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  1. 学会・会議発表論文
  2. 学会・会議発表論文

Control System Design of an Ultra-Small Deep Space Probe

http://hdl.handle.net/10228/00007256
http://hdl.handle.net/10228/00007256
4c4cc904-1659-4719-ae3e-5e72dcede794
名前 / ファイル ライセンス アクション
LaSEINE-2016_05.pdf LaSEINE-2016_05.pdf (1.8 MB)
Item type 会議発表論文 = Conference Paper(1)
公開日 2019-06-28
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_5794
資源タイプ conference paper
タイトル
タイトル Control System Design of an Ultra-Small Deep Space Probe
言語
言語 eng
著者 Bendoukhaa, Sidi Ahmed

× Bendoukhaa, Sidi Ahmed

WEKO 24774

Bendoukhaa, Sidi Ahmed

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Okuyama, Kei-ichi

× Okuyama, Kei-ichi

WEKO 24775

Okuyama, Kei-ichi

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Biancaa, Szasz

× Biancaa, Szasz

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Biancaa, Szasz

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Nishio, Masanori

× Nishio, Masanori

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Nishio, Masanori

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抄録
内容記述タイプ Abstract
内容記述 It's a grand opportunity to build new small deep space probe called Shinen2, developed by Kyushu Institute of Technology (KIT), in corporation with the different companies and institutions of engineering in Kagoshima University (Japan), NASA Johnson Space Center, was launched by the rocket H-IIA of Japan Aerospace Exploration Agency (JAXA) with Hayabusa 2, on December 3, 2014 in Tanegashima. This project involves Japanese students and foreigners, permitted a multi-cultural environment and an excellent tools for education. The students are in charge for the design, assembly, integration, tests of the space probe subsystems, and build-up of the existing ground stations facilities for tracking the telemetry data of Shinen2. It will enhance capacity building for the students, and scientific research for upcoming studies. The main approach to carry out the main mission of space probe. In parallel, to develop each subsystem of Shinen2: structure design, system bus architecture including the Communication Control Unit CCU, Power Control Unit PCU specifications, and new Particle Pixel Detector PPD for deep space radiation exploration. The development period for the space probe was only one year; it was extremely a short term. The mass budget and size were strictly limited while requiring a higher reliability. This paper describe a control system design for a small deep space probe which was developed to implement different missions and to satisfy the various requirements listed below.
備考
内容記述タイプ Other
内容記述 3rd International Conference on Power and Energy Systems Engineering, CPESE 2016, 8-12, September 2016, Kitakyushu, Japan
書誌情報 Energy Procedia

巻 100, p. 537-550, 発行日 2016-09
出版社
出版社 Elsevier
DOI
関連タイプ isIdenticalTo
識別子タイプ DOI
関連識別子 https://doi.org/10.1016/j.egypro.2016.10.216
ISSN
収録物識別子タイプ ISSN
収録物識別子 1876-6102
著作権関連情報
権利情報 Copyright (c) 2016 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
キーワード
主題Scheme Other
主題 Shinen2 project
キーワード
主題Scheme Other
主題 deep space probe
キーワード
主題Scheme Other
主題 system control unit
キーワード
主題Scheme Other
主題 sensor radiation
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
値 7710
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