uest ion 1: The attached gure (acbode .pdf) shows the Bode magnitude diagrams for the transfer function of the longitudinal dynamics of an experimental aircraft. Longitudinal aircraft dynamics typically.r have two second-order modes: a low frequency \"phugoid mode" and a higher frequency \"short period mode" . There are also two zeros in the transfer function, at frequencies between the natural frequencies of the two modes. a.) Estimate from the diagram the location of the phugoid and short period poles in the complex plane. Determine as accurately as possible the damping ratios and oscillation frequencies of each of these modes. b.) If the input to this transfer function is a constant of magnitude A. what will the steady-state output be? Assume the low frequency phase is zero. If instead the low frequency phase is 180, what would the steady-state output be? Bushaglan