Perturbation in orbital elements of a high elliptical orbit of satellite constellations

Osama Mostafa, Koki Fujita, Toshiya Hanada

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

抄録

This work aim to study the effects of various perturbations on the motion of satellites constellation in high elliptical inclined orbit in order to make continuous coverage. A computational model developed at Space Systems Dynamics Laboratory, Kyushu University to study the effect of these perturbations on Molniya and Tundra satellite constellations for various periods one, five and 10 years. The equations of motion under effect of these perturbations forces are solved numerically using Gaussian equations. The results show that the satellites constellation in Molniya orbit have stability under effect of gravity of third body more than Tundra orbit in order to make a continuous coverage.

本文言語英語
ホスト出版物のタイトルSpaceflight Mechanics 2017
編集者Jon A. Sims, Frederick A. Leve, Jay W. McMahon, Yanping Guo
出版社Univelt Inc.
ページ1733-1745
ページ数13
ISBN(印刷版)9780877036371
出版ステータス出版済み - 1 1 2017
イベント27th AAS/AIAA Space Flight Mechanics Meeting, 2017 - San Antonio, 米国
継続期間: 2 5 20172 9 2017

出版物シリーズ

名前Advances in the Astronautical Sciences
160
ISSN(印刷版)0065-3438

その他

その他27th AAS/AIAA Space Flight Mechanics Meeting, 2017
Country米国
CitySan Antonio
Period2/5/172/9/17

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

フィンガープリント 「Perturbation in orbital elements of a high elliptical orbit of satellite constellations」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル