In this paper, an efficient reliability method is proposed for space f
ramed structures. It is based on linearization of the mechanical behav
iour. The elastic-plastic behaviour of material is piecewise linearize
d by a plastic criterion taking into account the interaction of intern
al forces. The buckling effect is represented by using an equivalent n
egative strain-hardening, introduced to the material model. In order t
o identify the negative strain-hardening parameters, a powerful method
is given. The proposed model also takes into account the unloading of
members and the behaviour at criterion singular points. The structura
l reliability is estimated by the safety margin concepts. Numerical ex
amples show the high performance of the model, verified by a good prec
ision and a very tow computational time.