B3 汎用インタフェースを用いた超小型衛星用標準バスの設計開発(小型衛星)

概要

論文の詳細を見る
In recent years. the universities and institutes develop many microsatellites actively. But it is difficult for new developers to entry because so-called "Closed Integral" development method same as traditional satellite project. Feature of this research is each subsystem in the microsatellite is allocated in the same rank. Using the CAN (Controller Area Network), which have broad utility, we try to adopt the "Open Modular" development method for the microsatellite, and normalize at the subsystem or component level. In this presentation, we introduce these outlines.
2010-01-28