The Bootstrap applied to Passive Acoustic Aircraft Parameter Estimation

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The Bootstrap applied to Passive Acoustic Aircraft Parameter Estimation

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dc.contributor.author Reid, D.C.
dc.contributor.author Zoubir, A.M.
dc.contributor.author Boashash, B
dc.date.accessioned 2012-06-18T16:35:42Z
dc.date.available 2012-06-18T16:35:42Z
dc.date.issued 1996
dc.identifier.citation D.C. Reid, A. M. Zoubir and B. Boashash, “The Bootstrap applied to Passive Acoustic Aircraft Parameter Estimation”, Proceedings of the International Conference on Acoustics, Speech and Signal Processing (ICASSP-96), vol. 6, pp. 3153-3156, Atlanta, Georgia, USA, May 1996 en_US
dc.identifier.uri http://dx.doi.org/10.1109/icassp.1996.550545
dc.identifier.uri http://hdl.handle.net/10576/10856
dc.description.abstract This paper proposes and demonstrates a practical parameter estimation scheme for estimating the height, speed, range and acoustic frequency of an overflying aircraft. This scheme is based on the phase of the acoustic signal emitted by the aircraft as heard by a stationary observer. Bootstrap techniques are employed to determine confidence bounds for the aircraft parameters given only a single acoustic realisation. This estimation scheme, and the novel use of the bootstrap, are demonstrated by computer simulation and with aircraft acoustic data which was collected by the authors under accurately monitored experimental conditions. en_US
dc.language.iso en en_US
dc.publisher IEEE en_US
dc.title The Bootstrap applied to Passive Acoustic Aircraft Parameter Estimation en_US
dc.type Article en_US

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