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A Solar Panel-Integrated Modified Planner Inverted F Antenna for Low Earth Orbit Remote Sensing Nanosatellite Communication System
http://hdl.handle.net/10228/00007283
http://hdl.handle.net/10228/0000728346c75431-d19f-455c-8730-921f3ad1b722
名前 / ファイル | ライセンス | アクション |
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LaSEINE-2018_07.pdf (6.9 MB)
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Item type | 学術雑誌論文 = Journal Article(1) | |||||||||||
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公開日 | 2019-07-05 | |||||||||||
資源タイプ | ||||||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||||||
資源タイプ | journal article | |||||||||||
タイトル | ||||||||||||
タイトル | A Solar Panel-Integrated Modified Planner Inverted F Antenna for Low Earth Orbit Remote Sensing Nanosatellite Communication System | |||||||||||
言語 | ||||||||||||
言語 | eng | |||||||||||
著者 |
Alam, Touhidul
× Alam, Touhidul× Islam, Mohammad Tariqul× Ullah, Md. Amanath× 趙, 孟佑
WEKO
754
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抄録 | ||||||||||||
内容記述タイプ | Abstract | |||||||||||
内容記述 | One of the most efficient methods to observe the impact of geographical, environmental, and geological changes is remote sensing. Nowadays, nanosatellites are being used to observe climate change using remote sensing technology. Communication between a remote sensing nanosatellite and Earth significantly depends upon antenna systems. Body-mounted solar panels are the main source of satellite operating power unless deployable solar panels are used. Lower ultra-high frequency (UHF) nanosatellite antenna design is a crucial challenge due to the physical size constraint and the need for solar panel integration. Moreover, nanosatellite space missions are vulnerable because of antenna and solar panel deployment complexity. This paper proposes a solar panel-integrated modified planner inverted F antenna (PIFA) to mitigate these crucial limitations. The antenna consists of a slotted rectangular radiating patch with coaxial probe feeding and a rectangular ground plane. The proposed antenna has achieved a −10 dB impedance bandwidth of 6.0 MHz (447.5 MHz–453.5 MHz) with a small-sized (80 mm× 90 mm× 0.5 mm) radiating element. In addition, the antenna achieved a maximum realized gain of 0.6 dB and a total efficiency of 67.45% with the nanosatellite structure and a solar panel. The challenges addressed by the proposed antenna are to ensure solar panel placement between the radiating element and the ground plane, and provide approximately 55% open space to allow solar irradiance into the solar panel. | |||||||||||
書誌情報 |
Sensors 巻 18, 号 8, p. 2480-1-2480-11, 発行日 2018-07-31 |
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出版社 | ||||||||||||
出版者 | MDPI | |||||||||||
DOI | ||||||||||||
関連タイプ | isIdenticalTo | |||||||||||
識別子タイプ | DOI | |||||||||||
関連識別子 | https://doi.org/10.3390/s18082480 | |||||||||||
日本十進分類法 | ||||||||||||
主題Scheme | NDC | |||||||||||
主題 | 547 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | ISSN | |||||||||||
収録物識別子 | 1424-8220 | |||||||||||
著作権関連情報 | ||||||||||||
権利情報 | Copyright (c) 2018 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | remote sensing CubeSat | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | deployment free | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | nanosatellite | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | modified PIFA | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | UHF antenna | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | UHF communication | |||||||||||
出版タイプ | ||||||||||||
出版タイプ | VoR | |||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||
査読の有無 | ||||||||||||
値 | yes | |||||||||||
連携ID | ||||||||||||
7801 |