Formation control using differential atmospheric drag considering attitude constraints

Takehiro Yasuda, Mai Bando, Shinji Hokamoto

研究成果: ジャーナルへの寄稿会議記事査読

抄録

In formation flying control of spacecraft, orbital motion and attitude motion are often treated independently. On the other hand, it is necessary to realize the orbit control under the constraint of the attitude, when solar power satellite using the formation flying on the earth orbit is examined. Also, when perturbation forces such as atmospheric drag and solar radiation pressure are positively used for orbit control, the influence of attitude constraints is significant. In this paper, we describe the control method using atmospheric resistance with the earth orbit as a model, and consider the formation control under the constraint of attitude.

本文言語英語
ジャーナルProceedings of the International Astronautical Congress, IAC
2020-October
出版ステータス出版済み - 2020
イベント71st International Astronautical Congress, IAC 2020 - Virtual, Online
継続期間: 10月 12 202010月 14 2020

!!!All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 天文学と天体物理学
  • 宇宙惑星科学

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