Derive the linearized equation-of-motion that describes flight around straight-and-level trim for the side force of Y and side velocity of v. Your answer must be entirely in terms of lateral-directional states. You must include all the relevant terms but not include any additional unneeded terms. Assume ato = 0 but uo #0 at trim. Y = m(i +ru-pu) Derive the linearized equation-of-motion that describes flight around straight-and-level trim for the side force of Y and side velocity of v. Your answer must be entirely in terms of lateral-directional states. You must include all the relevant terms but not include any additional unneeded terms. Assume ato = 0 but uo #0 at trim. Y = m(i +ru-pu)