An optimal method of posture adjustment in aircraft fuselage joining assembly with engineering constraints
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DOI: 10.1016/j.cja.2017.05.006
Abstract: Abstract Posture of an aircraft fuselage can be evaluated based on the coordinate values of measure points fixed on the aircraft fuselage in aircraft final assembly. Posture adjustment is carried out by rotation and translation… read more here.
Keywords: aircraft; aircraft fuselage; posture adjustment;