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  1. 学術雑誌論文
  2. 5 技術(工学)

Design and environmental testing of imaging payload for a 6 U CubeSat at low Earth orbit: KITSUNE mission

http://hdl.handle.net/10228/0002000300
http://hdl.handle.net/10228/0002000300
7305cfc7-68f2-4103-ba1e-cc2cf3570544
名前 / ファイル ライセンス アクション
LaSEINE-2022_020.pdf LaSEINE-2022_020.pdf (2.8 MB)
アイテムタイプ 学術雑誌論文 = Journal Article(1)
公開日 2023-12-01
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 Design and environmental testing of imaging payload for a 6 U CubeSat at low Earth orbit: KITSUNE mission
言語 en
言語
言語 eng
著者 Azami, Muhammad Hasif Bin

× Azami, Muhammad Hasif Bin

en Azami, Muhammad Hasif Bin

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Orger, Necmi Cihan

× Orger, Necmi Cihan

en Orger, Necmi Cihan

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Schulz, Victor Hugo

× Schulz, Victor Hugo

en Schulz, Victor Hugo

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Oshiro, Takashi

× Oshiro, Takashi

en Oshiro, Takashi

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Alarcon, Jose Rodrigo Cordova

× Alarcon, Jose Rodrigo Cordova

en Alarcon, Jose Rodrigo Cordova

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Maskey, Abhas

× Maskey, Abhas

en Maskey, Abhas

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Nakayama, Kazuhiro

× Nakayama, Kazuhiro

en Nakayama, Kazuhiro

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Fukuda, Yoshiya

× Fukuda, Yoshiya

en Fukuda, Yoshiya

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Kojima, Kaname

× Kojima, Kaname

en Kojima, Kaname

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Yamauchi, Takashi

× Yamauchi, Takashi

en Yamauchi, Takashi

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増井, 博一

× 増井, 博一

WEKO 17583
e-Rad 30437793
Scopus著者ID 12792223900
九工大研究者情報 387

ja 増井, 博一

en Masui, Hirokazu


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趙, 孟佑

× 趙, 孟佑

WEKO 754
e-Rad 60243333
Scopus著者ID 7401727758
九工大研究者情報 168

ja 趙, 孟佑

en Cho, Mengu


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抄録
内容記述タイプ Abstract
内容記述 Earth observation (EO) missions remain a challenging task for small satellite platforms due to their demanding requirements and space environment effects. In this study, the camera payload development and mission requirements are presented together with the ground-based testing results for a 6U CubeSat called KITSUNE, operating at low Earth orbit. The major challenge of the payload development is maintaining the focus of the optical system despite the thermal vacuum environment in orbit since the low thermal capacity and rapid temperature variation of CubeSats hinder the camera focus. First, the payload is developed with an objective of a 5-m-class imaging mission, which has a 31.4 MP CMOS sensor and a lens with a 300-mm focal length. Second, polyimide heaters and multilayer insulators are utilized in order to maintain focus during imaging operations. Third, a collimator lens is used to aid in image capture during thermal vacuum tests. These images are analyzed thoroughly using various focus measure operators. The Diagonal Laplacian was found to be the most suitable operator due to the consistency in test results. The results also showed that the heat generated by the camera sensor significantly affects the lens temperature and, ultimately, the target temperature of the lens was defined at −1.8°C. Finally, the test results are discussed, including thermal vacuum, vibration, total ionization dose, and the effect of exposure to direct sunlight on the CMOS sensor.
言語 en
書誌情報 en : Frontiers in Space Technologies

巻 3, 発行日 2022-11-07
出版社
出版者 Frontiers
言語 en
DOI
識別子タイプ DOI
関連識別子 10.3389/frspt.2022.1000219
ISSN
収録物識別子タイプ EISSN
収録物識別子 2673-5075
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
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