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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38470


    Title: 在離軸角限制條件下之導引性能分析
    Other Titles: A performance analysis of off-boresight constraint method for missile guidance
    Authors: 袁平甲;陳正興;邱元宏;田豐
    Contributors: 淡江大學航空太空工程學系
    Keywords: 比例導引律;偏角追逐法;數值分析;Proportional Navigation;Off Boresight;Numerical Analysis
    Date: 1998-12
    Issue Date: 2010-01-11 15:19:31 (UTC+8)
    Publisher: 逢甲大學
    Abstract: 本文旨就尋標器離軸角先天條件的限制, 而使用純比例導引律並配合保持離軸角(Off-borsight)為定值的方法(偏角追逐法), 來解決尋標器追蹤迴路無法穩定追蹤的困擾, 並探討此方法對飛彈性能之影響。結果經由數值分析驗證與理論相符合, 確實可以在離軸角限制條件下命中目標, 相對缺點為需要花較多能量與時間。
    The purpose of this paper is to develop and investigate the pure proportional navigation missile guidance law under the constraint of off-boresight angle, which usually occurs in a seeker tracking loop. Numerical examples show that proposed guidance law provides a strategy to accommodate the above-mentioned constraint at the cost of consuming more energy and flight time.
    Relation: 中國航空太空學會八十七年年會暨第四十屆學術研討會論文集(下冊),頁567-574
    Appears in Collections:[航空太空工程學系暨研究所] 會議論文

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