The linear analysis of a uniform pantographic deployable column shows that,
in bending, its behavior is very similar to that of an equivalent solid co
lumn, whereas under axial loading the two columns display distinct differen
ces in their force and deformation distributions. The total change in the h
eight of a particular pantographic unit in the deployable structure consist
s of two parts, one due to relative rotation of bars in the unit, the other
to their bending. To account for configuration changes, the internal force
s must satisfy the equilibrium of each unit "after rotation." The additiona
l pantographic unit deformation due to bending of bars is found to be based
on these forces. The set of equilibrium and nonlinear deformation equation
s is solved iteratively. The "deformation-controlled" approach for solving
this system of equations shows the load maximum in the equilibrium paths th
at corresponds to the snap-through buckling of the top pantographic unit. I
t is found that the change in the number of units in the column introduces
only minor differences in the equilibrium paths as long as the column heigh
t and degree of deployment are kept constant. The axial stiffness of the pa
ntographic column is greatly increased and the snap-through buckling consid
erably postponed if just one additional constraint is introduced, namely th
e horizontal Link between the two nodes at a particular unit interface. The
optimal location of the Link is found.