| Summary: | 碩士 === 淡江大學 === 機械與機電工程學系碩士班 === 98 === This paper according to critical design of TUUSAT-1A subsystems uses simulator to verify the mission requirements. By the mission and frames TUUSAT-1A, after understanding the mission and frames construction of micro-satellite, then explain critical design of micro-satellite, including system design and the preliminary design. Then we give the detailed explanation to each tray configuration. For verification the TUUSAT-1A subsystem design, using the software TUUSIM that developed by research team, after combining with communication programs, to run mission simulation of attitude control, thermal control, electrical power and communication subsystem, finally discusses the result with critical design review.
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