Considerations on control for a tethered satellite system through angular momentum conservation

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

1 被引用数 (Scopus)

抄録

This study deals with orbital transfer of a tethered satellite system (TSS) on orbit. Dynamics of TSS is restricted to the angular momentum conservation law of the system around a planet. This constraint is not integrable (, that is called "nonholonomic constraint"), and the final state of TSS depends on a time history of the input. While previous works for orbital transfer mainly investigated dynamics of the system for specified time profiles of the tether-length, this study aims to make tether extension profiles to achieve some specified orbit. This paper, as a preliminary study, gives a brief overview of the previous works and investigates the fundamental property of the constraint based on the angular momentum conservation. Integrability and accessibility /controllability are analyzed and also numerically verified. For simplicity, TSS is modeled to a dumbbell-type satellite in this study.

本文言語英語
ホスト出版物のタイトルInternational Astronautical Federation - 55th International Astronautical Congress 2004
ページ751-756
ページ数6
2
出版ステータス出版済み - 2004
イベントInternational Astronautical Federation - 55th International Astronautical Congress 2004 - Vancouver, カナダ
継続期間: 10 4 200410 8 2004

その他

その他International Astronautical Federation - 55th International Astronautical Congress 2004
国/地域カナダ
CityVancouver
Period10/4/0410/8/04

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 宇宙惑星科学

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