High-precision measurement of satellite range and velocity using the EISCAT radar

This paper is a continuation of an earlier work by Nygrén et al. (2012), where the velocity of a hard target was determined from a set of echo pulses reflected by the target flying through the radar beam. Here the method is extended to include the determination of range at a high accuracy. The m...

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Main Authors: J. Markkanen, T. Nygrén, M. Markkanen, M. Voiculescu, A. Aikio
Format: Article
Language:English
Published: Copernicus Publications 2013-05-01
Series:Annales Geophysicae
Online Access:https://www.ann-geophys.net/31/859/2013/angeo-31-859-2013.pdf
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spelling doaj-85d7c9e9b4584092aef8f8149c269e832020-11-25T00:01:33ZengCopernicus PublicationsAnnales Geophysicae0992-76891432-05762013-05-013185987010.5194/angeo-31-859-2013High-precision measurement of satellite range and velocity using the EISCAT radarJ. Markkanen0T. Nygrén1M. Markkanen2M. Voiculescu3A. Aikio4EISCAT Scientific Association, Tähteläntie 54 B, 99600 Sodankylä, FinlandDepartment of Physics, University of Oulu, P.O. Box 3000, 90014, FinlandEigenor Ltd, Lompolontie 1, 99600 Sodankylä, FinlandDepartment of Physics, Faculty of Sciences, University "Dunărea de Jos" Galaţi, St. Domnească, No. 47, 800008 Galaţi, RomaniaDepartment of Physics, University of Oulu, P.O. Box 3000, 90014, FinlandThis paper is a continuation of an earlier work by Nygrén et al. (2012), where the velocity of a hard target was determined from a set of echo pulses reflected by the target flying through the radar beam. Here the method is extended to include the determination of range at a high accuracy. The method is as follows. First, the flight time of the pulse from the transmitter to the target is determined at an accuracy essentially better than the accuracy given by the sampling interval. This method makes use of the fact that the receiver filtering creates slopes at the phase flips of the phase modulated echo pulse. A precise flight time is found by investigating the echo amplitude within this slope. A value of velocity is calculated from each echo pulse as explained in the earlier paper. Next, the ranges together with velocities from a single beam pass are combined to a measurement vector for a linear inversion problem. The solution of the inversion problem gives the time-dependent range and velocity from the time interval of satellite flight through the radar beam. The method is demonstrated using the EISCAT (European Incoherent Scatter) UHF radar and radio pulses reflected by a satellite. The achieved standard deviations of range are about 5–50 cm and those of velocity are about 3–25 mm s<sup>−1</sup>.https://www.ann-geophys.net/31/859/2013/angeo-31-859-2013.pdf
collection DOAJ
language English
format Article
sources DOAJ
author J. Markkanen
T. Nygrén
M. Markkanen
M. Voiculescu
A. Aikio
spellingShingle J. Markkanen
T. Nygrén
M. Markkanen
M. Voiculescu
A. Aikio
High-precision measurement of satellite range and velocity using the EISCAT radar
Annales Geophysicae
author_facet J. Markkanen
T. Nygrén
M. Markkanen
M. Voiculescu
A. Aikio
author_sort J. Markkanen
title High-precision measurement of satellite range and velocity using the EISCAT radar
title_short High-precision measurement of satellite range and velocity using the EISCAT radar
title_full High-precision measurement of satellite range and velocity using the EISCAT radar
title_fullStr High-precision measurement of satellite range and velocity using the EISCAT radar
title_full_unstemmed High-precision measurement of satellite range and velocity using the EISCAT radar
title_sort high-precision measurement of satellite range and velocity using the eiscat radar
publisher Copernicus Publications
series Annales Geophysicae
issn 0992-7689
1432-0576
publishDate 2013-05-01
description This paper is a continuation of an earlier work by Nygrén et al. (2012), where the velocity of a hard target was determined from a set of echo pulses reflected by the target flying through the radar beam. Here the method is extended to include the determination of range at a high accuracy. The method is as follows. First, the flight time of the pulse from the transmitter to the target is determined at an accuracy essentially better than the accuracy given by the sampling interval. This method makes use of the fact that the receiver filtering creates slopes at the phase flips of the phase modulated echo pulse. A precise flight time is found by investigating the echo amplitude within this slope. A value of velocity is calculated from each echo pulse as explained in the earlier paper. Next, the ranges together with velocities from a single beam pass are combined to a measurement vector for a linear inversion problem. The solution of the inversion problem gives the time-dependent range and velocity from the time interval of satellite flight through the radar beam. The method is demonstrated using the EISCAT (European Incoherent Scatter) UHF radar and radio pulses reflected by a satellite. The achieved standard deviations of range are about 5–50 cm and those of velocity are about 3–25 mm s<sup>−1</sup>.
url https://www.ann-geophys.net/31/859/2013/angeo-31-859-2013.pdf
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