matlab code:
clc;
clear all;
close all;
s=tf('s');
g1=-(2*s+1)*(0.6*s-2)/((0.5*s+1)*(0.6*s+2));
g2=-(2*s+1)*(0.1*s-2)/((0.5*s+1)*(0.1*s+2));
g3=-10/(s+10);
g4=-(s+6)/(s*(s^2+3*s+6));
gs=g1*g3*g4;% sluggish system open loop TF
gr=g2*g3*g4;% rapid system open loop TF
sys1=feedback(gs,1);% close loop TF for sluggish system
sys2=feedback(gr,1);% close loop Tf for rapid system
pole(sys1)% closed loop poles of sluggish system
pole(sys2)% closed loop poles of rapid system
rlocus(gs);
figure
rlocus(gr)
ans =
-9.4526 + 0.0000i
-4.5228 + 2.2595i
-4.5228 - 2.2595i
0.2793 + 2.0314i
0.2793 - 2.0314i
-0.3937 + 0.0000i
ans =
-19.6267 + 0.0000i
-10.7712 + 0.0000i
-3.8885 + 0.0000i
-0.1697 + 2.7880i
-0.1697 - 2.7880i
-0.3742 + 0.0000i


sluggish pilot:
The gain should be less than 0.65
rapid pilot:
The gain should be less than 1.2
PROBLEM 1 A plane system is depicted in Figure 1, Here, τ denotes the delay of the pilot. A sluggish pilot is denoted by t 0.6 and a rapid pilot is denoted by t-0.1. Other parameters of the system ar...