成功大學博碩士論文系統

簡易檢索 / 詳目顯示

回結果列表

研究生：	林勇志 Lin, Yung-Jr
論文名稱：	透過控制區域網路之數位航電儀表系統 Digital Avionics using Control Area Network
指導教授：	林清一 Lin, Chin E.
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：	2007
畢業學年度：	95
語文別：	英文
論文頁數：	72
中文關鍵詞：	數位飛行儀表、飛機航電系統、航電匯流排系統
外文關鍵詞：	broadcast, flight data, small aircrafts, CAN bus
相關次數：	點閱：137 下載：3
分享至:	分享至facebook 分享至twitter

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

目前的小型飛機並未配備昂貴的高性能航電匯流排系統，然而基於性能提升的需求與成本的考量，以控制區域網路建構小型飛機航電系統是未來必要的發展方向。本論文探討控制區域網路在小型飛機上的應用，系統主要包含兩大功能，一為數位飛行儀表的改良與精進，另一為飛行資料在於監控端的軌跡重現與數據處理。本文從模擬與實驗混和驗證系統的功能，採用實測的飛行資料庫進行可行性模擬，再以高可靠度的CAN IP board、配合視窗設計進行測試，完成功能的驗證。視窗功能包含線上資訊的顯示，能同時執行錯誤訊息的偵測。本系統監控端設定為最高優先權的節點，可對整個匯流排作廣播與修正，以完成本論文在呈現區域網路匯流排操作與偵錯的能力。

At the present, the small aircrafts are not equipped with high performance, high cost avionics data bus system. Based on performance enhancement, CAN bus is one of the most qualified candidate for future implementation into small aircrafts. This thesis studies CAN bus system in application to small aircrafts for two function aspects: to improve flight instruments and to record flight data for performance recovery. This thesis verifies the system function capability from simulation and experiments. Some realist flight performance data from database are used for feasibility tests, and then high performance hardware CAN IP boards are introduced with suitable window displays for real experiment tests. The functions of windows display on line information, and execute fault detection at the same time. The monitor terminal is set as the highest priority node to broadcast all message and make revision the data bus operation to achieve CAN performance to small aircraft applications.

ABSTRACT	......................i
ABSTRACT IN CHINESE	......................ii
CONTENTS	......................iv
LIST OF FIGURES	......................vii
LIST OF TABLES	......................ix
CHAPTER I INTRODUCTION	......................1
          1.1 Motivation	......................1
          1.2 Research goal	......................4
          1.3 Overview of the thesis	......................4
CHAPTER II OVERVIEW ON SUPPORTING TECHNOLOGIES	......................5
          2.1 Control Area Network (CAN) bus	......................5
              2.1.1 History	......................5
              2.1.2 Protocol of CAN	......................7
          2.2 How CAN works [2]	......................10
              2.2.1 Data format of CAN [4]	......................10
              2.2.2 Standard format and Extended format Compatibility	......................12
              2.2.3 Bus lengths of CAN	......................13
          2.3 Comparison of data bus	......................13
              2.3.1 The Universal Asynchronous Receiver/Transmitter (UART)	......................13
              2.3.2 LIN (Local Interconnect Network)	......................16
              2.3.3 Compare of CAN, LIN, and UART	......................18
          2.4 CAN circuit board	......................19
          2.5 Avionics architecture	......................20
              2.5.1 Integrated Modular Avionics	......................21
              2.5.2 Line Replaceable Modules (LRMs)	......................22
          2.6 Summary of this chapter	......................23
          CHAPTER III AIRCRAFT INSTRUMENTS	......................24
          3.1 Aircraft instrument overview	......................24
              3.1.1 Principle of mechanical instrument	......................24
              3.1.2 Principle of gyroscopic instrument	......................25
          3.2. General flight instrument	......................26
              3.2.1. Air Speed Indicator (ASI)	......................27
              3.2.2 Attitude indicator (AI)	......................29
              3.2.3 Altitude indicator	......................29
              3.2.4 Turn coordinator	......................30
              3.2.5 Vertical speed indicator	......................30
              3.2.6 Heading indicator	......................30
          3.3 Electronic Flight Instrument	......................31
              3.3.1 Primary flight display (PFD)	......................31
              3.3.2 Multi-Function Display (MFD)	......................33
              3.3.3 Engine Indications and Crew Alerting System (EICAS)	......................33
              3.3.4 Document retrospection of digital flight instrument	......................33
          3.4 Spatial disorientation (SD) [15]	......................34
          3.5 Fight Instrument Design for Small Aircrafts	......................35
          3.6 Summary of this chapter	......................37
CHAPTER IV SYSTEM DESIGN AND ARCHITECTURE	......................39
          4.1 The test architecture	......................40
          4.2 Circuit Design of CAN IP Board	......................40
              4.2.1 Component function	......................42
              4.2.2 Handling of data stream	......................43
          4.3 Programming of the digital flight instrument	......................45
              4.3.1 Used tool	......................46
              4.3.2 Experiment architecture of PC node	......................46
              4.3.3 Arrangement of the interface	......................47
              4.3.4 Instrument setting function	......................49
              4.3.5 e-map	......................51
              4.3.6 Database	......................52
              4.3.7 Abnormal attitude warning display	......................52
          4.4 Summary of this chapter	......................55
CHAPTER V CAN DEMO MODULE TEST	......................56
          5.1 Data Receive experiment	......................56
              5.1.1 CAN demo module	......................57
              5.1.2 The e-map position test by GPS module	......................57
              5.1.3 The flight database test	......................58
              5.1.4 System test by G3	......................61
          5.2 Output experiment of PC node	......................63
          5.3 Summary of this chapter	......................66
CHAPTER VI CONCLUSIONS	......................67
REFERENCES	......................69
                                    

[1] Embedded Developers Pages, Available on website: http://hem.bredband.net/stafni/developer/frames.htm
[2] S. Bender, W. J. Fischer, A. Heinig, C. Kbhler, S, B. Schneider, “Multi-sensor controller with CAN bus interface”, Micro System Technologies, Potsdam, 1996.
[3] CAN in Automation (CiA), Privacy Policy, Available on website: http://www.can-cia.org/can/.
[4] Wikipedia, the free encyclopedia, Available on website:
http://en.wikipedia.org/wiki/OSI_model#Layer_1:_Physical_Layer.
[5] Mcore, M-CORE MMC2001 Reference Manual. Denver, Colo.: Motorola Literature Distribution, 1998.
[6] FUJITSU MICROCONTROLLERS, Available on website: http://www.fujitsu.com/emea/services/microelectronics.
[7] P. Conmy, M. Nicholson, J. McDermid, “Safety Assurance Contracts for Integrated Modular Avionics”, 8th Australian Workshop on Safety Critical Systems and Software, Canberra, CRPIT, Vol. 33, October 2003, pp. 69-78.
[8] ARINC Report 650, “Integrated Modular Avionics Packaging and Interfaces,” July 1994.
[9] Answers, encyclodictionalmanacapedia, Available on website: http://www.answers.com/topic/asi-operation-faa-png.
[10] CHELTON FLIGHT SYSTEMS, Available on website: http://www.cheltonflightsystems.com/version6_new_screens.htm.
[11] 簡良益、蔡長，(2001)，PaPaGo!SDK GIS 系統建置理論與實務，台北縣:研勤科技股份有限公司。
[12] Society of Automotive Engineers, (1988), “Design objectives for CRT displays for part 25 (transport) aircraft”, Aerospace Recommended Practice ARP 1874, Warrendale, PA.
[13] W. Sipes, C. S. Lessard, (2000), “A spatial disorientation survey of experienced Instructor pilots, Obtaining more complete information regarding the incidence and Prevalence of SD illusions”, Engineering in Medicine and Biology Magazine, 19(2), pp. 35-42.
[14] C. E. Lin, H. T. Lin. (July 2004), “Establishing a High Speed Interface in General Aircraft by Controller Area Network”, Master’s thesis, National Cheng Kung University, Tainan, Taiwan.

[15] J. Wynbrandt, AOPA (Aircraft Owners and Pilots Association) air safety foundation, (2004), Spatial Disorientation Confusion that Kills, Maryland.
[16] S. S. Krause, “Aircraft Safety: Accident Investigations, Analyses, & Applications”, The McGraw-Hill Companies, Inc., New York, 2003, ISBN 0-07-140974-2.
[17] I. N. Gleim, “Private Pilot Flight Maneuvers and Practical Test Prep.”, 3rd Edition, Gleim Publications, Inc., 2000, ISBN-13: 978-0917539855, pp. 19-31.
[18] I. Moi, A. Seabridge, “Civil avionics system”, London and Bury St Edmunds, UK. Professional Engineering Publishing Limited, 2003.
[19] Universitt Paderborn, E-learning Resources in Microelectronics, Available on website:
http://www.bolton.ac.uk/mind/paderborn/bus-systems/can-bus/can-bus.html.
[20] S. R. Holmes, A. Bunting, L. D. Brown,, L. K. Hiatt, G. M. Braithwaite, J. M Harrigan, (2003), “Survey of spatial disorientation in military pilots and navigators. Aviation, Space, and Environmental Medicine, Vol. 74, No. 9, September 2003, pp. 957-965.
[21] C. E. Lin, T. P. Chen, (July 2004), “Digital Aircraft Instrument System of Ultralight Aircraft with Digital Avionic”, Master’s thesis, National Cheng Kung University, Tainan, Taiwan.
[22] Plane crashes on Lanai, The small aircraft goes down in a remote area, Available on website: http://starbulletin.com/2001/06/15/news/story1.html

校內：2009-06-07公開
校外：2011-06-07公開

簡易檢索 / 詳目顯示

相關論文