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題名 | 戰機之戰術與性能對飛彈最大發射區與最小脫逃距離影響之探討=A Study of the Effects of Fighter Tactics and Performance on Missile Maximum Launch Area and Minimum Evasive Range |
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作者姓名(中文) | 孔健君; 蔣豐隆; 吳啟郁; |
作者姓名(外文) | Kung, Chien-chun; Chiang, Feng-lung; Wu, Chi-yu; |
書刊名 | 航空太空及民航學刊. 系列B |
卷期 | 42:2 2010.10[民99.10] |
頁次 | 頁83-88 |
分類號 | 595.95 |
語文 | chi |
關鍵詞 | 導引律; 迴授線性化; 最大飛彈發射區; 最小脫逃距離; Guidance law; Feedback linearization; Maximum capture areas; Minimum evasive ranges; |
中文摘要 | 本文以空戰模擬系統,建立了飛彈最大發射區與飛機最小脫逃距離,對傳統只能以靶機實機測試,提出了新的建構方式與理念,並探討戰機空戰智慧、性能及飛彈性能對兩項數據之影響。本文首先介紹飛彈最大發射區及飛機最小脫逃距離之概念,進而引入飛彈運動方程式及迴授線性化實現尾隨法導引律之方法,並定義相對距離爲函數之飛彈殺傷率。其次作戰智慧、戰機性能、飛彈性能對作戰與脫逃之影響,藉由最大飛彈發射區與飛機最小脫逃距離的繪製,可提醒最後脫逃之機會及建構發射飛彈之最佳時機,發展出先進戰機之最佳空戰策略,獲致更多之戰場優勢,藉以增加戰場之存活率。 |
英文摘要 | This paper will analysis the effects of combat tactics, performance of a fighter and the character of a missile on the missile maximum capture area and the fighter minimum evasive range which are found by using air-combat simulator. Firstly, we propose the ideas of the missile maximum capture area and the fighter minimum evasive range. Equations of motion of a missile and the feedback linearization control method to obtain the accelerations to implement pursuit guidance law are introduced. A damage scoring function by fragmentation warhead is also defined. Next, the missile maximum capture areas and the fighter minimum evasive ranges are studied in different air-combat cases, e.g., pilot's intelligence, aircraft's performance and the missile's character. With the information of maximum capture areas and minimum evasive ranges, the optimal distance to launch missile and the last chance to escape from missile can be predicted. |
本系統之摘要資訊系依該期刊論文摘要之資訊為主。