Development and delivery of a flexible assembly system based on reverse engineering, tolerance analysis and Determinant Assembly Approach of wing box The system shall be capable to scan surfaces and holes of several areas along the wing. Using a virtual best fit software, holes and surfaces will be replicated on mating components in order to perform the assembly via the part to part assembly approach in virtual and real environments For the full topic description see the Call Text Document (Annex of Workplan) published with this call.
