Quaternion based attitude stabilization in the circular restricted three-body problem

Yuki Akiyama, Mai Bando, Shinji Hokamoto

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

This paper presents a novel method to realize station-keeping and control attitude motion simultaneously on a libration point orbit based on the nonlinear output regulation. First, the coupled orbit-attitude motion of a rigid spacecraft subject to three-body dynamics is formulated using the quaternion. Next, the reference orbit and attitude are represented as the output of an autonomous system called exosystem, assuming the reference orbit and attitude are given by a truncated Fourier series. Then the controller is derived by solving the output regulation problem. The derived controller has the explicit form and can achieve the asymptotically tracking for any reference orbit and attitude represented in the Fourier series. The proposed controllers are applied and verified for the Sun-pointing attitude control and station-keeping along Sun-Earth L2 Halo orbits.

本文言語英語
ホスト出版物のタイトル68th International Astronautical Congress, IAC 2017
ホスト出版物のサブタイトルUnlocking Imagination, Fostering Innovation and Strengthening Security
出版社International Astronautical Federation, IAF
ページ750-762
ページ数13
ISBN(印刷版)9781510855373
出版ステータス出版済み - 2017
イベント68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017 - Adelaide, オーストラリア
継続期間: 9 25 20179 29 2017

出版物シリーズ

名前Proceedings of the International Astronautical Congress, IAC
2
ISSN(印刷版)0074-1795

その他

その他68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017
国/地域オーストラリア
CityAdelaide
Period9/25/179/29/17

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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