The differential equation for the constrained center of gravity pitching motion of an airplane is Δä + 6 Δά + 36 Δα=3.6
Posted: Fri Jul 01, 2022 6:39 am
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.