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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/35543

    Title: 整合全球定位系統與慣性導航系統的初始校準設計與實現
    Other Titles: Design and implementation of GPS/INS integrated system initial alignment
    Authors: 李正凱;Lee, Cheng-kai
    Contributors: 淡江大學航空太空工程學系碩士班
    馬德明;Ma, Der-ming
    Keywords: 慣性導航系統;全球定位系統;卡爾曼濾波器;機載電腦;嵌入式系統;OBC;Initial Alignment;INS/GPS;Embedded Linux;Kalman filter
    Date: 2006
    Issue Date: 2010-01-11 06:45:40 (UTC+8)
    Abstract: 本文將探討INS/GPS 整合導航系統中,初始化的校正以及位置、速
    統狀態。本論文以實際應用慣性量測設備並搭配GPS 建立整合導航系統
    應用Linux 實際建立一套多工即時處理的系統核心,以整合在現有的無人
    本論文附上所有原始碼包含以Matlab 撰寫的模擬程式、原始實驗數據
    The thesis is dealing with the problem of initial alignment of INS/GPS
    integrated system; and in flight calibration of position, speed, and attitude. The
    basic structure of the integrated system is treating the navigation data from
    inertial navigation system as the system dynamics while those from the global
    positioning system as the measurement and using the kalman filter to correlate
    the data. The question of divergence of implementing kalman filters is
    discussed. An embedded system, based on the Linux kernel, which
    implementing the integrated system is realized and targeting into a
    single-board computer as the on-board computer of an UAV. A ground station,
    utilizing the object-oriented programming, is also developed to monitor the
    status of the UAV.
    The accompanied CD-ROM contains the computer codes of Matlab
    m-files and OBC program, test data from ground tests, and communication
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Thesis

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