SOLVED: Problem 4. (2Pts) The longitudinal equations for an airplane having poor handling qualities follow. Use state feedback to provide stability augmentation so that the augmented aircraft has the following short- and long-period (phugoid) characteristics: Au 0.01 0.1 0 -32.2 Au Aw 0.40 -0.8 180 Aw -10 Aq  0.003 -0.5 Aq -2.8|8e Ae 0 4e 0 Ssp 0.6, Wnsp 3.0 rad/s Sp 0.05, Wn sp 0.1 rad/s using the Ackermann's Formula to design the feedback gain to locate the closed-loop eigenvalues:

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