• 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