MMIC on-Wafer Test Method Based on Hybrid Balanced and ...
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electronics
Article
MMIC on-Wafer Test Method Based on HybridBalanced and Unbalanced RF Pad Structures
Yue Bian , Yifan Gu, Xu Ding, Zhiyu Wang *, Jiongjiong Mo and Faxin Yu
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China;[email protected] (Y.B.); [email protected] (Y.G.); [email protected] (X.D.);[email protected] (J.M.); [email protected] (F.Y.)* Correspondence: [email protected]; Tel.: +86-0571-8795-1581
Received: 20 August 2018; Accepted: 14 September 2018; Published: 19 September 2018
Abstract: Nowadays, more and more MMICs (Microwave Monolithic Integrated Circuit), such aslimiters and switches, are designed to have balanced and unbalanced test pad structures to solvethe challenging size restrictions and integration requirements for MMICs. Hybrid balanced andunbalanced RF (Radio Frequency) probes are adopted for an on-wafer test of the heteromorphystructures. The thru standard based on single balanced or unbalanced structures cannot meet theimpedance matching requirements of the hybrid RF probes at the same time, which leads to adramatic decreasing of the calibration accuracy and cannot satisfy the requirement of MMIC test.Therefore, in this paper, the calibration error estimating of hybrid RF probes based on traditionalSOLR (Short Open Load Reciprocal) calibration method is performed , and an on-wafer test approachof MMIC based on hybrid balanced and unbalanced RF probes is proposed which combines the OSL(Open Short Load) second-order de-embedding technique with vector error correction and the matrixtransformation technique. The calibration reference plane can be accurately shifted to the probe tipwith this method, which greatly improves the test accuracy , and an automatic test system is built forthis method based on the object-oriented C# language.
Keywords: balanced and unbalanced structures; on-wafer test; OSL de-embedding; matrixtransformation; automatic test system
1. Introduction
Nowadays, with stringent size restrictions and integration requirements for MMICs, a greatnumber of MMICs, such as limiters and switches, adopt balanced and unbalanced test pad structuresin layout design, like GS (Ground Signal) pad or SG pad, to replace large-size balanced pads suchas GSG pad. These chips require both balanced and unbalanced RF probes for on-wafer testing.Due to the differences of transmission modals of electromagnetic fields, traditional on-wafer thrustandards based on single balanced or unbalanced structure adopt different structural dimensionsto match the characteristic impedances of corresponding RF probes. However, traditional thrustandards cannot meet the impedance matching requirements of hybrid balanced and unbalancedRF probes at the same time, resulting in a sharp decrease in calibration accuracy. In the research ofwidely used calibration methods, such as SOLT (Short Open Load Thru), TRL (Thru Reflect Line) ,and LRRM (Line Reflect-Reflect Match), researchers have presented several solutions [1–7] to improvethe on-wafer calibration and measurement. However, traditional thru standards are unavoidablein these calibration methods, which poses a severe challenge for on-wafer testing based on hybridbalanced and unbalanced probes.
A MMIC test based on hybrid balanced and unbalanced RF probes belongs to heteromorphystructure tests, the S-parameter of which cannot be directly measured by traditional calibration method.
Electronics 2018, 7, 208; doi:10.3390/electronics7090208 www.mdpi.com/journal/electronics
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For heteromorphy structures, two main kinds of solutions have been proposed by researchers. One isto remove the insertion loss of the RF probes and other adapters by scalar calculation based on thedirect compensation method. However, this method does not include vector error correction and, thus,cannot be applied to high-frequency and high-precision test due to the lack of accuracy. The other is touse the OSL second-order de-embedding method [8] to obtain the S-parameters of the RF probes andother adapters with high accuracy , and then achieve the S-parameters of the heteromorphy structureby vector error correction and de-embedding [9–12] But the measurement accuracy of this method isquite sensitive to errors between the ideal calibration plane and the actual calibration plane.
In this paper, after evaluating the calibration error of MMIC tests with hybrid balanced andunbalanced RF probes based on the traditional SOLR calibration technique [13–17], an MMIC on-wafertest method based on balanced and unbalanced RF pad structure is proposed. This method combinesan OSL second-order de-embedding technique with vector error correction , and cascade matrixtransformation technique, which introduces the vector error correction to the actual calibration planeand further improves the accuracy of the S-parameter extraction of the RF probe. After the vectorerror correction and de-embedding, the calibration reference plane can be accurately transferred to theprobe tips, as a result, significantly improving the test accuracy. Besides, an automatic test system isbuilt with the aid of the C# object-oriented language [18], which realizes the automatic performance ofinstrument control, data acquisition, result correction, data analysis , and graphical presentation ofthe results.
The rest of this paper is divided into four sections: The first section evaluates the calibration errorof the traditional test method, the second section introduces on-wafer test method of heteromorphystructure based on hybrid balanced and unbalanced RF probes in detail, the third section analyzes andverifies the approach based on the test results , and the last section draws the conclusion.
2. The Calibration Error Evaluation of Traditional Test Method
More and more MMICs adopt balanced and unbalanced test pad structures in layout designdue to the stringent size restrictions and integration requirements. For this kind of heteromorphystructures, the calibration error of two traditional test methods are evaluated. The SPDT switch chipand limiter chip with both GSG and SG pads shown in Figure 1 are used as an example. The bottoms ofboth chips are metalized. The first method turns each unbalanced SG pad into a conventional GSG padby wire bonding to a GSG through structure, so that the structure of balanced GSG pads at both endscan be calibrated with classic method. Then, the S-parameters of the chips are obtained by S-parameterde-embedding of the GSG through structure together with the bonding wire from the measured results.The results of the “wire-bonding” method are highly consistent with the real values , and are thusused as references in this paper. However, after the test, the micro-assembly of the chips cannot befully recovered without damage. Thus, this method can only be applied to evaluation tests but notto large-scale on-wafer test. The second method directly adopts SOLR for heteromorphy structureon-wafer calibration by ignoring the calibration error. The comparison between the test results of thesetwo methods is shown in Figure 2. Although the “direct SOLR” method does not destroy the chip,it cannot be applied due to the large result deviation.
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(a) (b)
(c) (d)
Figure 1. Illustration of hybrid balanced and unbalanced MMIC test structure and methods with RF
probes, with (a,b) corresponding to GSG‐GSG test method after bonding and SG‐GS test method of
switch, (c,d) corresponding to GSG‐GSG test method after bonding and SG‐GS test method of
limiter.
(a) (b)
(c) (d)
Figure 2. Comparison of the S‐parameters results between different methods, with (a,b)
corresponding to return loss and insertion loss of switch, (c,d) corresponding to return loss and
insertion loss of limiter.
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-10
0
2 4 6 8 10 12 14 16 18 20
Ret
urn
Los
s(d
B)
Frequency(GHz)
Switch
DUT_Bonding_S11
DUT_SOLR_S11
DUT_Bonding_S22
DUT_SOLR_S22
-4
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
2 4 6 8 10 12 14 16 18 20
Inse
rtio
n L
oss(
dB)
Frequency(GHz)
Switch
DUT_Bonding_S21
DUT_SOLR_S21
DUT_Bonding_S12
DUT_SOLR_S12
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-25
-20
-15
-10
-5
0
8 8.5 9 9.5 10 10.5 11 11.5 12
Ret
urn
Los
s(d
B)
Frequency(GHz)
Limiter
DUT_Bonding_S11
DUT_SOLR_S11
DUT_Bonding_S22
DUT_SOLR_S22
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
8 8.5 9 9.5 10 10.5 11 11.5 12
Inse
rtio
n L
oss(
dB
)
Frequency(GHz)
Limiter
DUT_Bonding_S21
DUT_SOLR_S21
DUT_Bonding_S12
DUT_SOLR_S12
Figure 1. Illustration of hybrid balanced and unbalanced MMIC test structure and methods with RFprobes, with (a,b) corresponding to GSG-GSG test method after bonding and SG-GS test method ofswitch, (c,d) corresponding to GSG-GSG test method after bonding and SG-GS test method of limiter.
Electronics 2018, 7, x FOR PEER REVIEW 3 of 12
(a) (b)
(c) (d)
Figure 1. Illustration of hybrid balanced and unbalanced MMIC test structure and methods with RF
probes, with (a,b) corresponding to GSG‐GSG test method after bonding and SG‐GS test method of
switch, (c,d) corresponding to GSG‐GSG test method after bonding and SG‐GS test method of
limiter.
(a) (b)
(c) (d)
Figure 2. Comparison of the S‐parameters results between different methods, with (a,b)
corresponding to return loss and insertion loss of switch, (c,d) corresponding to return loss and
insertion loss of limiter.
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0
2 4 6 8 10 12 14 16 18 20
Ret
urn
Los
s(d
B)
Frequency(GHz)
Switch
DUT_Bonding_S11
DUT_SOLR_S11
DUT_Bonding_S22
DUT_SOLR_S22
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-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
2 4 6 8 10 12 14 16 18 20
Inse
rtio
n L
oss(
dB)
Frequency(GHz)
Switch
DUT_Bonding_S21
DUT_SOLR_S21
DUT_Bonding_S12
DUT_SOLR_S12
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-5
0
8 8.5 9 9.5 10 10.5 11 11.5 12
Ret
urn
Los
s(d
B)
Frequency(GHz)
Limiter
DUT_Bonding_S11
DUT_SOLR_S11
DUT_Bonding_S22
DUT_SOLR_S22
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
8 8.5 9 9.5 10 10.5 11 11.5 12
Inse
rtio
n L
oss(
dB
)
Frequency(GHz)
Limiter
DUT_Bonding_S21
DUT_SOLR_S21
DUT_Bonding_S12
DUT_SOLR_S12
Figure 2. Comparison of the S-parameters results between different methods, with (a,b) correspondingto return loss and insertion loss of switch, (c,d) corresponding to return loss and insertion loss of limiter.
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Further reasons of the failure of the second test method are as follows. The signal flow graph ofthe eight-error terms model used in the SOLR calibration method is shown in Figure 3. VNA (VectorNetwork Analyzer, Keysight, CA, USA) is adopted for testing. The transmission matrix betweenthe VNA transceiver’s plane and the MMIC plane is represented by a two-port error matrix [19–21].The product error equations related to thru calibration is shown in Equations (1) and (2).
e10 · e32 =ERR · ETF
ERR + EDR(ELF− ESR)(1)
e01 · e23 =ERF · ETR
ERF + EDF(ELR− ESF)(2)
ELF =S11T − EDF
[ERF + ESF(S11T − EDF)](3)
ELR =S22T − EDR
[ERR + ESR(S22T − EDR)](4)
ETF = (S21T − EXF)(1− ESF · ELF) (5)
ETR = (S12T − EXR)(1− ESR · ELR) (6)
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Further reasons of the failure of the second test method are as follows. The signal flow graph of
the eight‐error terms model used in the SOLR calibration method is shown in Figure 3. VNA (Vector
Network Analyzer, Keysight, CA, USA) is adopted for testing. The transmission matrix between the
VNA transceiver’s plane and the MMIC plane is represented by a two‐port error matrix [19–21]. The
product error equations related to thru calibration is shown in Equations (1) and (2).
10 32 ( )
ERR ETFe e
ERR EDR ELF ESR
⋅⋅ =
+ - (1)
01 23 ( )
ERF ETRe e
ERF EDF ELR ESF
⋅⋅ =
+ - (2)
11
11[ ( )]T
T
S EDFELF
ERF ESF S EDF
-=
+ - (3)
22
22[ ( )]T
T
S EDRELR
ERR ESR S EDR
-=
+ - (4)
21( )(1 )TETF S EXF ESF ELF= - - ⋅ (5)
12( )(1 )TETR S EXR ESR ELR= - - ⋅ (6)
Among them, EDF (forward directivity error), EDR (reverse directivity error), ESF (forward
source mismatch error), ESR (reverse source mismatch error), ERF (forward reflection tracking
error), ERR (reverse reflection tracking error) can be obtained by the calibration of Open, Short and
Load standards. Other error terms, ELF (forward load mismatch error), ELR (reverse load mismatch
error), ETF (forward transmission tracking error), and ETR (reverse transmission tracking error)
require the test of thru standard. As shown in Equations (3)–(6), ( 1, 2; 1, 2)ijTS i j= = represents the
S‐parameter of thru standard. For this kind of passive and reciprocal device, there is 12 21T TS S= , and
the EXF (forward crosstalk error) and EXR (reverse crosstalk error) can be ignored.
S21
S11 S22
S12
e22 e33 e00 e11
e10
e01
e32
a2 e23
DUT
b2a1
b1
VNA
ERROR ERROR
b1M
a1M
a2M
b1M
Reference Plane
Figure 3. Schematic diagram of the 8‐error‐terms model.
For the tests with different types of probes, full‐wave electromagnetic simulations are
performed to obtain the S‐parameters of the corresponding thru structures shown in Figure 4 and
Figure 5, referring to the right angle ISS (Impedance Standard Substrate) for up to 67 GHz provided
by Cascade (Substrate Material: Alumina; Thickness: 625 μm ± 25 μm; Dielectric constant: 9.9).
Then, after substituting the S‐parameters of the thru structures into the error model Equations
(3)–(6), the error terms are obtained. As shown in Figure 6, when using the SG‐GSG probes (Figure
4b) or SG‐GS probes (Figure 4c) for SOLR calibration, the port impedance mismatch have a
significant impact on the error model parameters, causing large deviation in the test results of
MMICs [22]. Moreover, in order to meet the port matching conditions, the gap between S and G
should be modified when using the SG‐GS probes for SOLR calibration, as shown in Figure 4d, but
there is no corresponding ISS. Therefore, the traditional GSG thru standard cannot meet the SG port
Figure 3. Schematic diagram of the 8-error-terms model.
Among them, EDF (forward directivity error), EDR (reverse directivity error), ESF (forwardsource mismatch error), ESR (reverse source mismatch error), ERF (forward reflection tracking error),ERR (reverse reflection tracking error) can be obtained by the calibration of Open, Short and Loadstandards. Other error terms, ELF (forward load mismatch error), ELR (reverse load mismatch error),ETF (forward transmission tracking error) , and ETR (reverse transmission tracking error) require thetest of thru standard. As shown in Equations (3)–(6), SijT(i = 1, 2; j = 1, 2) represents the S-parameterof thru standard. For this kind of passive and reciprocal device, there is S12T = S21T , and the EXF(forward crosstalk error) and EXR (reverse crosstalk error) can be ignored.
For the tests with different types of probes, full-wave electromagnetic simulations are performedto obtain the S-parameters of the corresponding thru structures shown in Figures 4 and 5, referring tothe right angle ISS (Impedance Standard Substrate) for up to 67 GHz provided by Cascade (SubstrateMaterial: Alumina; Thickness: 625 µm ± 25 µm; Dielectric constant: 9.9). Then, after substituting theS-parameters of the thru structures into the error model Equations (3)–(6), the error terms are obtained.As shown in Figure 6, when using the SG-GSG probes (Figure 4b) or SG-GS probes (Figure 4c) for SOLRcalibration, the port impedance mismatch have a significant impact on the error model parameters,causing large deviation in the test results of MMICs [22]. Moreover, in order to meet the port matchingconditions, the gap between S and G should be modified when using the SG-GS probes for SOLRcalibration, as shown in Figure 4d, but there is no corresponding ISS. Therefore, the traditional GSG
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thru standard cannot meet the SG port matching requirements and the correct ELF, ELR, ETR , and ETFerror model parameters cannot be obtained. As a result, the errors of product terms e10 · e32 and e01 · e23
derived from them are further enlarged, resulting in unreliable test results shown in Figure 2.
Electronics 2018, 7, x FOR PEER REVIEW 5 of 12
matching requirements and the correct ELF, ELR, ETR, and ETF error model parameters cannot be
obtained. As a result, the errors of product terms 10 32e e⋅ and 01 23e e⋅ derived from them are
further enlarged, resulting in unreliable test results shown in Figure 2.
(a) (b)
(c) (d)
Figure 4. Models for electromagnetic simulation of thru with different types of probes, while (a)
represents GSG‐GSG model; (b) represents SG‐GSG model; (c) represents initial SG‐GS model; (d)
represents improved SG‐GS model.
(a) (b)
(c) (d)
Figure 5. Simulated S‐parameter comparison of thru with different types of probes, while (a)
represents GSG‐GSG model; (b) represents SG‐GSG model; (c) represents initial SG‐GS
model; (d) represents improved SG‐GS model.
-60
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-10
0
2 4 6 8 10 12 14 16 18 20
S11
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved-20
-15
-10
-5
0
5
2 4 6 8 10 12 14 16 18 20
S12
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
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-10
-5
0
5
2 4 6 8 10 12 14 16 18 20
S21
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
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0
2 4 6 8 10 12 14 16 18 20
S22
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
Figure 4. Models for electromagnetic simulation of thru with different types of probes, while (a)represents GSG-GSG model; (b) represents SG-GSG model; (c) represents initial SG-GS model;(d) represents improved SG-GS model.
Electronics 2018, 7, x FOR PEER REVIEW 5 of 12
matching requirements and the correct ELF, ELR, ETR, and ETF error model parameters cannot be
obtained. As a result, the errors of product terms 10 32e e⋅ and 01 23e e⋅ derived from them are
further enlarged, resulting in unreliable test results shown in Figure 2.
(a) (b)
(c) (d)
Figure 4. Models for electromagnetic simulation of thru with different types of probes, while (a)
represents GSG‐GSG model; (b) represents SG‐GSG model; (c) represents initial SG‐GS model; (d)
represents improved SG‐GS model.
(a) (b)
(c) (d)
Figure 5. Simulated S‐parameter comparison of thru with different types of probes, while (a)
represents GSG‐GSG model; (b) represents SG‐GSG model; (c) represents initial SG‐GS
model; (d) represents improved SG‐GS model.
-60
-50
-40
-30
-20
-10
0
2 4 6 8 10 12 14 16 18 20
S11
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved-20
-15
-10
-5
0
5
2 4 6 8 10 12 14 16 18 20
S12
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
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-10
-5
0
5
2 4 6 8 10 12 14 16 18 20
S21
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
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-30
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0
2 4 6 8 10 12 14 16 18 20
S22
(dB
)
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
Figure 5. Simulated S-parameter comparison of thru with different types of probes, while (a) representsGSG-GSG model; (b) represents SG-GSG model; (c) represents initial SG-GS model; (d) representsimproved SG-GS model.
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(a) (b)
(c) (d)
Figure 6. Comparison of error terms of SOLR calibration, with (a–d) corresponding to ELF, ELR, ETF
and ETR respectively.
From above, it can be known that the traditional on‐wafer thru standard based on balanced
structure cannot meet the impedance matching requirements of the hybrid balanced and unbalanced
RF probes at the same time. Therefore, the calibration accuracy is greatly reduced. In the following
section, a new solution which can be applied for wafer‐scale test with good accuracy is presented.
3. On‐Wafer Test Method of Heteromorphy Structure
In order to solve the accuracy issues of the existing test methods, this paper proposes an
on‐wafer test approach of MMIC based on hybrid balanced and unbalanced RF probes by combining
OSL second‐order de‐embedding technique with vector error correction and cascade matrix
transformation technique. With the aid of vector error correction, the calibration reference plane is
accurately extended to the probe tip surface.
The signal flow graph of OSL second‐order de‐embedding is shown in Figure 7. Firstly, the
coaxial calibration is performed; then the Open, Short and Load standards, with known reflection
coefficients iG , are measured to obtain the reflection coefficient MiG at the coaxial calibration plane.
Assuming that the Load calibration matches well ( 0L ), the S‐parameters of the RF probes can be
obtained according to Equations (7) and (8). Generally, the three‐order polynomial models of the
capacitance and the inductance are used to characterize the Open, Short and Load standards, and
their reflection coefficients OG , SG and LG can be obtained with the help of Equations (9) and
(10).
21 12111
1 221i
Mii
S SbS
a S
(7)
11 22 21 12
( ) ( ) ( )( )( ), ,
( ) ( )S ML MO O MS ML S O MS ML MO ML
MLS O MS MO S O MS MO
S S S S
(8)
0
0
ii
i
Z Z
Z Z
-G =
+ (9)
0
0.2
0.4
0.6
0.8
1
1.2
2 4 6 8 10 12 14 16 18 20
EL
F
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
0
0.2
0.4
0.6
0.8
1
1.2
2 4 6 8 10 12 14 16 18 20
EL
R
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
0
0.2
0.4
0.6
0.8
1
1.2
2 4 6 8 10 12 14 16 18 20
ET
F
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
0
0.2
0.4
0.6
0.8
1
1.2
2 4 6 8 10 12 14 16 18 20
ET
R
Frequency(GHz)
GSG_GSG
SG_GSG
SG_GS_Initial
SG_GS_Improved
Figure 6. Comparison of error terms of SOLR calibration, with (a–d) corresponding to ELF, ELR, ETFand ETR respectively.
From above, it can be known that the traditional on-wafer thru standard based on balancedstructure cannot meet the impedance matching requirements of the hybrid balanced and unbalancedRF probes at the same time. Therefore, the calibration accuracy is greatly reduced. In the followingsection, a new solution which can be applied for wafer-scale test with good accuracy is presented.
3. On-Wafer Test Method of Heteromorphy Structure
In order to solve the accuracy issues of the existing test methods, this paper proposes an on-wafertest approach of MMIC based on hybrid balanced and unbalanced RF probes by combining OSLsecond-order de-embedding technique with vector error correction and cascade matrix transformationtechnique. With the aid of vector error correction, the calibration reference plane is accurately extendedto the probe tip surface.
The signal flow graph of OSL second-order de-embedding is shown in Figure 7. Firstly, the coaxialcalibration is performed; then the Open, Short and Load standards, with known reflection coefficientsΓi , are measured to obtain the reflection coefficient ΓMi at the coaxial calibration plane. Assuming thatthe Load calibration matches well ( ΓL = 0 ), the S-parameters of the RF probes can be obtainedaccording to Equations (7) and (8). Generally, the three-order polynomial models of the capacitanceand the inductance are used to characterize the Open, Short and Load standards , and their reflectioncoefficients ΓO , ΓS and ΓL can be obtained with the help of Equations (9) and (10).
ΓMi =b1
a1= S11 +
S21S12Γi1− S22Γi
(7)
S11 = ΓML, S22 = ΓS(ΓML−ΓMO)+ΓO(ΓMS−ΓML)ΓSΓO(ΓMS−ΓMO)
, S21S12 = (ΓS−ΓO)(ΓMS−ΓML)(ΓMO−ΓML)ΓSΓO(ΓMS−ΓMO)
(8)
Γi =Zi − Z0
Zi + Z0(9)
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ZO = 1/(j2π f CO) = 1/(j2π f (C0 + C1 × f + C2 × f 2 + C3 × f 3))
ZS = j2π f LS = j2π f (L0 + L1 × f + L2 × f 2 + L3 × f 3)
ZL = RL + j2π f LL = RL + j2π f (L0 + L1 × f + L2 × f 2 + L3 × f 3)
(10)
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2 30 1 2 3
2 30 1 2 3
2 30 1 2 3
1/( 2 ) 1/( 2 ( ))
2 2 ( )
2 2 ( )
O O
S S
L L L L
Z j fC j f C C f C f C f
Z j fL j f L L f L f L f
Z R j fL R j f L L f L f L f
p p
p p
p p
= = + ´ + ´ + ´
= = + ´ + ´ + ´
= + = + + ´ + ´ + ´
(10)
S21
S11 S22
S12
Probe
(i=O,S,L)
DUT Measurement PlaneCoaxial Calibration Plane
ΓMi, Γi,
OpenShortLoad
(i=O,S,L)
Figure 7. Signal flow chart of the OSL method.
Actually, there are certain deviations between the ideal calibration plane and the actual
calibration plane (physical contact) of the non‐ideal standards due to the existence of the
transmission line. The attenuation and phase shift introduced by the deviation can be described by
an equivalent transmission line model. And the transmission line correction algorithm is further
used to eliminate these deviations by Equations (11)–(14). The simplified equivalent model is shown
in Figure 8, where iG represents the reflection coefficient of the ideal standard, 'iG is the actual
coefficient after correction, and rle- is the correction factor. α and β are the attenuation constant and phase constant of the transmission line, offset_loss and offset_delay are the insertion loss and time
delay of the transmission line, generally provided by the ISS manufacturer [23]. Function 910f is
the curve fitting factor, and offset_Z0 is the characteristic impedance of the transmission line with a
typical value of 50 Ω.
L: Load
L0 L1
L2
L3
L0 L1
L2
L3
RL
i=O,S,L
C0 C1 C2 C3
e-γl
e-γl
i=O,S,L
ActualCalibration
Plane
Γi,Γi',
O: Open
S: Short
IdealCalibration
Plane
Figure 8. Schematic diagram of the Standard parameter model.
90
_ _
2 _ 10
offset loss offset delay fl
offset Za
é ù⋅ê ú= ê úë û
(11)
2 _l f offset delay lb p a= ⋅ + (12)
Figure 7. Signal flow chart of the OSL method.
Actually, there are certain deviations between the ideal calibration plane and the actual calibrationplane (physical contact) of the non-ideal standards due to the existence of the transmission line.The attenuation and phase shift introduced by the deviation can be described by an equivalenttransmission line model. And the transmission line correction algorithm is further used to eliminatethese deviations by Equations (11)–(14). The simplified equivalent model is shown in Figure 8, whereΓi represents the reflection coefficient of the ideal standard, Γi
′ is the actual coefficient after correction, and e−rl is the correction factor. α and β are the attenuation constant and phase constant of thetransmission line, offset_loss and offset_delay are the insertion loss and time delay of the transmissionline, generally provided by the ISS manufacturer [23]. Function
√f /109 is the curve fitting factor ,
and offset_Z0 is the characteristic impedance of the transmission line with a typical value of 50 Ω.
Electronics 2018, 7, x FOR PEER REVIEW 7 of 12
2 30 1 2 3
2 30 1 2 3
2 30 1 2 3
1/( 2 ) 1/( 2 ( ))
2 2 ( )
2 2 ( )
O O
S S
L L L L
Z j fC j f C C f C f C f
Z j fL j f L L f L f L f
Z R j fL R j f L L f L f L f
p p
p p
p p
= = + ´ + ´ + ´
= = + ´ + ´ + ´
= + = + + ´ + ´ + ´
(10)
S21
S11 S22
S12
Probe
(i=O,S,L)
DUT Measurement PlaneCoaxial Calibration Plane
ΓMi, Γi,
OpenShortLoad
(i=O,S,L)
Figure 7. Signal flow chart of the OSL method.
Actually, there are certain deviations between the ideal calibration plane and the actual
calibration plane (physical contact) of the non‐ideal standards due to the existence of the
transmission line. The attenuation and phase shift introduced by the deviation can be described by
an equivalent transmission line model. And the transmission line correction algorithm is further
used to eliminate these deviations by Equations (11)–(14). The simplified equivalent model is shown
in Figure 8, where iG represents the reflection coefficient of the ideal standard, 'iG is the actual
coefficient after correction, and rle- is the correction factor. α and β are the attenuation constant and phase constant of the transmission line, offset_loss and offset_delay are the insertion loss and time
delay of the transmission line, generally provided by the ISS manufacturer [23]. Function 910f is
the curve fitting factor, and offset_Z0 is the characteristic impedance of the transmission line with a
typical value of 50 Ω.
L: Load
L0 L1
L2
L3
L0 L1
L2
L3
RL
i=O,S,L
C0 C1 C2 C3
e-γl
e-γl
i=O,S,L
ActualCalibration
Plane
Γi,Γi',
O: Open
S: Short
IdealCalibration
Plane
Figure 8. Schematic diagram of the Standard parameter model.
90
_ _
2 _ 10
offset loss offset delay fl
offset Za
é ù⋅ê ú= ê úë û
(11)
2 _l f offset delay lb p a= ⋅ + (12)
Figure 8. Schematic diagram of the Standard parameter model.
αl =[
o f f set_loss · o f f set_delay2o f f set_Z0
]√f
109 (11)
βl = 2π f · o f f set_delay + αl (12)
Electronics 2018, 7, 208 8 of 13
e−rl = e−(α+jβ)l (13)
Γ′i = Γie−2rl (14)
After substituting Γi′ into Equation (8), the corrected two-port S-parameters of the RF probes can
be extracted. The RF probes are passive reciprocal devices, whose S-parameters meet the formula S12 =
S21 = ±√
S21S12 , resulting in phase uncertainty problem [24]. To solve this problem, phase continuityand supplementary condition Phase|0Hz = 0 are introduced to select the phase branch, as shown inFigure 9. The true phase-frequency response of S21 both before and after the square root should becontinuous and the phase at zero frequency point is zero degree. First, the initial folded phase responseof S21S12 (red solid line) is unfolded (blue dot-dash line) based on the principle of phase continuity.Afterwards, a 180 cycle extension is performed along the vertical axis and a branch (blue dot-dashline) with a zero-frequency phase of 0 is selected , and the phase frequency response of the phasebranch is divided by 2 to obtain a true phase frequency response (black dash line).
Electronics 2018, 7, x FOR PEER REVIEW 8 of 12
( )rl j le e a b- - += (13)
' 2rli ie
-G =G (14)
After substituting 'iG into Equation (8), the corrected two‐port S‐parameters of the RF probes
can be extracted. The RF probes are passive reciprocal devices, whose S‐parameters meet the
formula 21 1212 21= S SS S = , resulting in phase uncertainty problem [24]. To solve this problem, phase
continuity and supplementary condition 0| 0HzPhase = are introduced to select the phase branch, as
shown in Figure 9. The true phase‐frequency response of 21S both before and after the square root
should be continuous and the phase at zero frequency point is zero degree. First, the initial folded
phase response of 21 12S S (red solid line) is unfolded (blue dot‐dash line) based on the principle of
phase continuity. Afterwards, a 180° cycle extension is performed along the vertical axis and a
branch (blue dot‐dash line) with a zero‐frequency phase of 0° is selected, and the phase frequency
response of the phase branch is divided by 2 to obtain a true phase frequency response (black dash
line).
Figure 9. The phase response characteristics.
After obtaining the S‐parameters ( AS , BS ) of the balanced and unbalanced RF probes, the
overall S‐parameter of the MMIC at coaxial calibration plane ( MS ), including the hybrid balanced
and unbalanced RF probes, is measured. Then, the cascade matrix transformation technique is used
to obtain the S‐parameter of the MMIC ( DS ) by probe parameters ( AS , BS ) de‐embedding from the
test result ( MS ). The block diagram of the test system is shown in Figure 10.
DUTProbe A Probe B
VNA
Deembedding Plane
Calibration Plane
Figure 10. Schematic diagram of the measurement system frame.
The scattering parameter matrixes MS , AS and BS are transformed into the transmission
parameter matrixes MT , AT and BT by using Equation (15), where MT , AT , BT and DT meet
Equation (16). Then the inverse matrix operation is performed, and the transmission parameter
-3500
-3000
-2500
-2000
-1500
-1000
-500
0
500
1000
1500
0 5 10 15 20 25 30 35 40
Ph
ase(°
)
Frequency(GHz)
Phase Response Measured_S21S12
Unwrapped_S21S12
Calculated_S21
Figure 9. The phase response characteristics.
After obtaining the S-parameters ( SA , SB ) of the balanced and unbalanced RF probes, the overallS-parameter of the MMIC at coaxial calibration plane ( SM ), including the hybrid balanced andunbalanced RF probes, is measured. Then, the cascade matrix transformation technique is used toobtain the S-parameter of the MMIC ( SD ) by probe parameters ( SA , SB ) de-embedding from the testresult ( SM ). The block diagram of the test system is shown in Figure 10.
Electronics 2018, 7, x FOR PEER REVIEW 8 of 12
( )rl j le e a b- - += (13)
' 2rli ie
-G =G (14)
After substituting 'iG into Equation (8), the corrected two‐port S‐parameters of the RF probes
can be extracted. The RF probes are passive reciprocal devices, whose S‐parameters meet the
formula 21 1212 21= S SS S = , resulting in phase uncertainty problem [24]. To solve this problem, phase
continuity and supplementary condition 0| 0HzPhase = are introduced to select the phase branch, as
shown in Figure 9. The true phase‐frequency response of 21S both before and after the square root
should be continuous and the phase at zero frequency point is zero degree. First, the initial folded
phase response of 21 12S S (red solid line) is unfolded (blue dot‐dash line) based on the principle of
phase continuity. Afterwards, a 180° cycle extension is performed along the vertical axis and a
branch (blue dot‐dash line) with a zero‐frequency phase of 0° is selected, and the phase frequency
response of the phase branch is divided by 2 to obtain a true phase frequency response (black dash
line).
Figure 9. The phase response characteristics.
After obtaining the S‐parameters ( AS , BS ) of the balanced and unbalanced RF probes, the
overall S‐parameter of the MMIC at coaxial calibration plane ( MS ), including the hybrid balanced
and unbalanced RF probes, is measured. Then, the cascade matrix transformation technique is used
to obtain the S‐parameter of the MMIC ( DS ) by probe parameters ( AS , BS ) de‐embedding from the
test result ( MS ). The block diagram of the test system is shown in Figure 10.
DUTProbe A Probe B
VNA
Deembedding Plane
Calibration Plane
Figure 10. Schematic diagram of the measurement system frame.
The scattering parameter matrixes MS , AS and BS are transformed into the transmission
parameter matrixes MT , AT and BT by using Equation (15), where MT , AT , BT and DT meet
Equation (16). Then the inverse matrix operation is performed, and the transmission parameter
-3500
-3000
-2500
-2000
-1500
-1000
-500
0
500
1000
1500
0 5 10 15 20 25 30 35 40
Ph
ase(°
)
Frequency(GHz)
Phase Response Measured_S21S12
Unwrapped_S21S12
Calculated_S21
Figure 10. Schematic diagram of the measurement system frame.
Electronics 2018, 7, 208 9 of 13
The scattering parameter matrixes SM , SA and SB are transformed into the transmission parametermatrixes TM , TA and TB by using Equation (15), where TM , TA , TB and TD meet Equation (16).Then the inverse matrix operation is performed , and the transmission parameter matrix TD of theDUT is obtained according to Equation (17). Finally, the transmission parameter TD of the DUT isconverted into desired scattering parameter SD according to Equation (18).[
Ti11 Ti12Ti21 Ti22
]=
(1
Si21
)[Si12Si21 − Si11Si22 Si11
−Si22 1
], i = M, A, B (15)
[TM] = [TA][TD][TB] (16)
[TD] = [TA]−1[TM][TB]
−1 (17)[SD11 SD12
SD21 SD22
]=
(1
TD22
)[TD12 TD11TD22 − TD12TD21
1 −TD12
](18)
4. Test Results and Analysis
Based on the on-wafer test method of the heteromorphy structure proposed in Section 3, this paperdesigned an on-wafer test system shown in Figure 11 to validate the solution. The system consists of avector network analyzer (Keysight PNA N5224A), GSG and SG RF probes (Cascade ACP-A-GSG-150,ACP-A-SG-150) and a microwave probe station (Cascaded Summit 11000BS). The switch and limiterchips mentioned in Figure 1 are selected as test samples. The photos of the MMICs are shown inFigure 11a,b , and the photo of the on-wafer test system based on the hybrid GSG-SG RF probes isshown in Figure 11c.
Electronics 2018, 7, x FOR PEER REVIEW 9 of 12
matrix DT of the DUT is obtained according to Equation (17). Finally, the transmission parameter
DT of the DUT is converted into desired scattering parameter DS according to Equation (18).
11 12 12 21 11 22 11
21 22 2221
1,i=M,A,B
1i i i i i i i
i i ii
T T S S S S S
T T SS
æ öé ù é ù-÷çê ú ê ú÷=ç ÷çê ú ê ú÷ç -è øë û ë û (15)
[ ] [ ][ ][ ]M A D BT T T T= (16)
[ ] [ ] [ ][ ]1 1
D A M BT T T T- -=
(17)
11 12 12 11 22 12 21
21 22 1222
1
1D D D D D D D
D D DD
S S T T T T T
S S TT
æ öé ù é ù-÷çê ú ê ú÷=ç ÷çê ú ê ú÷ç -è øë û ë û (18)
4. Test Results and Analysis
Based on the on‐wafer test method of the heteromorphy structure proposed in Section 3, this
paper designed an on‐wafer test system shown in Figure 11 to validate the solution. The system
consists of a vector network analyzer (Keysight PNA N5224A), GSG and SG RF probes (Cascade
ACP‐A‐GSG‐150, ACP‐A‐SG‐150) and a microwave probe station (Cascaded Summit 11000BS). The
switch and limiter chips mentioned in Figure 1 are selected as test samples. The photos of the
MMICs are shown in Figure 11a,b, and the photo of the on‐wafer test system based on the hybrid
GSG‐SG RF probes is shown in Figure 11c.
(a) (b) (c)
Figure 11. Photos of the switch and limiter chips and the test system. (a) The photo of the switch chip;
(b) The photo of the limiter chip; (c) The photo of the test system.
The S‐parameters of the SG and GSG probes obtained from the presented OSL method with
vector error correction are compared with the parameters provided by Cascade. It can be seen from
Figure 12 that the data obtained from the presented method is basically the same with factory data.
(a) (b)
GSG
SG SG
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1
0
2 4 6 8 10 12 14 16 18 20
Mag
(d
B)
Frequency(GHz)
Probe_A_OSL
Probe_A_Cascade
-200
-150
-100
-50
0
50
100
150
200
2 4 6 8 10 12 14 16 18 20
Pha
se(º
)
Frequency(GHz)
Probe_A_OSL
Probe_A_Cascade
Figure 11. Photos of the switch and limiter chips and the test system. (a) The photo of the switch chip;(b) The photo of the limiter chip; (c) The photo of the test system.
The S-parameters of the SG and GSG probes obtained from the presented OSL method with vectorerror correction are compared with the parameters provided by Cascade. It can be seen from Figure 12that the data obtained from the presented method is basically the same with factory data.
The S-parameters comparison between the test results of the method proposed in this paper andthe test results of the “wire-bonding” method mentioned in Section 2 is shown in Figure 13. It can beseen that the two results are quite close. The accuracy of our method is highly enhanced comparingwith the “direct SOLR” method shown in Figure 2.
Electronics 2018, 7, 208 10 of 13
Electronics 2018, 7, x FOR PEER REVIEW 9 of 12
matrix DT of the DUT is obtained according to Equation (17). Finally, the transmission parameter
DT of the DUT is converted into desired scattering parameter DS according to Equation (18).
11 12 12 21 11 22 11
21 22 2221
1,i=M,A,B
1i i i i i i i
i i ii
T T S S S S S
T T SS
æ öé ù é ù-÷çê ú ê ú÷=ç ÷çê ú ê ú÷ç -è øë û ë û (15)
[ ] [ ][ ][ ]M A D BT T T T= (16)
[ ] [ ] [ ][ ]1 1
D A M BT T T T- -=
(17)
11 12 12 11 22 12 21
21 22 1222
1
1D D D D D D D
D D DD
S S T T T T T
S S TT
æ öé ù é ù-÷çê ú ê ú÷=ç ÷çê ú ê ú÷ç -è øë û ë û (18)
4. Test Results and Analysis
Based on the on‐wafer test method of the heteromorphy structure proposed in Section 3, this
paper designed an on‐wafer test system shown in Figure 11 to validate the solution. The system
consists of a vector network analyzer (Keysight PNA N5224A), GSG and SG RF probes (Cascade
ACP‐A‐GSG‐150, ACP‐A‐SG‐150) and a microwave probe station (Cascaded Summit 11000BS). The
switch and limiter chips mentioned in Figure 1 are selected as test samples. The photos of the
MMICs are shown in Figure 11a,b, and the photo of the on‐wafer test system based on the hybrid
GSG‐SG RF probes is shown in Figure 11c.
(a) (b) (c)
Figure 11. Photos of the switch and limiter chips and the test system. (a) The photo of the switch chip;
(b) The photo of the limiter chip; (c) The photo of the test system.
The S‐parameters of the SG and GSG probes obtained from the presented OSL method with
vector error correction are compared with the parameters provided by Cascade. It can be seen from
Figure 12 that the data obtained from the presented method is basically the same with factory data.
(a) (b)
GSG
SG SG
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1
0
2 4 6 8 10 12 14 16 18 20
Mag
(d
B)
Frequency(GHz)
Probe_A_OSL
Probe_A_Cascade
-200
-150
-100
-50
0
50
100
150
200
2 4 6 8 10 12 14 16 18 20
Pha
se(º
)
Frequency(GHz)
Probe_A_OSL
Probe_A_Cascade
Electronics 2018, 7, x FOR PEER REVIEW 10 of 12
(c) (d)
Figure 12. Extracted S‐parameter results of the probes, with (a,b) corresponding to amplitude and
phase of S21 of the SG probe (probe A), respectively; (c,d) corresponding to amplitude and phase of
S21 of the GSG probe (probe B), respectively.
The S‐parameters comparison between the test results of the method proposed in this paper
and the test results of the “wire‐bonding” method mentioned in Section 2 is shown in Figure 13. It
can be seen that the two results are quite close. The accuracy of our method is highly enhanced
comparing with the “direct SOLR” method shown in Figure 2.
(a) (b)
(c) (d)
Figure 13. Comparison of the S‐parameters measurement results between different methods, with
(a,b) corresponding to return loss and insertion loss of switch, (c,d) corresponding to return loss and
insertion loss of limiter.
Since the method proposed in this paper requires a large number of complex and matrix
operations, object‐oriented C# language is used to build an automatic test program. The results
interface of the test program is shown in Figure 14. The program can execute a fully automatic
operation covering instrument control, data acquisition, results correction, data analysis and display
of graphical results, which avoids human interference, and solves the test efficiency problems faced
with the wafer‐scale test.
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1
0
2 4 6 8 10 12 14 16 18 20
Mag
(d
B)
Frequency(GHz)
Probe_B_OSL
Probe_B_Cascade
-200
-150
-100
-50
0
50
100
150
200
2 4 6 8 10 12 14 16 18 20
Pha
se(
º)
Frequency(GHz)
Probe_B_OSL
Probe_B_Cascade
-60
-50
-40
-30
-20
-10
0
2 4 6 8 10 12 14 16 18 20
Ret
urn
Los
s(d
B)
Frequency(GHz)
Switch
DUT_Bonding_S11
DUT_Deembedding_S11
DUT_Bonding_S22
DUT_Deembedding_S22
-4
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
2 4 6 8 10 12 14 16 18 20
Inse
rtio
n L
oss(
dB)
Frequency(GHz)
Switch
DUT_Bonding_S21
DUT_Deembedding_S21
DUT_Bonding_S12
DUT_Deembedding_S12
-40
-35
-30
-25
-20
-15
-10
-5
0
8 8.5 9 9.5 10 10.5 11 11.5 12
Ret
urn
Los
s(d
B)
Frequency(GHz)
Limiter
DUT_Bonding_S11
DUT_Deembedding_S11
DUT_Bonding_S22
DUT_Deembedding_S22
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
8 8.5 9 9.5 10 10.5 11 11.5 12
Inse
rtio
n L
oss(
dB
)
Frequency(GHz)
Limiter
DUT_Bonding_S21
DUT_Deembedding_S21
DUT_Bonding_S12
DUT_Deembedding_S12
Figure 12. Extracted S-parameter results of the probes, with (a,b) corresponding to amplitude andphase of S21 of the SG probe (probe A), respectively; (c,d) corresponding to amplitude and phase of S21
of the GSG probe (probe B), respectively.
Electronics 2018, 7, x FOR PEER REVIEW 10 of 12
(c) (d)
Figure 12. Extracted S‐parameter results of the probes, with (a,b) corresponding to amplitude and
phase of S21 of the SG probe (probe A), respectively; (c,d) corresponding to amplitude and phase of
S21 of the GSG probe (probe B), respectively.
The S‐parameters comparison between the test results of the method proposed in this paper
and the test results of the “wire‐bonding” method mentioned in Section 2 is shown in Figure 13. It
can be seen that the two results are quite close. The accuracy of our method is highly enhanced
comparing with the “direct SOLR” method shown in Figure 2.
(a) (b)
(c) (d)
Figure 13. Comparison of the S‐parameters measurement results between different methods, with
(a,b) corresponding to return loss and insertion loss of switch, (c,d) corresponding to return loss and
insertion loss of limiter.
Since the method proposed in this paper requires a large number of complex and matrix
operations, object‐oriented C# language is used to build an automatic test program. The results
interface of the test program is shown in Figure 14. The program can execute a fully automatic
operation covering instrument control, data acquisition, results correction, data analysis and display
of graphical results, which avoids human interference, and solves the test efficiency problems faced
with the wafer‐scale test.
-0.6
-0.5
-0.4
-0.3
-0.2
-0.1
0
2 4 6 8 10 12 14 16 18 20
Mag
(d
B)
Frequency(GHz)
Probe_B_OSL
Probe_B_Cascade
-200
-150
-100
-50
0
50
100
150
200
2 4 6 8 10 12 14 16 18 20
Pha
se(
º)
Frequency(GHz)
Probe_B_OSL
Probe_B_Cascade
-60
-50
-40
-30
-20
-10
0
2 4 6 8 10 12 14 16 18 20
Ret
urn
Los
s(d
B)
Frequency(GHz)
Switch
DUT_Bonding_S11
DUT_Deembedding_S11
DUT_Bonding_S22
DUT_Deembedding_S22
-4
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
2 4 6 8 10 12 14 16 18 20
Inse
rtio
n L
oss(
dB)
Frequency(GHz)
Switch
DUT_Bonding_S21
DUT_Deembedding_S21
DUT_Bonding_S12
DUT_Deembedding_S12
-40
-35
-30
-25
-20
-15
-10
-5
0
8 8.5 9 9.5 10 10.5 11 11.5 12
Ret
urn
Los
s(d
B)
Frequency(GHz)
Limiter
DUT_Bonding_S11
DUT_Deembedding_S11
DUT_Bonding_S22
DUT_Deembedding_S22
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
8 8.5 9 9.5 10 10.5 11 11.5 12
Inse
rtio
n L
oss(
dB
)
Frequency(GHz)
Limiter
DUT_Bonding_S21
DUT_Deembedding_S21
DUT_Bonding_S12
DUT_Deembedding_S12
Figure 13. Comparison of the S-parameters measurement results between different methods, with (a,b)corresponding to return loss and insertion loss of switch, (c,d) corresponding to return loss and insertionloss of limiter.
Electronics 2018, 7, 208 11 of 13
Since the method proposed in this paper requires a large number of complex and matrixoperations, object-oriented C# language is used to build an automatic test program. The resultsinterface of the test program is shown in Figure 14. The program can execute a fully automaticoperation covering instrument control, data acquisition, results correction, data analysis and displayof graphical results, which avoids human interference , and solves the test efficiency problems facedwith the wafer-scale test.Electronics 2018, 7, x FOR PEER REVIEW 11 of 12
Figure 14. The result interface of the automatic test system.
5. Conclusions
This paper evaluates the calibration errors of a hybrid balanced and unbalanced RF probes test
with the traditional SOLR method and proposes an MMIC test method based on hybrid balanced
and unbalanced RF probes. A SPDT switch chip and a limiter chip are measured for method
validation. This method combines the OSL second‐order de‐embedding technique with the vector
error correction and cascade matrix transformation technique. The accuracy of the extraction of the
RF probe is improved by this method. As a result, the calibration reference plane can be accurately
translated to the probe tip, which significantly improves the test accuracy. Furthermore, with the aid
of the object‐oriented C# language, an automatic test system is built to be effectively applied to
wafer‐level testing of MMIC products.
Author Contributions: Methodology, Y.B.; Software, X.D.; Validation, J.M.; Data Curation, Y.G.; Writing:
Original Draft Preparation, Y.B.; Writing: Review and Editing, Z.W.; Supervision, Z.W.; Project Administration,
F.Y.; Funding Acquisition, J.M.
Funding: This research was funded by the National Natural Science Foundation of China grant number
61604128 and the Fundamental Research Funds for the Central Universities grant number 2017QN81002.
Acknowledgments: The authors would like to thank the Institute of Aerospace Electronics Engineering of
Zhejiang University for providing research platform and technical support.
Conflicts of Interest: The authors declare no conflict of interest.
References
1. Jiang, H.U.; Sun, L.L. A Novel SOLT Calibration for Direct Measurement of On‐Wafer DUTs. J. Microw.
2006, 22, 135–137
2. Yob, R.C.; Mahyuddin, N.M.; Ain, M.F. Implementation of Signal Flow Graph Rules Analysis on
Short‐Open‐Load‐Thru Calibration Algorithm. In Proceedings of the 9th International Conference on
Robotic, Vision, Signal Processing and Power Applications, Penang, Malaysia, 2–3 February 2016.
3. Seguinot, C.; Kennis, P.; Legier, J.F. Multimode TRL. A new concept in microwave measurements: Theory
and experimental verification. IEEE Trans. Microw. Theory Tech. 1998, 46, 536–542.
4. Yadav, C.; Deng, M.; Matos, M.D.; Fregonese, S.; Zimmer, T. Importance of complete characterization
setup on on‐wafer TRL calibration in sub‐THz range. In Proceedings of the 2018 IEEE International
Conference on Microelectronic Test Structures (ICMTS), Austin, TX, USA, 19–22 March 2018.
5. Phung, G.N.; Schmückle, F.J.; Doerner, R.; Heinrich, W.; Probst, T.; Arz, U. Effects Degrading Accuracy of
CPW mTRL Calibration at W Band. In Proceedings of the IEEE/MTT‐S International Microwave
Symposium (IMS), Philadelphia, PA, USA, 10–15 June 2018.
Figure 14. The result interface of the automatic test system.
5. Conclusions
This paper evaluates the calibration errors of a hybrid balanced and unbalanced RF probes testwith the traditional SOLR method and proposes an MMIC test method based on hybrid balanced andunbalanced RF probes. A SPDT switch chip and a limiter chip are measured for method validation.This method combines the OSL second-order de-embedding technique with the vector error correctionand cascade matrix transformation technique. The accuracy of the extraction of the RF probe isimproved by this method. As a result, the calibration reference plane can be accurately translatedto the probe tip, which significantly improves the test accuracy. Furthermore, with the aid of theobject-oriented C# language, an automatic test system is built to be effectively applied to wafer-leveltesting of MMIC products.
Author Contributions: Methodology, Y.B.; Software, X.D.; Validation, J.M.; Data Curation, Y.G.; Writing: OriginalDraft Preparation, Y.B.; Writing: Review and Editing, Z.W.; Supervision, Z.W.; Project Administration, F.Y.;Funding Acquisition, J.M.
Funding: This research was funded by the National Natural Science Foundation of China grant number 61604128and the Fundamental Research Funds for the Central Universities grant number 2017QN81002.
Acknowledgments: The authors would like to thank the Institute of Aerospace Electronics Engineering ofZhejiang University for providing research platform and technical support.
Conflicts of Interest: The authors declare no conflict of interest.
References
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