modern control - ems.guc.edu.egems.guc.edu.eg/download.ashx?id=446&file=tut9_446.pdf · dr....
TRANSCRIPT
![Page 1: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/1.jpg)
Modern Control
GUC Faculty of Engineering and Material Science Department of Mechatronics
Tutorial #9
Stability
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
![Page 2: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/2.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Stability
Internal
• Eigen values stability
• Lyapunov stability
External
• Bounded input –bounded output (BIBO)
stability
Stability types
![Page 3: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/3.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Eigen values stability
![Page 4: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/4.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Problem 1:
Asses the stability of the following system Using Eigen values stability analysis
414
10A
Eigenvalues:
-2 + 3.16i
-2 - 3.16i System is asymptotically stable
![Page 5: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/5.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
414
10A
2 + 3.16i
2 - 3.16i
Eigenvalues: System is unstable
40
10A
0
-4
Eigenvalues: System is marginally stable due to zero
pole (and no positive poles).
Stable in the sense of Lyapunov (i.s.l)
014
10A
Eigenvalues: 0 + 3.74i
0 - 3.74i
System is marginally stable due to
zero real part poles (and no positive
real poles).
Stable in the sense of Lyapunov
(i.s.l)
![Page 6: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/6.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Lyapunov Stability Theorem
And to asses the stability of a system using Lyapunov theorem, we use Lyapunov equation
System A matrix
![Page 7: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/7.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
![Page 8: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/8.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Problem 2:
Asses the stability of the following system Using Lyapunov stability analysis
414
10A
10
01
414
10
41
140
2212
1211
2212
1211
pp
pp
pp
pp
10
01Q
2212
1211
pp
ppP P is symmetric
![Page 9: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/9.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
10
01
414
414
44
1414
221222
121112
22122111
2212
ppp
ppp
pppp
p P-
10
01
82144
14428
2212221211
22121112
PP P PP
P PP P-
Solving for P11 , P12, P22, we get
0.1340.0357
0.03572.02P
And its eigenvalues are 2.0185, and 0.1333, which show that the P matrix is Positive Definite, and hence the system is Asymptotically stable.
![Page 10: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/10.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09-0.02
0
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0.16
x1 (m)
x2 (
m/s
ec)
Phase plane
![Page 11: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/11.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
414
10A
By performing the same procedures as the previous problem
10
01
82144
14428
2212221211
22121112
PP P PP
P PP P-
Solving for P11 , P12, P22, we get
0.134-0.0357
0.03572.02-P
And its eigenvalues are -2.02, and -0.133, which show that the P matrix is Negative Definite, and hence the system is unstable.
![Page 12: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/12.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
-400 -200 0 200 400 600 800 1000 1200 1400 1600-1000
-500
0
500
1000
1500
2000
2500
3000
x1 (m)
x2 (
m/s
ec)
Phase plane
![Page 13: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/13.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
40
10A
By performing the same procedures as the previous problem
10
01
824
40
22121211
1211
PP PP
PP
Here, the no. of unknowns is less than the no. of equations, hence there is no possibility for a unique P matrix, and Lyapunov test fails.
![Page 14: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/14.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
By performing the same procedures as the previous problem
10
01
214
1428
122211
221112
P PP
PP P
Here, the no. of unknowns is less than the no. of equations, hence there is no possibility for a unique P matrix, and Lyapunov test fails.
014
10A
![Page 15: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/15.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
External test
Bounded-input, bounded-output (BIBO) stability
In this stability test, we apply a bounded input to the system (impulse or step input), And then we check the output. If the output is bounded, then the system is BIBO stable.
Important note:
![Page 16: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/16.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
Problem 3:
solution
The system is bounded-input, bounded-output stable because the impulse response
2( ) (1 ) th t t e
The three-dimensional controller canonical form realization is specified by
CCF CCF CCF
0 1 0 0
0 0 1 0 2 1 1
8 4 2 1
A B C
2
3 2 2 2
2 ( 2)( 1) ( 1)( )
2 4 8 ( 2)( 2) ( 2)
s s s s sH s
s s s s s s
![Page 17: Modern Control - ems.guc.edu.egems.guc.edu.eg/Download.ashx?id=446&file=tut9_446.pdf · Dr. Ayman Ali El-Badawy » ¼ º « ¬ ª 14 4 0 1 A 2 + 3.16i 2 - 3.16i Eigenvalues: System](https://reader035.vdocument.in/reader035/viewer/2022071001/5fbd8c346dacb744d417a1a3/html5/thumbnails/17.jpg)
GUC Faculty of Engineering and Material Science Department of Mechatronics
Modern Control MCTR 702 Dr. Ayman Ali El-Badawy
The observability matrix
CCF
CCF CCF
2
CCF CCF
2 1 1
8 2 3
24 4 8
C
Q C A
C A