Satellite Attitude Control and Power Tracking with VSCMGs during Large-angle and Agile Attitude Maneuvers

Hiroyuki Yoshihara, Masaki Takahashi

研究成果: Conference contribution

抄録

In recent years, the use of VSCMG/IPACS for satellites has been considered, because Earth observation satellites are required to have agility and miniaturization. However, in previous research, the control laws of VSCMG/IPACS at large-angle and agile attitude maneuvers have not been studied. In this study, we clarify that it is impossible for conventional methods to achieve large-angle and agile attitude maneuvers, while accurately tracking power. Therefore, we propose a system capable of simultaneous satellite attitude control and power tracking with VSCMG during large-angle and agile attitude maneuvers. The proposed steering law switches the steering laws according to singularities, and enables the satellite to change attitude quickly without power errors. In addition, numerical simulations demonstrate through comparison that the proposed steering law is more useful than conventional steering laws.

本文言語English
ホスト出版物のタイトル2019 12th Asian Control Conference, ASCC 2019
出版社Institute of Electrical and Electronics Engineers Inc.
ページ1613-1618
ページ数6
ISBN(電子版)9784888983006
出版ステータスPublished - 2019 6月
イベント12th Asian Control Conference, ASCC 2019 - Kitakyushu-shi, Japan
継続期間: 2019 6月 92019 6月 12

出版物シリーズ

名前2019 12th Asian Control Conference, ASCC 2019

Conference

Conference12th Asian Control Conference, ASCC 2019
国/地域Japan
CityKitakyushu-shi
Period19/6/919/6/12

ASJC Scopus subject areas

  • コンピュータ サイエンスの応用
  • 制御と最適化
  • 機械工学

フィンガープリント

「Satellite Attitude Control and Power Tracking with VSCMGs during Large-angle and Agile Attitude Maneuvers」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル