Optimization ofreaction wheel system with regenerative function for spacecraft attitude control

• Project/Area Number: 22560780
• Research Category: Grant-in-Aid for Scientific Research (C)
• Allocation Type: Single-year Grants
• Section: 一般
• Research Field: Aerospace engineering
• Research Institution: Osaka 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: ¥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.

Research Products

• [Presentation] An Optimal Design of H-infinity Static Output Feedback Controller using LMI for Collocated Gyroscopic System (2012)
  • 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
• [Presentation] Model Predictive Control of Spacecraft Attitude with Regenerative Reaction Wheels (2012)
  • 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
• [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
• [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
• [Presentation] An Optimal Design of H-Infinity Static Output Feedback Controller Using LMI for Collocated Gyroscopic System (2012)
  • Author(s): Tomoyuki Nagashio
  • Organizer: 51th IEEE Conference on Decision and Control
  • Place of Presentation: Maui, Hawaii