Development and validation of a self-adaptive system for automated assembly of major composite aerostructures
Specific Challenge: An automated system shall be developed for the assembly of regional aircraft composite fuselage panels, by means of innovative features for recognition of actual position and shape of parts to be drilled, with the aim to generate the correct pattern of holes with “best fit” algorithm to be developed. Application will be the Read more about Development and validation of a self-adaptive system for automated assembly of major composite aerostructures[…]