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微衛星電腦系統與電源子系統之整合研究

Integration of Computer Subsystems and Power Subsystem for Micro-Satellite

摘要


本文主要為衛星電腦MPC555、電源系統與地面站之軟、硬體整合。設計出衛星在運行模式下所要執行的任務與流程,包括督控及管理衛星的運作、資料與訊息的處理與儲存、接收並執行地面站之命令與星上突發狀況的處理能力。並利用電腦系統即時多工的特性,設計出飛行軟體,使其具備衛星電腦初始化與自治運作、命令接收與處理,以及資料的儲存、處理與下傳等功能,並建立其運作模式下之健康狀態監測、安全模式、電源健康狀態監測、酬載拍照、GPS監測、遙測資料儲存等應用工作,以符合太空任務之需求。

並列摘要


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.

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