f) On-Orbit and Ground Support Systems
Development of Fudai Sun Sensor (FSS)
2009 年 7 巻 ists26 号 p. Tf_25-Tf_30
詳細
2009 年 7 巻 ists26 号 p. Tf_25-Tf_30
This paper describes the design process of the Fudai sun sensor (FSS) installed in a 50-kg-class micro-satellite, SOHLA-1. The FSS has been developed by the students of Osaka Prefecture University (OPU) with technical support from the Japan Aerospace Exploration Agency (JAXA) and Advanced Engineering Services (AES) Co. Ltd. In this project, the students experienced a series of processes required for developing satellite components, namely, design, production, test, launch, and operation.
