Aeronautical and Space Sciences Japan
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
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  • [title in Japanese]
    SHIN-ICHIRO SAKAI
    2008 Volume 56 Issue 652 Pages 130-138
    Published: May 05, 2008
    Released on J-STAGE: April 22, 2019
    DOIhttps://doi.org/10.14822/kjsass.56.652_130
    JOURNAL FREE ACCESS
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    This paper describes the attitude control system of the REIMEI satellite: a 70 kg microsatellite for scientific aurora observation. One of the instruments for the observation is an aurora imager, thus three axis attitude control capability of 0.5 deg accuracy was required. To achieve the requirements within limited resources, such as mass, volume, electrical power, cost or human resource, unique approaches were taken for design, test and operation of the attitude control system. Some of these points are introduced in this paper with in-orbit evaluation results.

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