The forward transfer function G(s) with a H(s) feedback configuration of an uncompensated Basic Satellite Launching System is as shown in figures 1 and 2.A- in the picture B- Compute the percent overshoot, peak time and settling time, using second order approximation through pole zero cancellation and unity feedback configuration shown in figure 2.C- Summarise the results (a) and (b) in tabular form and comment on the stability of both systems based on time response graph for (a) and computed values in (b). % a)s = tf ('s');a = 4; b = 2; c = 2; d = 1; e = 10; f = 4;G = a* (s+d)/ (s * (s + c) * (s + b));H = el (s + f);figure()bode (G* H)grid onG1 = feedback (G, H);disp ('a')stepinfo (G1)figure()step (G1)grid on, legend ('with H (s)')% b)%uncompensated systemG2 = feedback (G, 1);%u sin g%u sin g pole zero canclellationK = 1.678 ^2 + 1.7214^2;G1_app = zpk ([ ], [−1. 6478 + 1. 7214i – 1. 6478 – 1. 7214i], k);disp ('b')stepinfo (G1_app)figure()step (G1_app)grid on, legend (with unity feedback')%c)%comparison G(s)=a(s+d)s(s+c)(s+b)H(s)=e(s+f)R(s)G(s)→ C(s)H(s)Figure 1: Uncompensated basic Satellite launching systemR(s)G(s)→ C(s)Figure 2: Uncompensated basic Satellite launching system with unity feedback

The Given Transfer function is GS=as+dss+cs+b HS=es+f The Time and frequency response of the…

Answered: The forward transfer function G(s) with…

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...

See similar textbooks

Related questions

Question

The forward transfer function G(s) with a H(s) feedback configuration of an uncompensated Basic Satellite Launching System is as shown in figures 1 and 2.

A- in the picture

B- Compute the percent overshoot, peak time and settling time, using second order approximation through pole zero cancellation and unity feedback configuration shown in figure 2.

C- Summarise the results (a) and (b) in tabular form and comment on the stability of both systems based on time response graph for (a) and computed values in (b).

% a)
s = tf ('s');
a = 4; b = 2; c = 2; d = 1; e = 10; f = 4;
G = a* (s+d)/ (s * (s + c) * (s + b));
H = el (s + f);
figure()
bode (G* H)
grid on
G1 = feedback (G, H);
disp ('a')
stepinfo (G1)
figure()
step (G1)
grid on, legend ('with H (s)')
% b)
%uncompensated system
G2 = feedback (G, 1);
%u sin g
%u sin g pole zero canclellation
K = 1.678 ^2 + 1.7214^2;
G1_app = zpk ([ ], [−1. 6478 + 1. 7214i – 1. 6478 – 1. 7214i], k);
disp ('b')
stepinfo (G1_app)
figure()
step (G1_app)
grid on, legend (with unity feedback')
%c)
%comparison

G(s)
=
a(s+d)
s(s+c)(s+b)
H(s)
=
e
(s+f)
R(s)
G(s)
→ C(s)
H(s)
Figure 1: Uncompensated basic Satellite launching system
R(s)
G(s)
→ C(s)
Figure 2: Uncompensated basic Satellite launching system with unity feedback

Expert Solution

Step by step

Solved in 4 steps with 3 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, electrical-engineering and related others by exploring similar questions and additional content below.

Similar questions