An electric propulsion configured small halo orbit around L2

Jun'ichiro Kawaguchi; Kohta Tarao

An electric propulsion configured small halo orbit around L2

^*Corresponding author for this work

Research output: Contribution to conference › Paper › peer-review

Abstract

For future applications, a Lagrange point of Sun-Earth system, L1 or L2 is conceived one of the best point for astronomy and connection ports for outer planets. This paper describes a new useful control method for realizing and keeping small circular Halo orbits around the L2 point, The resulted Halo orbit obtained is compact and circular realized with satisfactorily small thrust. The paper concludes the strategy is applied to many kinds of missions.

Original language	English
Pages	3089-3096
Number of pages	8
Publication status	Published - 2005
Externally published	Yes
Event	International Astronautical Federation - 56th International Astronautical Congress 2005 - Fukuoka, Japan Duration: 17 Oct 2005 → 21 Oct 2005

Conference

Conference	International Astronautical Federation - 56th International Astronautical Congress 2005
Country/Territory	Japan
City	Fukuoka
Period	17/10/05 → 21/10/05

Cite this

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title = "An electric propulsion configured small halo orbit around L2",

abstract = "For future applications, a Lagrange point of Sun-Earth system, L1 or L2 is conceived one of the best point for astronomy and connection ports for outer planets. This paper describes a new useful control method for realizing and keeping small circular Halo orbits around the L2 point, The resulted Halo orbit obtained is compact and circular realized with satisfactorily small thrust. The paper concludes the strategy is applied to many kinds of missions.",

author = "Jun'ichiro Kawaguchi and Kohta Tarao",

year = "2005",

language = "English",

pages = "3089--3096",

note = "International Astronautical Federation - 56th International Astronautical Congress 2005 ; Conference date: 17-10-2005 Through 21-10-2005",

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AU - Kawaguchi, Jun'ichiro

AU - Tarao, Kohta

PY - 2005

Y1 - 2005

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AB - For future applications, a Lagrange point of Sun-Earth system, L1 or L2 is conceived one of the best point for astronomy and connection ports for outer planets. This paper describes a new useful control method for realizing and keeping small circular Halo orbits around the L2 point, The resulted Halo orbit obtained is compact and circular realized with satisfactorily small thrust. The paper concludes the strategy is applied to many kinds of missions.

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M3 - Paper

AN - SCOPUS:34250805565

SP - 3089

EP - 3096

T2 - International Astronautical Federation - 56th International Astronautical Congress 2005

Y2 - 17 October 2005 through 21 October 2005

ER -

An electric propulsion configured small halo orbit around L2

Abstract

Conference

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