“…; qg. In particular, the wing skin-to-spar adhesive joints are recognized as the most fatigue-sensitive structural elements of a lightweight composite UAV because the progressive debonding, evolving from the wing-root along these joints, can compromise the global aeroelastic performance of the vehicle (Bauchau & Loewy, 1997;Styuart, Demasi, Livne, & Lin, 2008;Styuart, Demasi, Livne, & Mor, 2011;Styuart et al, 2007;Wang, Inman, & Farrar, 2005). All probabilistic information necessary to fully embed and execute this analysis step within the proposed SHM-DP framework are contained in the joint PDF of the load intensity measure vector denoted as f IM (im).…”