This paper discusses the optimal geometry for maximum stiffness of controll
ed truss-type structures subjected to a class of unknown disturbances, unde
r a constant volume constraint. The stiffness is defined by a quadratic fun
ction of the worst distortion at the controlled degrees of freedom after ap
plying optimal control. The disturbance is arbitrary but is limited by a qu
adratic bound. Herein, the design variables are the spatial coordinates of
a predetermined set of nodes. Based on earlier publications, it is indicate
d that if the structure is controlled by N-c ideal actuators this min- max
problem is equivalent to minimizing the Nc+1 th singular value of the distu
rbance influence matrix. This implies that the first N-c singular modes are
taken care of by the control system. Consequently the designed structures
are often highly unstable without control. A methodology is presented to de
sign sub-optimal structures which addresses this problem. In order to allev
iate the effects of a possible failure of the control system, limits on the
levels of the lower singular values are incorporated in the design process
. Numerical examples illustrate the approach and indicate clearly the benef
icial effect of this technique which increases the stiffness of the structu
re while maintaining stability in the case of a breakdown of the control sy
stem. (C) 2001 Published by Elsevier Science Ltd.