English  |  正體中文  |  简体中文  |  Items with full text/Total items : 76531/76531 (100%)
Visitors : 29752536      Online Users : 273
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version

    Please use this identifier to cite or link to this item: http://ir.lib.ncu.edu.tw/handle/987654321/1677

    Title: ESEMS太空氣象科學酬載叢集;ESEMS Scientific Space Meteorology Payload Cluster
    Authors: 許盈晧;Ying-Hao Hsu
    Contributors: 光機電工程研究所
    Keywords: 系統;太空氣象科學儀器之研製與應用計畫;整測;磁力計;電子溫度探測儀;電離層;磁層;數位訊號處裡器;韌體;科學;太空;太空氣象;量測;酬載;微衛星;衛星;Electron Temperature Probe;ETP;Integration;Micro Satellite;Payload;Measurement;MRM;Magnetometer;Digital Signal Processor;DSP;Payload System;Science;Educational Scientific Experiment Micro Satellit;Ionosphere;Magnetosphere;Space;ESEMS;System Firmware
    Date: 2008-07-10
    Issue Date: 2009-09-21 09:57:32 (UTC+8)
    Publisher: 國立中央大學圖書館
    Abstract: 本論文以開發承載操作ESEMS(Educational Scientific Experiment Micro Satellite)太空氣象科學儀器之研製與應用計畫 之科學酬載以及其平台為目標,期望能達到高精度的酬載量測應用。 本酬載叢集內包含兩項科學酬載:磁阻式磁力計(MRM, Magnet- Resistive Magnetometer)以及電子溫度探測計(ETP, Electron Temperature Probe)。希望能藉由量測電離層和磁層內的太空氣象 變化,分析之後得到地震或其他相關氣象事件發生的前兆。 另一部份的重點則是在於酬載平台的硬體及韌體整合。為了能 夠確保資料的準確性,以及酬載平台和衛星之間能正常相互運作, 我們針對各酬載和主控模組間進行了硬體的整合和最佳化,並設立 了一套酬載操作以及系統整體運作的流程,且開發出了對應的系統 韌體,以期能夠正確的執行我們設定的任務目標和相關功能。 The main purpose of this thesis is to develop and integrate a platform which handling the science payloads of ESEMS project. Hope that it can reach the goal of high precision measurement and related applications. The payload cluster contains two science payloads, which are MRM (Magnet-Resistive Magnetometer) and ETP (Electron Temperature Probe).By the measuring of ionosphere and magnetosphere, we’re willing to find some signs of prediction of earth-quake or other meteorology issues. We also focus on the integration of functions of system hardware and firmware. To make sure that the data we measured is correct, also, to make sure that the operation between our payload cluster and satellite works properly, the workability of each module has been integrated and optimized. We also construct a procedure of payload and overall system operation. And, we’ve developed a corresponding system firmware to execute our mission objective and system function properly.
    Appears in Collections:[光機電工程研究所 ] 博碩士論文

    Files in This Item:

    File SizeFormat

    All items in NCUIR are protected by copyright, with all rights reserved.

    社群 sharing

    ::: Copyright National Central University. | 國立中央大學圖書館版權所有 | 收藏本站 | 設為首頁 | 最佳瀏覽畫面: 1024*768 | 建站日期:8-24-2009 :::
    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library IR team Copyright ©   - 隱私權政策聲明