Localization of Low Flying Aircraft Using Acoustic Vector Sensor

Author:

Saravanakumar A.,Senthilkumar K.,Sadasivan S.

Abstract

This paper addresses a method for estimating the linear flying trajectory of a fixed-wing aircraft based on narrow-band passive acoustical technique, which measures the instantaneous frequency of the acoustic signal emitted by the target and received by Acoustic Vector Sensor (AVS) placed on the ground. AVS consist of one microphone and three vector sensors orthogonal to each other. The received instantaneous frequency varies due to the acoustical Doppler Effect under the condition that the target flies at a constant velocity and the trajectory is a straight line. A four parameter model was developed to describe the aircraft trajectory. The four parameters are the targets travel speed, the source acoustical frequency, the time at which the target gets to the closest point of approach (CPA) to the sensor, and the CPA slant range to the sensor. Nonlinear least square (NLS) theory was used to estimate these parameters. The three dimensional AVS consists of three orthogonally placed particle velocity sensors and one sound pressure microphone. The four parameters mentioned above are measured using microphone. The particle velocity sensors are used for finding the direction of acoustic source.

Reference14 articles.

1. Brian G. Ferguson., Lionel G. Criswick and Kam W. Lo., "Locating Far-field Impulsive Sound Sources in Air by Triangulation", J. Acoustic. Soc. Am., Vol.111, No.1, 2002.

2. Arye Nehorai and Eytan Paldi., "Acoustic Vector- Sensor Array Processing", IEEE Transaction on Signal Processing, Vol. 42, No.9, 1994, pp.2481-2491.

3. Brian G. Ferguson and Kam,W. Lo., "Turboprop and Rotary Wing Aircraft Flight Parameter Estimation Using Both Narrow-band and Broadband passive Acoustic Signal-processing Methods", Acoustical Society of America, 2009.

4. Ferguson, B.G. and Quinn, B.G., "Application of the Short-time o Fourier Transform and the Wigner- Ville Distribution to the Acoustic Localization of Aircraft", J. Acoust. Soc. Am., Vol.96 (2), 1994, pp.821l-827.

5. Kam, W. Lo.and Ferguson, B.G., "Broadband Passive Acoustic Technique for Target Motion Parameter Estimation", IEEE Transactions of Aerospace and Electronic Systems, 2000.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3