| 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 |
| 相關次數: | 點閱:116 下載:3 |
| 分享至: |
| 查詢本校圖書館目錄 查詢臺灣博碩士論文知識加值系統 勘誤回報 |
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.
[1] Padfield, G.D., Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modeling, AIAA, 1996.
[2] Padfield, G.D. “Simulating flying qualities at the helicopter/ship dynamic interface,” Annual Forum Proceedings - American Helicopter Society, Vol. 2, pp 883-904, 1994.
[3] Ferrier, B.; Semenza, J. “Development, simulation and testing of the Landing Period Designator (LPD) helicopter recovery aid,” Annual Forum Proceedings - American Helicopter Society, Vol. 2, pp 739-750, 1994.
[4] Lumsden, R. Bruce; Ferrier, Bernard “Along side analysis of type 23 ship motion as a function of mechanical and dynamic limits of an EH101-like helicopter using the landing period designator helicopter recovery device,” Annual Forum Proceedings - American Helicopter Society, Vol. 1, p 772-780, 1995.
[5] Ferrier, B.; Manning, T. Source “Simulation and testing of the Landing Period Designator (LPD) helicopter recovery aid,” Naval Engineers Journal, Vol. 110, No. 1, pp. 189-205, 1998.
[6] Ferrier, B.; Langlois, B.; Bergeron, F.; Reboulet, C.; Fuertes, V.; Barral, J.-C. “Design and test using simulation techniques of an automated UAV-VTOL shipboard recovery system,” Annual Forum Proceeding- American Helicopter Society, Vol. 2, pp. 1381-1393, 1998.
[7] J.R. Platt, “Wind Detection in a Microcosim: Ship/Aircraft Environment Sensors,” IEEE Aerospace and Electronic Systems Magazine, Vol. 13, No. 2, pp. 26-33, 1998.
[8] Cheeseman, I.C. and Bennett, W.E., “The Effect of the Ground on a Helicopter Rotor in Forward Flight”, Aeronautical Research Council R&M No 3021, 1957.
[9] Xin, Hong; Prasad, J.V.R.; Peters, D.A.; Nagashima, T.; Iboshi, N. “Finite state inflow model for simulation of helicopter hovering in ground effect,” Annual Forum Proceedings - American Helicopter Society, Vol. 2, pp. 777-784, 1998
[10] U.S. Military Handbook MIL-HDBK-1797, 19 December 1997
[11] U.S. Military Specification MIL-F-8785C, 5 November 1980.
[12] Hoblit, F., "Gust Loads on Aircraft: Concepts and Applications," AIAA Education Series, 1988.
[13] Dooyang, L.; Nilay, S.; Joseph, F.H.; Lyle, N.L. “Simulation and Control of Shipboard Launch and Recovery Operations,” American Helicopter Society 59th Annual Forum, Phoenix, Arizona, 2003.
[14] Loek T.Renirie and Tjamme Hoekstra, “Helicopter-Ship Qualification Testing”, Journal of the American Helicopter Society , January 1981.
[15] Gareth D.Padfield, “The making of helicopter flying qualities: a requirements perspective ”, AERONAUTICAL JOURNAL, December 1998.
[16] D.A. Peters & T.Nagashima & N. lboshi ,”A finite state inflow model for simulation of helicopter hovering in ground effect”, American Helicopter Society, May 20-22,1998
[17] Lyle N.Long & Joseph F. Horn,” Simulation of helicopter shipboard launch and recovery with time-accurate airwakes”,American helicopter society, May 2003
[18] Robert G & Atef R,“State-of–the–art on deck dynamic interface analysis”, American helicopter society,1999
[19] 賴志群, 蔡文祥"利用電腦視覺技術以圓形資訊作物體定位之研究及其在運載工具自動化和虛擬實境之應用”,交大資科所博士論文, 1999
[20] 陳永名, 王怡仁: “直昇機即時模擬及性能分析”, 淡江大學航太工程所碩士論文, 2002
[21] 林哲生, “利用FPGA晶片實現無人飛行載具姿態控制系統”,國立成功大學航空太空工程研究所博士論文,2000
[22] 陳德徽,“以DSP晶片實現飛彈導控整合電路 ”,國立成功大學航空太空工程研究所碩士論文,2004
[23] 許東榮, “應用DSP、FPGA及GPS模組實現無人飛行載具之自動導航駕駛系統” 國立成功大學航空太空工程研究所碩士論文,2002
[24] 邱岱偉, “直昇機動態模擬的建立” 國立成功大學航空太空工程研究所碩士論文,1998
[25] 張伯偉, “直昇機的六自由度非線性 控制” 國立成功大學航空太空工程研究所碩士論文,1998
[26] 劉如豐, “直昇機飛行控制與非線性模擬” 國立成功大學航空太空工程研究所碩士論文,1999
[27] 孔健君,張伯偉,李金龍 , “直昇機起降之動態系統模擬” ,經濟部九十三年度科技專案研發成果,船舶技術發展第二期四年計畫,中正理工學院航空系與聯合船舶設計發展中心,2004