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題名 | A Composite Guidance for ASM with IIR Homing=空對地飛彈紅外線影像終端歸向之複合導引法則研究 |
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作者 | 陶德仁; | 書刊名 | 新新科技年刊 |
卷期 | 12 2016.01[民105.01] |
頁次 | 頁102-112 |
分類號 | 595.95 |
關鍵詞 | 空對地飛彈; 複合控制; 奇異攝動; 尋優中途導引律; 強健性; 尋優滑模歸向導引律; 被動紅外線歸向; 路徑限制; 複合導引; Air to surface missile; Composite control; Singular perturbation; Optimal midcourse guidance law; Robust; Optimal sliding mode homing guidance law; Passive IIR homing; Path constraint; Composite guidance; |
語文 | 英文(English) |
中文摘要 | 本文旨在探討水平發射之空對地飛彈,紅外線影像終端歸向之複合導引法則。對此空對地攔截任務之中途導引,將運用複合控制原理,就奇異攝動理論推導之尋優中途導引律,加以簡化修正。而對終端歸向導引,則將具有強健性之尋優滑模控制歸向導引律,應用於受到路徑限制之場景。最後附有不同場景的數值模擬結果。 |
英文摘要 | A composite guidance strategy for air to surface missiles(ASM) with IIR seekers is synthesized in this study. For the midcourse of this kind of air to surface mission, the singular perturbation(SP) solution to the optimal midcourse guidance law is simplified based on the composite control approach. Besides, a robust optimal sliding mode guidance law with path constraints is constructed for passive IIR homing. Numerical simulation results are also shown for several cases. |
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