English  |  正體中文  |  简体中文  |  Items with full text/Total items : 62805/95882 (66%)
Visitors : 3882905      Online Users : 301
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU 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: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/84776

    Title: 旋翼型無人載具之非線性動態模擬
    Other Titles: Simulation of Nonlinear Dynamics of Unmanned Aerial Helicopter
    Authors: 曾奕智;Tseng, Y. C;蕭富元;Hsiao, F. Y.;陳延銓;Chen, Y. C.;朱崇傑;Chu, C. C.
    Contributors: 淡江大學航空太空工程學系
    Keywords: 無人直昇機;系統鑑別;雷虎翼手龍90無人直昇機;預測誤差估測法Unmanned aerial helicopter (UAH);System identification;Raptor-90;Prediction error estimation methods (PEM)
    Date: 2007
    Issue Date: 2013-03-22 19:37:45 (UTC+8)
    Publisher: 中山科學研究院及國防大學
    Abstract: 本論文在探討發展小型無人直昇機"翔蛉"(H-Ling,為雷虎翼手龍90級)的參數化模型及利用各種系統鑑別的技術來鑑別參數,包括ARX、CIFER和PEM。此項計畫的最終目標是建立一個全功能的自主飛行旋翼機。我們首先簡短回顧了小型直昇機的運動方程式,然後簡單介紹PEM的數學原理。藉由收集到的試飛數據,我們將直昇機的參數全數鑑別出來。本文亦提供利用各種鑑別理論所得的圖表,來呈現這些結果的一致性,也間接證明那些結果的正確性。
    In this paper we are going to develop a parameterized model for a small-scale unmanned helicopter H-Ling (a Thunder Tiger Raptor-90) and its identification using various techniques, including ARX, CIFER and PEM. The ultimate goal of this project is to extend the current work to build a fully functional autonomous rotorcraft. The equations of motion of a small-scaled rotorcraft are briefly reviewed first. We then briefly introduce the mathematics of PEM. With the flight test data, we obtain the identified parameters of the dynamical model. Numerical simulations and table of identified parameters are provided to show the consistency and correctness of our results.
    Relation: 第16屆國防科技學術研討會96年度國防科技學術合作計畫成果發表會論文集,8頁
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

    Files in This Item:

    File Description SizeFormat
    旋翼型無人載具之非線性動態模擬_中文摘要.docx摘要14KbMicrosoft Word128View/Open
    旋翼型無人載具之非線性動態模擬_西文摘要.docx摘要14KbMicrosoft Word107View/Open

    All items in 機構典藏 are protected by copyright, with all rights reserved.

    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback