SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER

We consider the problem of slant range distance measurement from aircrafts in conditions of complex spatial structure. The range determination in active laser range finders, including slant range, is based on measuring the time difference of two time points, the time point when the pulse exits the l...

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Main Authors: Le Dinh Vu, Evgeny G. Lebedko
Format: Article
Language:English
Published: Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University) 2017-07-01
Series:Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki
Subjects:
Online Access:http://ntv.ifmo.ru/file/article/16888.pdf
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spelling doaj-ba8dc322bc1a4f638495779b4a9c32342020-11-25T00:30:33ZengSaint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University)Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki2226-14942500-03732017-07-0117460561110.17586/2226-1494-2017-17-4-605-611SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDERLe Dinh Vu 0Evgeny G. Lebedko 1postgraduate, ITMO University, Saint Petersburg, 197101, Russian FederationD.Sc., Full Professor, ITMO University, Saint Petersburg, 197101, Russian FederatioWe consider the problem of slant range distance measurement from aircrafts in conditions of complex spatial structure. The range determination in active laser range finders, including slant range, is based on measuring the time difference of two time points, the time point when the pulse exits the laser range finders, and the time point when the pulse comes back, after being reflected from a target. The signal emission reflected from a target is a variable of random process, because of the irradiated surface length, even under narrow field radiation. When determining the slant range distance from aircraft to a target, it is necessary to identify the signal emission reflected from a target, from background signal reflected by underlying surface. We propose two methods of slant range measurements, provided identification of target that is located on the underlying surface with complex structure. The first method is based on the measurement of slant range distance when the lower edge of the radiation field is aligned with the pointing direction. The second method is based on the measurement of slant range distance when the upper edge of the radiation field is aligned with the pointing direction. We propose structural schemes based on these methods and describe their operation principles. Evaluation of the advantages and disadvantages for each method is given.http://ntv.ifmo.ru/file/article/16888.pdfslant range measurementreflective impulse characteristicspulsed laser range finderunderlying surfacebeam divergence angle
collection DOAJ
language English
format Article
sources DOAJ
author Le Dinh Vu
Evgeny G. Lebedko
spellingShingle Le Dinh Vu
Evgeny G. Lebedko
SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki
slant range measurement
reflective impulse characteristics
pulsed laser range finder
underlying surface
beam divergence angle
author_facet Le Dinh Vu
Evgeny G. Lebedko
author_sort Le Dinh Vu
title SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
title_short SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
title_full SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
title_fullStr SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
title_full_unstemmed SLANT RANGE MEASUREMENT BY IMPULSE LASER RANGE FINDER
title_sort slant range measurement by impulse laser range finder
publisher Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University)
series Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki
issn 2226-1494
2500-0373
publishDate 2017-07-01
description We consider the problem of slant range distance measurement from aircrafts in conditions of complex spatial structure. The range determination in active laser range finders, including slant range, is based on measuring the time difference of two time points, the time point when the pulse exits the laser range finders, and the time point when the pulse comes back, after being reflected from a target. The signal emission reflected from a target is a variable of random process, because of the irradiated surface length, even under narrow field radiation. When determining the slant range distance from aircraft to a target, it is necessary to identify the signal emission reflected from a target, from background signal reflected by underlying surface. We propose two methods of slant range measurements, provided identification of target that is located on the underlying surface with complex structure. The first method is based on the measurement of slant range distance when the lower edge of the radiation field is aligned with the pointing direction. The second method is based on the measurement of slant range distance when the upper edge of the radiation field is aligned with the pointing direction. We propose structural schemes based on these methods and describe their operation principles. Evaluation of the advantages and disadvantages for each method is given.
topic slant range measurement
reflective impulse characteristics
pulsed laser range finder
underlying surface
beam divergence angle
url http://ntv.ifmo.ru/file/article/16888.pdf
work_keys_str_mv AT ledinhvu slantrangemeasurementbyimpulselaserrangefinder
AT evgenyglebedko slantrangemeasurementbyimpulselaserrangefinder
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