Unit - 5
Frequency domain analysis-II
Q1) Sketch the bode plot for transfer function
G(S) =
A1)
Replace S = j
G(j=
This is type 0 system. So initial slope is 0 dB decade. The starting point is given as
20 log10 K = 20 log10 1000
= 60 dB
Corner frequency 1 = = 10 rad/sec
2 = = 1000 rad/sec
Slope after 1 will be -20 dB/decade till second corner frequency i.e 2 after 2 the slope will be -40 dB/decade (-20+(-20)) as there are poles
For phase plot
= tan-1 0.1 - tan-1 0.001
For phase plot
100 -900
200 -9.450
300 -104.80
400 -110.360
500 -115.420
600 -120.00
700 -124.170
800 -127.940
900 -131.350
1000 -134.420
The plot is shown in figure.
Fig: Magnitude Plot for G(S) =
Q2) For the given transfer function determine
G(S) =
Gain cross over frequency phase cross over frequency phase mergence and gain margin
A2)
Initial slope = 1
N = 1, (K)1/N = 2
K = 2
Corner frequency
1 = = 2 (slope -20 dB/decade
2 = = 20 (slope -40 dB/decade
Phase
= tan-1 - tan-1 0.5 - tan-1 0.05
= 900- tan-1 0.5 - tan-1 0.05
1 -119.430
5 -172.230
10 -195.250
15 -209.270
20 -219.30
25 -226.760
30 -232.490
35 -236.980
40 -240.570
45 -243.490
50 -245.910
Finding gc (gain cross over frequency
M =
4 = 2 ( (
6 (6.25104) + 0.2524 +2 = 4
Let 2 = x
X3 (6.25104) + 0.2522 + x = 4
X1 = 2.46
X2 = -399.9
X3 = -6.50
For x1 = 2.46
gc = 3.99 rad/sec(from plot )
For phase margin
PM = 1800 -
= 900 – tan-1 (0.5×gc) – tan-1 (0.05 × gc)
= -164.50
PM = 1800 - 164.50
= 15.50
For phase cross over frequency (pc)
= 900 – tan-1 (0.5 ) – tan-1 (0.05 )
-1800 = -900 – tan-1 (0.5 pc) – tan-1 (0.05 pc)
-900 – tan-1 (0.5 pc) – tan-1 (0.05 pc)
Taking than on both sides
Tan 900 = tan-1
Let tan-1 0.5 pc = A, tan-1 0.05 pc = B
= 00
= 0
1 =0.5 pc 0.05pc
pc = 6.32 rad/sec
The plot is shown in figure.
Fig. Magnitude Plot for G(S) =
Q3) For the given transfer function
G(S) =
Plot the rode plot find PM and GM
A3)
T1 = 0.5 1 = = 2 rad/sec
Zero so, slope (20 dB/decade)
T2 = 0.2 2 = = 5 rad/sec
Pole, so slope (-20 dB/decade)
T3 = 0.1 = T4 = 0.1
3 = 4 = 10 (2 pole ) (-40 db/decade)
1. Initial slope 0 dB/decade till 1 = 2 rad/sec
2. From 1 to2 (i.e. 2 rad /sec to 5 rad/sec) slope will be 20 dB/decade
3. From 2 to 3 the slope will be 0 dB/decade (20 + (-20))
4. From 3 ,4 the slope will be -40 dB/decade (0-20-20)
Phase plot
= tan-1 0.5 - tan-1 0.2 - tan-1 0.1 - tan-1 0.1
500 -177.30
1000 -178.60
1500 -179.10
2000 -179.40
2500 -179.50
3000 -179.530
3500 -179.60
GM = 00
PM = 61.460
The plot is shown in figure.
Fig. Magnitude and Phase plot for G(S) =
Q4) For the given transfer function plot the bode plot (magnitude plot)
G(S) =
A4)
Given transfer function
G(S) =
Converting above transfer function to standard from
G(S) =
=
1. As type 1 system, so initial slope will be -20 dB/decade
2. Final slope will be -60 dB/decade as order of system decides the final slope
3. Corner frequency
T1 = , 11= 5 (zero)
T2 = 1, 2 = 1 (pole)
4. Initial slope will cut zero dB axis at
(K)1/N = 10
i.e = 10
5. Finding n and
T(S) =
T(S)=
Comparing with standard second order system equation
S2+2ns +n2
n = 11 rad/sec
n = 5
11 = 5
= = 0.27
6. Maximum error
M = -20 log 2
= +6.5 dB
7. As K = 10, so whole plot will shift by 20 log 10 10 = 20 Db
The plot is shown in figure.
Fig. Magnitude plot for G(S) =
Q5) For the given plot determine the transfer function
Fig. Magnitude plot
A5)
From figure, we can conclude that
1. Initial slope = -20 dB/decade so type -1
2. Initial slope alls 0 dB axis at = 10 so
K1/N N = 1
(K)1/N = 10.
3. Corner frequency
1 = = 0.2 rad/sec
2 = = 0.125 rad/sec
4. At = 5 the slope becomes -40 dB/decade, so there is a pole at = 5 as slope changes from -20 dB/decade to -40 dB/decade
5. At = 8 the slope changes from -40 dB/decade to -20 dB/decade hence is a zero at = 8 (-40+(+20)=20)
6. Hence transfer function is
T(S) =
Q6) For G(s) = Plot magnitude and phase plot using bode plot?
A6)
TF =
M =
MdB = -20 log10 ( at T=2
MdB
1 -20 log10
10 -20 log10
100 -20 log10
MdB = =
0.1 -20 log10 = 1.73 10-3
0.1 -20 log10 = -0.1703
0.5 -20 log10 = -3dB
1 -20 log10 = -6.98
10 -20 log10 = -26.03
100 -20 log10 = -46.02
Without approximation
For second order system
TF =
TF =
=
=
=
M=
MdB=
Case 1 <<
<< 1
MdB= 20 log10 = 0 dB
Case 2 >>
>> 1
MdB = -20 log10
= -20 log10
= -20 log10
< 1 is very large so neglecting other two terms
MdB = -20 log10
= -40 log10
Case 3 when case 1 is equal to case 2
-40 log10 = 0
= 1
The natural frequency is our corner frequency
Max error at i.e at corner frequency
MdB = -20 log10
For
MdB = -20 log10
error for
Completely the error depends upon the value of (error at corner frequency)
The maximum error will be
MdB = -20 log10
M = -20 log10
= 0
is resonant frequency and at this frequency we are getting the maximum error so the magnitude will be
M = -+
=
Mr =
MdB = -20 log10
MdB = -20 log10
= tan-1
Mr =
Q7) Plot the magnitude plot for G(S) =
A7)
G(j) =
M = ; = -1800 (-20tan-1)
MdB = +20 log -2
MdB = -40 log10
MdB
0.01 80
0.1 40
1 0 (pole at origin)
10 -40
100 -80
Slope = 40dbdecade
Q8) Plot the bode for G(S) = S2
A8)
M= 2 MdB = 20 log102
= 1800 = 40 log10
W MdB
0.01 -80
0.1 -40
1 0
10 40
100 80
Q9) Plot magnitude plot for G(S) =
A9)
G(j) =
M =
MdB = 20 log10 K-20 log10
= tan-1() –tan-1()
= 0-900 = -900
K=1 K=10 MDb MdB=-20 log10 =20 -20 log100.01 40 60 0.1 20 40 1 0 20 10 -20 0 100 -40 -20 |
Q10) Explain gain and phase cross over frequency?
A10)
Gain Cross Over Frequency:
The frequency at which the bode plot culls the 0db axis is called as Gain Cross Over Frequency.
Phase Cross Over Frequency:
The Frequency at which the phase plot culls the -1800 axis.
GM=MdB= -20 log [ G (jw)]
.:
.:
1) When gain cross over frequency is smaller then phase curves over frequency the system is stable and vice versa.
i) More the difference b/WPC and WGC core is the stability of system
Ii) If GM is below 0dB axis than take ilb +ve and stable. If GM above 0dB axis, that is take -ve
GM= ODB - 20 log M
Iii) The IM should also lie above -1800 for making the system (i.e. pm=+ve
Iv) For a stable system GM and PM should be -ve
v) GM and PM both should be +ve more the value of GM and PM more the system is stable.
Vi) If Wpc and Wgc are in same line Wpc= Wgc than system is marginally stable. As we get GM=0dB.