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Journal Article Design, Implementation, and Validation of KOMPSAT-2 Software Simulator
Cited 8 time in scopus Download 7 time Share share facebook twitter linkedin kakaostory
Authors
San Guk Lee, Sung Ki Cho, Byoung Sun Lee, Jae Hoon Kim
Issue Date
2005-04
Citation
ETRI Journal, v.27, no.2, pp.140-152
ISSN
1225-6463
Publisher
한국전자통신연구원 (ETRI)
Language
English
Type
Journal Article
DOI
https://dx.doi.org/10.4218/etrij.05.0104.0057
Abstract
In this paper, we present design features, implementation, and validation of a satellite simulator subsystem for the Korea Multi-Purpose Satellite-2 (KOMPSAT-2). The satellite simulator subsystem is implemented on a personal computer to minimize costs and trouble on embedding onboard flight software into the simulator. An object-oriented design methodology is employed to maximize software reusability. Also, instead of a high-cost commercial database, XML is used for the manipulation of spacecraft characteristics data, telecommand, telemetry, and simulation data. The KOMPSAT-2 satellite simulator subsystem is validated by various simulations for autonomous onboard launch and early orbit phase operations, anomaly operation, and science fine mode operation. It is also officially verified by successfully passing various tests such as the satellite simulator subsystem test, mission control element system integration test, interface test, site installation test, and acceptance test.
KSP Keywords
Acceptance Test, Commercial database, Design features, Flight Software, Interface test, KOMPSAT-2, Mission control element, Object-Oriented Design, Satellite simulator, Simulation data, Software Reusability