Orbital Transfer of a Tethered Satellite System by Feedback Control

DOI
  • KOGA Shohei
    九州大学大学院　工学府　航空宇宙工学専攻
  • HOKAMOTO Shinji
    九州大学大学院　工学府　航空宇宙工学専攻

Bibliographic Information

Other Title
  • テザー衛星の軌道変更問題に対するフィードバック制御の検討

Description

This study deals with orbital transfer of a Tethered Satellite System (TSS) into the desired orbit by changing the tether length and cutting the tether. In coplanar motion of a TSS, its pitch angle, pitch angular rate, and tether length should be simultaneously controlled at specified position on orbit, for the desired orbital transfer. In this study, the state equation is described as non-holonomic system with drift term and time-varying coefficient. This paper proposes a feedback control law for the system, and discusses its effectiveness through numerical simulations.

Journal

Keywords

Details 詳細情報について

  • CRID
    1390001205645109120
  • NII Article ID
    130004600199
  • DOI
    10.11511/jacc.50.0.105.0
  • Text Lang
    ja
  • Data Source
    • JaLC
    • CiNii Articles
  • Abstract License Flag
    Disallowed

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