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Study on 3D Attitude Control in Space

Research Project

Project/Area Number 04555053
Research Category

Grant-in-Aid for Developmental Scientific Research (B)

Allocation TypeSingle-year Grants
Research Field 機械力学・制御工学
Research InstitutionThe University of Tokyo

Principal Investigator

MIURA Hirofumi  The University of Tokyo. Engineering, Professor, 工学部, 教授 (50010682)

Co-Investigator(Kenkyū-buntansha) 小松 督  (株)東芝, 小向工場, 研究主務
IIKURA Shouishi  Toshiba Corporation. Center for R & D, Chief Researcher, 研究開発センター, 主任研究員
SHIMOYAMA Isao  The University of Tokyo. Engineering, Associate Professor, 工学部, 助教授 (60154332)
TADASHI Komatsu  Toshiba Corporation. Komukai, Researcher
Project Period (FY) 1992 – 1993
Project Status Completed (Fiscal Year 1993)
Budget Amount *help
¥11,400,000 (Direct Cost: ¥11,400,000)
Fiscal Year 1993: ¥3,300,000 (Direct Cost: ¥3,300,000)
Fiscal Year 1992: ¥8,100,000 (Direct Cost: ¥8,100,000)
KeywordsSpace Craft / Space Robot / CMG / Reaction Wheel / Attitude Control
Research Abstract

This research is the study on attitude control of the space craft(including space robot, artificial satelite, etc.). In 1992, the experimental apparatus for simulating microgravity and suporting a body freely in 6 degress of freedom was designed and constructed. In 1993, the cotrol technology of microgravity simulator in the vertical direction was mainly studied.
As it is very difficult to simulate the micro gravity in the vertical direction, the experiment of the motion of a body in the microgravity is done in 2D space. That mean, a body is supported freely in the horizontal plane, using air bearing, for instance.
The purpose of this research is to develop the experimental apparatus which can support a body freely in the vertical direction, too. In 1992, the counter weight was used to cancel the weight of a body. In 1993, as mentioned above, a controlled system was constructed to cancel the weight of a body. The acceleration is measured by a loadcell and that information is fed back to the system to keep the acceleration of the ceter of gravity zero.
For the horizontal direction, the usual air floated system is used. For the attitude, gimbals supporting mechanism is used.
In this research, the new idea for controlling the attitude of a body in the space is introduced.
The space craft is devided into the multi bodies system. Each body is connected to the next body by universal joint including an actuator which can yield the internal force. By the relative motion of bodies, the attitude of the total system can be controlled. The experimental results on three bodies system shows availability of this idea.

Report

(3 results)
  • 1993 Annual Research Report   Final Research Report Summary
  • 1992 Annual Research Report
  • Research Products

    (12 results)

All Other

All Publications (12 results)

  • [Publications] 安田進: "分割された機体の相対運動による宇宙機の姿勢制御" 東京大学工学部修士論文(指導教官 三浦宏文). (1993)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] 吉田隆雄 ほか: "宇宙ロボットの研究" 東京大学工学部卒業論文(指導教官 三浦宏文・下山勲). (1993)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] 安田進 ほか: "分割された機体の相対運動による宇宙機の姿勢制御" 第10回日本ロボット学会学術講演会予稿集. 497-498 (1992)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] Susumu Yasuda: "The attitude control of the space craft by the relative motion of devided bodies" Master thesis(The university of Tokyo). (1993)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] Takao Yoshida: "Study on space robot" Graduation thesis(The univ.of Tokyo). (1993)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] Susumu Yasuda: "The attitude control of the space craft by the relative motion of devided bodies" Proceedings of Robitcs Society of Japan(10th annual meeting). 497-498 (1992)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1993 Final Research Report Summary
  • [Publications] 安田進: "分割された機体の相対運動による宇宙機の姿勢制御" 東京大学工学部修士論文(指導教官 三浦宏文). (1993)

    • Related Report
      1993 Annual Research Report
  • [Publications] 吉田隆雄,飯塚喜軌: "宇宙ロボットの研究" 東京大学卒業論文(指導教官 三浦宏文・下山勲). (1993)

    • Related Report
      1993 Annual Research Report
  • [Publications] 安田進・下山勲・三浦宏文: "分割された機体の相対運動による宇宙機の姿勢制御" 第10回日本ロボット学会学術講演会予稿集. 497-498 (1992)

    • Related Report
      1993 Annual Research Report
  • [Publications] 安田 進,下山 勲,三浦 宏文: "分割された機体の相対運動による宇宙機の姿勢制御" 第10回日本ロボット学会学術講演会予稿集. 63-64 (1992)

    • Related Report
      1992 Annual Research Report
  • [Publications] 荒居 健,内牧 信三,下山 勲,三浦 宏文: "宇宙浮遊のマニピュレータの制御の研究" 日本機械学会ロボティクス・メカトロニクス講演会講演論文集. 687-688 (1992)

    • Related Report
      1992 Annual Research Report
  • [Publications] Susumu Yasuda,Isao Shimoyama,Hirofumi Miura: "Attitude Control of a Spacecraft by Relative Motion of Divided Bodies" 1992 ISAS 2nd Workshop on Astrodynamics and Flight Mechanics. 171-174 (1992)

    • Related Report
      1992 Annual Research Report

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Published: 1992-04-01   Modified: 2016-04-21  

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