頁籤選單縮合
題 名 | CLOS導引律用於TVM終端歸向之解析研究=The Analysis of CLOS Guidance Law in TVM Missile Terminal Interception |
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作 者 | 趙嘉琦; 李守誠; 宋真堯; | 書刊名 | 中正嶺學報 |
卷 期 | 34:1 民94.11 |
頁 次 | 頁1-16 |
分類號 | 595.95 |
關鍵詞 | 視向線指令; Locke法; Jalali-naini法; 文式法; CLOS; Command to line of sight; Locke method; Jalali-naini method; Wen's method; |
語 文 | 中文(Chinese) |
中文摘要 | 本文討論TVM(Tracking Via Missile)飛彈攔截彈道飛彈之解析研究,飛彈於終端階段使用視向線指令(command to Line of Sight, CLOS)導引律,但TVM用CLOS導引律係屬於傳統CLOS導引律,比較其不同之處為參考點由地面控制站移往就位點,以及飛彈與目標速率比值(P)由1.5以上降文氏法均重新修正,使之符合TVM飛彈攔截高速彈道飛彈的真實狀況。本研究並估算在假設條件下,最佳之就位點與就位角度之數值,達成最準確和最大能量之攔擁撞擊。 |
英文摘要 | In this paper, it discus the analytical method of ATBM interception via TVM (Tracking Via Missile), it use the modified CLOS (Command to Line of Sight) in the terminal phase. The major difference between conventional CLOS is observation (Reference) point, which is changed from the ground to seeker “lock-on” position in collision. The second difference occur in the constant P, which is the ratio of speed of missile and target, the value is decreased from 1.5 to 0.7~0.5 and form as a head-on collision. It also give a rigorous study for some methods of CLOS, such as Locke method, Jalali-Naini method and Wen’s method, to make some refining result. Under some assumption, the paper give a prediction for the best lock-on point, and the angle of lock-on, it can obtain a collision with the most accurate and the best energy consumption in the interception course. |
本系統中英文摘要資訊取自各篇刊載內容。