首页 | 本学科首页   官方微博 | 高级检索  
     检索      

飞机大部件对接中的位姿计算方法
引用本文:罗芳,邹方,周万勇.飞机大部件对接中的位姿计算方法[J].航空制造技术,2011(3):91-94.
作者姓名:罗芳  邹方  周万勇
作者单位:北京航空制造工程研究所
摘    要:在飞机的大部件对接中,为了达到较高的对接精度,需要准确地分析大部件的位姿,因此大部件位姿计算方法是首先需要解决的问题.本文简要介绍了奇异值分解法、三点法、最小二乘法计算位姿,并以三点法计算的结果作为最小二乘法的初值.比较了3种方法在点无误差和有误差时的部件拟合误差,分析了测量点的个数对部件拟合误差的影响,讨论了误差对部...

关 键 词:大部件对接  位姿计算  最小二乘法  奇异值分解法  三点法

Posture Calculating Algorithm in Large Aircraft Component Butt
Luo Fang,Zou Fang,Zhou Wanyong.Posture Calculating Algorithm in Large Aircraft Component Butt[J].Aeronautical Manufacturing Technology,2011(3):91-94.
Authors:Luo Fang  Zou Fang  Zhou Wanyong
Abstract:To satisfy the requirement of automated alignment and joining of fuselage sections and wings in digital assembly for an aircraft,component's posture calculating method is the first question that should be considered.There are three methods which can be used in posture calculating:single value decomposition,three point method and least square method.Three point method's result is used as the least square's initial value.The fitting error of the lease square method is discussed from point's number and point's...
Keywords:Large component butt Posture calculating The least square method Single value decomposition Three point method  
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号