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

6 引用 (Scopus)

抄録

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

Fingerprint

orbit determination
debris
Debris
Orbits
Satellites
orbitals
space debris
Space debris
satellite orbits
Earth orbits
simulation
intersections
inclination
regression analysis
Earth (planet)
Computer simulation
estimates
parameter

All Science Journal Classification (ASJC) codes

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

これを引用

An orbit determination from debris impacts on measurement satellites. / Fujita, Koki; Tasaki, Mitsuhiko; Furumoto, Masahiro; Hanada, Toshiya.

:: Advances in Space Research, 巻 57, 番号 2, 15.01.2016, p. 620-626.

研究成果: ジャーナルへの寄稿記事

Fujita, Koki ; Tasaki, Mitsuhiko ; Furumoto, Masahiro ; Hanada, Toshiya. / An orbit determination from debris impacts on measurement satellites. :: Advances in Space Research. 2016 ; 巻 57, 番号 2. pp. 620-626.
@article{4bf08a3611474f39b4c55a083e68b828,
title = "An orbit determination from debris impacts on measurement satellites",
abstract = "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.",
author = "Koki Fujita and Mitsuhiko Tasaki and Masahiro Furumoto and Toshiya Hanada",
year = "2016",
month = "1",
day = "15",
doi = "10.1016/j.asr.2015.11.005",
language = "English",
volume = "57",
pages = "620--626",
journal = "Advances in Space Research",
issn = "0273-1177",
publisher = "Elsevier Limited",
number = "2",

}

TY - JOUR

T1 - An orbit determination from debris impacts on measurement satellites

AU - Fujita, Koki

AU - Tasaki, Mitsuhiko

AU - Furumoto, Masahiro

AU - Hanada, Toshiya

PY - 2016/1/15

Y1 - 2016/1/15

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=84954078685&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84954078685&partnerID=8YFLogxK

U2 - 10.1016/j.asr.2015.11.005

DO - 10.1016/j.asr.2015.11.005

M3 - Article

AN - SCOPUS:84954078685

VL - 57

SP - 620

EP - 626

JO - Advances in Space Research

JF - Advances in Space Research

SN - 0273-1177

IS - 2

ER -