Modem limit-state design codes are based on limits of structural resis
tance. To determine the 'true' ultimate load-carrying capacity of spat
ial structures, an advanced analysis method which considers the intera
ction of actual behaviour of individual members with that of the struc
ture is required. In the present work, a large-displacement inelastic
analysis technique has been adopted to compute the maximum strength of
spatial structures considering both member and structure instability.
The actual behaviour of individual members in a spatial structure is
depicted in the form of an inelastic strut model considering member in
itial imperfections as 'enlarged' out-of-straightness. The maximum str
ength of the strut is computed based on a member with 'equivalent out-
of-straightness' so as to achieve the specification's strength for an
axially loaded column. The results obtained by the strut model are sho
wn to agree well with those determined using plastic-zone analysis. Th
e nonlinear equilibrium equations resulting from geometrical and mater
ial nonlinearities are solved using an incremental-iterative numerical
scheme based on generalised displacement control method. The effectiv
eness of the proposed advanced analysis over the conventional analysis
/design approach is demonstrated by application to several space truss
problems. The design implications associated with the use of the adva
nced analysis ape discussed. (C) 1997 Elsevier Science Ltd.