Coupling among pitch motion, axial vibration, and orbital motion of large space structures

Kosei Ishimura, Ken Higuchi

研究成果: Article査読

16 被引用数 (Scopus)

抄録

The parameter dependency of large space structures on the coupling among attitude motion, structural vibration, and orbital motion has been investigated, particularly for structures such as tethered satellite systems. Tethered satellites are noticed for their possible applications. From space solar power systems to deorbit system, the applications of tethered satellites spread out over various fields. In this paper, we investigate planar motion of a satellite model, which consists of two tip particles and a massless spring. For such a space structure, the characteristics of the planar motion are shown to be determined by the mass ratio of tip particles, the natural frequency ratio of axial vibration to orbital motion, and the axial length ratio of the spring to the orbital radius. Among these three parameters, the natural frequency ratio has the greatest influence on the coupling phenomenon. Furthermore, the parameter range over which the coupling phenomenon occurs is specified.

本文言語English
ページ(範囲)61-71
ページ数11
ジャーナルJournal of Aerospace Engineering
21
2
DOI
出版ステータスPublished - 2008 3 24
外部発表はい

ASJC Scopus subject areas

  • 土木構造工学
  • 材料科学(全般)
  • 航空宇宙工学
  • 機械工学

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