天堂国产午夜亚洲专区-少妇人妻综合久久蜜臀-国产成人户外露出视频在线-国产91传媒一区二区三区

當(dāng)前位置:主頁 > 科技論文 > 航空航天論文 >

Y-12E型飛機(jī)性能算法研究與實(shí)現(xiàn)

發(fā)布時間:2018-10-29 13:14
【摘要】:近年來我國通用航空產(chǎn)業(yè)迅猛發(fā)展,許多縣市計劃新建或正在新建通用航空機(jī)場。在新建機(jī)場時,機(jī)場設(shè)計特別是跑道長度需要根據(jù)執(zhí)飛機(jī)型的性能來確定;在實(shí)際運(yùn)營中,承運(yùn)人也需要進(jìn)行飛機(jī)性能分析。通航飛機(jī)性能計算量的增加,帶來了開發(fā)通航機(jī)型飛機(jī)性能分析工具的迫切需求。運(yùn)-12E(Y-12E)型飛機(jī)是我國通航機(jī)場的常用機(jī)型,本文對其飛機(jī)性能分析方法展開研究,對工作量大、耗時長、易出錯的傳統(tǒng)人工查詢飛機(jī)性能手冊的計算方式進(jìn)行改進(jìn)。以Y-12E型飛機(jī)飛行手冊為計算依據(jù),以中國民用航空規(guī)章(CCAR-23部)中通勤類飛機(jī)適航規(guī)定為規(guī)范,并結(jié)合成熟的飛機(jī)性能理論,研究開發(fā)了Y-12E型飛機(jī)性能分析軟件。論文首先對Y-12E型飛機(jī)的起飛性能、著陸性能以及飛行計劃進(jìn)行分析。在飛機(jī)性能分析基礎(chǔ)上,對飛機(jī)性能計算涉及到的有關(guān)數(shù)據(jù)處理和算法展開研究;在Y-12E型飛機(jī)性能數(shù)據(jù)的處理中,為將紙質(zhì)圖表進(jìn)行數(shù)字化處理,利用Windows屏幕坐標(biāo)與圖像坐標(biāo)的轉(zhuǎn)換關(guān)系,開發(fā)了一套紙質(zhì)圖表的數(shù)字采樣工具,實(shí)現(xiàn)了圖表的導(dǎo)入、標(biāo)定、數(shù)據(jù)讀取和采集功能,加快了圖表的數(shù)字化處理速度;進(jìn)一步提出使用MATLAB自帶的曲線擬合工具箱進(jìn)行數(shù)據(jù)補(bǔ)全的方法,使用三角剖分算法和重心插值法進(jìn)行插值計算,并利用MATLAB自帶scarreredInterpolant函數(shù)進(jìn)行方法和結(jié)果驗(yàn)證。論文接著進(jìn)行Y-12E飛機(jī)性能軟件的開發(fā),該軟件主要包括機(jī)場管理、起飛性能、著陸性能和飛行計劃四個模塊,詳細(xì)分析了每個模塊的功能和計算方法;基礎(chǔ)性能表和機(jī)場信息采用SQLite數(shù)據(jù)庫存儲;整個軟件利用C++語言在Qt框架下開發(fā)完成,模塊化的架構(gòu)開發(fā)思路保證了軟件后續(xù)的維護(hù)和擴(kuò)展。最后,論文分別以具體的實(shí)例,對起飛模塊、著陸模塊、飛行計劃模塊進(jìn)行驗(yàn)證,得到的計算結(jié)果準(zhǔn)確,說明Y-12E型飛機(jī)性能計算軟件中性能計算方法無誤,可以用做Y-12E型飛機(jī)性能分析工具。
[Abstract]:In recent years, China's general aviation industry has developed rapidly. Many counties and cities plan to build or are building new general aviation airports. When a new airport is built, the design of the airport, especially the length of the runway, should be determined according to the performance of the aircraft, and in actual operation, the carrier also needs to analyze the performance of the aircraft. With the increase of aircraft performance calculation, there is an urgent need to develop aircraft performance analysis tools. Yun-12E (Y-12E) aircraft is a common type of aircraft in China's navigable airport. This paper studies the performance analysis method of its aircraft, and improves the traditional manual calculation method of aircraft performance, which is time-consuming, time-consuming and error-prone. Based on the flight manual of Y-12E aircraft, the airworthiness regulations of commuter aircraft in China Civil Aviation regulations (CCAR-23), and the mature aircraft performance theory, a performance analysis software for Y-12E aircraft is developed. Firstly, the takeoff performance, landing performance and flight plan of Y-12 E aircraft are analyzed. On the basis of aircraft performance analysis, the data processing and algorithm involved in aircraft performance calculation are studied. In the processing of Y-12E aircraft performance data, in order to digitize the paper chart, a set of digital sampling tools of paper chart is developed by using the conversion relationship between Windows screen coordinate and image coordinate, and the chart is imported and calibrated. The function of data reading and collecting speeds up the digitization of charts and graphs. Furthermore, the method of data complement with curve fitting toolbox of MATLAB is put forward, the interpolation calculation is done by triangulation algorithm and barycenter interpolation method, and the method and result are verified by MATLAB scarreredInterpolant function. The thesis then develops Y-12E aircraft performance software, which mainly includes four modules: airport management, take-off performance, landing performance and flight plan. The functions and calculation methods of each module are analyzed in detail. The basic performance table and airport information are stored in SQLite database, and the whole software is developed with C language under the framework of Qt. The modular framework development idea ensures the subsequent maintenance and extension of the software. Finally, the paper verifies the take-off module, landing module and flight plan module with specific examples, and the result is accurate, which shows that the performance calculation method of Y-12E aircraft performance calculation software is correct. Can be used as Y-12 E aircraft performance analysis tool.
【學(xué)位授予單位】:中國民航大學(xué)
【學(xué)位級別】:碩士
【學(xué)位授予年份】:2016
【分類號】:V212.13

【相似文獻(xiàn)】

相關(guān)期刊論文 前10條

1 覺謀凱;曹義華;張瑞民;;降雨對飛機(jī)性能影響的計算分析[J];飛行力學(xué);2010年03期

2 陳治懷;趙煒;;基于飛機(jī)性能軟件的飄降越障檢查軟件開發(fā)[J];中國民航大學(xué)學(xué)報;2007年S1期

3 司古;聶榮;;一本罕見的日本飛機(jī)性能手冊[J];航空知識;2007年12期

4 尹湛;陳曦光;;從飛機(jī)性能的角度談機(jī)型與航線的匹配[J];中國民用航空;2013年04期

5 孫石磊;谷潤平;;《飛機(jī)性能工程》精品課程網(wǎng)站的設(shè)計與建設(shè)[J];保定學(xué)院學(xué)報;2010年03期

6 包曉丹;段煉;;中川機(jī)場氣象條件對飛機(jī)性能的影響[J];空中交通管理;2010年01期

7 易榮華;蒙皮劃傷對飛機(jī)性能和壽命的影響[J];洪都科技;1995年01期

8 姜長英;一次失敗的飛機(jī)性能測驗(yàn)[J];航空史研究;1995年04期

9 李旭;王玉;;民用飛機(jī)飄降總軌跡計算分析[J];中國民航大學(xué)學(xué)報;2008年03期

10 謝春生;趙煜;李海斌;;飛機(jī)選型應(yīng)進(jìn)行的航線分析研究[J];中國民航飛行學(xué)院學(xué)報;2009年05期

相關(guān)會議論文 前2條

1 任慶磊;林麒;;等離子體改善飛機(jī)性能的應(yīng)用[A];福建省科協(xié)第四屆學(xué)術(shù)年會提升福建制造業(yè)競爭力的戰(zhàn)略思考專題學(xué)術(shù)年會論文集[C];2004年

2 任慶磊;林麒;;等離子體改善飛機(jī)性能的應(yīng)用[A];福建省科協(xié)第四屆學(xué)術(shù)年會——提升福建制造業(yè)競爭力的戰(zhàn)略思考專題學(xué)術(shù)年會論文集[C];2004年

相關(guān)碩士學(xué)位論文 前2條

1 邢洪亞;Y-12E型飛機(jī)性能算法研究與實(shí)現(xiàn)[D];中國民航大學(xué);2016年

2 喬為奇;飛機(jī)性能工程圖數(shù)字化處理與應(yīng)用[D];山東大學(xué);2006年



本文編號:2297790

資料下載
論文發(fā)表

本文鏈接:http://sikaile.net/kejilunwen/hangkongsky/2297790.html


Copyright(c)文論論文網(wǎng)All Rights Reserved | 網(wǎng)站地圖 |

版權(quán)申明:資料由用戶c6058***提供,本站僅收錄摘要或目錄,作者需要刪除請E-mail郵箱bigeng88@qq.com