML format. Describes the basis of a theoretical and experimental project, directed at the design and evaluation of a practical active noise control system suitable for a single light engine aircraft. The performance of virtual sensors were evaluated both analytically and experimentally in progressively more complex environments to identify their capabilities and limitations. Electronic reproduction.[Australia] :Australian Digital Theses Program,2001.

Identiferoai:union.ndltd.org:ADTP/114825
Date January 2000
CreatorsKestell, Colin D. (Colin David)
Source SetsAustraliasian Digital Theses Program
LanguageEnglish
Detected LanguageEnglish
RelationSUA

Page generated in 0.0021 seconds