Stability analysis and sun-tracking attitude control of spacecraft under solar radiation pressure

Naohiro Hayashi, Go Ono, Yuya Mimasu, Jun'Ichiro Kawaguchi

研究成果: Conference contribution

抄録

In an interplanetary mission, the influence of solar radiation pressure (SRP) is a dominant disturbance in terms of the attitude control of a spacecraft, and a continuous disturbance may shorten a mission life time. On the other hand, it was observed that a spin axis of a spinning spacecraft under the SRP tracks the Sun direction, and this is called an attitude drift motion The objective of this study is to analyze the stability of a spin motion and an attitude drift motion of a spacecraft generally and quantitatively. This stability analysis enables Sun-tracking attitude control by using the attitude drift motion only with spin rate control.

本文言語English
ホスト出版物のタイトルAstrodynamics 2013 - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the AAS/AIAA Astrodynamics Specialist Conference
出版社Univelt Inc.
ページ2045-2055
ページ数11
ISBN(印刷版)9780877036050
出版ステータスPublished - 2014
外部発表はい
イベント2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013 - Hilton Head Island, SC, United States
継続期間: 2013 8 112013 8 15

出版物シリーズ

名前Advances in the Astronautical Sciences
150
ISSN(印刷版)0065-3438

Conference

Conference2013 AAS/AIAA Astrodynamics Specialist Conference, Astrodynamics 2013
国/地域United States
CityHilton Head Island, SC
Period13/8/1113/8/15

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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