Survey on Harness Design for CubeSats: Understanding the Constraints of CubeSats Design and Toward an Optical Wireless Bus for CubeSats

DOI
  • Tokumitsu Masahiro
    Division of Computer Science and Engineering, Department of Integrated Engineering, National Institute of Technology
  • Tsuji Masatoshi
    Department of Electrical and Computer Engineering, National Institute of Technology
  • Nakaya Jun
    Department of Electronic Robot Engineering, Faculty of Engineering, Aichi University of Technology

説明

CubeSats of nanosatellites have attracted the attention of space scientists and engineers seeking to observe the space environment and develop innovative technologies in space engineering. The CubeSat is a class of miniaturized satellites with a form factor based on a 10 cm cube. However, the dimensional constraints of CubeSats restrict the embedding of relatively large mission devices, such as attitude control systems, into the satellites. Moreover, the harness used to transfer the data and supply power to the mission devices also occupies physical space to embed the mission devices. Therefore, this research surveys earlier studies on nanosatellite harness design. In addition, we consider the possibility of an optical wireless harness for the satellite bus system to achieve a more effective and reliable design for the CubeSats.

収録刊行物

キーワード

詳細情報 詳細情報について

  • CRID
    1390015333257566848
  • DOI
    10.5954/icarob.2023.gs7-3
  • ISSN
    21887829
  • 本文言語コード
    en
  • データソース種別
    • JaLC
    • Crossref
    • OpenAIRE
  • 抄録ライセンスフラグ
    使用不可

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