Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
第16回アストロダイナミクスシンポジウム講演後刷り集 2006
雑誌名(英)
Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics
In the case of spinning spacecraft attitude determination, detection of sun angle in high resolution and wide field of view is needed. We have developed the Rocket Sun Aspect Sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 degree. Furthermore, in order attitude determination of the spacecraft, two reference vectors and angles between the reference objects and spacecraft are needed, for example, sun and geomagnetic angle. Therefore, we developed the attitude determination system on the ground and software to receive rocket telemetry data, and calculate sun and geomagnetic angle. In this flight test, we verified the motion of RSAS and this attitude determination system by M-V-8 launch.
Flight test of rocket sun aspect sensor and attitude determination system on the ground by M-V-8 launch
