Quasi-satellite orbit transfers via multi-revolutional periodic orbits

Kento Ichinomiya, Nicola Baresi, Yasuhiro Kawakatsu, Tomohiro Yanao

研究成果: Conference contribution

3 被引用数 (Scopus)

抄録

This paper explores the application of multi-revolutional periodic orbits to transfer between single-revolutional quasi-satellite orbits around the Martian moon Phobos. Multi-revolutional periodic orbits are retrograde trajectories that repeat after multiple revolutions around Phobos. At first, we generate them by conventional predictor-corrector scheme and bifurcation analysis and find many candidate options for trajectory design analyses. Next, we explore transfer solutions between different single-revolutional periodic quasi-satellite orbits. We find that, if we choose appropriate multi-revolutional periodic orbits, we can reduce the transfer time and ΔV, as well as increase the robustness of the transfers from a contingency analysis standpoint.

本文言語English
ホスト出版物のタイトルSpaceflight Mechanics 2019
編集者Francesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
出版社Univelt Inc.
ページ713-732
ページ数20
ISBN(印刷版)9780877036593
出版ステータスPublished - 2019 1 1
イベント29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, United States
継続期間: 2019 1 132019 1 17

出版物シリーズ

名前Advances in the Astronautical Sciences
168
ISSN(印刷版)0065-3438

Conference

Conference29th AAS/AIAA Space Flight Mechanics Meeting, 2019
国/地域United States
CityMaui
Period19/1/1319/1/17

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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