Fitting method for optimal position and attitude of large aircraft component

The invention discloses a fitting method for the optimal position and posture of a large part of an airplane, and relates to the technical field of airplane digital assembly. In the actual situation, the situation that the feature points do not meet the permitted out-of-tolerance range all the time...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	XIONG XILIN, CAI MING, GUO HONGDA, WANG FEI, ZHOU WENQIANG, WANG XIAN, YE CHUNYAO, LI BIN, LIU SHUNTAO, JIANG YUANYUAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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