本文選題：性能軟件 + 審定著陸距離��； 參考：《中國民用航空飛行學(xué)院》2016年碩士論文

【摘要】：飛機性能軟件是航空公司飛行運行中飛機性能參數(shù)的計算軟件,它利用飛機和發(fā)動機特性參數(shù),考慮機場和航路信息計算飛機飛行性能(包括起飛、爬升、巡航、下降和著陸等性能),它保障了航空公司飛行運行的經(jīng)濟性和安全性。目前我國主流機型的性能軟件均由波音、空客公司提供,我國對其核心技術(shù)并未完全掌握。隨著我國生產(chǎn)制造自主商用大飛機的迫切需求,研發(fā)一款穩(wěn)定性,準確性,自主性,易用性都比較好的國產(chǎn)大飛機性能軟件顯得非常重要。整個飛機性能軟件包括的內(nèi)容非常多(如起飛,爬升越障,巡航,下降以及著陸等),本文以飛機性能軟件中的著陸距離模塊為基礎(chǔ),重點是對著陸距離計算方法的研究,特別是結(jié)合中國民航相關(guān)的法律、規(guī)章(CCAR25, CCAR121等)深入研究了審定著陸距離和實際著陸距離的算法,并根據(jù)國產(chǎn)某飛機氣動力數(shù)據(jù)庫和推力數(shù)據(jù)庫等參數(shù)設(shè)計新的著陸數(shù)學(xué)模型及計算方法,并根據(jù)每一段的建模方式給出計算方法和算法流程。最后本文根據(jù)民航咨詢通告里到達時著陸距離評估的實際要求,對到達時著陸距離進行計算、分析和評估。
[Abstract]:Aircraft performance software is the calculation software of aircraft performance parameters in flight operation of airlines. It uses aircraft and engine characteristic parameters to calculate aircraft flight performance (including take-off, climb, cruise, etc.) considering airport and flight path information. Performance such as descent and landing ensures the economy and safety of airline flight operations. At present, the performance software of the mainstream aircraft is provided by Boeing and Airbus, but the core technology is not fully grasped in our country. With the urgent need of manufacturing autonomous commercial aircraft in our country, it is very important to develop a domestic large aircraft performance software with good stability, accuracy, autonomy and ease of use. The whole aircraft performance software includes a lot of contents (such as take-off, climb, cruise, descent and landing, etc.). This paper is based on the landing distance module in the aircraft performance software, focusing on the research of the landing distance calculation method. In particular, combined with the relevant laws and regulations of China's civil aviation, CCAR25, CCAR121, etc.), the algorithms for determining the landing distance and the actual landing distance are studied in depth. A new landing mathematical model and calculation method are designed according to the parameters such as aerodynamic database and thrust database of an aircraft made in China, and the calculation method and algorithm flow are given according to the modeling method of each section. Finally, according to the actual requirements of landing distance assessment in civil aviation advisory notice, the landing distance at arrival is calculated, analyzed and evaluated.
【學(xué)位授予單位】：中國民用航空飛行學(xué)院
【學(xué)位級別】：碩士
【學(xué)位授予年份】：2016
【分類號】：V212.131

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本文編號：1975102