The differential equation for the constrained center of gravity pitching motion of an airplane is Δä + 6 Δά + 36 Δα=3.6

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The differential equation for the constrained center of gravity pitching motion of an airplane is Δä + 6 Δά + 36 Δα=3.6

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The differential equation for the constrained center of gravity pitching motion of an airplane is Δä + 6 Δά + 36 Δα=3.6 Δδε 1) Rewrite this equation in the state space form. 2) Determine the eigenvalues of the A matrix.
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