Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission

A compact UHF antenna has been presented in this paper for nanosatellite space mission. A square ground plane with slotted rectangular radiating element have been used. Coaxial probe feeding is used to excite. The rectangular slot of the radiating patch is responsible for resonating at lower UHF ban...

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Main Authors: Rahmatillah, Rahmi, Aheieva, Kateryna, Lap, Chow Chee, Cho, Mengu, Touhidul Alam, Mohammad Tariqul Islam, Md. Amanath Ullah
Other Authors: Maktoomi, Mohammad
Format: Article
Language:English
Published: 2018
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Online Access:https://hdl.handle.net/10356/89721
http://hdl.handle.net/10220/47131
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-897212020-03-07T13:57:26Z Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission Rahmatillah, Rahmi Aheieva, Kateryna Lap, Chow Chee Cho, Mengu Touhidul Alam Mohammad Tariqul Islam Md. Amanath Ullah Maktoomi, Mohammad School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering UHF Antenna Nanosatellite Space A compact UHF antenna has been presented in this paper for nanosatellite space mission. A square ground plane with slotted rectangular radiating element have been used. Coaxial probe feeding is used to excite. The rectangular slot of the radiating patch is responsible for resonating at lower UHF bands. One of the square faces of the nanosatellite structure works as the ground plane for the slotted radiating element. The fabricated prototype of the proposed antenna has achieved an impedance bandwidth (S11< -10dB) of 7.0 MHz (398 MHz– 405 MHz) with small size of 97 mm× 90 mm radiating element. The overall ground plane size is 100 mm × 100 mm × 0.5 mm. The proposed antenna has achieved a gain of 1.18 dB with total efficiency of 62.5%. The proposed antenna addresses two design challenges of nanosatellite antenna, (a) assurance of the placement of solar panel beneath the radiating element; (b) providing about 50% open space for solar irradiance to pass onto the solar panel, enabling the solar panel to achieve up to 93.95% of power under of normal conditions. MOE (Min. of Education, S’pore) Published version 2018-12-20T07:40:07Z 2019-12-06T17:31:57Z 2018-12-20T07:40:07Z 2019-12-06T17:31:57Z 2018 Journal Article Touhidul Alam., Mohammad Tariqul Islam., Md. Amanath Ullah., Rahmatillah, R., Aheieva, K., Lap, C. C., & Cho, M. (2018). Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission. PLOS ONE, 13(11), e0205587-. doi: 10.1371/journal.pone.0205587 https://hdl.handle.net/10356/89721 http://hdl.handle.net/10220/47131 10.1371/journal.pone.0205587 en PLOS ONE © 2018 Alam et al. This is an open access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited. 14 p. application/pdf
institution Nanyang Technological University
building NTU Library
country Singapore
collection DR-NTU
language English
topic DRNTU::Engineering::Electrical and electronic engineering
UHF Antenna
Nanosatellite Space
spellingShingle DRNTU::Engineering::Electrical and electronic engineering
UHF Antenna
Nanosatellite Space
Rahmatillah, Rahmi
Aheieva, Kateryna
Lap, Chow Chee
Cho, Mengu
Touhidul Alam
Mohammad Tariqul Islam
Md. Amanath Ullah
Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
description A compact UHF antenna has been presented in this paper for nanosatellite space mission. A square ground plane with slotted rectangular radiating element have been used. Coaxial probe feeding is used to excite. The rectangular slot of the radiating patch is responsible for resonating at lower UHF bands. One of the square faces of the nanosatellite structure works as the ground plane for the slotted radiating element. The fabricated prototype of the proposed antenna has achieved an impedance bandwidth (S11< -10dB) of 7.0 MHz (398 MHz– 405 MHz) with small size of 97 mm× 90 mm radiating element. The overall ground plane size is 100 mm × 100 mm × 0.5 mm. The proposed antenna has achieved a gain of 1.18 dB with total efficiency of 62.5%. The proposed antenna addresses two design challenges of nanosatellite antenna, (a) assurance of the placement of solar panel beneath the radiating element; (b) providing about 50% open space for solar irradiance to pass onto the solar panel, enabling the solar panel to achieve up to 93.95% of power under of normal conditions.
author2 Maktoomi, Mohammad
author_facet Maktoomi, Mohammad
Rahmatillah, Rahmi
Aheieva, Kateryna
Lap, Chow Chee
Cho, Mengu
Touhidul Alam
Mohammad Tariqul Islam
Md. Amanath Ullah
format Article
author Rahmatillah, Rahmi
Aheieva, Kateryna
Lap, Chow Chee
Cho, Mengu
Touhidul Alam
Mohammad Tariqul Islam
Md. Amanath Ullah
author_sort Rahmatillah, Rahmi
title Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
title_short Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
title_full Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
title_fullStr Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
title_full_unstemmed Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission
title_sort design and compatibility analysis of a solar panel integrated uhf antenna for nanosatellite space mission
publishDate 2018
url https://hdl.handle.net/10356/89721
http://hdl.handle.net/10220/47131
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