Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment

Hirohisa Kojima; Kana Hiraiwa; Yasuhiro Yoshimura

doi:10.1016/j.actaastro.2017.11.020

Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment

Hirohisa Kojima, Kana Hiraiwa, Yasuhiro Yoshimura

Research output: Contribution to journal › Article › peer-review

10 Citations (Scopus)

Abstract

This paper presents the results of line-of-sight (LOS) attitude control using control moment gyros under a micro-gravity environment generated by parabolic flight. The W-Z parameters are used to describe the spacecraft attitude. In order to stabilize the current LOS to the target LOS, backstepping-based feedback control is considered using the W-Z parameters. Numerical simulations and experiments under a micro-gravity environment are carried out, and their results are compared in order to validate the proposed control methods.

Original language	English
Pages (from-to)	118-125
Number of pages	8
Journal	Acta Astronautica
Volume	143
DOIs	https://doi.org/10.1016/j.actaastro.2017.11.020
Publication status	Published - Feb 2018
Externally published	Yes

All Science Journal Classification (ASJC) codes

Aerospace Engineering

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10.1016/j.actaastro.2017.11.020

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title = "Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment",

abstract = "This paper presents the results of line-of-sight (LOS) attitude control using control moment gyros under a micro-gravity environment generated by parabolic flight. The W-Z parameters are used to describe the spacecraft attitude. In order to stabilize the current LOS to the target LOS, backstepping-based feedback control is considered using the W-Z parameters. Numerical simulations and experiments under a micro-gravity environment are carried out, and their results are compared in order to validate the proposed control methods.",

author = "Hirohisa Kojima and Kana Hiraiwa and Yasuhiro Yoshimura",

note = "Funding Information: This study was supported by a Grant-in-Aid for Scientific Research (B) (No. 25289309 ) from JSPS . The authors would like to express their gratitude to Diamond Air Service Inc. for providing the micro-gravity environment for this study. Publisher Copyright: {\textcopyright} 2017 IAA",

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AU - Yoshimura, Yasuhiro

N1 - Funding Information: This study was supported by a Grant-in-Aid for Scientific Research (B) (No. 25289309 ) from JSPS . The authors would like to express their gratitude to Diamond Air Service Inc. for providing the micro-gravity environment for this study. Publisher Copyright: © 2017 IAA

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AB - This paper presents the results of line-of-sight (LOS) attitude control using control moment gyros under a micro-gravity environment generated by parabolic flight. The W-Z parameters are used to describe the spacecraft attitude. In order to stabilize the current LOS to the target LOS, backstepping-based feedback control is considered using the W-Z parameters. Numerical simulations and experiments under a micro-gravity environment are carried out, and their results are compared in order to validate the proposed control methods.

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Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment

Abstract

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