DocumentCode :
2436629
Title :
Bearing Line Tracking and Bearing-Only Target Motion Analysis
Author :
Bonneton, Fabien ; Jauffret, Claude
Author_Institution :
Univ. du Sud Toulon-Var, La Garde
fYear :
2007
fDate :
3-10 March 2007
Firstpage :
1
Lastpage :
9
Abstract :
The framework of this paper is a passive sonar system, more precisely at the core of bearing estimation and bearings-only target motion analysis (BO-TMA). A cosine of relative bearing estimation and bearings v.s. time image is first obtained by a conventional frequency-domain beam-former [D.H Johnson et al, 1993]. Computing the first two moments of each line of this image, we evaluate the likelihood of the cosine of relative bearing of the target. Then, the cosine of relative bearing and its derivative are considered as the two components of a state vector of a linear dynamic system. This state vector is then estimated (or extracted) by a classical algorithm of the hidden Markov model (HMM) arsenal, whose parameters are adjusted according to the statistical assumptions. Unlike, we consider the presence of one sole target, but the beginning and the end of the line are unknown and must be estimated too. The extracted track is used as measurements set of the BO-TMA. Finally, the confrontation of the TMA results allow us to evaluate the performance of the triplet (beam-former, bearing extraction, BO-TMA).
Keywords :
frequency-domain analysis; hidden Markov models; sonar signal processing; target tracking; bearing line tracking; bearing-only target motion analysis; frequency-domain beam-former; hidden Markov model arsenal; linear dynamic system; passive sonar system; Array signal processing; Direction of arrival estimation; Frequency; Hidden Markov models; Motion analysis; Sensor arrays; Signal processing algorithms; Sonar; Target tracking; Vectors; BO-TMA; Beamforming; Bearing estimation; HMM;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2007.353037
Filename :
4161447
Link To Document :
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