Abstract
Recent missions of Japanese spacecraft for space researches are briefly presented, and their requirements on the attitude control are reviewed both for three-axis controlled satellites and spin-stabilized ones. The attitude control schemes developed and the systems designed are described by putting emphases on their specific features and the problems encountered during the developments. Key technology areas which will require further attention to achieve the near-future science missions under study are identified.
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More From: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series C
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