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

Bibliography: p. 199-207. 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.

Identiferoai:union.ndltd.org:ADTP/90800
Date January 2000
CreatorsKestell, Colin D. (Colin David)
Source SetsAustraliasian Digital Theses Program
LanguageEnglish
Detected LanguageEnglish
RelationSUA

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