First consider rotation predominantly about the third principal axis, writing . To first order the third Euler equation gives , while the transverse components satisfy
Therefore
and the same equation holds for .
Order the principal moments as . The coefficient above is negative, so perturbations about axis three oscillate and remain bounded. Cyclically applying the same linear stability of principal-axis rotation calculation about axis one gives
so that rotation is also stable. About axis two, however,
which has an exponentially growing solution. Thus the intermediate axis theorem gives