本文選題：LabVIEW + IMA　； 參考：《西安工業(yè)大學(xué)》2017年碩士論文

【摘要】：航空電子系統(tǒng)在飛機(jī)中占有十分重要的地位,伴隨我國(guó)航空航天事業(yè)的發(fā)展,綜合模塊化航空電子系統(tǒng)(IMA)的功能檢測(cè)和故障排查越發(fā)顯示出其重要性。自動(dòng)檢測(cè)系統(tǒng)的設(shè)計(jì)和研發(fā)也受到了國(guó)內(nèi)外專(zhuān)家的高度重視,虛擬儀器技術(shù)的發(fā)展為我們提供了快捷、方便的技術(shù)手段,我們可以運(yùn)用虛擬儀器技術(shù)靈活的組建各種自動(dòng)測(cè)試系統(tǒng)以達(dá)到硬件資源和軟件資源的共享及使用。論文以中航工業(yè)某研究所航空電子系統(tǒng)中航空控制板故障自動(dòng)檢測(cè)平臺(tái)的研發(fā)為背景,設(shè)計(jì)出了一種航空控制板故障自動(dòng)檢測(cè)系統(tǒng)。經(jīng)過(guò)對(duì)比和研究國(guó)內(nèi)外檢測(cè)平臺(tái)的搭建方法,本文提出了一種基于PXI總線、PXI機(jī)箱、光纖通信設(shè)備、NI板卡、LabVIEW8.0專(zhuān)業(yè)開(kāi)發(fā)板,及LM3S600的航空控制板故障檢測(cè)系統(tǒng)通用平臺(tái),該平臺(tái)能夠?qū)崿F(xiàn)設(shè)備的自動(dòng)檢測(cè)及故障定位,將以太網(wǎng)作為媒介傳送故障信息至相關(guān)工作人員處,方便工作人員從遠(yuǎn)端完成設(shè)備故障狀態(tài)確認(rèn)、故障排查等工作。這對(duì)工程師完成故障排查及檢修工作帶來(lái)了極大的便利性,提高了人員工作效率,同時(shí)也為航空電子設(shè)備的運(yùn)行提供了良好的保障。硬件設(shè)計(jì),依據(jù)檢測(cè)綱要和待測(cè)試項(xiàng)的具體指標(biāo)設(shè)計(jì)出該測(cè)試平臺(tái)。以NI板卡集成為硬件基礎(chǔ),平臺(tái)設(shè)計(jì)包括基于LabVIEW的上位機(jī)監(jiān)控程序的開(kāi)發(fā)、PXI機(jī)箱及光纖通信套件的選用、測(cè)試結(jié)果遠(yuǎn)端傳輸設(shè)計(jì)、傳遞信息媒介選擇等。用于新老設(shè)備間進(jìn)行匹配的電路板,我們自主設(shè)計(jì)了以LM3S600航空控制板為核心構(gòu)成的電子負(fù)載板以完成該功能。軟件設(shè)計(jì),在LabVIEW8.0專(zhuān)業(yè)開(kāi)發(fā)版的軟件環(huán)境下,進(jìn)行系統(tǒng)軟件的設(shè)計(jì)與調(diào)試。軟件界面能夠直觀反映設(shè)備的硬件配置及功能控制,能夠使得狀態(tài)機(jī)和系統(tǒng)有機(jī)的結(jié)合在一起,從而用LabVIEW完成了軟件主要框架的搭建工作。分層調(diào)用可以使測(cè)試子項(xiàng)程序模塊得到動(dòng)態(tài)控制,基于Access的故障定位查詢,可快速準(zhǔn)確的定位到故障點(diǎn)。同時(shí)系統(tǒng)可將檢測(cè)到的數(shù)據(jù)進(jìn)行分析,并將結(jié)果實(shí)時(shí)顯示和儲(chǔ)存。測(cè)試數(shù)據(jù)的遠(yuǎn)程傳輸,我們可通過(guò)Lab VIEW 的 Web Publish Tool 得以實(shí)現(xiàn)。該測(cè)試設(shè)備的成功研發(fā)與應(yīng)用,為我國(guó)航空電子系統(tǒng)測(cè)試領(lǐng)域的發(fā)展起到了非常積極的作用。
[Abstract]:Avionics system occupies a very important position in aircraft. With the development of China's aviation and space industry, the function detection and troubleshooting of integrated modular avionics system (IMA) is becoming more and more important. The design and research and development of the automatic detection system have also been highly valued by the experts at home and abroad, and the development of virtual instrument technology. It provides us with quick and convenient technical means. We can use virtual instrument technology to build various automatic test systems to achieve the sharing and use of hardware resources and software resources. The paper is based on the research and development of the aircraft control board fault automatic detection platform in the avionics system of a Research Institute of China aeronautical industry. A kind of automatic fault detection system for air control board is developed. After comparing and studying the construction methods of detection platform at home and abroad, this paper presents a general platform based on PXI bus, PXI chassis, fiber communication equipment, NI card, LabVIEW8.0 professional development board, and LM3S600 for aviation control board barrier detection system. This platform can implement equipment. Automatic detection and fault location, the Ethernet as the medium to transmit fault information to the relevant staff, convenient staff from the far end to complete the equipment fault status confirmation, troubleshooting and other work. This has brought great convenience to the engineer to complete the troubleshooting and maintenance work, improved the efficiency of the personnel and also for the voyage. The operation of the air electronic equipment provides a good guarantee. The hardware design is designed according to the testing outline and the specific indexes of the test items. The hardware base is integrated with the NI card. The platform design includes the development of the monitor program based on the LabVIEW, the selection of the PXI chassis and the optical fiber communication suite, and the remote transmission of the test results. Design, transmission of information media selection, and so on. Used for matching circuit board between new and old equipment, we independently designed the electronic load board composed of LM3S600 air control board as the core to complete this function. Software design and software design and debugging under the software environment of LabVIEW8.0 professional development version. The software interface can be straight. The view reflects the hardware configuration and function control of the equipment, which can combine the state machine and the system organically, so as to complete the construction of the main framework of the software with LabVIEW. The hierarchical call can make the test sub program module get dynamic control, based on the Access fault location query, and can quickly and accurately locate the fault point. The system can analyze the detected data and display and store the results in real time. The remote transmission of the test data can be realized through the Web Publish Tool of Lab VIEW. The successful development and application of the test equipment have played a very active role in the development of China's avionics system testing field.
【學(xué)位授予單位】：西安工業(yè)大學(xué)
【學(xué)位級(jí)別】：碩士
【學(xué)位授予年份】：2017
【分類(lèi)號(hào)】：V243;TP311.52

【參考文獻(xiàn)】

相關(guān)期刊論文 前6條

1 李勁;;我國(guó)未來(lái)空天飛機(jī)綜合電子信息系統(tǒng)的發(fā)展建議[J];電訊技術(shù);2010年03期

2 梁德文;;戰(zhàn)斗機(jī)航空電子系統(tǒng)最新的發(fā)展趨勢(shì)—網(wǎng)絡(luò)化[J];電訊技術(shù);2008年06期

3 霍曼,鄧中衛(wèi);國(guó)外軍用飛機(jī)航空電子系統(tǒng)發(fā)展趨勢(shì)[J];航空電子技術(shù);2004年04期

4 霍曼;綜合航空電子技術(shù)發(fā)展展望[J];航空電子技術(shù);2000年03期

5 周進(jìn);;21世紀(jì)的航空電子系統(tǒng)-PAVE PACE計(jì)劃[J];火控雷達(dá)技術(shù);1990年04期

6 鄒宇;航空電子系統(tǒng)的綜合設(shè)計(jì)與火力控制系統(tǒng)[J];機(jī)載火控;1984年03期

相關(guān)博士學(xué)位論文 前1條

1 張朋;機(jī)載雷達(dá)信號(hào)動(dòng)態(tài)實(shí)時(shí)測(cè)試技術(shù)研究[D];電子科技大學(xué);2015年

相關(guān)碩士學(xué)位論文 前10條

1 程政;航空電源系統(tǒng)測(cè)試平臺(tái)控制技術(shù)研究[D];南昌航空大學(xué);2015年

2 周濤;通用測(cè)試軟件開(kāi)發(fā)平臺(tái)測(cè)試子系統(tǒng)的設(shè)計(jì)與實(shí)現(xiàn)[D];電子科技大學(xué);2014年

3 張浩然;基于LabVIEW的小型無(wú)人機(jī)地面站系統(tǒng)研究與設(shè)計(jì)[D];長(zhǎng)春理工大學(xué);2014年

4 楊?lèi)?ài)華;基于Labview的車(chē)載電子電氣系統(tǒng)測(cè)試平臺(tái)設(shè)計(jì)[D];河北工業(yè)大學(xué);2013年

5 陶怡;基于IPC的航空嵌入式系統(tǒng)軟件測(cè)試研究[D];西安電子科技大學(xué);2013年

6 董天天;航空電子系統(tǒng)的測(cè)試的設(shè)計(jì)與實(shí)現(xiàn)[D];西安電子科技大學(xué);2013年

7 黃楷;飛控系統(tǒng)供電狀態(tài)綜合測(cè)試平臺(tái)方案設(shè)計(jì)[D];哈爾濱工業(yè)大學(xué);2012年

8 周彩霞;基于LabVIEW的航空發(fā)動(dòng)機(jī)附件試驗(yàn)器測(cè)控系統(tǒng)[D];西安科技大學(xué);2012年

9 鄧小松;航空電子設(shè)備測(cè)試系統(tǒng)設(shè)計(jì)[D];成都理工大學(xué);2012年

10 張國(guó)晉;基于FC-AE-ASM的航電測(cè)試接口的設(shè)計(jì)與實(shí)現(xiàn)[D];電子科技大學(xué);2012年

，

本文編號(hào)：2039040