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Optimization ofreaction wheel system with regenerative function for spacecraft attitude control

Research Project

Project/Area Number 22560780
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionOsaka Prefecture University (2011-2012)
The University of Electro-Communications (2010)

Principal Investigator

NAGASHIO Tomoyuki  大阪府立大学, 工学(系)研究科(研究院), 准教授 (80334580)

Project Period (FY) 2010 – 2012
Project Status Completed (Fiscal Year 2012)
Budget Amount *help
¥4,420,000 (Direct Cost: ¥3,400,000、Indirect Cost: ¥1,020,000)
Fiscal Year 2012: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2011: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2010: ¥2,600,000 (Direct Cost: ¥2,000,000、Indirect Cost: ¥600,000)
Keywords誘導 / 航法 / 制御 / 姿勢制御 / 最適化 / 回生機構 / リアクションホイール / 宇宙機 / 半正定値計画問題
Research Abstract

This research work has studied saving electric power of spacecraft attitude maneuver mission by using a regenerative function of reaction wheel system. They consist of a modeling method using a discrete time series system, an optimization method using a cost function for the both of attitude angle error and consumption of electric power, and investigation using experimental device. From the results, it has been confirmed that the proposed method is effective compared with general control schemes.

Report

(4 results)
  • 2012 Annual Research Report   Final Research Report ( PDF )
  • 2011 Annual Research Report
  • 2010 Annual Research Report
  • Research Products

    (5 results)

All 2012

All Presentation (5 results)

  • [Presentation] An Optimal Design of H-infinity Static Output Feedback Controller using LMI for Collocated Gyroscopic System2012

    • Author(s)
      Yuki Kurotaki, Tomoyuki Nagashio Takashi Kida
    • Organizer
      Proc. of 51th IEEE Conference on Decision and Control
    • Place of Presentation
      Maui, Hawaii
    • Year and Date
      2012-12-13
    • Related Report
      2012 Final Research Report
  • [Presentation] Model Predictive Control of Spacecraft Attitude with Regenerative Reaction Wheels2012

    • Author(s)
      Ayaka Senoo, Takeya Asakawa, Tomoyuki Nagashio, Takashi Kida
    • Organizer
      International workshop on Modern Science and Technology 2012 PROCEEDINGS
    • Place of Presentation
      Tokyo, Japan
    • Year and Date
      2012-08-31
    • Related Report
      2012 Final Research Report
  • [Presentation] パラメータ依存リアプノフ関数を用いたディスクリプタ方程式によるゲインスケジュール制御系の設計と柔軟宇宙機への適用2012

    • Author(s)
      中山啓, 長塩知之, 木田隆
    • Organizer
      第29回誘導制御シンポジウム資料、宇宙航空研究開発機構
    • Place of Presentation
      筑波宇宙センター
    • Year and Date
      2012-05-18
    • Related Report
      2012 Final Research Report
  • [Presentation] パラメータ依存リアプノフ関数を用いたディスクリプタ方程式によるゲインスケジュール制御系の設計と柔軟宇宙機への適用2012

    • Author(s)
      長塩知之
    • Organizer
      計測自動制御学会第29回誘導制御シンポジウム
    • Place of Presentation
      宇宙航空研究開発機構 筑波宇宙センター
    • Related Report
      2012 Annual Research Report
  • [Presentation] An Optimal Design of H-Infinity Static Output Feedback Controller Using LMI for Collocated Gyroscopic System2012

    • Author(s)
      Tomoyuki Nagashio
    • Organizer
      51th IEEE Conference on Decision and Control
    • Place of Presentation
      Maui, Hawaii
    • Related Report
      2012 Annual Research Report

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Published: 2010-08-23   Modified: 2019-07-29  

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