Data Handling System Design for COMS

통신해양기상위성의 데이터처리 시스템 설계

  • Published : 2009.05.07

Abstract

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.

Keywords