書誌事項
- タイトル別名
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- 4123 The Attitude Control Experiments of "HIT-SAT" and the Future Development Satellite
抄録
"HIT-SAT" is a small satellite to demonstrate performance of the bus systems of "Hokkaido Satellite". The main purpose of the attitude control system of "HIT-SAT" is to get basis data for the attitude control and determination system of "Hokkaido Satellite". "HIT-SAT" was launched on Sep. 23, 2006 by M-V-7. Attitude control system of "HIT-SAT" could get magnetometer data and gyro data on orbit. This paper describes the attitude determination from magnetometer data obtained on orbit.
収録刊行物
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- 年次大会講演論文集
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年次大会講演論文集 2007.5 (0), 391-392, 2007
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001206064330496
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- NII論文ID
- 110007084996
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- ISSN
- 24331325
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可