Japan Aerospace Exploration Agency Technology Development Department, Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Technology Development Department, Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Technology Development Department, Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Dept. of Space Transportation Eng., Inst. of Space and Astronautical Science
JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
巻
JAXA-SP-06-006
ページ
359 - 362
発行年
2006-11-01
抄録（英）
In order to detect attitude for spinning rocket we have developed a sun aspect sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 degree. Furthermore, we have developed the attitude determination system using data of sun sensor and geomagnetic aspect sensor on the ground. The sun sensor was flight tested with ISAS rocket (M-V-8) on 23rd February 2006. Purposes of the test were environmental test (vibration shock etc.) during launching. It was found the sun sensor had no trouble during flight and able to determine attitude for spinning rocket.
ロケット搭載用太陽センサの飛翔実験および地上における姿勢決定システム
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