5.2. For the roll response shown in Figure P5.2, estimate the aileron control power L 8a and the roll damping derivative Lp. Information on the characteristics of the airplane is in the figure. 6 4 P (t) [deg/sec] 2 0 0 1 FIGURE P5.2 Roll rate time history. Time sec V = 224 ft/sec S = 542 ft² b = 54 ft Ix = 42,273 slug/ft² Δδ. = 50 p = 0.00205 slug/ft³ 2 3