This paper deals with the computer analysis of a particular class of d
eployable structures, which we have developed over recent years. These
structures consist only of rods, hindged together to form a deployabl
e backbone, of some passive cables, which are slack when the backbone
is fully or partially folded but become taut when it is fully deployed
, and one or more active cables, which activate deployment and set up
suitable states of prestress, once the structure is in its fully deplo
yed configuration. We discuss one aspect of the computer analysis of t
hese structures, namely the task of setting up the equilibrium and fle
xibility matrices required for the deployment, prestressing and struct
ural response computations of three macro-elements: the active cable,
i.e. a slender, constant-tension element consisting of two or more str
aight segments; the pantograph unit, consisting of two coplanar, strai
ght beams joined by a shear connector; and the backbone module for the
octahedral mast, which consists of a flat, square cross of rods and a
n additional rod going through a pivot-and-slider joint at the centre
of the cross. Compact matrices for these elements are derived using a
recently developed matrix reduction technique. Three applications of t
hese macro-elements are given, illustrating their use in simple deploy
able structures.