Low energy escape using tube dynamics associated with quasi-halo orbit

Kazutoshi Takemura, Nicola Baresi, Yasuhiro Kawakatsu, Hiroaki Yoshimura

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Analysis of tube dynamics under two dimensions has been analyzed by Koon et al.2 However, analysis in three dimensions has not been done sufficiently. In this work, we discuss on designing Mars escape trajectory in the three-body system via invariant manifolds. In contrast with the conventional methods, we propose to use invariant manifolds from quasi-periodic invariant tori and investigate quasi-halo orbits and their associated tubes. Finally, we show how the invariant manifolds of quasi-periodic orbits can provide new escape trajectories from the Martian system in the circular restricted three-body problem.

Original languageEnglish
Title of host publicationSpaceflight Mechanics 2019
EditorsFrancesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
PublisherUnivelt Inc.
Pages701-711
Number of pages11
ISBN (Print)9780877036593
Publication statusPublished - 2019 Jan 1
Event29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, United States
Duration: 2019 Jan 132019 Jan 17

Publication series

NameAdvances in the Astronautical Sciences
Volume168
ISSN (Print)0065-3438

Conference

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

Fingerprint

escape
halos
Orbits
trajectory
Trajectories
tubes
orbits
trajectories
energy
Mars
three body problem
mars
analysis
method

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Takemura, K., Baresi, N., Kawakatsu, Y., & Yoshimura, H. (2019). Low energy escape using tube dynamics associated with quasi-halo orbit. In F. Topputo, A. J. Sinclair, M. P. Wilkins, & R. Zanetti (Eds.), Spaceflight Mechanics 2019 (pp. 701-711). [AAS 19-408] (Advances in the Astronautical Sciences; Vol. 168). Univelt Inc..

Low energy escape using tube dynamics associated with quasi-halo orbit. / Takemura, Kazutoshi; Baresi, Nicola; Kawakatsu, Yasuhiro; Yoshimura, Hiroaki.

Spaceflight Mechanics 2019. ed. / Francesco Topputo; Andrew J. Sinclair; Matthew P. Wilkins; Renato Zanetti. Univelt Inc., 2019. p. 701-711 AAS 19-408 (Advances in the Astronautical Sciences; Vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Takemura, K, Baresi, N, Kawakatsu, Y & Yoshimura, H 2019, Low energy escape using tube dynamics associated with quasi-halo orbit. in F Topputo, AJ Sinclair, MP Wilkins & R Zanetti (eds), Spaceflight Mechanics 2019., AAS 19-408, Advances in the Astronautical Sciences, vol. 168, Univelt Inc., pp. 701-711, 29th AAS/AIAA Space Flight Mechanics Meeting, 2019, Maui, United States, 19/1/13.
Takemura K, Baresi N, Kawakatsu Y, Yoshimura H. Low energy escape using tube dynamics associated with quasi-halo orbit. In Topputo F, Sinclair AJ, Wilkins MP, Zanetti R, editors, Spaceflight Mechanics 2019. Univelt Inc. 2019. p. 701-711. AAS 19-408. (Advances in the Astronautical Sciences).
Takemura, Kazutoshi ; Baresi, Nicola ; Kawakatsu, Yasuhiro ; Yoshimura, Hiroaki. / Low energy escape using tube dynamics associated with quasi-halo orbit. Spaceflight Mechanics 2019. editor / Francesco Topputo ; Andrew J. Sinclair ; Matthew P. Wilkins ; Renato Zanetti. Univelt Inc., 2019. pp. 701-711 (Advances in the Astronautical Sciences).
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