基于数字孪生的机身对接精度优化控制方法
赵永胜,赵志勇,李迎,张涛
Optimal control method of fuselage docking accuracy based on digital twin
Yong-sheng ZHAO,Zhi-yong ZHAO,Ying LI,Tao ZHANG
表 3
对接后机身筒段坐标
Tab.3
Coordinates of fuselage barrel section after docking
序号
$X$
/mm
$Y$
/mm
$Z$
/mm
1
−67.851
134.420
−272.060
2
−86.006
268.002
76.409
3
−208.747
930.715
188.840
4
−270.093
1162.814
−103.943
5
−1170.726
−69.842
−252.045
6
−1214.856
201.168
211.063
7
−1312.421
737.478
194.271
8
−1367.247
1001.686
−265.625