DocumentCode
2587208
Title
Acoustic detection of low flying aircraft
Author
Nielsen, Richard O.
Author_Institution
Boeing Co., Anaheim, CA, USA
fYear
2009
fDate
11-12 May 2009
Firstpage
101
Lastpage
106
Abstract
A passive acoustic system, consisting of a set of acoustic nodes and a central processing node, is a good candidate for the covert detection of low flying aircraft as they cross our nation´s borders. Small arrays of microphones have been used to estimate aircraft speed, heading, frequency spectrum and altitude at the closest point of approach. We extend this work by considering maneuvering aircraft and by testing a narrowband algorithm that gives angle estimates sooner, and over a longer period of time, than the broadband version. A new narrowband algorithm is provided for estimating position versus time as the aircraft flies through a grid of widely spaced omni-directional microphones (separated by several miles). We classify aircraft as helicopter, piston engine aircraft (specifically, numbers of propeller blades and cylinders), turboprop aircraft or jet aircraft. Our approach has been validated via testing at various airports against ground truth data.
Keywords
acoustic signal detection; aerospace instrumentation; helicopters; acoustic nodes; angle estimation; central processing node; low flying aircraft acoustic detection; microphone array; narrowband algorithm testing; Acoustic signal detection; Aircraft propulsion; Engines; Frequency estimation; Helicopters; Microphone arrays; Narrowband; Pistons; Propellers; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Technologies for Homeland Security, 2009. HST '09. IEEE Conference on
Conference_Location
Boston, MA
Print_ISBN
978-1-4244-4178-5
Type
conf
DOI
10.1109/THS.2009.5168021
Filename
5168021
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