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PAPER SIMULATION USING ADS CAD:
MIRRORED COUPLING STRUCTURES FOR
MICROWAVE
SIGNAL SPLITTING AND COMBINING
Omid Abolghasemi
Dr. Vahid Nayyeri
ABSTRACT
•method of creating multi-port couplers by mirroring conventional
coupler structures.
•maintain stable phase shifting between ports, equal power dividing,
and port isolation.
•Example structures: a four-way coupler by mirroring 90 hybrid
couplers and an eight-way coupler by mirroring Saleh power-dividing
couplers were built and tested according to the method discussed.
•good match between theoretical analysis and measurements.
2
DEPARTMENT OF SATELLITE
ENGINEERING
INTRODUCTION
•couplers were designed to meet different system requirements, e.g.,
Wilkinson couplers [1], 90 quadrature couplers [2], rat-race couplers
[3], Lange couplers [4],Saleh’s multi-way dividers [5], and Bagley
polygon couplers[15]–[18]. maintain stable phase shifting between
ports, equal power dividing, and port isolation.
•It is not easy to find new coupler structures, especially those couplers
with multi-ports, equal power division, and stable phase shifting.
•method of creating a new group of coupler structures by mirroring
conventional coupling structures.
3
DEPARTMENT OF SATELLITE
ENGINEERING
I. INTRODUCTION
•A general theoretical S-parameter analysis method is then suggested
for such coupler analysis.
•To validate the method, we derive the S-parameters of a six-port
coupler by mirroring the conventional 90 quadrature couplers, which
is compared with Agilent Technologies’ Advanced Design System
(ADS) (computer-aided design (CAD) software) simulation results.
•In order to validate our design theory, we designed and fabricated a
four-way coupler (by mirroring 90 quadrature couplers) and an eight-
way coupler (by mirroring Saleh’s four-way couplers [5]) according to
the theory discussed. Tested results showed that these couplers
maintain useful features of the original couplers, such as equal power
division, stable phase shifting between output ports, and good
isolation between ports.
4
DEPARTMENT OF SATELLITE
ENGINEERING
II. DESIGN THEORY
Fig. 2. (a) Mirrored structures with a transmission line
between two selected ports, and a passive network
connecting these two ports with all other ports. (b) Using
the transmission line as mirror edge, new structure with
more input/output ports can be created. note: all
impedance used are normalized impedance, and all lines
are 90 in length unless otherwise stated.
5
DEPARTMENT OF SATELLITE
ENGINEERING
•for the structure of Fig. 2(a), it is
expected that port P1 and P2
remain isolated and input power
will be equally divided between
port P3 to P6;
•for the mirrored structure of Fig.
2(b), it is expected that input
power is equally divided between
port P3, P4, P6, and input port P1
will be isolated with port P2 and
P5.
II. DESIGN THEORY
6
DEPARTMENT OF SATELLITE
ENGINEERING
II. DESIGN THEORY FIG. 2(A) ADS
SIMULATION
7
DEPARTMENT OF SATELLITE
ENGINEERING
II. DESIGN THEORY FIG. 2(B) ADS
SIMULATION
8
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS
Fig. 7. Mirrored couplers optimized for
maximizing working bandwidth.(a)
Mirrored quadrature coupler structure.
(b) Mirrored Saleh coupler structure
9
DEPARTMENT OF SATELLITE
ENGINEERING
•Built & Simulate Two structures:
the four-way coupler shown in Fig.
7(a) and the eight-way coupler
shown in Fig. 7(b). The commonly
used RO4003C 32 mil 1/4-oz
laminate was selected for these
coupler design and fabrication.
III. REALIZATION AND TESTS
1
0
DEPARTMENT OF SATELLITE
ENGINEERING
TABLE I
•(top) KEY PARAMETERS OF THE
MIRRORED STRUCTURE OF FIG.
7(a) AFTER OPTIMIZATION.
(bottom) KEY PARAMETERS OF
THE MIRRORED STRUCTURE OF
FIG. 7(b) AFTER OPTIMIZATION
•RO4003C 32 mil 1/4-oz
•obtaining 600-MHz bandwidth
centered at 6.1 GHz
III. REALIZATION AND TESTS FIG.
7(A)
11
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A) ADS IDEAL
SIMULATION
12
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A) ADS
REALIZED SIMULATION
13
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A) ADS
REALIZED SIMULATION
14
DEPARTMENT OF SATELLITE
ENGINEERING
Substrate Definition
•ADS Database
•Rogers RO4000® Series
High Frequency Circuit
Materials Datasheet
III. REALIZATION AND TESTS FIG. 7(A) ADS
REALIZED SIMULATION
15
DEPARTMENT OF SATELLITE
ENGINEERING
Substrate Definition
•Layers Setup
III. REALIZATION AND TESTS FIG. 7(A)
16
DEPARTMENT OF SATELLITE
ENGINEERING
Fig. 10. Back-to-back configurations of the designed four-
way mirrored quadrature coupler and high power. (a) Back-
to-back connection of the four-way mirrored quadrature
coupler. (b) Four-way power combining using the designed
coupler.
III. REALIZATION AND TESTS FIG. 7(A)
IMPORT INTO ADS MOMENTUM
17
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A)
SIMULATION USING ADS MOMENTUM
18
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A)
SIMULATION USING ADS MOMENTUM OUTPUTS
19
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG.
7(B)
20
DEPARTMENT OF SATELLITE
ENGINEERING
eight-way coupler shown in Fig. 6(b). The commonly used RO4003C 32 mil 1/4-oz
laminate was selected for these coupler design and fabrication.
III. REALIZATION AND TESTS FIG.
7(A)
21
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(B) ADS IDEAL
SIMULATION
22
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A)
IMPORT INTO ADS MOMENTUM
23
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A)
SIMULATION USING ADS MOMENTUM
24
DEPARTMENT OF SATELLITE
ENGINEERING
III. REALIZATION AND TESTS FIG. 7(A)
SIMULATION USING ADS MOMENTUM OUTPUTS
25
DEPARTMENT OF SATELLITE
ENGINEERING
CONCLUSIONS
1. Shift in Frequency may caused by simulating SMA connectors or
other not mentioned components
2. With the method, it suggests that new coupling structures could be
obtained by mirroring passive structures; and the most important
is these mirrored structures can maintain useful features of the
original structures, such as equal power splitting, stable phase
shifting between output ports, good port matching and isolation,
and more.
25
DEPARTMENT OF SATELLITE
ENGINEERING
REFERENCES:
27
DEPARTMENT OF SATELLITE
ENGINEERING

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Microwave Mirrored Coupling Structures for Microwave Signal Splitting and Combining

  • 1. PAPER SIMULATION USING ADS CAD: MIRRORED COUPLING STRUCTURES FOR MICROWAVE SIGNAL SPLITTING AND COMBINING Omid Abolghasemi Dr. Vahid Nayyeri
  • 2. ABSTRACT •method of creating multi-port couplers by mirroring conventional coupler structures. •maintain stable phase shifting between ports, equal power dividing, and port isolation. •Example structures: a four-way coupler by mirroring 90 hybrid couplers and an eight-way coupler by mirroring Saleh power-dividing couplers were built and tested according to the method discussed. •good match between theoretical analysis and measurements. 2 DEPARTMENT OF SATELLITE ENGINEERING
  • 3. INTRODUCTION •couplers were designed to meet different system requirements, e.g., Wilkinson couplers [1], 90 quadrature couplers [2], rat-race couplers [3], Lange couplers [4],Saleh’s multi-way dividers [5], and Bagley polygon couplers[15]–[18]. maintain stable phase shifting between ports, equal power dividing, and port isolation. •It is not easy to find new coupler structures, especially those couplers with multi-ports, equal power division, and stable phase shifting. •method of creating a new group of coupler structures by mirroring conventional coupling structures. 3 DEPARTMENT OF SATELLITE ENGINEERING
  • 4. I. INTRODUCTION •A general theoretical S-parameter analysis method is then suggested for such coupler analysis. •To validate the method, we derive the S-parameters of a six-port coupler by mirroring the conventional 90 quadrature couplers, which is compared with Agilent Technologies’ Advanced Design System (ADS) (computer-aided design (CAD) software) simulation results. •In order to validate our design theory, we designed and fabricated a four-way coupler (by mirroring 90 quadrature couplers) and an eight- way coupler (by mirroring Saleh’s four-way couplers [5]) according to the theory discussed. Tested results showed that these couplers maintain useful features of the original couplers, such as equal power division, stable phase shifting between output ports, and good isolation between ports. 4 DEPARTMENT OF SATELLITE ENGINEERING
  • 5. II. DESIGN THEORY Fig. 2. (a) Mirrored structures with a transmission line between two selected ports, and a passive network connecting these two ports with all other ports. (b) Using the transmission line as mirror edge, new structure with more input/output ports can be created. note: all impedance used are normalized impedance, and all lines are 90 in length unless otherwise stated. 5 DEPARTMENT OF SATELLITE ENGINEERING •for the structure of Fig. 2(a), it is expected that port P1 and P2 remain isolated and input power will be equally divided between port P3 to P6; •for the mirrored structure of Fig. 2(b), it is expected that input power is equally divided between port P3, P4, P6, and input port P1 will be isolated with port P2 and P5.
  • 6. II. DESIGN THEORY 6 DEPARTMENT OF SATELLITE ENGINEERING
  • 7. II. DESIGN THEORY FIG. 2(A) ADS SIMULATION 7 DEPARTMENT OF SATELLITE ENGINEERING
  • 8. II. DESIGN THEORY FIG. 2(B) ADS SIMULATION 8 DEPARTMENT OF SATELLITE ENGINEERING
  • 9. III. REALIZATION AND TESTS Fig. 7. Mirrored couplers optimized for maximizing working bandwidth.(a) Mirrored quadrature coupler structure. (b) Mirrored Saleh coupler structure 9 DEPARTMENT OF SATELLITE ENGINEERING •Built & Simulate Two structures: the four-way coupler shown in Fig. 7(a) and the eight-way coupler shown in Fig. 7(b). The commonly used RO4003C 32 mil 1/4-oz laminate was selected for these coupler design and fabrication.
  • 10. III. REALIZATION AND TESTS 1 0 DEPARTMENT OF SATELLITE ENGINEERING TABLE I •(top) KEY PARAMETERS OF THE MIRRORED STRUCTURE OF FIG. 7(a) AFTER OPTIMIZATION. (bottom) KEY PARAMETERS OF THE MIRRORED STRUCTURE OF FIG. 7(b) AFTER OPTIMIZATION •RO4003C 32 mil 1/4-oz •obtaining 600-MHz bandwidth centered at 6.1 GHz
  • 11. III. REALIZATION AND TESTS FIG. 7(A) 11 DEPARTMENT OF SATELLITE ENGINEERING
  • 12. III. REALIZATION AND TESTS FIG. 7(A) ADS IDEAL SIMULATION 12 DEPARTMENT OF SATELLITE ENGINEERING
  • 13. III. REALIZATION AND TESTS FIG. 7(A) ADS REALIZED SIMULATION 13 DEPARTMENT OF SATELLITE ENGINEERING
  • 14. III. REALIZATION AND TESTS FIG. 7(A) ADS REALIZED SIMULATION 14 DEPARTMENT OF SATELLITE ENGINEERING Substrate Definition •ADS Database •Rogers RO4000® Series High Frequency Circuit Materials Datasheet
  • 15. III. REALIZATION AND TESTS FIG. 7(A) ADS REALIZED SIMULATION 15 DEPARTMENT OF SATELLITE ENGINEERING Substrate Definition •Layers Setup
  • 16. III. REALIZATION AND TESTS FIG. 7(A) 16 DEPARTMENT OF SATELLITE ENGINEERING Fig. 10. Back-to-back configurations of the designed four- way mirrored quadrature coupler and high power. (a) Back- to-back connection of the four-way mirrored quadrature coupler. (b) Four-way power combining using the designed coupler.
  • 17. III. REALIZATION AND TESTS FIG. 7(A) IMPORT INTO ADS MOMENTUM 17 DEPARTMENT OF SATELLITE ENGINEERING
  • 18. III. REALIZATION AND TESTS FIG. 7(A) SIMULATION USING ADS MOMENTUM 18 DEPARTMENT OF SATELLITE ENGINEERING
  • 19. III. REALIZATION AND TESTS FIG. 7(A) SIMULATION USING ADS MOMENTUM OUTPUTS 19 DEPARTMENT OF SATELLITE ENGINEERING
  • 20. III. REALIZATION AND TESTS FIG. 7(B) 20 DEPARTMENT OF SATELLITE ENGINEERING eight-way coupler shown in Fig. 6(b). The commonly used RO4003C 32 mil 1/4-oz laminate was selected for these coupler design and fabrication.
  • 21. III. REALIZATION AND TESTS FIG. 7(A) 21 DEPARTMENT OF SATELLITE ENGINEERING
  • 22. III. REALIZATION AND TESTS FIG. 7(B) ADS IDEAL SIMULATION 22 DEPARTMENT OF SATELLITE ENGINEERING
  • 23. III. REALIZATION AND TESTS FIG. 7(A) IMPORT INTO ADS MOMENTUM 23 DEPARTMENT OF SATELLITE ENGINEERING
  • 24. III. REALIZATION AND TESTS FIG. 7(A) SIMULATION USING ADS MOMENTUM 24 DEPARTMENT OF SATELLITE ENGINEERING
  • 25. III. REALIZATION AND TESTS FIG. 7(A) SIMULATION USING ADS MOMENTUM OUTPUTS 25 DEPARTMENT OF SATELLITE ENGINEERING
  • 26. CONCLUSIONS 1. Shift in Frequency may caused by simulating SMA connectors or other not mentioned components 2. With the method, it suggests that new coupling structures could be obtained by mirroring passive structures; and the most important is these mirrored structures can maintain useful features of the original structures, such as equal power splitting, stable phase shifting between output ports, good port matching and isolation, and more. 25 DEPARTMENT OF SATELLITE ENGINEERING