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研究生:溫建平
研究生(外文):Chaing-Ping Wen
論文名稱:非最小相位BTT飛彈之非線性控制
指導教授:袁 京
學位類別:碩士
校院名稱:國立臺灣大學
系所名稱:機械工程學研究所
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:2001
畢業學年度:89
語文別:中文
論文頁數:110
中文關鍵詞:BTT飛彈非最小相位非線性控制
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對於高性能Bank-to-Turn飛彈而言,彈體之高速滾轉及其不對稱外型所造成系統的嚴重藕合一直是BTT飛彈控制的主要課題。以往採線性控制理論者,其適用範圍均僅適用於低速滾轉或滾轉率變化很慢的情形下;一些應用非線性控制設計採忽略系統中某些項,並以近似系統設計控制器,但卻有穩定度上的疑慮。本文即針對BTT飛彈之控制提出一控制策略:以回授線性化將系統輸出輸入予以線性化,此舉雖然可使系統輸出達到目標,然因系統的非極小相位特性,其內部動態並不穩定。因此本文提出以狀態回授的方式,在回授線性化後將系統輸出視為內部動態的輸入,在系統暫態響應期間調整輸出,藉以穩定內部動態並達到系統追蹤的目的。另外以Lyapunov方法設計一補償器,改善系統的追蹤性能與穩定度。最後利用數值模擬測試本文控制策略所能提供之性能,並就飛彈在不同的飛行條件下探討系統之強健性。

摘要……………………………………………………………………I
目錄……………………………………………………………………II
圖目錄…………………………………………………………………IV
符號說明..……………………………………………………………VII
第一章 導論…………………………………………………………1
1-1.STT與BTT型飛彈簡介……………………………………………1
1-2.非極小相位系統…………………………………………………1
1-3.文獻回顧與研究動機……………………………………………1
1-4.本文主要貢獻……………………………………………………3
1-5.本文簡介…………………………………………………………3
第二章 飛彈之數學模型……………………………………………6
2-1.飛彈各運動狀態變數定義及假設………………………………6
2-2.飛彈數學模型之推導……………………………………………7
第三章 飛彈控制系統………………………………………………20
3-1.控制目標…………………………………………………………20
3-2.回授線性化與內部動態之穩定度………………………………20
3-3.內部動態穩定化…………………………………………………29
3-3.1 線性化系統之可控性………………………………………29
3-3.2 改寫正交形式………………………………………………31
3-3.3 狀態回授穩定內部動態……………………………………37
3-3.4 Lyapunov補償器……………………………………………42
第四章 數值模擬與討論……………………………………………48
4-1.模擬結果…………………………………………………………48
4-2.結果討論…………………………………………………………50
4-3.大攻角模型之控制討論…………………………………………51
第五章 結論與未來展望……………………………………………96
5-1.結論………………………………………………………………96
5-2.未來展望…………………………………………………………96
參考文獻………………………………………………………………97

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