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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/37899

    Title: 微衛星TUUSAT-1A任務與飛行軟體操作模式規劃
    Other Titles: The Operational Mode Design of Mission and Flight Software for Microsatellite TUUSAT-1A
    Authors: 林宗憲;洪祖昌;王銀添;林嘉茂;林煥榮;徐超明
    Contributors: 淡江大學機械與機電工程學系
    Keywords: 微衛星;任務模式;飛行軟體;Microsatellite;Mission model;Flight software
    Date: 2004-12-12
    Issue Date: 2010-01-11 14:18:09 (UTC+8)
    Abstract: 本文主要討論微衛星TUUSAT-1A任務操作模式與飛行軟體規劃設計,首先介紹衛星任務目的與需求、各次系統需求與硬體元件規格,依任務需求規劃衛星的操作 區域與任務操作模式。任務模式共分為發射過程模式、進入軌道模式、穩定模式 、運行模式與安全模式,運行模式又依操作區域分為Receive、Download、 Capture、Beacon與Mailbox等次模式,各模式間的切換與執行邏輯皆以流程圖的 方式描述。飛行軟體依照次系統需求定義飛行軟體的基本功能,最後並規劃飛行 軟體的架構與未來發展方向。
    This paper emphasizes on the operation mode and Flight Software design for a microsatellite TUUSAT-1A. The mission objectives and requirements of TUUSAT-1A are presented. The subsystems requirements and specifications are also described. The operation modes and areas are designed according to the mission requirements. The operation modes include the Launch, Orbit, Stable, Operation and Safe Modes. The Operation Mode consists of Receive, Download, Capture, Beacon and Mailbox Submodes. The alternation and executive logics between each mode are described by the flowcharts. The basic capabilities of onboard Flight Software are defined according to subsystem requirements. The architecture of Flight Software is also designed according to the operation modes design, as well as the future development.
    Relation: 中國航空太空學會第四十六屆年會暨會員大會、2004航太學會/民航學會聯合學術研討會、國科會航太學門專題研究計畫成果發表會、教育部航太科技教育改進計畫成果發表會論文集,8頁
    Appears in Collections:[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Proceeding

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