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UNIT III
FREQUENCY RESPONSE
AND
SYSTEM ANALYSIS
What is Frequency Response?
• The response of a system can be partitioned into both the transient
response and the steady state response.
• We can find the transient response by using Fourier integrals.
• The steady state response of a system for an input sinusoidal signal is
known as the frequency response.
• If a sinusoidal signal is applied as an input to a Linear Time-Invariant
(LTI) system, then it produces the steady state output, which is also a
sinusoidal signal.
• The input and output sinusoidal signals have the same frequency, but
different amplitudes and phase angles.
• Let the input signal be
• The open loop transfer function will be
• We can represent in terms of magnitude and phase as shown below.
• Substitute, in the above equation.
• The output signal is
t)
Asin(
=
r(t) o

)
G(j
=
G(s) 
)
G(j
|
)
G(j
=|
)
G(j 

 
)
G(j
o

 
)
G(
|
)
G(j
=|
)
G(j o
o
o 

 
))
G(
t
sin(
|
)
G(j
|
A
=
c(t) o
o
o 

 

• The amplitude of the output sinusoidal signal is obtained by multiplying the
amplitude of the input sinusoidal signal and the magnitude of G(jω) at ω = ω0
• The phase of the output sinusoidal signal is obtained by adding the phase of the
input sinusoidal signal and the phase of G(jω)at ω = ω0.
Where,
• A is the amplitude of the input sinusoidal signal.
• ω0 is angular frequency of the input sinusoidal signal.
• We can write, angular frequency ω0 as shown below.
ω0 =2πf0
• Here, f0 is the frequency of the input sinusoidal signal. Similarly, you can follow
the same procedure for closed loop control system.
Frequency Domain Specifications
• The frequency domain specifications are resonant peak, resonant
frequency and bandwidth.
Consider the transfer function of the second order closed loop control
system as,
Substitute, s = jω in the above equation.
2
2
2
2
=
R(s)
C(s)
=
T(s)
n
n
n
S
S 




2
2
2
)
(j
2
)
j
(
=
)
T(j
n
n
n








u
j
u
u
sub
j
j
n
n
n
n
n
n
n
n
n
n





















2
)
1
(
1
=
)
T(j
)
2
(
)
1
(
1
=
)
T(j
)
2
1
(
)
(j
2
-
=
)
T(j
2
2
2
2
2
2
2
2
2
2










• Magnitude of T(jω) is
• Phase of T(jω) is
2
2
2
)
2
(
)
1
(
1
=
)
T(j
M
u
u 











 2
1
-
1
2
tan
-
=
)
T(j
u
u


Resonant Frequency
• It is the frequency at which the magnitude of the frequency response
has peak value for the first time.
• It is denoted by ωr. At ω=ωr the first derivate of the magnitude
of T(jω) is zero.
Differentiating M with respect to u
Substitute
2
r 2
1
(
= 

u
n
r
r =
u


2
n
r 2
1
(
= 

 
Resonant Peak
• It is the peak (maximum) value of the magnitude of T(jω). It is
denoted by Mr.
• At u = ur, the Magnitude of T(jω) is
• Resonant peak in frequency response corresponds to the peak
overshoot in the time domain transient response for certain values of
damping ratio So, the resonant peak and peak overshoot are correlated
to each other.
2
r
2
1
2
1
M

 

Bandwidth
• It is the range of frequencies over which, the magnitude of T(jω) drops to 70.7%
from its zero frequency value.
• At ω=0, the value of u will be zero.
• Substitute, u=0 in M.
M=1
• Therefore, the magnitude of T(jω) is one at ω=0.
• At 3-dB frequency, the magnitude of T(jω) will be 70.7% of magnitude
of T(jω) at ω=0.
i.e., at ω=ωB,M=0.707(1) = 0.707
Bandwidth in the frequency response is inversely proportional to the rise time in the
time domain transient response.
)
4
4
2
(
2
1
= 4
2
2
n
b 



 



Use of Logarithmic Scales to Represent Wide Ranges
dB
• In many places you will see the symbol dB
– This is decibel
– It is a logarithmic measure of power
• dB = 10 * log (Powerout/Powerin)
gain
• It is logarithmic so
–
–
–
10dB is a 10x change in power
20dB is a 100x change in power
3dB is a 2x change in power
V2
• Since power is proportional to
– A 10x change in voltage is a 100x
• This is a 20dB change
– 6dB is a 2x change in voltage
change in power
Plotting Gain vs. Frequency
• Want to plot log(gain) vs. log(frequency)
• dB
–
is already log of the gain
So
•
•
the plots look semilog
Log of frequency in the x direction dB in
the y direction
– But this is the log-log plot that we want
• Please remember that dB measures power
– 10x in voltage = 20dB
Bode Plot
• The Bode plot or the Bode diagram consists of two plots −
Magnitude plot
Phase plot
• In both the plots,
x - axis represents angular frequency (logarithmic scale).
y - axis represents the magnitude (linear scale) of open loop transfer
function in the magnitude plot and the phase angle (linear scale) of the
open loop transfer function in the phase plot.
• The magnitude of the open loop transfer function in dB is -
M=20log|G(jω)H(jω)|
• The phase angle of the open loop transfer function in degrees is -
ϕ=∠G(jω)H(jω)
Note − The base of logarithm is 10.
Type of term G(jω)H(jω) Slope(dB/dec) Magnitude (dB) Phase angle(degrees)
Constant K 0 20logK 0
Zero at origin jω 20 20logω 90
‘n’ zeros at origin (jω)n 20n 20nlogω 90n
Pole at origin 1/jω −20 −20logω −90or270
‘n’ poles at origin (1/jω)n −20n −20nlogω −90n or 270n
Simple zero
1+jωr
20
0 for ω < 1/r
20logωr for ω >1/r
0 for ω < 1/r
90 for ω > 1/r
Simple pole 1/ (1+jωr) -20
0 for ω < 1/r
-20logωr for ω >1/r
0 for ω < 1/r
-90 or 270 for ω > 1/r
Type of term G(jω)H(jω)
Slope
(dB/dec)
Magnitude (dB)
Phase
angle(degrees)
Second order
derivative term
ωn
2 (1−(ω2/ωn
2) + (2jδω/ωn)) 40
40logωn for ω < ωn
20log(2δωn
2) for ω = ωn
40logωn for ω > ωn
0 for ω < ωn
90 for ω = ωn
180 for ω > ωn
Second order
integral term
1
ωn
2 (1−(ω2/ωn
2) + (2jδω/ωn))
-40
-40logωn for ω < ωn
-20log(2δωn
2) for ω = ωn
-40logωn for ω > ωn
0 for ω < ωn
-90 for ω = ωn
-180 for ω > ωn
Consider the open loop transfer function G(s)H(s)=K.
• Magnitude M=20logK dB
• Phase angle ϕ=0 degrees
• If K=1, then magnitude is 0 dB.
• If K > 1, then magnitude will be positive.
• If K < 1, then magnitude will be negative.
• The magnitude plot is a horizontal line, which is independent of
frequency.
• The 0 dB line itself is the magnitude plot when the value of K is one.
• For the positive values of K, the horizontal line will shift 20logK dB
above the 0 dB line.
• For the negative values of K, the horizontal line will shift 20logK dB
below the 0 dB line.
• The Zero degrees line itself is the phase plot for all the positive values
of K.
Consider the open loop transfer function G(s)H(s)=s
• Magnitude M=20logω dB
• Phase angle ϕ=90
• At ω=0.1 rad/sec, the magnitude is -20 dB.
• At ω=1 rad/sec, the magnitude is 0 dB.
• At ω=10 rad/sec, the magnitude is 20 dB.
• The magnitude plot is a line, which is having a slope of 20 dB/dec.
• This line started at ω=0.1 rad/sec having a magnitude of -20 dB and it
continues on the same slope.
• It is touching 0 dB line at ω=1 rad/sec.
• In this case, the phase plot is 900 line.
Consider the open loop transfer function G(s)H(s)=1+sτ.
• Magnitude
• Phase angle
• For ω < (1/τ) , the magnitude is 0 dB and phase angle is 0 degrees.
• For ω > (1/τ) , the magnitude is 20logωτ dB and phase angle is 900.
db
2
2
1
=
20log
M 



 

 -1
tan
-
=
• The magnitude plot is having magnitude of 0 dB up to ω= (1/τ) rad/sec.
• From ω= (1/τ) rad/sec, it is having a slope of 20 dB/dec.
• In this case, the phase plot is having phase angle of 0 degrees up to ω=
(1/τ) rad/sec and from here, it is having phase angle of 900.
• This Bode plot is called the asymptotic Bode plot.
• As the magnitude and the phase plots are represented with straight lines,
the Exact Bode plots resemble the asymptotic Bode plots. The only
difference is that the Exact Bode plots will have simple curves instead of
straight lines.
Rules for Construction of Bode Plots
• Represent the open loop transfer function in the standard time constant
form.
• Substitute, s=jω in the above equation.
• Find the corner frequencies and arrange them in ascending order.
• Consider the starting frequency of the Bode plot as 1/10th of the minimum
corner frequency or 0.1 rad/sec whichever is smaller value and draw the
Bode plot upto 10 times maximum corner frequency.
• Draw the magnitude plots for each term and combine these plots properly.
• Draw the phase plots for each term and combine these plots properly.
Note − The corner frequency is the frequency at which there is a change in
the slope of the magnitude plot.
Stability Analysis using Bode Plots
From the Bode plots, we can say whether the control system is stable,
marginally stable or unstable based on the values of these parameters.
• Gain cross over frequency and phase cross over frequency
• Gain margin and phase margin
• Phase Cross over Frequency
The frequency at which the phase plot is having the phase of -1800 is
known as phase cross over frequency. It is denoted by ωpc. The unit
of phase cross over frequency is rad/sec.
• Gain Cross over Frequency
The frequency at which the magnitude plot is having the magnitude of
zero dB is known as gain cross over frequency. It is denoted by ωgc.
The unit of gain cross over frequency is rad/sec.
• The stability of the control system based on the relation between the
phase cross over frequency and the gain cross over frequency
Stability Analysis
• If the phase cross over frequency ωpc is greater than the gain cross
over frequency ωgc , then the control system is stable.
• If the phase cross over frequency ωpc is equal to the gain cross over
frequency ωgc, then the control system is marginally stable.
• If the phase cross over frequency ωpc is less than the gain cross over
frequency ωgc, then the control system is unstable.
Gain Margin
• Gain margin GM is equal to negative of the magnitude in dB at phase
cross over frequency.
• Where, Mpc is the magnitude at phase cross over frequency. The unit
of gain margin (GM) is dB.
)
(
log
20
)
(
1
log
20
1
20log
GM pc
pc
pc
j
G
j
G
M














Phase Margin
• The formula for phase margin PM is
PM = 180 + ɸgc
• here, ɸgc is the phase angle at gain cross over frequency. The unit of
phase margin is degrees.
• The stability of the control system is based on the relation between
gain margin and phase margin
• If both the gain margin GM and the phase margin PM are positive,
then the control system is stable.
• If both the gain margin GM and the phase margin PM are equal to
zero, then the control system is marginally stable.
• If the gain margin GM and / or the phase margin PM are/is negative,
then the control system is unstable.
Polar Plot
• In Bode plots, we have two separate plots for both magnitude and
phase as the function of frequency.
• Polar plot is a plot which can be drawn between magnitude and
phase. Here, the magnitudes are represented by normal values
only.
• The polar form of G(jω)H(jω) is
G(jω)H(jω)=|G(jω)H(jω)|∠G(jω)H(jω)
The Polar plot is a plot, which can be drawn between the
magnitude and the phase angle of G(jω)H(jω) by varying ω from
zero to ∞.
• This graph sheet consists of concentric circles and radial lines.
• The concentric circles and the radial lines represent the magnitudes
and phase angles respectively.
• These angles are represented by positive values in anti-clock wise
direction. Similarly, we can represent angles with negative values in
clockwise direction.
• For example, the angle 2700 in anti-clock wise direction is equal to the
angle −900 in clockwise direction.
Rules for Drawing Polar Plots
• Substitute, s=jω in the open loop transfer function.
• Write the expressions for magnitude and the phase of G(jω)H(jω).
• Find the starting magnitude and the phase of G(jω)H(jω) by
substituting ω=0. So, the polar plot starts with this magnitude and
the phase angle.
• Find the ending magnitude and the phase of G(jω)H(jω) by
substituting ω=∞. So, the polar plot ends with this magnitude and
the phase angle.
• Check whether the polar plot intersects the real axis, by making
the imaginary term of G(jω)H(jω) equal to zero and find the
value(s) of ω.
• Check whether the polar plot intersects the imaginary axis, by
making real term of G(jω)H(jω) equal to zero and find the
value(s) of ω.
• For drawing polar plot more clearly, find the magnitude and
phase of G(jω)H(jω) by considering the other value(s) of ω.
Example
• Consider the open loop transfer function of a closed loop control
system
• Step 1 − Substitute, s=jω in the open loop transfer function.
)
2
)(
1
(
5
=
G(S)H(S)

 S
S
S
)
2
j
)(
1
j
(
j
5
=
)
)H(j
G(j

 




• The magnitude of the open loop transfer function is
• The phase angle of the open loop transfer function is
)
4
(
)
1
(
5
=
M
2
2

 


)
2
/
(
tan
)
(
tan
-
90
-
= -1
-1


 
• Step 2 − The following table shows the magnitude and the phase angle
of the open loop transfer function at ω=0 rad/sec and ω=∞ rad/sec.
• So, the polar plot starts at (∞,−900) and ends at (0,−2700). The first and
the second terms within the brackets indicate the magnitude and phase
angle respectively.
Frequency Magnitude Phase Angles(degrees)
0 ∞ -90 or 270
∞ 0 90 or - 270
• Step 3 − Based on the starting and the ending polar co-ordinates, this
polar plot will intersect the negative real axis.
• The phase angle corresponding to the negative real axis is −1800 or
1800.
• So, by equating the phase angle of the open loop transfer function to
either −1800 or 1800, we will get the ω value as √2.
• By substituting ω=√2 in the magnitude of the open loop transfer
function, we will get M=0.83.
• Therefore, the polar plot intersects the negative real axis
when ω=√2 and the polar coordinate is (0.83,−1800).
Gain Margin
• Gain margin GM is defined as the inverse of the magnitude G(jω) at
phase cross over frequency. The Phase cross over frequency is the
frequency at which the phase of G(jω) is 180.
Phase Margin
• Phase margin PM is defined as, phase margin, PM = 180 + ɸgc where
ɸgc phase angle of G(jω) at gain cross over frequency. The Gain cross
over frequency is the frequency at which the magnitude of G(jω) is
unity.
Phase Margin
• The formula for phase margin PM is
PM = 180 + ɸgc
• here, ɸgc is the phase angle at gain cross over frequency. The unit of
phase margin is degrees.
• The stability of the control system is based on the relation between
gain margin and phase margin

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bode plot.pptx

  • 2. What is Frequency Response? • The response of a system can be partitioned into both the transient response and the steady state response. • We can find the transient response by using Fourier integrals. • The steady state response of a system for an input sinusoidal signal is known as the frequency response. • If a sinusoidal signal is applied as an input to a Linear Time-Invariant (LTI) system, then it produces the steady state output, which is also a sinusoidal signal. • The input and output sinusoidal signals have the same frequency, but different amplitudes and phase angles.
  • 3. • Let the input signal be • The open loop transfer function will be • We can represent in terms of magnitude and phase as shown below. • Substitute, in the above equation. • The output signal is t) Asin( = r(t) o  ) G(j = G(s)  ) G(j | ) G(j =| ) G(j     ) G(j o    ) G( | ) G(j =| ) G(j o o o     )) G( t sin( | ) G(j | A = c(t) o o o     
  • 4. • The amplitude of the output sinusoidal signal is obtained by multiplying the amplitude of the input sinusoidal signal and the magnitude of G(jω) at ω = ω0 • The phase of the output sinusoidal signal is obtained by adding the phase of the input sinusoidal signal and the phase of G(jω)at ω = ω0. Where, • A is the amplitude of the input sinusoidal signal. • ω0 is angular frequency of the input sinusoidal signal. • We can write, angular frequency ω0 as shown below. ω0 =2πf0 • Here, f0 is the frequency of the input sinusoidal signal. Similarly, you can follow the same procedure for closed loop control system.
  • 5. Frequency Domain Specifications • The frequency domain specifications are resonant peak, resonant frequency and bandwidth. Consider the transfer function of the second order closed loop control system as, Substitute, s = jω in the above equation. 2 2 2 2 = R(s) C(s) = T(s) n n n S S      2 2 2 ) (j 2 ) j ( = ) T(j n n n        
  • 7. • Magnitude of T(jω) is • Phase of T(jω) is 2 2 2 ) 2 ( ) 1 ( 1 = ) T(j M u u              2 1 - 1 2 tan - = ) T(j u u  
  • 8. Resonant Frequency • It is the frequency at which the magnitude of the frequency response has peak value for the first time. • It is denoted by ωr. At ω=ωr the first derivate of the magnitude of T(jω) is zero. Differentiating M with respect to u Substitute 2 r 2 1 ( =   u n r r = u   2 n r 2 1 ( =    
  • 9. Resonant Peak • It is the peak (maximum) value of the magnitude of T(jω). It is denoted by Mr. • At u = ur, the Magnitude of T(jω) is • Resonant peak in frequency response corresponds to the peak overshoot in the time domain transient response for certain values of damping ratio So, the resonant peak and peak overshoot are correlated to each other. 2 r 2 1 2 1 M    
  • 10. Bandwidth • It is the range of frequencies over which, the magnitude of T(jω) drops to 70.7% from its zero frequency value. • At ω=0, the value of u will be zero. • Substitute, u=0 in M. M=1 • Therefore, the magnitude of T(jω) is one at ω=0. • At 3-dB frequency, the magnitude of T(jω) will be 70.7% of magnitude of T(jω) at ω=0. i.e., at ω=ωB,M=0.707(1) = 0.707 Bandwidth in the frequency response is inversely proportional to the rise time in the time domain transient response. ) 4 4 2 ( 2 1 = 4 2 2 n b         
  • 11. Use of Logarithmic Scales to Represent Wide Ranges
  • 12. dB • In many places you will see the symbol dB – This is decibel – It is a logarithmic measure of power • dB = 10 * log (Powerout/Powerin) gain • It is logarithmic so – – – 10dB is a 10x change in power 20dB is a 100x change in power 3dB is a 2x change in power V2 • Since power is proportional to – A 10x change in voltage is a 100x • This is a 20dB change – 6dB is a 2x change in voltage change in power
  • 13. Plotting Gain vs. Frequency • Want to plot log(gain) vs. log(frequency) • dB – is already log of the gain So • • the plots look semilog Log of frequency in the x direction dB in the y direction – But this is the log-log plot that we want • Please remember that dB measures power – 10x in voltage = 20dB
  • 14. Bode Plot • The Bode plot or the Bode diagram consists of two plots − Magnitude plot Phase plot • In both the plots, x - axis represents angular frequency (logarithmic scale). y - axis represents the magnitude (linear scale) of open loop transfer function in the magnitude plot and the phase angle (linear scale) of the open loop transfer function in the phase plot.
  • 15. • The magnitude of the open loop transfer function in dB is - M=20log|G(jω)H(jω)| • The phase angle of the open loop transfer function in degrees is - ϕ=∠G(jω)H(jω) Note − The base of logarithm is 10.
  • 16. Type of term G(jω)H(jω) Slope(dB/dec) Magnitude (dB) Phase angle(degrees) Constant K 0 20logK 0 Zero at origin jω 20 20logω 90 ‘n’ zeros at origin (jω)n 20n 20nlogω 90n Pole at origin 1/jω −20 −20logω −90or270 ‘n’ poles at origin (1/jω)n −20n −20nlogω −90n or 270n Simple zero 1+jωr 20 0 for ω < 1/r 20logωr for ω >1/r 0 for ω < 1/r 90 for ω > 1/r Simple pole 1/ (1+jωr) -20 0 for ω < 1/r -20logωr for ω >1/r 0 for ω < 1/r -90 or 270 for ω > 1/r
  • 17. Type of term G(jω)H(jω) Slope (dB/dec) Magnitude (dB) Phase angle(degrees) Second order derivative term ωn 2 (1−(ω2/ωn 2) + (2jδω/ωn)) 40 40logωn for ω < ωn 20log(2δωn 2) for ω = ωn 40logωn for ω > ωn 0 for ω < ωn 90 for ω = ωn 180 for ω > ωn Second order integral term 1 ωn 2 (1−(ω2/ωn 2) + (2jδω/ωn)) -40 -40logωn for ω < ωn -20log(2δωn 2) for ω = ωn -40logωn for ω > ωn 0 for ω < ωn -90 for ω = ωn -180 for ω > ωn
  • 18. Consider the open loop transfer function G(s)H(s)=K. • Magnitude M=20logK dB • Phase angle ϕ=0 degrees • If K=1, then magnitude is 0 dB. • If K > 1, then magnitude will be positive. • If K < 1, then magnitude will be negative.
  • 19.
  • 20. • The magnitude plot is a horizontal line, which is independent of frequency. • The 0 dB line itself is the magnitude plot when the value of K is one. • For the positive values of K, the horizontal line will shift 20logK dB above the 0 dB line. • For the negative values of K, the horizontal line will shift 20logK dB below the 0 dB line. • The Zero degrees line itself is the phase plot for all the positive values of K.
  • 21. Consider the open loop transfer function G(s)H(s)=s • Magnitude M=20logω dB • Phase angle ϕ=90 • At ω=0.1 rad/sec, the magnitude is -20 dB. • At ω=1 rad/sec, the magnitude is 0 dB. • At ω=10 rad/sec, the magnitude is 20 dB.
  • 22.
  • 23. • The magnitude plot is a line, which is having a slope of 20 dB/dec. • This line started at ω=0.1 rad/sec having a magnitude of -20 dB and it continues on the same slope. • It is touching 0 dB line at ω=1 rad/sec. • In this case, the phase plot is 900 line.
  • 24. Consider the open loop transfer function G(s)H(s)=1+sτ. • Magnitude • Phase angle • For ω < (1/τ) , the magnitude is 0 dB and phase angle is 0 degrees. • For ω > (1/τ) , the magnitude is 20logωτ dB and phase angle is 900. db 2 2 1 = 20log M         -1 tan - =
  • 25.
  • 26. • The magnitude plot is having magnitude of 0 dB up to ω= (1/τ) rad/sec. • From ω= (1/τ) rad/sec, it is having a slope of 20 dB/dec. • In this case, the phase plot is having phase angle of 0 degrees up to ω= (1/τ) rad/sec and from here, it is having phase angle of 900. • This Bode plot is called the asymptotic Bode plot. • As the magnitude and the phase plots are represented with straight lines, the Exact Bode plots resemble the asymptotic Bode plots. The only difference is that the Exact Bode plots will have simple curves instead of straight lines.
  • 27. Rules for Construction of Bode Plots • Represent the open loop transfer function in the standard time constant form. • Substitute, s=jω in the above equation. • Find the corner frequencies and arrange them in ascending order. • Consider the starting frequency of the Bode plot as 1/10th of the minimum corner frequency or 0.1 rad/sec whichever is smaller value and draw the Bode plot upto 10 times maximum corner frequency. • Draw the magnitude plots for each term and combine these plots properly. • Draw the phase plots for each term and combine these plots properly. Note − The corner frequency is the frequency at which there is a change in the slope of the magnitude plot.
  • 28. Stability Analysis using Bode Plots From the Bode plots, we can say whether the control system is stable, marginally stable or unstable based on the values of these parameters. • Gain cross over frequency and phase cross over frequency • Gain margin and phase margin
  • 29. • Phase Cross over Frequency The frequency at which the phase plot is having the phase of -1800 is known as phase cross over frequency. It is denoted by ωpc. The unit of phase cross over frequency is rad/sec. • Gain Cross over Frequency The frequency at which the magnitude plot is having the magnitude of zero dB is known as gain cross over frequency. It is denoted by ωgc. The unit of gain cross over frequency is rad/sec. • The stability of the control system based on the relation between the phase cross over frequency and the gain cross over frequency
  • 30. Stability Analysis • If the phase cross over frequency ωpc is greater than the gain cross over frequency ωgc , then the control system is stable. • If the phase cross over frequency ωpc is equal to the gain cross over frequency ωgc, then the control system is marginally stable. • If the phase cross over frequency ωpc is less than the gain cross over frequency ωgc, then the control system is unstable.
  • 31. Gain Margin • Gain margin GM is equal to negative of the magnitude in dB at phase cross over frequency. • Where, Mpc is the magnitude at phase cross over frequency. The unit of gain margin (GM) is dB. ) ( log 20 ) ( 1 log 20 1 20log GM pc pc pc j G j G M              
  • 32. Phase Margin • The formula for phase margin PM is PM = 180 + ɸgc • here, ɸgc is the phase angle at gain cross over frequency. The unit of phase margin is degrees. • The stability of the control system is based on the relation between gain margin and phase margin
  • 33. • If both the gain margin GM and the phase margin PM are positive, then the control system is stable. • If both the gain margin GM and the phase margin PM are equal to zero, then the control system is marginally stable. • If the gain margin GM and / or the phase margin PM are/is negative, then the control system is unstable.
  • 34. Polar Plot • In Bode plots, we have two separate plots for both magnitude and phase as the function of frequency. • Polar plot is a plot which can be drawn between magnitude and phase. Here, the magnitudes are represented by normal values only. • The polar form of G(jω)H(jω) is G(jω)H(jω)=|G(jω)H(jω)|∠G(jω)H(jω) The Polar plot is a plot, which can be drawn between the magnitude and the phase angle of G(jω)H(jω) by varying ω from zero to ∞.
  • 35.
  • 36. • This graph sheet consists of concentric circles and radial lines. • The concentric circles and the radial lines represent the magnitudes and phase angles respectively. • These angles are represented by positive values in anti-clock wise direction. Similarly, we can represent angles with negative values in clockwise direction. • For example, the angle 2700 in anti-clock wise direction is equal to the angle −900 in clockwise direction.
  • 37. Rules for Drawing Polar Plots • Substitute, s=jω in the open loop transfer function. • Write the expressions for magnitude and the phase of G(jω)H(jω). • Find the starting magnitude and the phase of G(jω)H(jω) by substituting ω=0. So, the polar plot starts with this magnitude and the phase angle. • Find the ending magnitude and the phase of G(jω)H(jω) by substituting ω=∞. So, the polar plot ends with this magnitude and the phase angle.
  • 38. • Check whether the polar plot intersects the real axis, by making the imaginary term of G(jω)H(jω) equal to zero and find the value(s) of ω. • Check whether the polar plot intersects the imaginary axis, by making real term of G(jω)H(jω) equal to zero and find the value(s) of ω. • For drawing polar plot more clearly, find the magnitude and phase of G(jω)H(jω) by considering the other value(s) of ω.
  • 39. Example • Consider the open loop transfer function of a closed loop control system • Step 1 − Substitute, s=jω in the open loop transfer function. ) 2 )( 1 ( 5 = G(S)H(S)   S S S ) 2 j )( 1 j ( j 5 = ) )H(j G(j       
  • 40. • The magnitude of the open loop transfer function is • The phase angle of the open loop transfer function is ) 4 ( ) 1 ( 5 = M 2 2      ) 2 / ( tan ) ( tan - 90 - = -1 -1    
  • 41. • Step 2 − The following table shows the magnitude and the phase angle of the open loop transfer function at ω=0 rad/sec and ω=∞ rad/sec. • So, the polar plot starts at (∞,−900) and ends at (0,−2700). The first and the second terms within the brackets indicate the magnitude and phase angle respectively. Frequency Magnitude Phase Angles(degrees) 0 ∞ -90 or 270 ∞ 0 90 or - 270
  • 42. • Step 3 − Based on the starting and the ending polar co-ordinates, this polar plot will intersect the negative real axis. • The phase angle corresponding to the negative real axis is −1800 or 1800. • So, by equating the phase angle of the open loop transfer function to either −1800 or 1800, we will get the ω value as √2. • By substituting ω=√2 in the magnitude of the open loop transfer function, we will get M=0.83. • Therefore, the polar plot intersects the negative real axis when ω=√2 and the polar coordinate is (0.83,−1800).
  • 43. Gain Margin • Gain margin GM is defined as the inverse of the magnitude G(jω) at phase cross over frequency. The Phase cross over frequency is the frequency at which the phase of G(jω) is 180. Phase Margin • Phase margin PM is defined as, phase margin, PM = 180 + ɸgc where ɸgc phase angle of G(jω) at gain cross over frequency. The Gain cross over frequency is the frequency at which the magnitude of G(jω) is unity.
  • 44. Phase Margin • The formula for phase margin PM is PM = 180 + ɸgc • here, ɸgc is the phase angle at gain cross over frequency. The unit of phase margin is degrees. • The stability of the control system is based on the relation between gain margin and phase margin