4123 The Attitude Control Experiments of "HIT-SAT" and the Future Development Satellite

• MATSUSHIMA Kouta

  Hokkaido University

• ISHIMURA Kosei

  Hokkaido University

• IGARASHI Daigaku

  Hokkaido University

• TOTANI Tsuyoshi

  Hokkaido University

• SAKAKIBARA Takahiro

  Hokkaido University

• SATORI Shin

  Hokkaido Institute of Technology

• MITSUHASHI Ryuichi

  Hokkaido Institute of Technology

• AOYANAGI Yoshihide

  Hokkaido Institute of Technology

• TANAKA Yoshinori

  Hokkaido Institute of Technology

• SATO Tatsuhiro

  Hokkaido Institute of Technology

• NAKAMURA Akihiro

  AIDMA Ltd.

• YASUNAKA Toshihiko

  Uematsu Electric Co. Ltd.

• HORI Koutaro

  B.U.G., Inc.

• HIROTA Norihisa

Bibliographic Information

Other Title

• 4123 HIT-SATの姿勢制御結果と北海道衛星への展開(S74-2 小型宇宙システム(2),S74 小型宇宙システム)

Abstract

"HIT-SAT" is a small satellite to demonstrate performance of the bus systems of "Hokkaido Satellite". The main purpose of the attitude control system of "HIT-SAT" is to get basis data for the attitude control and determination system of "Hokkaido Satellite". "HIT-SAT" was launched on Sep. 23, 2006 by M-V-7. Attitude control system of "HIT-SAT" could get magnetometer data and gyro data on orbit. This paper describes the attitude determination from magnetometer data obtained on orbit.

Journal

• The proceedings of the JSME annual meeting

  The proceedings of the JSME annual meeting 2007.5 (0), 391-392, 2007

  The Japan Society of Mechanical Engineers

Keywords

• CubeSat
• HIT-SAT
• Attitude Determination System
• Attitude Control System

Details

• CRID: 1390001206064330496
• NII Article ID: 110007084996
• DOI: 10.1299/jsmemecjo.2007.5.0_391
• ISSN: 24331325
• Web Site: https://www.jstage.jst.go.jp/article/jsmemecjo/2007.5/0/2007.5_391/_pdf
• Text Lang: ja
• Data Source:
  • JaLC
  • Crossref
  • CiNii Articles
• Abstract License Flag: Disallowed