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7/26/2019 1314sem1finalexam_soln-cntrl
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SEE 3113
Question 1
a)
i) The exponential term increases indefinitely
ii) No. That will only be the case if there is no sign change from ROZ
downwards.
iii) The system is unstable
b)
i) The system is unstable because of the negative sign occurred in the
characteristic equation.
ii)
S5 1 4 3
S4 -1 -4 -2
S3 1 0
S2
41
-2 0
S1
41
412 2
+
0 0
S
0
-2 0 0
3 right hand-plane, 2 left hand-plane. The systemis unstable.
c) Since the system oscillates, it is marginally stable. The characteristic equation
of the system becomes:
1 +( + 2)
3 +
2 + 3
+ 2
= 0
Or 3 + 2 + ( + 3) + 2( + 1) = 0
Rouths
s3
1 K+3
s2
p 2(K+1)
s1
(
+ 3)
2(
+ 1)
0
s0
2(K+1)
1
1
1
3
3
1
2
2
1
1
2
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SEE 3113
At marginal value of K (+3)2(+1) = 0Or
=2(+1)+3
Again at this value of p,
() =2 + 2( + 1) = 0Or
2 =2( + 1) = 2( + 1)
Given =2.5rad/sec. Therefore:
2(+1) = 2.5[1mark]
= 2( + 1)6.25
Substitute equation (1) into (2)2(+1)+3 =2(+1)6.25 K=3.25Therefore
p=2(3.25+1)/6.25= 1.36
(2)
1
1
2
2
1
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SEE 3113
Question 2
a)
By looking at the locations of the open loop poles and zeros. If there are some
on the LHP and some on the RHP, so the root locus will cross the imaginary
axis.
b)
()() = (+1)(+5)(+1)+(62)+5+2Then,
s2 K + 1 5K + 2
s1 6K 2 0
s0 5K + 2 0
Therefore K > 0.333
From auxiliary equation and substituting K = 0.333,
43 2 +113 = 0 = 1.66
c)
i. K = 0: closed loop poles = 1+j ; 1-j
ii. K -> infinity: closed loop poles = -1 ; -5
iii. 2 branches
iv. symmetrical about real axis
v. no asymptote angle
vi. no asymptotes crossings
vii locus on real axis : between -5 and -1
viii Departure angles = 180 90 + 26.6 + 9.5 = 126.1
ix jw-crossings : from part (b), s =1.66x
. (+1)(+5)(2+2) = 0solving this will obtain 1.325 and -2.075so the break-in point is at -2.075
therefore the root locus:
2
1
1.5
1.5
2
1
1
2
1
2
1
2
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SEE 3113
d)
From the root locus, if the damping ratio is 0.6
the dominant poles are at
1.13
1.52
and the value of K = 1.14
-5 -4 -3 -2 -1 0 1-2
-1.5
-1
-0.5
0
0.5
1
1.5
2
Root Locus
Real Axis
ImaginaryAxis
2
2
3
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SEE 3113
Question 3
a)
b) A vehicle speed control system is shown in Figure Q3b.
2
11
2
2
0.5
1
0.5
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SEE 3113
c) Roughly sketch the root locus of the uncompensated and compensated systems
in part (b) above.
5
2
2
1
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SEE 3113
2.5
2.5
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SEE 3113
Question 4
a)
i) A measurement of output response of a system in frequency domain. The
output response consists of the magnitude and phase values as the
frequency is varied.
ii) By obtaining the gain margin and phase margin. The system is said to
stable if the gain and phase margins are positive.
b)
i) By using the straight line approximation methods, plot the Bode plot of the
open-loop system for K= 1.
ii) Gain Margin = 53.2 dB
Phase Margin = 91.6
iii)Stable. Positive values of GM and PM
iv)The value of gain Kneeded is 40.3 dB
-200
-150
-100
-50
0
50
Magnitude(dB)
10-2
10-1
100
101
102
103
104
-270
-225
-180
-135
-90
-45
Phase(deg)
Bode Diagram
Frequency (rad/sec)
1.5
1.5
7
7
1
1
2
2
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SEE 3113
v)
Bode Diagram
Frequency (rad/sec)
10-2
10-1
100
101
102
103
104
-270
-225
-180
-135
-90
-45
System: G1
Phase Margin (deg): 44.6
Delay Margin (sec ): 0.0652
At frequency (r ad/sec): 11.9
Closed Loop Stable? Yes
Phase(de
g)
-150
-100
-50
0
50
100
System: G1
Gain Margin (dB): 12.9
At frequency (r ad/sec): 27.2
Closed Loop Stable? Yes
Magnitude(dB) 2
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SEE 3113
Question 5
a)
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SEE 3113
b)