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    題名: Integration of Computer Subsystems and Power Subsystem for Micro-satellite
    作者: Huan-Jung Lin1, Zuu-Chang Hong **,2, Tzung-Hang Lee2, and Yung-Chuang Wen2
    貢獻者: 機械與機電工程學系暨研究所
    關鍵詞: 微衛星;衛星電腦;電源系統;飛行軟體;Microsatellite;Onboard computer;Power supply unit;Flight software
    日期: 2012
    上傳時間: 2015-03-06 19:15:52 (UTC+8)
    摘要: In this paper, the integration among on-board computer-MPC555,
    power supply unit, and ground station is presented. The design is to execute
    the mission performance under the satellite orbiting mode, includes
    supervising and managing satellite operation, handling and archiving
    information and message, receiving and executing the ground station
    command and the satellite bursting incident. Where the multi-task and
    real-time functions of an embedded system are accomplished, then the satellite flight software is established. The flight software includes
    initialization and autonomous operation of onboard computer which
    performs several tasks of satellite operation to meet mission requirement.
    Under operation mode, these tasks are capable of monitoring satellite’s
    health data, power supply unit , GPS status and handling incident events.
    關聯: Journal of Aeronautics, Astronautics and Aviation, Series B, 44(1), pp.001-008
    顯示於類別:[機械與機電工程學系暨研究所] 期刊論文

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