Control system designing for correcting wing–fuselage assembly deformation of a large aircraft
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DOI: 10.1108/aa-01-2016-006
Abstract: Purpose In aircraft wing–fuselage assembly, the distributed multi-point support layout of positioners causes fuselage to deform under gravity load, leading to assembly difficulty and assembly stress. This paper aims to propose a hybrid force position… read more here.
Keywords: fuselage; wing fuselage; control; fuselage assembly ... See more keywords