통신해양기상위성의 데이터처리 시스템 설계

Data Handling System Design for COMS

  • 발행 : 2009.05.07

초록

In this paper, we will describe architecture and key characteristic for the DHS which is used in COMS. DHS is implemented in the fully redundant SCU, the dual redundant MIL-STD-1553B system bus, the payload interface units(MPIU and MI2U), the redundant ADE. the SCU interface with the other main digital units of the spacecraft through the MIL-STD-1553B.

키워드