The development and utilization of an uncertainty model for structures
that undergo a change in operational environment is presented. The mo
tivating application is the development of an on-orbit (0-g) uncertain
ty model for structural central based solely an ground (1-g) modeling
and experimentation, although other applications can be used. A parame
tric uncertainty model (mean errors and bounds on modal parameters) is
developed for a nominal environment and then localized to specific de
grees of freedom (mass and stiffness uncertainties) using a first-orde
r sensitivity method. The nominal mass and stiffness uncertainties are
then projected into a modified environment to create an analogous, mo
dified uncertainty model. The middeck active control experiment is int
roduced to verify the prediction of a space-based uncertainty model.