A spin-stabilized spacecraft carrying liquid fuel in communicating res
ervoirs, such as METEOSAT Second Generation (MSG), may have its fueled
inertia properties significantly influenced by the phenomenon of inte
r-reservoir liquid migration driven by centrifugal forces. Previous au
thors have exposed this phenomenon in terms of a Wobble Amplification
Factor (WAF). We generalize this description to that of a Wobble Ampli
fication Tensor (WAT) and we consider the effect of reservoir alignmen
t errors. Most importantly, we demonstrate the importance of modeling
the migration of the total center of mass in the body-fixed frame, an
effect omitted in the previously published works.