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研究生: 李金龍
Lee, Chin-Lung
論文名稱: 運用DSP晶片實現直升機起降船舶之動態模擬系統
DSP-Based Implementation and Dynamic Simulation Of Helicopter Shipboard Launch and Recovery System
指導教授: 楊憲東
Yang, Ciann-Dong
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2005
畢業學年度: 93
語文別: 中文
論文頁數: 113
中文關鍵詞: 操作環境LMI飛行控制器數位訊號處理器直昇機起降控制
外文關鍵詞: Digital Signal Processor(DSP), Helicopter Lunch and Recovery Control, LMI flight Controller, Operational Environment
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  •   自從七O年代起,積體電路(Integrated Circuit, IC)由於功能穩定的優點而在硬體電路界冒出芽來,原因不外乎是其微小、精密、運算快速,甚至價格便宜等特性。由於這些優點,吾人在本文中利用德州儀器公司生產的DSP晶片來實現直昇機的起降模擬系統。藉由MATLAB及Simulink來執行複雜的控制迴路計算,再利用Real Time Workshop(RTW)將控制器迴路編譯成C code,下載到DSP內執行。吾人期望透過這樣的研究能達成直昇機自動駕駛系統微小化、輕量化的目的。

      本論文最大的貢獻在於將直昇機的非線性模型、LMI飛行控制器、船舶運動、以及直昇機海面起降的操作環境,都整合在同一個迴路下,並且以DSP晶片做為系統的控制器,實現硬體迴路(Hardware-in-the-loop)的設計。

     From 1970’s, the development of Integrated Circuit (IC) has grown into more important in hardware circuit, because of its stable capability. Without a doubt, the reasons are its smallness, preciseness, high speed, and cheapness. Due to these advantages, we use DSP chip which is manufactured by Texas Instrument to implement this dynamic simulation system in this thesis. The complicated helicopter control loops are simulated by MATLAB & Simulink, translated to C code by real-time workshop (RTW), and finally downloaded to DSP .What we have expect is making the helicopter auto-pilot system lighter and smaller through this research.

     The contribution in this thesis is combination of system design on a loop : helicopter nonlinear model, LMI flight controller, ship motion, and helicopter shipboard operational environment. We utilize DSP chip for controller of this system to implement the designing of hardware-in-the-loop.

    摘 要 I Abstract II 誌 謝 III 目 錄 IV 圖表目錄 VI 第一章 緒論 1 1.1 前言 1 1.2 研究背景與文獻回顧 2 1.3 各章概述 6 第二章 直昇機之動態模式 7 2.1 直昇機模式之五大次系統 7 2.2 直昇機下洗流(Inflow)模型 11 2.3 直昇機起降模擬之流程 14 2.4 直昇機動態方程式的線性化 15 2.5 直昇機致動器模式 19 第三章 飛行穩定控制系統 22 3.1 利用線性矩陣不等式設計狀態迴授穩定控制器 23 3.1.1 多目標狀態迴授合成 24 3.1.2 性能 27 3.2 實例模擬 29 3.3 飛行品質(Flight Quality)分析 35 3.3.1 飛行品質的評定參考觀點 36 3.3.2 飛行品質的評定方式 36 第四章 操作環境與動態介面 37 4.1 船舶甲板運動 (Deck Motion) 38 4.2 空氣擾流模型 (Airwake Model) 40 4.3 陣風模型 (Wind Gust Model Model) 50 4.4 地面效應模型 (Ground-effect Model) 52 4.4.1 下洗流(Inflow, Downwash) 53 4.4.2 氣墊效應(Fountain Effect) 58 4.4.3 地面效應的整體探討 63 4.5 直昇機起降系統之飛行品質驗證測試 72 第五章 直昇機起降系統之DSP晶片實現 79 5.1 TMS320C6701 DSP 與硬體模擬迴路(Hardware-in- the-loop) 80 5.1.1 TI C6701數位訊號處理器 80 5.1.2 硬體迴路模擬Hardware-in-the-loop 82 5.2 以DSP實現直昇機起降船舶動態系統 85 5.3 直昇機起降路徑的規劃與模擬結果討論 94 5.3.1 直昇機降落於行駛中的船舶 96 5.3.1 直昇機於行駛中的船舶起飛 101 第六章 結論及未來展望 105 6.1 結論 105 6.2 未來展望 107 REFERENCE 108 參考文獻 111 附 錄 112

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