In typical aircraft, longitudinal flight linearization can be modelled using a second- order system as in Figure Q3(a)(i). Figure Q3(a)(i) shows pole zero map on s- plane for the second-order system of the unit step. By referring to the pole-zero location, Determine the type of second-order response and sketch the nature of step response of the system. Solve for the damping ratio, Cand natural frequency, h. H) Find the values of percent overshoot, %OS and peak time, Tp in) Find the closed loop transfer function and calculate the unknown gains, K, and K. 0.2 K. Co) s(s+ 1) s+1 Figure Q3(a)(i) 5.44 2 4.41 5.44

In typical aircraft, longitudinal flight linearization can be modelled using a second- order system as in Figure Q3(a)(i). Figure Q3(a)(i) shows pole zero map on s- plane for the second-order system of the unit step. By referring to the pole-zero location, Determine the type of second-order response and sketch the nature of step response of the system. Solve for the damping ratio, Cand natural frequency, h. H) Find the values of percent overshoot, %OS and peak time, Tp in) Find the closed loop transfer function and calculate the unknown gains, K, and K. 0.2 K. Co) s(s+ 1) s+1 Figure Q3(a)(i) 5.44 2 4.41 5.44

Introductory Circuit Analysis (13th Edition)

13th Edition

ISBN:9780133923605

Author:Robert L. Boylestad

Publisher:Robert L. Boylestad

Chapter1: Introduction

Section: Chapter Questions

Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...

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