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dc.contributor.authorMartín Román, Sara-Regina
dc.contributor.authorGenesca Francitorra, Meritxell
dc.contributor.authorRomeu Robert, Jordi
dc.contributor.authorArcos Villamarín, Robert
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria Mecànica
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Teoria del Senyal i Comunicacions
dc.date.accessioned2014-12-10T13:39:40Z
dc.date.created2014-04-01
dc.date.issued2014-04-01
dc.identifier.citationMartin, S.R. [et al.]. Passive acoustic method for aircraft states estimation based on the Doppler effect. "IEEE transactions on aerospace and electronic systems", 01 Abril 2014, vol. 50, núm. 2, p. 1330-1346.
dc.identifier.issn0018-9251
dc.identifier.urihttp://hdl.handle.net/2117/24983
dc.description.abstractA passive acoustic method to locate moving sound sources is applied to maneuvering aircraft. The advantages of the method are that it is suitable for all kinds of aircraft, not only propeller-driven, and is not restricted to low height above the ground. Its applicability could be, for instance, to supplement aircraft noise monitoring systems or to supervise small airports' activities. The method is based on the relation between the relative Doppler effect observed from a set of at least seven microphone receivers, distributed in the airport surroundings, and the aircraft position and speed. The method requires knowledge of the position of the aircraft at the start of takeoff. The ambiguity function is used to calculate the relative Doppler stretch of the spectrum of the sound between pairs of microphones. The results of applying the ambiguity function are the inputs to a system of equations that relates the aircraft position and speed to the relative Doppler frequency stretches. This system of equations is solved using a genetic algorithm. The performance of the method was tested by computer simulation. The results showed that the location errors are of the same order of magnitude as the size of an average aircraft, even if the takeoff position is not accurately known.
dc.format.extent17 p.
dc.language.isoeng
dc.subjectÀrees temàtiques de la UPC::Física::Acústica::Física del so
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Navegació aèria
dc.subject.lcshDoppler effect
dc.subject.lcshDoppler navigation
dc.subject.lcshNavigation (Aeronautics)
dc.subject.otherParameter-estimation
dc.subject.otherTime-delay
dc.subject.otherLocalization
dc.subject.otherArray
dc.subject.otherStretch
dc.subject.otherSensor
dc.titlePassive acoustic method for aircraft states estimation based on the Doppler effect
dc.typeArticle
dc.subject.lemacNavegació aèria
dc.subject.lemacRadar en aeronàutica
dc.contributor.groupUniversitat Politècnica de Catalunya. LEAM - Laboratori d'Enginyeria Acústica i Mecànica
dc.contributor.groupUniversitat Politècnica de Catalunya. ANTENNALAB - Grup d'Antenes i Sistemes Radio
dc.identifier.doi10.1109/TAES.2013.120176
dc.description.peerreviewedPeer Reviewed
dc.rights.accessRestricted access - publisher's policy
local.identifier.drac15342100
dc.description.versionPostprint (published version)
dc.date.lift10000-01-01
local.citation.authorMartin, S.R.; Genesca, M.; Romeu, J.; Arcos, R.
local.citation.publicationNameIEEE transactions on aerospace and electronic systems
local.citation.volume50
local.citation.number2
local.citation.startingPage1330
local.citation.endingPage1346


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