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7-4 Nyquist Stability
Criterion
1. Introduction to Nyquist stability criterion
The Nyquist stability criterion determines the stability
of a closed-loop system from its open-loop frequency
response and open-loop poles, and there is no need for
actually determining the closed-loop poles.
To determine the stability of a closed-loop system, one
must investigate the closed-loop characteristic equation
of the system.
)
(s
G
)
(s
H
We consider the following typical closed-loop system:
From the above diagram, we have
( )
( )
1 ( ) ( )
G s
s
G s H s
 

1 2
1 2
( ) ( )
( ) : , ( ) :
( ) ( )
N s N s
G s H s
D s D s
 
where
( ) 1 ( ) ( )
F s G s H s
 
We define
which is also called the characteristic equation of the
closed-loop system and will play an important role in
stability analysis. In fact, we have
1 2 1 2
1 2
( ) ( ) ( ) ( )
( )
( ) ( )
D s D s N s N s
F s
D s D s


Further, we assume that deg(N1N2)<deg(D1D2), which
implies that both the denominator and nominator
polynomials of F(s) have the same degree.
2. Preliminary Study
Consider, for example, the following open-loop transfer
function:
2
( ) ( )
1
G s H s
s


1
( ) 1 ( ) ( ) ( )
1
s
F s G s H s F s
s

   

whose closed-loop characteristic equation is
which is analytic everywhere except at its singular
points. For each point analytic in s plane, F(s) maps
the point into F(s) plane. For example,
s=2+j:F(s)=2j.
Further, we have the following conclusion:
Conformal mapping: For any given continuous closed
path in the s plane that does not go through any singular
points, there corresponds a closed curve in the F(s) plane.
s-plane F(s) plane
j

s
[ ]
0
 s
1
s
2
s
3
s
F s
[ ( )]
Im
Re
0
 F
1
F s
( )
2
F s
( )
3
F s
( )
0
-2 -1 1 2 3
s-plane
A B C
F
G
D
E
H
s: clockwise
1
-1 0 2 3
F(s)-Plane
A‫׳‬
C ‫׳‬
G ‫׳‬
D ‫׳‬
E ‫׳‬ H ‫׳‬
F: clockwise
2
( )
s
F s
s


Example. Consider
( ) ( 2) ( 0)
0
F s s s
      

F encircles the origin:
( 2) 0
( 0) 0
  
  
s
s
Case 1:
-2 1 0
s-plane
A B C
F
G
D
E
H
s: clockwise
1
-1 0
F(s) plane
A‫׳‬
C ‫׳‬
G ‫׳‬
D ‫׳‬
E ‫׳‬
F: clockwise
2
( )
s
F s
s


( ) ( 2) ( 0)
360
F s s s
      
 
F encircles the origin:
( 2) 360
( 0) 0
   
  
s
s
Case 2:
2
( )
s
F s
s


-2 -1 0
s-plane
A B C
F
G
D
E
H
s: clockwise
1
-1 0
F(s) plane
A‫׳‬ C ‫׳‬
H ‫׳‬ D ‫׳‬
E ‫׳‬
B‫׳‬
F ‫׳‬
G ‫׳‬
F: counterclockwise
( ) ( 2) ( 0)
360
F s s s
      

F encircles the origin:
0
( 2) 0
( 0) 360
  
   
s
s
Case 3:
2
( )
s
F s
s


Case 4:
It can be verified that when s encloses both the pole and
zero in the clockwise direction, the number of the F
encircles the origin is 1+1=0.
1
-z
2
z
1
p
-
2
p
- 0
s 1

2

2
 1



j
0
F
)
(s
F

u
jv
S

F

If, for example, F(s) has two zeros and one pole are
enclosed by s, it can be deduced from the above
analysis that F encircles the origin of F plane one time
in the clockwise direction as s traces out s.
Mapping theorem (The principle of argument)
Let F(s) be a ratio of two polynomials in s. Let P be the
number of poles and Z be the number of zeros of F(s)
that lie inside a closed contour s, which does not pass
through any poles and zeros of F(s).
Then the s in the s-plane is mapped into the F(s) plane
as a closed curve, F. The total number N of
counterclockwise encirclements of the origin of the
F(s), as s traces out s in the clockwise direction, is
equal to
N=PZ
3.The Nyquist Stability Criterion
)
(s
G
)
(s
H
1 2 1 2
1 2
( ) ( ) ( ) ( )
( )
( ) ( )
=
D s D s N s N s
F s
D s D s


closed -loop characteristic equation
open -loop characteristic equation
For a stable system, all the zeros of F(s) must lie in the
left-half s-plane.
Therefore, we choose a contour s, say, Nyquist path, in
the s-plane that encloses the entire right-half s-plane. The
contour consists of the entire j axis ( varies from  to
+) and a semicircular path of infinite radius in the right-
half s plane.
Nyquist contour
r 
0
S

s
jw
s-plane
As a result, the Nyquist path
encloses all the zeros and poles of
F(s)=1+G(s)H(s) that have
positive real parts.
Now, let
P be the number of the unstable open-loop poles,
which is assumed to be known,
N be the number of encirclements of the origin of
F(s) in counterclockwise direction, which, by
drawing the curve, is also known, and
Z be the number of the unstable closed-loop poles,
which is unknown.
Then by applying the Mapping Theorem, we have
N=PZ.
If Z=0, the system is stable; if Z>0, the system is unstable
with the number of unstable poles being Z.
Question: How to obtain the curve of F(s) as s traces
out s in clockwise direction?
Nyquist contour
r 
0
S

s
jw
s-plane
It is clear that when s traverses the semicircle of infinite
radius, F(s) remains a constant. That is, the encirclements
of the origin of F(s) only determines by F(j ) as  varies
from  to + provided that no zeros or poles lie on the
j axis.
lim ( )
lim [1 ( ) ( )] const.
s
s
F s
G s H s


  
By assumption,
Example.
Consider a unity feedback system whose open-loop
transfer function is as follows
2 1
( ) ( ) 1
1 1
s
G s F s G
s s

    
 
The system is stable.
1

P 1

N
0


 N
P
Z
1
 1
F(j)
0
j
Further, since
( ) 1
F s G
 
compare the two curves below:
1
 1
F(j)
0
j
2
 1

GH(j)
0
j
Clearly, the encirclement of the origin in F plane is
equivalent to the encirclement of 1 point in GH
plane!
Example.
Consider a unity feedback system whose open-loop
transfer function is as follows
0.5
( )
1
G s
s


The system is unstable.
1

P 0

N
1


 N
P
Z
1

5
.
0

G(s)
0
Example.
Consider a single-loop control system, where
)
1
1
.
0
)(
1
(
100
)
(
)
(



s
s
s
H
s
G
0
,
0 
 N
P
0


 N
P
Z
The system is stable. G(s)H(s)
1

0
Determine its stability.
Nyquist stability criterion
A system is stable if and only if from
N = PZ
we can obtain that Z=0, where P is the number of the
open-loop poles in the right-hand half s-plane and N is the
number of the encirclements of the point (1, j0) of
G(j)H(j) in the counterclockwise direction.
Because the plot of G(j )H(j) and the plot of
G(j )H(j) are symmetrical with each other about the
real axis. Hence, we can modify the stability criterion as
N = (P – Z)/2,
where only the polar plot of G(j)H(j) with  varying
from 0 to + is necessary.
G(s)H(s)
0
-1
Re
Im
G(s)H(s)
0
-1
Re
Im
Example.
Consider a unity feedback system whose open-loop
transfer function is as follows
2
( )
1
G s
s


The system is stable.
1 ( )
2 2
(1 )
0
2
P Z
N
Z
Z

 

  
Investigate its stability by using Nyquist criterion.
Solution: Obviously, P=1 (nonminimum phase plant).
Now, drawing its Nyquist plot yields:
2
 1

G(j)
0
j
Example.
Consider a unity feedback system whose open-loop
transfer function is as follows
1 2 3
( ) , 0, 0
( 1)( 1)( 1)
i
K
G s T K
T s T s T s
  
  
Using Nyquist plot, determine its stability.
Solution: Obviously, P=0. Now, drawing its Nyquist
plot yields:
0
Im
Re
1

   0
 
1
 
N
3
K
0
Im
Re
1

   0
 
0

P
0
Im
Re
1

   0
 
0

N
1
K 2
K
4. Nyquist Criterion Based on Bode diagram
Again, we consider the open-loop transfer function with
Nyquist curve below:
1 2 3
( ) , 0, 0
( 1)( 1)( 1)
i
K
G s T K
T s T s T s
  
  
where P=0, N=1 and the
system is unstable. The key
is the point that the Nyquist
curve crosses the negative
real axis is less than 1
(abs(A)>1).
0
Im
Re
1

   0
 
1
 
N
3
K
A
The Bode diagram is:
1
1
T
2
1
T 3
1
T
dB
[ 20]

[ 40]

[ 60]

20logK
w
w
0
180

0
270

c
w
0
0
G

The system is unstable because the phase angle plot
crosses the1800 line in the region of 20logG(j)>0.
N=1
The Nyquist Theorem can be interpreted as:
Theorem: The system is stable if and only if from
N+ N = (P – Z)/2
we can obtain that Z=0.
We use N to denote the number of crosses of 1800 line
in the region of 20logG(j)>0 if each across makes
the phase angle less than 1800. Similarly, we use N+ to
denote the number of crosses of 1800 line in the region
of 20logG(j)>0 if each across makes the phase angle
larger than 1800.
Example. Both the Nyquist plot and Bode diagram of
an open-loop minimum phase transfer function are
shown below. Determine its stability.
)
(
GH
L lg
20


GH

1

2
 3

1
 2
 3

0
1

)
(
)
(
0
180

0 0
2 2
 
 
     
P Z Z
N N Z
5. Special case when G(s)H(s) involves Poles
and Zeros on the j Axis
Consider the following open-loop transfer function:
( ) ( )
( 1)
K
G s H s
s Ts


which does not satisfy the Nyquist Theorem because s is
a singular point. Therefore, the contour s must be
modified. A way of modifying the contour near the
origin is to use a quarter-circle with an infini-tesimal
radius (>0):
j
s e q
e
 
where  varies from 00 to 900 as  varies from 0 to 0+.
A modified contour s :
The modified s implies
that we regard 1/s as a
stable pole.
0 0
1 1
, :0 90
j
e
s
q
q
e
-
= × - ® -
where 1/s rotates from 00 to 900 with an infinite radius
as  varies from 0 to 0+.
1
T


Radius
Re

j
s-plane
j0+
=0
Then, for the controlled plant with integral factor 1/s, we
have
The integral factor 1/s rotates from 00 to 900 with an
infinite radius as  varies from 0 to 0+.
1
T

Radius
r  

Radius
Re

j
j0+
=0
j

Radius
B
C
C’
Radius
r  
-1
GH-plane
u
jv
The Nyquist curve starts from real axis when =0 and
rotates 900 as =0+.
N = (P – Z)/2 Z=0, the system is stable.


j
s-plane
1
T

B’
L(dB)
f w
( )
135
 
90
 
10
180
 
20dB/ dec



1 1 3
T

40dB/ dec

0
 
0
 

Example. Let the open-loop transfer function be
2
( ) ( ) , 0, 0
( 1)
K
G s H s T K
s Ts
  

Determine its stability by using Nyquist Theorem.
Solution: When =0,
2 0
2 2
( ) ( ) , 0, 0 ;
( 1)
j
K K
G s H s e
s T s

   

q
w q
e
0
2 180
  
q
Hence, when >0+,
0 1
( ) ( ) 180 tan
G j H j T
w w w

   
When =0+,
0
Im
Re
1

  
0
 

0
P 

0


P=0, N=1 N=(PZ)/2  Z=2. The system is
unstable.
)
(
L
-40dB/dec
-60dB/dec
0
180

0
90

0
270

T
1
0
( ) / ( )
0dB
0
0
P=0, N=1, N+=0  N+N=(P Z)/2  Z=2. The
system is unstable.
6. Stability Analysis
Example. Let the open-loop transfer function be
2
1 2
2
1
( 1)
( ) ( ) , 0, 0, 0
( 1)
K T s
G s H s T T K
s T s

   

Determine its stability by using Nyquist Theorem.
Solution: When =0,
2 0
2
2 2
1
( 1)
( ) ( ) , 0, 0 ;
( 1)
j
K T s K
G s H s e
s T s


   

q
w q
e
0
0 , 2 180

   
w q
Hence, when >0+,
0 1 1
1 2
( ) ( ) 180 tan tan
G j H j T T
w w w w
 
     
When =0+
If T1>T2, the Nyquist curve is shown below. Since P=0,
N=1 N=(P Z)/2  Z=2. The system is unstable.



0


Re
Im

 0

-1 0
)
(
L
-40dB/dec
-60dB/dec
0
180

0
90

0
270

1
1
T
0
( ) / ( )
0dB
0
0
-40dB/dec
2
1
T
If T2>T1, the Nyquist curve is shown below. Since P=0,
N=0 N=(P Z)/2  Z=0. The system is stable.



0


Re
Im

 0

-1
0
r  
)
(
L
-40dB/dec
-20dB/dec
0
180

0
90

1
1
T
0
( ) / ( )
0d
B
0
0
-40dB/dec
2
1
T
P=0, N=1/2, N+=1/2  N+N=(P Z)/2  Z=0.
The system is stable.
Example. Consider a unity feedback system whose
open-loop transfer function is as follows
( )
( 1)


K
G s
s T s
The system is unstable.
1 ( )
2 2
(1 )
2
2
P Z
N
Z
Z

  

  
Investigate its stability by using Nyquist criterion.
Solution: Obviously, P=1 (nonminimum phase plant).
Now, drawing its Nyquist plot yields:
-1
j
  
0
 

0
 
7. Conditionally Stable Systems
A conditionally stable system is stable for the value
of the open-loop gain lying between critical values, but
it is unstable if the open-loop gain is either increased or
decreased sufficiently.
0
Im
Re
1
    0
 
0
P 
Example. Consider a single-loop control system,
where open-loop transfer function is
)
4
2
(
)
( 2



s
s
s
K
s
G )
(s
G
Determine the range of K so that the system keeps
stable.
2
w 
n
0 0 0
( ) 90 90 180
w
     
n
G j
( 2) 1
2 4
 

K
G j
8

K
r  
Example. Consider a single-loop control system,
where open-loop transfer function is
1 2
3
( 1)( 1)
( )
K s s
G s
s
t t
 

Discuss its stability by using Nyquist stability
criterion.

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7-2.Nyquist Stability Criterion.ppt

  • 2. 1. Introduction to Nyquist stability criterion The Nyquist stability criterion determines the stability of a closed-loop system from its open-loop frequency response and open-loop poles, and there is no need for actually determining the closed-loop poles. To determine the stability of a closed-loop system, one must investigate the closed-loop characteristic equation of the system.
  • 3. ) (s G ) (s H We consider the following typical closed-loop system: From the above diagram, we have ( ) ( ) 1 ( ) ( ) G s s G s H s    1 2 1 2 ( ) ( ) ( ) : , ( ) : ( ) ( ) N s N s G s H s D s D s   where ( ) 1 ( ) ( ) F s G s H s   We define
  • 4. which is also called the characteristic equation of the closed-loop system and will play an important role in stability analysis. In fact, we have 1 2 1 2 1 2 ( ) ( ) ( ) ( ) ( ) ( ) ( ) D s D s N s N s F s D s D s   Further, we assume that deg(N1N2)<deg(D1D2), which implies that both the denominator and nominator polynomials of F(s) have the same degree.
  • 5. 2. Preliminary Study Consider, for example, the following open-loop transfer function: 2 ( ) ( ) 1 G s H s s   1 ( ) 1 ( ) ( ) ( ) 1 s F s G s H s F s s       whose closed-loop characteristic equation is which is analytic everywhere except at its singular points. For each point analytic in s plane, F(s) maps the point into F(s) plane. For example, s=2+j:F(s)=2j. Further, we have the following conclusion:
  • 6. Conformal mapping: For any given continuous closed path in the s plane that does not go through any singular points, there corresponds a closed curve in the F(s) plane. s-plane F(s) plane j  s [ ] 0  s 1 s 2 s 3 s F s [ ( )] Im Re 0  F 1 F s ( ) 2 F s ( ) 3 F s ( )
  • 7. 0 -2 -1 1 2 3 s-plane A B C F G D E H s: clockwise 1 -1 0 2 3 F(s)-Plane A‫׳‬ C ‫׳‬ G ‫׳‬ D ‫׳‬ E ‫׳‬ H ‫׳‬ F: clockwise 2 ( ) s F s s   Example. Consider ( ) ( 2) ( 0) 0 F s s s         F encircles the origin: ( 2) 0 ( 0) 0       s s Case 1:
  • 8. -2 1 0 s-plane A B C F G D E H s: clockwise 1 -1 0 F(s) plane A‫׳‬ C ‫׳‬ G ‫׳‬ D ‫׳‬ E ‫׳‬ F: clockwise 2 ( ) s F s s   ( ) ( 2) ( 0) 360 F s s s          F encircles the origin: ( 2) 360 ( 0) 0        s s Case 2:
  • 9. 2 ( ) s F s s   -2 -1 0 s-plane A B C F G D E H s: clockwise 1 -1 0 F(s) plane A‫׳‬ C ‫׳‬ H ‫׳‬ D ‫׳‬ E ‫׳‬ B‫׳‬ F ‫׳‬ G ‫׳‬ F: counterclockwise ( ) ( 2) ( 0) 360 F s s s         F encircles the origin: 0 ( 2) 0 ( 0) 360        s s Case 3:
  • 10. 2 ( ) s F s s   Case 4: It can be verified that when s encloses both the pole and zero in the clockwise direction, the number of the F encircles the origin is 1+1=0.
  • 11. 1 -z 2 z 1 p - 2 p - 0 s 1  2  2  1    j 0 F ) (s F  u jv S  F  If, for example, F(s) has two zeros and one pole are enclosed by s, it can be deduced from the above analysis that F encircles the origin of F plane one time in the clockwise direction as s traces out s.
  • 12. Mapping theorem (The principle of argument) Let F(s) be a ratio of two polynomials in s. Let P be the number of poles and Z be the number of zeros of F(s) that lie inside a closed contour s, which does not pass through any poles and zeros of F(s). Then the s in the s-plane is mapped into the F(s) plane as a closed curve, F. The total number N of counterclockwise encirclements of the origin of the F(s), as s traces out s in the clockwise direction, is equal to N=PZ
  • 13. 3.The Nyquist Stability Criterion ) (s G ) (s H 1 2 1 2 1 2 ( ) ( ) ( ) ( ) ( ) ( ) ( ) = D s D s N s N s F s D s D s   closed -loop characteristic equation open -loop characteristic equation For a stable system, all the zeros of F(s) must lie in the left-half s-plane.
  • 14. Therefore, we choose a contour s, say, Nyquist path, in the s-plane that encloses the entire right-half s-plane. The contour consists of the entire j axis ( varies from  to +) and a semicircular path of infinite radius in the right- half s plane. Nyquist contour r  0 S  s jw s-plane As a result, the Nyquist path encloses all the zeros and poles of F(s)=1+G(s)H(s) that have positive real parts.
  • 15. Now, let P be the number of the unstable open-loop poles, which is assumed to be known, N be the number of encirclements of the origin of F(s) in counterclockwise direction, which, by drawing the curve, is also known, and Z be the number of the unstable closed-loop poles, which is unknown. Then by applying the Mapping Theorem, we have N=PZ. If Z=0, the system is stable; if Z>0, the system is unstable with the number of unstable poles being Z. Question: How to obtain the curve of F(s) as s traces out s in clockwise direction?
  • 16. Nyquist contour r  0 S  s jw s-plane It is clear that when s traverses the semicircle of infinite radius, F(s) remains a constant. That is, the encirclements of the origin of F(s) only determines by F(j ) as  varies from  to + provided that no zeros or poles lie on the j axis. lim ( ) lim [1 ( ) ( )] const. s s F s G s H s      By assumption,
  • 17. Example. Consider a unity feedback system whose open-loop transfer function is as follows 2 1 ( ) ( ) 1 1 1 s G s F s G s s         The system is stable. 1  P 1  N 0    N P Z 1  1 F(j) 0 j
  • 18. Further, since ( ) 1 F s G   compare the two curves below: 1  1 F(j) 0 j 2  1  GH(j) 0 j Clearly, the encirclement of the origin in F plane is equivalent to the encirclement of 1 point in GH plane!
  • 19. Example. Consider a unity feedback system whose open-loop transfer function is as follows 0.5 ( ) 1 G s s   The system is unstable. 1  P 0  N 1    N P Z 1  5 . 0  G(s) 0
  • 20. Example. Consider a single-loop control system, where ) 1 1 . 0 )( 1 ( 100 ) ( ) (    s s s H s G 0 , 0   N P 0    N P Z The system is stable. G(s)H(s) 1  0 Determine its stability.
  • 21. Nyquist stability criterion A system is stable if and only if from N = PZ we can obtain that Z=0, where P is the number of the open-loop poles in the right-hand half s-plane and N is the number of the encirclements of the point (1, j0) of G(j)H(j) in the counterclockwise direction.
  • 22. Because the plot of G(j )H(j) and the plot of G(j )H(j) are symmetrical with each other about the real axis. Hence, we can modify the stability criterion as N = (P – Z)/2, where only the polar plot of G(j)H(j) with  varying from 0 to + is necessary. G(s)H(s) 0 -1 Re Im G(s)H(s) 0 -1 Re Im
  • 23. Example. Consider a unity feedback system whose open-loop transfer function is as follows 2 ( ) 1 G s s   The system is stable. 1 ( ) 2 2 (1 ) 0 2 P Z N Z Z        Investigate its stability by using Nyquist criterion. Solution: Obviously, P=1 (nonminimum phase plant). Now, drawing its Nyquist plot yields: 2  1  G(j) 0 j
  • 24. Example. Consider a unity feedback system whose open-loop transfer function is as follows 1 2 3 ( ) , 0, 0 ( 1)( 1)( 1) i K G s T K T s T s T s       Using Nyquist plot, determine its stability. Solution: Obviously, P=0. Now, drawing its Nyquist plot yields:
  • 25. 0 Im Re 1     0   1   N 3 K 0 Im Re 1     0   0  P 0 Im Re 1     0   0  N 1 K 2 K
  • 26. 4. Nyquist Criterion Based on Bode diagram Again, we consider the open-loop transfer function with Nyquist curve below: 1 2 3 ( ) , 0, 0 ( 1)( 1)( 1) i K G s T K T s T s T s       where P=0, N=1 and the system is unstable. The key is the point that the Nyquist curve crosses the negative real axis is less than 1 (abs(A)>1). 0 Im Re 1     0   1   N 3 K A
  • 27. The Bode diagram is: 1 1 T 2 1 T 3 1 T dB [ 20]  [ 40]  [ 60]  20logK w w 0 180  0 270  c w 0 0 G  The system is unstable because the phase angle plot crosses the1800 line in the region of 20logG(j)>0. N=1
  • 28. The Nyquist Theorem can be interpreted as: Theorem: The system is stable if and only if from N+ N = (P – Z)/2 we can obtain that Z=0. We use N to denote the number of crosses of 1800 line in the region of 20logG(j)>0 if each across makes the phase angle less than 1800. Similarly, we use N+ to denote the number of crosses of 1800 line in the region of 20logG(j)>0 if each across makes the phase angle larger than 1800.
  • 29. Example. Both the Nyquist plot and Bode diagram of an open-loop minimum phase transfer function are shown below. Determine its stability. ) ( GH L lg 20   GH  1  2  3  1  2  3  0 1  ) ( ) ( 0 180  0 0 2 2           P Z Z N N Z
  • 30. 5. Special case when G(s)H(s) involves Poles and Zeros on the j Axis Consider the following open-loop transfer function: ( ) ( ) ( 1) K G s H s s Ts   which does not satisfy the Nyquist Theorem because s is a singular point. Therefore, the contour s must be modified. A way of modifying the contour near the origin is to use a quarter-circle with an infini-tesimal radius (>0): j s e q e   where  varies from 00 to 900 as  varies from 0 to 0+.
  • 31. A modified contour s : The modified s implies that we regard 1/s as a stable pole. 0 0 1 1 , :0 90 j e s q q e - = × - ® - where 1/s rotates from 00 to 900 with an infinite radius as  varies from 0 to 0+. 1 T   Radius Re  j s-plane j0+ =0 Then, for the controlled plant with integral factor 1/s, we have
  • 32. The integral factor 1/s rotates from 00 to 900 with an infinite radius as  varies from 0 to 0+. 1 T  Radius r    Radius Re  j j0+ =0 j
  • 33.  Radius B C C’ Radius r   -1 GH-plane u jv The Nyquist curve starts from real axis when =0 and rotates 900 as =0+. N = (P – Z)/2 Z=0, the system is stable.   j s-plane 1 T  B’
  • 34. L(dB) f w ( ) 135   90   10 180   20dB/ dec    1 1 3 T  40dB/ dec  0   0   
  • 35. Example. Let the open-loop transfer function be 2 ( ) ( ) , 0, 0 ( 1) K G s H s T K s Ts     Determine its stability by using Nyquist Theorem. Solution: When =0, 2 0 2 2 ( ) ( ) , 0, 0 ; ( 1) j K K G s H s e s T s       q w q e 0 2 180    q Hence, when >0+, 0 1 ( ) ( ) 180 tan G j H j T w w w      When =0+,
  • 36. 0 Im Re 1     0    0 P   0   P=0, N=1 N=(PZ)/2  Z=2. The system is unstable.
  • 37. ) ( L -40dB/dec -60dB/dec 0 180  0 90  0 270  T 1 0 ( ) / ( ) 0dB 0 0 P=0, N=1, N+=0  N+N=(P Z)/2  Z=2. The system is unstable.
  • 38. 6. Stability Analysis Example. Let the open-loop transfer function be 2 1 2 2 1 ( 1) ( ) ( ) , 0, 0, 0 ( 1) K T s G s H s T T K s T s       Determine its stability by using Nyquist Theorem. Solution: When =0, 2 0 2 2 2 1 ( 1) ( ) ( ) , 0, 0 ; ( 1) j K T s K G s H s e s T s        q w q e 0 0 , 2 180      w q Hence, when >0+, 0 1 1 1 2 ( ) ( ) 180 tan tan G j H j T T w w w w         When =0+
  • 39. If T1>T2, the Nyquist curve is shown below. Since P=0, N=1 N=(P Z)/2  Z=2. The system is unstable.    0   Re Im   0  -1 0
  • 41. If T2>T1, the Nyquist curve is shown below. Since P=0, N=0 N=(P Z)/2  Z=0. The system is stable.    0   Re Im   0  -1 0 r  
  • 42. ) ( L -40dB/dec -20dB/dec 0 180  0 90  1 1 T 0 ( ) / ( ) 0d B 0 0 -40dB/dec 2 1 T P=0, N=1/2, N+=1/2  N+N=(P Z)/2  Z=0. The system is stable.
  • 43. Example. Consider a unity feedback system whose open-loop transfer function is as follows ( ) ( 1)   K G s s T s The system is unstable. 1 ( ) 2 2 (1 ) 2 2 P Z N Z Z         Investigate its stability by using Nyquist criterion. Solution: Obviously, P=1 (nonminimum phase plant). Now, drawing its Nyquist plot yields: -1 j    0    0  
  • 44. 7. Conditionally Stable Systems A conditionally stable system is stable for the value of the open-loop gain lying between critical values, but it is unstable if the open-loop gain is either increased or decreased sufficiently. 0 Im Re 1     0   0 P 
  • 45. Example. Consider a single-loop control system, where open-loop transfer function is ) 4 2 ( ) ( 2    s s s K s G ) (s G Determine the range of K so that the system keeps stable. 2 w  n 0 0 0 ( ) 90 90 180 w       n G j ( 2) 1 2 4    K G j 8  K r  
  • 46. Example. Consider a single-loop control system, where open-loop transfer function is 1 2 3 ( 1)( 1) ( ) K s s G s s t t    Discuss its stability by using Nyquist stability criterion.