Aircraft Integrated 
Structural Health Assessment II
- Call Identifier FP7-AAT-2007-RTD-1 
Project Number: 212912


The safe use of complex engineering structures such as aircrafts can only be guaranteed when efficient means of damage assessment are in place. Whereas aircraft design is nowadays based on a damage tolerance approach and time based inspection cycles, it is envisaged that the large cost associated with this approach can be drastically reduced by switching to a condition based maintenance schedule. This does require continuous health monitoring capabilities using integrated sensing technology and autonomous damage assessment.

Presentations Open Project Meeting - 28 oktober 2011
Key-results in-brief
Introduction and Project Objectives
Publications and presentations
Co-ordinator contact details

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