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ID:32189223
大小:1.49 MB
页数:66页
时间:2019-02-01
《民用飞机巡航段航迹规划和制导方法分析》由会员上传分享,免费在线阅读,更多相关内容在学术论文-天天文库。
1、上海交通大学工学硕士学位论文ABSTRACTtheoptimizationmethodofcostfunctionaccordingtominimumdirectoperatecostisderived,andthecorrespondingcalculationmethodsofoptimizationtrajectoryofverticalflightprofilesforclimb,cruiseanddescentphaseareobtained.TheoptimaltrajectorycomputingprogramwritteninVCandMatlabisdeveloped,and
2、theoptimalflighttrajectoryforcruisephaseiscarriedoutwiththeperformancedateofaspecificaircraft.Keywords:Flightmanagementsystem,performanceoptimization,4Dguidance,optimizationtrajectory,realtimeplatform第IV页万方数据上海交通大学工学硕士学位论文目录目录摘要........................................................................
3、..........................................................................................IABSTRACT...................................................................................................................................................III第一章绪论..............................................
4、.....................................................................................................11.1研究背景和意义....................................................................................................................................11.2研究内容和方法.............................................
5、.......................................................................................21.3国内外研究现状....................................................................................................................................41.3.1水平航路优化研究现状......................................................
6、...........................................................41.3.2垂直剖面轨迹优化研究发展概况.................................................................................................51.4本文主要工作..................................................................................................................
7、......................6第二章飞机轨迹优化和四维制导相关原理及模型...................................................................................82.1飞机的水平航线动态寻优..........................................................
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