The nonlinear transfer behaviour of an assembled structure such as a l
arge lightweight space structure is caused by the nonlinear influence
of structural connections. Bolted or riveted joints are the primary so
urce of damping compared to material damping, if no special damping tr
eatment is added to the structure. Simulation of this damping amount i
s very important in the design phase of a structure. Several well know
n lumped parameter joint models used in the past to describe the dynam
ic transfer behaviour of isolated joints by Coulomb friction elements
are capable of describing global states of slip and stick only. The pr
esent paper investigates the influence of joints by a mixed experiment
al and numerical strategy. A detailed Finite Element model is establis
hed to provide understanding of different slip-stick mechanisms in the
contact area. An advanced lumped parameter model is developed and ide
ntified by experimental investigations for an isolated bolted joint. T
his model is implemented in a Finite Element program for calculating t
he dynamic response of assembled structures incorporating the influenc
e of micro-and macroslip of several bolted joints.