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24.4 A 6.5Gb/s Shared bus using electromagnetic connectors for downsizing and lightening satellite processor system by 60%

https://jaxa.repo.nii.ac.jp/records/39546
https://jaxa.repo.nii.ac.jp/records/39546
d22d3eb9-edcf-44f0-85bf-2189b75e30d6
Item type 会議発表論文 / Conference Paper(1)
公開日 2015-08-28
タイトル
タイトル 24.4 A 6.5Gb/s Shared bus using electromagnetic connectors for downsizing and lightening satellite processor system by 60%
言語 en
言語
言語 eng
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
アクセス権
アクセス権 metadata only access
アクセス権URI http://purl.org/coar/access_right/c_14cb
著者 Kosuge, Atsutake

× Kosuge, Atsutake

en Kosuge, Atsutake

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Ishizuka, Shu

× Ishizuka, Shu

en Ishizuka, Shu

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Abe, Mami

× Abe, Mami

en Abe, Mami

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Ichikawa, Satoshi

× Ichikawa, Satoshi

en Ichikawa, Satoshi

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Kuroda, Tadahiro

× Kuroda, Tadahiro

en Kuroda, Tadahiro

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著者所属(英)
en
Keio University
著者所属(英)
en
Keio University
著者所属(英)
en
Japan Aerospace Exploration Agency (JAXA)
著者所属(英)
en
Japan Aerospace Exploration Agency (JAXA)
著者所属(英)
en
Keio University
出版者(英)
出版者 Institute of Electrical and Electronics Engineers, Inc.(IEEE)
書誌情報 en : Solid- State Circuits Conference - (ISSCC), 2015 IEEE International

p. 1-3, 発行日 2015-02
会議概要(会議名, 開催地, 会期, 主催者等)(英)
内容記述タイプ Other
内容記述 Solid- State Circuits Conference - (ISSCC), 2015 IEEE International (February 22-26, 2015.), San Francisco, CA, USA
抄録(英)
内容記述タイプ Other
内容記述 Processor systems that are mounted in satellites must be small and light, having high data transfer rates, and high storage capacity [1]. A small reduction in size and weight could reduce the cost of launching a satellite by a significant amount. The next generation of earth observation satellites will require data transmission rates to a maximum of 20Gb/s and at least one terabyte of storage capacity. The volume, weight, and communication speed of the processor system is determined by the backplane connectors (Fig. 20.4.1). It is difficult to achieve a connector that can pass signals of 2.5Gb/s or more. The signal reflection that occurs when signals are branched at connectors and at the wire stubs of branches decreases the transmission speed, so only point-to-point connections are possible. Once the satellite is launched, repair or replacement is not possible, and system redundancy is introduced. Accordingly, 512 backplane wires would be required. The signal connector would require 1,024pins, including the ground pins used to prevent crosstalk, and would be 512mm wide, which is even wider than the circuit board of each module.
ISBN
識別子タイプ ISBN
関連識別子 978-1-4799-6223-5
DOI
識別子タイプ DOI
関連識別子 http://dx.doi.org/10.1109/ISSCC.2015.7063112
関連名称 info:doi/10.1109/ISSCC.2015.7063112
資料番号
内容記述タイプ Other
内容記述 資料番号: PA1510077000
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