5 (2 pts) The aircraft shown below has two degrees of freedom: sideslip angle (, expressed in rad, per unit rotation) and lateral displacement (y, expressed in ft, per unit translation). Say the resulting eigen solution yields the following results: @1,2 = On the following pictures, draw representative eigen vectors 0.9, 2.2 rad/s, and (mode shapes) for each of these 2 modes (draw on top of the below drawings), following the given sign convention. +Y SIGN CONVENTION mode 2: mode 1: +