An orbit determination from debris impacts on measurement satellites

Koki Fujita, Mitsuhiko Tasaki, Masahiro Furumoto, Toshiya Hanada

研究成果: ジャーナルへの寄稿記事

7 引用 (Scopus)

抜粋

This work proposes a method to determine orbital plane of a micron-sized space debris cloud utilizing their impacts on measurement satellites. Given that debris impacts occur on a line of intersection between debris and satellites orbital planes, a couple of debris orbital parameters, right ascension of the ascending node, inclination, and nodal regression rate can be determined by impact times and locations measured from more than two satellites in different earth orbits. This paper proves that unique solution for the debris orbital parameters is obtained from the measurement data, and derives a computational scheme to estimate them. The effectiveness of the proposed scheme is finally demonstrated by a simulation test, in which measurement data are obtained from a numerical simulation considering realistic debris' and satellites' orbits.

元の言語英語
ページ(範囲)620-626
ページ数7
ジャーナルAdvances in Space Research
57
発行部数2
DOI
出版物ステータス出版済み - 1 15 2016

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Geophysics
  • Atmospheric Science
  • Space and Planetary Science
  • Earth and Planetary Sciences(all)

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