
Development and Testing of Satellite Operation System for Korea Multipurpose Satellite‐I
Author(s) -
Mo HeeSook,
Lee HoJin,
Lee SeongPal
Publication year - 2000
Publication title -
etri journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.295
H-Index - 46
eISSN - 2233-7326
pISSN - 1225-6463
DOI - 10.4218/etrij.00.0100.0101
Subject(s) - redundancy (engineering) , interoperability , computer science , satellite system , reliability (semiconductor) , engineering , communications satellite , satellite , scheme (mathematics) , embedded system , systems engineering , reliability engineering , operating system , gnss applications , power (physics) , physics , quantum mechanics , aerospace engineering , mathematical analysis , mathematics
The Satellite Operation System (SOS) has been developed for a low earth orbiting remote sensing satellite, Korea Multipurpose Satellite‐I, to monitor and control the spacecraft as well as to perform the mission operation. SOS was designed to operate on UNIX in the HP workstations. In the design of SOS, flexibility, reliability, expandability and interoperability were the main objectives. In order to achieve these objectives, a CASE tool, a database management system, consultative committee for space data systems recommendation, and a real‐time distributed processing middle‐ware have been integrated into the system. A database driven structure was adopted as the baseline architecture for a generic machine‐independent, mission specific database. Also a logical address based inter‐process communication scheme was introduced for a distributed allocation of the network resources. Specifically, a hot‐standby redundancy scheme was highlighted in the design seeking for higher system reliability and uninterrupted service required in a real‐time fashion during the satellite passes. Through various tests, SOS had been verified its functional, performance, and interface requirements. Design, implementation, and testing of the SOS for KOMPSAT‐I is presented in this paper.