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JCR Impact Factor: 0.700
JCR 5-Year IF: 0.700
SCOPUS CiteScore: 1.8
Issues per year: 4
Current issue: Aug 2024
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PUBLISHER

Stefan cel Mare
University of Suceava
Faculty of Electrical Engineering and
Computer Science
13, Universitatii Street
Suceava - 720229
ROMANIA

Print ISSN: 1582-7445
Online ISSN: 1844-7600
WorldCat: 643243560
doi: 10.4316/AECE


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2024-Jun-20
Clarivate Analytics published the InCites Journal Citations Report for 2023. The InCites JCR Impact Factor of Advances in Electrical and Computer Engineering is 0.700 (0.700 without Journal self-cites), and the InCites JCR 5-Year Impact Factor is 0.600.

2023-Jun-28
Clarivate Analytics published the InCites Journal Citations Report for 2022. The InCites JCR Impact Factor of Advances in Electrical and Computer Engineering is 0.800 (0.700 without Journal self-cites), and the InCites JCR 5-Year Impact Factor is 1.000.

2023-Jun-05
SCOPUS published the CiteScore for 2022, computed by using an improved methodology, counting the citations received in 2019-2022 and dividing the sum by the number of papers published in the same time frame. The CiteScore of Advances in Electrical and Computer Engineering for 2022 is 2.0. For "General Computer Science" we rank #134/233 and for "Electrical and Electronic Engineering" we rank #478/738.

2022-Jun-28
Clarivate Analytics published the InCites Journal Citations Report for 2021. The InCites JCR Impact Factor of Advances in Electrical and Computer Engineering is 0.825 (0.722 without Journal self-cites), and the InCites JCR 5-Year Impact Factor is 0.752.

2022-Jun-16
SCOPUS published the CiteScore for 2021, computed by using an improved methodology, counting the citations received in 2018-2021 and dividing the sum by the number of papers published in the same time frame. The CiteScore of Advances in Electrical and Computer Engineering for 2021 is 2.5, the same as for 2020 but better than all our previous results.

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  2/2014 - 5

 HIGHLY CITED PAPER 

Cold Start Strategy of the CubeSat GPS Receiver

KOVAR, P. See more information about KOVAR, P. on SCOPUS See more information about KOVAR, P. on IEEExplore See more information about KOVAR, P. on Web of Science, JELEN, S. See more information about JELEN, S. on SCOPUS See more information about JELEN, S. on SCOPUS See more information about JELEN, S. on Web of Science
 
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Download PDF pdficon (716 KB) | Citation | Downloads: 878 | Views: 2,107

Author keywords
cold start, CubeSat, LEO orbit, space GPS receiver

References keywords
navigation(8), space(7), receiver(6), satellite(4), gnss(4)
Blue keywords are present in both the references section and the paper title.

About this article
Date of Publication: 2014-05-31
Volume 14, Issue 2, Year 2014, On page(s): 29 - 34
ISSN: 1582-7445, e-ISSN: 1844-7600
Digital Object Identifier: 10.4316/AECE.2014.02005
Web of Science Accession Number: 000340868100005
SCOPUS ID: 84901825251

Abstract
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The cold start of the LEO satellite GPS receiver is complicated due to a large Doppler frequency shift, Doppler frequency rate of the navigation signals and a rapid change of the satellite visibility. The cold start time can be shortened by a proper strategy of a selection of the satellites to be searched for. The cold start simulator was developed and used for optimization of the sequence of the satellites search, for development and testing of an advanced satellite selection algorithm that utilizes information on the satellites already detected and for optimization of a frequency search range. The best performance was achieved by using an advanced selection strategy. The strategy is based on the selection of the satellites nearest to the detected satellite, using the average angle between the Earth center (apex) and the satellites. Furthermore, the simulation shows that it is not practical to investigate all frequencies within the range of the maximum possible Doppler frequency shift of the carrier wave of the navigation signal, but investigate approximately +/- 35 kHz range and, if not successful, switch to the next satellite. The simulations proved that a simple GPS receiver with the sequential search algorithms can operate in the LEO orbit.


References | Cited By

Cited-By Clarivate Web of Science

Web of Science® Times Cited: 5 [View]
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Cited-By SCOPUS

SCOPUS® Times Cited: 5
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Cited-By CrossRef

[1] Experiences with the GPS in Unstabilized CubeSat, Kovar, Pavel, International Journal of Aerospace Engineering, ISSN 1687-5966, Issue , 2020.
Digital Object Identifier: 10.1155/2020/8894984
[CrossRef]

[2] Simulation of Navigation Receiver for Ultra-Small Satellite, Spiridonov, A. A., Ushakov, D. V., Saechnikov, V. A., Devices and Methods of Measurements, ISSN 2414-0473, Issue 4, Volume 10, 2019.
Digital Object Identifier: 10.21122/2220-9506-2019-10-4-331-340
[CrossRef]

[3] Parallel Frequency Acquisition Algorithm for BeiDou Software Receiver Based on Coherent Downsampling, Zeng, Qingxi, Gao, Chang, Qiu, Wenqi, Zhou, Zhaihe, Lyu, Chade, Journal of Navigation, ISSN 0373-4633, Issue 2, Volume 73, 2020.
Digital Object Identifier: 10.1017/S0373463319000699
[CrossRef]

[4] piNAV L1—GPS receiver for small satellites, Kovář, P., Gyroscopy and Navigation, ISSN 2075-1087, Issue 2, Volume 8, 2017.
Digital Object Identifier: 10.1134/S2075108717020079
[CrossRef]

Updated 2 days, 6 hours ago

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Faculty of Electrical Engineering and Computer Science
Stefan cel Mare University of Suceava, Romania


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