Attitude control strategy of a transformable spacecraft for orbital station-keeping around sun-earth L2

Yuki Kubo; Toshihiro Chujo; Javier Hernando-Ayuso; Junichiro Kawaguchi

Attitude control strategy of a transformable spacecraft for orbital station-keeping around sun-earth L2

Yuki Kubo, Toshihiro Chujo, Javier Hernando-Ayuso, Junichiro Kawaguchi

Research output: Contribution to journal › Conference article › peer-review

Abstract

This paper proposes the control method which achieves fuel-free station-keeping around Sun-Earth L2 point (SEL2). This station-keeping is driven with only solar radiation pressure (SRP), and therefore the orbit is maintained without fuel consumption by controlling attitude of a spacecraft toward the sun. Furthermore, this attitude control is also achieved without fuel by using the technique of non-holonomic turn. The target orbit is the artificial orbit around SEL2, the size of which is much smaller than typical halo orbits, and thus provides more stationary thermal condition to spacecrafts.

Original language	English
Journal	Proceedings of the International Astronautical Congress, IAC
Volume	2018-October
Publication status	Published - 2018
Externally published	Yes
Event	69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 - Bremen, Germany Duration: 2018 Oct 1 → 2018 Oct 5

Keywords

Artificial Orbit
Halo Orbit
Non-Holonomic Turn
SEL2
Solar Radiation Pressure

ASJC Scopus subject areas

Aerospace Engineering
Astronomy and Astrophysics
Space and Planetary Science

Cite this

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title = "Attitude control strategy of a transformable spacecraft for orbital station-keeping around sun-earth L2",

abstract = "This paper proposes the control method which achieves fuel-free station-keeping around Sun-Earth L2 point (SEL2). This station-keeping is driven with only solar radiation pressure (SRP), and therefore the orbit is maintained without fuel consumption by controlling attitude of a spacecraft toward the sun. Furthermore, this attitude control is also achieved without fuel by using the technique of non-holonomic turn. The target orbit is the artificial orbit around SEL2, the size of which is much smaller than typical halo orbits, and thus provides more stationary thermal condition to spacecrafts.",

keywords = "Artificial Orbit, Halo Orbit, Non-Holonomic Turn, SEL2, Solar Radiation Pressure",

author = "Yuki Kubo and Toshihiro Chujo and Javier Hernando-Ayuso and Junichiro Kawaguchi",

note = "Publisher Copyright: Copyright {\textcopyright} 2018 by the International Astronautical Federation (IAF). All rights reserved.; 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 ; Conference date: 01-10-2018 Through 05-10-2018",

year = "2018",

language = "English",

volume = "2018-October",

journal = "Proceedings of the International Astronautical Congress, IAC",

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TY - JOUR

T1 - Attitude control strategy of a transformable spacecraft for orbital station-keeping around sun-earth L2

AU - Kubo, Yuki

AU - Chujo, Toshihiro

AU - Hernando-Ayuso, Javier

AU - Kawaguchi, Junichiro

PY - 2018

Y1 - 2018

N2 - This paper proposes the control method which achieves fuel-free station-keeping around Sun-Earth L2 point (SEL2). This station-keeping is driven with only solar radiation pressure (SRP), and therefore the orbit is maintained without fuel consumption by controlling attitude of a spacecraft toward the sun. Furthermore, this attitude control is also achieved without fuel by using the technique of non-holonomic turn. The target orbit is the artificial orbit around SEL2, the size of which is much smaller than typical halo orbits, and thus provides more stationary thermal condition to spacecrafts.

AB - This paper proposes the control method which achieves fuel-free station-keeping around Sun-Earth L2 point (SEL2). This station-keeping is driven with only solar radiation pressure (SRP), and therefore the orbit is maintained without fuel consumption by controlling attitude of a spacecraft toward the sun. Furthermore, this attitude control is also achieved without fuel by using the technique of non-holonomic turn. The target orbit is the artificial orbit around SEL2, the size of which is much smaller than typical halo orbits, and thus provides more stationary thermal condition to spacecrafts.

KW - Artificial Orbit

KW - Halo Orbit

KW - Non-Holonomic Turn

KW - SEL2

KW - Solar Radiation Pressure

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M3 - Conference article

AN - SCOPUS:85065287047

VL - 2018-October

JO - Proceedings of the International Astronautical Congress, IAC

JF - Proceedings of the International Astronautical Congress, IAC

SN - 0074-1795

T2 - 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018

Y2 - 1 October 2018 through 5 October 2018

ER -

Attitude control strategy of a transformable spacecraft for orbital station-keeping around sun-earth L2

Abstract

Keywords

ASJC Scopus subject areas

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