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Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon

This dissertation reports on the investigation to determine which orbits, ionospheric conditions and seasons of the year that will facilitate the reception of the high frequency (HF) beacon signal from the 1 U CubeSat ZACUBE 1 by the SuperDARN HF radar in Antarctica, and by the HF direction-finding...

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Main Author: Agaba, Doreen
Other Authors: Inggs, Michael
Format: Thesis
Language:English
Published: Department of Electrical Engineering 2015
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access_status_str Open Access
author Agaba, Doreen
author2 Inggs, Michael
author_browse Agaba, Doreen
Inggs, Michael
author_facet Inggs, Michael
Agaba, Doreen
author_sort Agaba, Doreen
collection Thesis
description This dissertation reports on the investigation to determine which orbits, ionospheric conditions and seasons of the year that will facilitate the reception of the high frequency (HF) beacon signal from the 1 U CubeSat ZACUBE 1 by the SuperDARN HF radar in Antarctica, and by the HF direction-finding (DF) systems in both Pretoria and Hermanus. The primary objective of the HF beacon on ZACUBE 1 is to provide a continuous radio signal to calibrate and verify the elevation-resolving algorithm of the SuperDARN HF Radar antenna at SANAE IV in Antarctica. The signal will also be used to characterise the beam pattern of this and other HF radar antennas in the SuperDARN network, and to characterise the ionosphere over the Earth’s polar region. A secondary objective of the HF beacon on the satellite is to measure the ionospheric total electron content (TEC) by using either measurements of the carrier phase delays or of the Faraday rotation of the signal. An orbit analysis was done for the CubeSat using parameters for an orbit at an altitude of 600 km and inclination angles of 97.8° and 65°. To account for the propagation effects of the radio wave at 14.099 MHz, the IRI-2007 model and the Chapman layer model were used to define the ionosphere. A ray tracing algorithm written in MATLAB was used to simulate the ray paths. To evaluate the results, a documented ray tracing algorithm known as Haselgrove ray tracing was used. The results obtained show that for an orbit at an inclination above 70° and altitude of 600 km, a number of rays actually traverse the ionosphere and reach the receivers during most of the year for a sufficient period of time during every pass. The least refraction is experienced during winter, therefore it is the best time for the calibration of the radar antenna. The results indicate that the objectives of the CubeSat mission should be achieved.
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id oai:open.uct.ac.za:11427/13917
institution University of Cape Town (South Africa)
language eng
last_indexed 2026-06-10T12:33:57.504Z
license_str Not specified — see source repository
provenance_str_mv Harvested via OAI-PMH from UCTD — University of Cape Town Open Access Repository
publishDate 2015
publishDateRange 2015
publishDateSort 2015
publisher Department of Electrical Engineering
publisherStr Department of Electrical Engineering
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source_str UCTD — University of Cape Town Open Access Repository
spelling oai:open.uct.ac.za:11427/13917 Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon Agaba, Doreen Inggs, Michael Cilliers, Pierre Electrical Engineering This dissertation reports on the investigation to determine which orbits, ionospheric conditions and seasons of the year that will facilitate the reception of the high frequency (HF) beacon signal from the 1 U CubeSat ZACUBE 1 by the SuperDARN HF radar in Antarctica, and by the HF direction-finding (DF) systems in both Pretoria and Hermanus. The primary objective of the HF beacon on ZACUBE 1 is to provide a continuous radio signal to calibrate and verify the elevation-resolving algorithm of the SuperDARN HF Radar antenna at SANAE IV in Antarctica. The signal will also be used to characterise the beam pattern of this and other HF radar antennas in the SuperDARN network, and to characterise the ionosphere over the Earth’s polar region. A secondary objective of the HF beacon on the satellite is to measure the ionospheric total electron content (TEC) by using either measurements of the carrier phase delays or of the Faraday rotation of the signal. An orbit analysis was done for the CubeSat using parameters for an orbit at an altitude of 600 km and inclination angles of 97.8° and 65°. To account for the propagation effects of the radio wave at 14.099 MHz, the IRI-2007 model and the Chapman layer model were used to define the ionosphere. A ray tracing algorithm written in MATLAB was used to simulate the ray paths. To evaluate the results, a documented ray tracing algorithm known as Haselgrove ray tracing was used. The results obtained show that for an orbit at an inclination above 70° and altitude of 600 km, a number of rays actually traverse the ionosphere and reach the receivers during most of the year for a sufficient period of time during every pass. The least refraction is experienced during winter, therefore it is the best time for the calibration of the radar antenna. The results indicate that the objectives of the CubeSat mission should be achieved. 2015-09-15T10:02:49Z 2015-09-15T10:02:49Z 2012 Master Thesis Masters MPhil http://hdl.handle.net/11427/13917 eng application/pdf Department of Electrical Engineering Faculty of Engineering and the Built Environment University of Cape Town
spellingShingle Electrical Engineering
Agaba, Doreen
Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
thesis_degree_str Master's
title Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
title_full Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
title_fullStr Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
title_full_unstemmed Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
title_short Calibration of a SuperDARN Radar Antenna by means of a Satellite Beacon
title_sort calibration of a superdarn radar antenna by means of a satellite beacon
topic Electrical Engineering
url http://hdl.handle.net/11427/13917
work_keys_str_mv AT agabadoreen calibrationofasuperdarnradarantennabymeansofasatellitebeacon