agilent technologies ~ advancements in noise measurement by ken wong, 08-2008
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Agilent Technologies ~ Advancements in Noise Measurement by Ken Wong, 08-2008. Source: www.agilent.com. Reproduced with Permission, Courtesy of Agilent Technologies, Inc. by Bob Laughlin.TRANSCRIPT
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 1
Advancements in Noise Measurement
byKen Wong, Senior Member IEEER&D Principal EngineerComponent Test DivisionAgilent Technologies, Inc.
Reproduced with Permission, Courtesy of Agilent Technologies, Inc. by Bob Laughlin.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 2
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Measurements• Y-Factor • Cold source • Noise Parameters• Noise Wave• Correcting for Source Impedance Mismatch • Correcting for Receiver Mismatch and Noise
VNA Noise Figure Measurements• Setup (S)• Setting Input (Fwd) and Output (Rev) Powers• Choosing Noise Bandwidth• Setting Noise Averaging Factor• Choosing the Receiver Gain Setting
Objectives
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 3
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calibration • Noise Source Calibration (S)• S-parameter Calibration (S)• Noise Tuner Calibration (S)
Verification• Mismatch Line• Amp Characteristics• Combined S11• Combined Gain• Combined Noise Figure
Objectives (cont)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 4
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
The Early Days
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 5
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Agilent’s Noise Figure Legacy
340A 195889701980
SA with NF2002
8560/90 with NF1995
85120 1999
NFA2000
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 6
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Definition
( )( )
/(noise factor) 1
/ *= = = +
∗in out add
a in a inout
S N N NFS N G N G N
Ga
Sin
Nin Nout
Sout
00
* ; *= =
= = +out a in out a in addT T T TS G S N G N N
DEVICE
Ga ≡ Available Gain, NF (Noise Figure) ≡ 10*log10(F) dB
D. Vondran, “Noise Figure Measurement: Corrections Related to Match and Gain,” Microwave J., pp 22-38, Mar. 1999Collantes, J. M., R. D. Pollard, et al. (2002). "Effects of DUT mismatch on the noise figure characterization: a comparative analysis of two Y-factor techniques." Instrumentation and Measurement, IEEE Transactions on 51(6): 1150-1156.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 7
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Definition in Terms of Noise Temperature
0
1*
= = +out e
a in
N TFG N T
T0 Nout
0* ; * * *= ∗ =in add a eN k T B N G k T B
DEVICE
0-23
290 ; bandwidth
Boltzmann's constant = 1.380 6505×10 joule/kelvin effective input noise temperature of device
≡ ≡
≡≡e
T K B
kT
Te, Ga
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 8
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Effective Temperature Versus Noise Figure
1.00
10.00
100.00
1000.00
0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0
NF (dB)
Te (K
)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 9
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Definition In Terms Of Noise Parameters
2si sY ne
niNoiseless two-port
( )2
2
min min 2 20
4
1 1
Γ − Γ⎛ ⎞= + − = +⎜ ⎟
+ Γ − Γ⎝ ⎠
opt sn ns opt
s opt s
R RF F Y Y FG Z
2si sY Noisy
two-port
IRE Subcommittee 7.9 On Noise: “Representation Of Noise In Linear Two-ports,” Proc. IRE, Vol. 48, Pp. 69-74, Jan. 1960
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 10
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise parameters Definition (cont)
Γopt ≡ optimum input noise matchZ0 = reference impedanceΓs = source match
( )2
2
min min 2 20
4
1 1
Γ −Γ⎛ ⎞= + − = +⎜ ⎟
+ Γ − Γ⎝ ⎠
opt sn ns opt
s opt s
R RF F Y Y FG Z
Yopt ≡ optimum input admittanceYs = source admittanceGs = real part of Ys
Fmin ≡ minimum noise factorRn ≡ noise resistance
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 11
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Source ENR – Excess Noise Ratio
h c10
0
T TENR 10log
T⎛ ⎞−
≡ ⎜ ⎟⎝ ⎠
Th = Hot Noise TemperatureTc = Cold Noise TemperatureT0 = 290 K
Tc = T0 when noise sources are calibrated by reference labs.
Noise source346C 10 MHz – 26.5 GHz
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 12
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Y factor Method
( )0 0
*1 1* 1 *
−= = + = +
−out e hot cold
a in
N T T Y TFG N T Y T
Thot
Pout
DEVICE
Te, GaTcold
Pout,hot=kBGa(Thot + Te) Pout,cold=kBGa(Tcold + Te)
,
,
1
out hot hot colde
out cold
P T YTY TP Y
−= =
−
Assumes ALL Reflections are the same.
“Fundamentals of RF and Microwave Noise Figure Measurements,” Hewlett-Packard Application Note 57-1, Palo Alto, CA July 1983
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 13
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Actual Y factor Measurement Calibration
Ga(R)
Thot
Nout(R)
RECEIVER
Te(R)TcoldPout
Γi(rec)
Γs(cold)
Γs(hot)
Receiver Calibration
( )( ) ( )
( )( ) 0 0
*1 1* 1 *Γ
−= = + = +
−s
out R e R hot coldR
a R in
N T T Y TFG N T Y T
Assumes Γs(hot) = Γs(cold)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 14
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Actual Y factor Measurement
Ga(D)
Thot
Nout(D)
DEVICE
Te(D)Tcold Nout(all)
RECEIVER
Pout
Γs(hot)Γs(cold) Γo(device) Γi(rec)
Γi(device)
Ga(R)Te(R)
( )( )0
*11 *Γ
−= +
−s
hot coldall
T Y TFY T
( )( )
( ) ( )( )
1Γ
Γ
−= − o device
s
R
device alla D
FF F
G
Note that ( )( ) ( )Γ Γ≠o device sR RF F
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 15
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Some Y factor Measurement Assumptions
( ) ( )( )
( ) ( )
−=
−hot all cold all
a devicehot R cold R
N NG
N N
( )( ) ( )Γ Γ=o device sR RF F
( ) ( )Γ = Γs hot s cold
Notes:Ga (available gain) is a function of S11, S22 and ΓsΓs ≡ source reflection of the incident signal
True only if S11 and S22 are <<1
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 16
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Four Examples Of Y-Factor Measurements
What you want for good NF accuracy!
Noise source
Noise source
Automated multi-instrument
(ATE) environment
On-wafer environment
On-wafer multi-instrument
(ATE) environment
1 2
3 4
Noise source Noise source
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 17
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Cold Noise Source Technique
Ga PN
nDut
0 a
PF 1
kT BG= +
Need to know gain very accuratelyGa is a function of of S11, S22 and Γs
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 18
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
T = T cal
PN
T ~ 10,000K
DUT
T = T meas
PN
Calibrate
Measure
Cold Noise Figure Cal and Measurement
kGB k Gain Bandwidth= ⋅ ⋅
hot cold
hot cold
P PkGB
T T−
=−
hot 0r
nhot0
ncold
T T 1FPT 1P
−= ⋅
⎛ ⎞−⎜ ⎟⎝ ⎠
nDut r
a
P1F F 1G kGB
⎛ ⎞= ⋅ − +⎜ ⎟⎝ ⎠
ΓsΓo(device)
Γi(rec)
Γi(device)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 19
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Parameters
2si sY ne
niNoiseless two-port
Noise figure varies as a function of source impedance
Noise figure varies as a function of source impedance
( )2s
2
opt
2
sopt
o
nmin
Γ1Γ1
ΓΓZ
4RFF−+
−+=
Four noise parameters: Fmin, Rn, Γopt (mag), Γopt (phase)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 20
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise parameters Definition
Γopt ≡ optimum input noise matchZ0 = reference impedanceΓs = source match
( )2
2
min min 2 20
4
1 1
Γ −Γ⎛ ⎞= + − = +⎜ ⎟
+ Γ − Γ⎝ ⎠
opt sn ns opt
s opt s
R RF F Y Y FG Z
Yopt ≡ optimum input admittanceYs = source admittanceGs = real part of Ys
Fmin ≡ minimum noise factorRn ≡ noise resistance
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 21
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise parameters Definition –Noise Temperature
Γopt ≡ optimum input noise matchZ0 = reference impedanceΓs = source match
( )
( )2 2
0 0min min 2 2
0
4
1 1
− Γ −Γ= + = +
+Γ − Γ
n s opt opt snn
s opt s
R T Y Y T RT T TG Z
Yopt ≡ optimum input admittanceYs = source admittanceGs = real part of Ys
Tmin ≡ minimum noise TemperatureRn ≡ noise resistanceT0 ≡ 290°K
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 22
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
• Plots of noise figure circles versus impedance (at one frequency)
• Fmin is lowest noise figure and occurs at Γopt
• F changes with Γ• F changes with device bias
Noise Parameters
Fmin at Γopt
Increasing noise figure
Increasing noise figure
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 23
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Measuring Noise parameters
DUT
VNA
Noise source
TUNER
NFM
A. C. Davidson, B. W. Leake, et al. (1989). "Accuracy improvements in microwave noise parameter measurements." Microwave Theory and Techniques, IEEE Transactions on 37(12): 1973-1978.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 24
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise wave representation – S-parameters
a1
b1 a2
b2[S]bn1
bn2
11 11 12 1
22 21 22 2
n
n
bb s s abb s s a⎛ ⎞⎛ ⎞ ⎛ ⎞ ⎛ ⎞
= + ⎜ ⎟⎜ ⎟ ⎜ ⎟ ⎜ ⎟⎝ ⎠ ⎝ ⎠ ⎝ ⎠ ⎝ ⎠
P. Penfield, Jr "Wave Representation of Amplifier Noise." IRE Transactions On Circuit Theory: Mach (1962) pp. 84-86K. Hartmann, “Noise Characterization of Linear Circuits,” IEEE Transactions on Circuits and Systems, Vol. cAS-23, No. 10, Oct. 1976, pp. 581-590R.P. Meys, “A Wave Approach to the Noise Properties of Linar Microwave Devices,” IEEE Transactions on Microwave Theory and Techniques, Vol. MTT-26, No. 1, Jan. 1978, pp 34-37S. W. Wedg ,and D. B. Rutledge (1992). "Wave techniques for noise modeling and measurement." Microwave Theory and Techniques, IEEE Transactions on 40(11): 2004-2012.
2 *1 1 2 11 12
2* 21 222 1 2
C⎛ ⎞ ⎛ ⎞⎜ ⎟= = ⎜ ⎟⎜ ⎟ ⎝ ⎠⎝ ⎠
n n ns
n n n
b b b cs cscs csb b b
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 25
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Measurement using (S) noise correlation matrix
( )( )
2 2
2 2 *11 11 11
2 *2 2 1 222 12
1 1 11 2 122 2
21
21
* *21 2121 21
2 21
1
1 1 2 Re 1
, ,
⎧ ⎫− Γ + Γ +⎛ ⎞⎪ ⎪= ⎜ ⎟⎨ ⎬⎜ ⎟−Γ ⎡ ⎤−Γ + −Γ Γ⎪ ⎪⎝ ⎠ ⎣ ⎦⎩ ⎭
= = = = = =
s s s
outs s s s
n n nn
TkP
S S S
b b bcs csX b cs X XS
XB s
X
SS
X
S
Noise output power from two-port is
J. Randa, W. Wiatr, “Conte Carlo Estimation of Noise Parameter Uncertainties,” IEE Proc. Sci. Meas. Technology, Vol. 149, No. 6, Nov. 2002, pp. 333-337
( )0= +out av eP kBG T T
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 26
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise correlation matrix (CS) in terms of noise parameters
( )( ) ( ) ( )
( ) ( )
2
2 11 11min 11 21 min 112 2
0 0
2
21121 min 11 21 min2 2
0 0
1 4 141 1 11 1
4 1 41 1
1 1
opt n opt optn
opt opt
n opt opt n opt
opt opt
s R sRF s s F sZ Z
R s Rs F s s F
Z Z
⎛ ⎞⎛ ⎞− Γ Γ − Γ⎜ ⎟⎜ ⎟− − + − −⎜ ⎟⎜ ⎟+ Γ +Γ⎜ ⎟⎝ ⎠⎜ ⎟= ⎜ ⎟⎜ ⎟⎛ ⎞ ⎛ ⎞Γ − Γ Γ⎜ ⎟⎜ ⎟ ⎜ ⎟− − −⎜ ⎟⎜ ⎟ ⎜ ⎟⎜ ⎟+ Γ +Γ⎝ ⎠ ⎝ ⎠⎝ ⎠
sC
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 27
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
New Noise Measurement System
DUT
Noise Tuner
Noise Receiver Inside
ADAPTER Noise Source
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 28
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
ECal as Noise Tuner
PNA-X varies source match around 50 ohms using an ECal module ECal can provide 7 impedance states
(Z1, F1), (Z2, F2), …
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 29
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure in PNA – contributions
Speed and accuracy –• Single Connection S-parameters and Noise Figure• Fast Step Frequency Sweep • Complete Mismatch Correction
Use of ECal or Compatible Impedance Tuner
Embedding and De-embedding of Probes in On-Wafer Noise Measurements
Can Accommodate Coax Noise Source for On-Wafer Noise Measurements
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 30
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calibration of the receiver
5 unknowns, linear equation
i
( )( )
2 2
2 2
1
2 21*
11 11 11
221
1
1 1 2 Re 1
⎧ ⎫− Γ + Γ +⎛ ⎞⎪ ⎪⎜ ⎟= ⎨ ⎬⎜ ⎟−Γ ⎡ ⎤−Γ + −Γ Γ⎪ ⎪⎝ ⎠ ⎣ ⎦⎩ ⎭
s s s
outs s s s
TkP
X S
X
S XS
B S
Note: The PNA-X uses a different form of the above equation.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 31
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calibration of receiver- solution of equations
Require Minimum Of 5 Equations To Solve
Can Be Over-determined
At Least One Measurement Must Be Made With Different Source Temperature
Use Noise Source (Known ENR, Measure ΓCold, ΓHot)
ECal Module Provides 7 Terminations
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 32
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Mode Instrument Default Settings
S-parameter Mode Source Power -30 dBm
Noise RF BW 4 MHz
Noise IF BW 2 MHz
Noise Averaging Point to Point (1 = 10K)
Noise Receiver Gain 30 dB
Factory Receiver Cal ON
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 33
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Measurement Instrument Setup
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 34
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Measurement Softkeys
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 35
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Set Up
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 36
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Set Up
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 37
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Measurement Calibration
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 38
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Cal
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 39
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
S-parameters and Noise Calibrations
Noise Tuner
ADAPTER
Ph, Pc, Γh, Γc
Noise Source
This step provides 2 of the five measurements required.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 40
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
S-parameters and Noise Calibrations
Noise Tuner
ADAPTER This step provides the rest of measurements required to calibrate the noise receiver. Pnt(i), Γnt(i)Γnr
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 41
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
S-parameters and Noise Calibrations
Noise Tuner
S-parameter calibration completes the calibration sequence.
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 42
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Measurement of DUT
Known from Measured S-parameters
( )( )
2 2
2 2
1
2 21*
11 11 11
221
1
1 1 2 Re 1
⎧ ⎫− Γ + Γ +⎛ ⎞⎪ ⎪⎜ ⎟= ⎨ ⎬⎜ ⎟−Γ ⎡ ⎤−Γ + −Γ Γ⎪ ⎪⎝ ⎠ ⎣ ⎦⎩ ⎭
s s s
outs s s s
TkP
X S
X
S XS
B S
4 unknowns, linear equation
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 43
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
DUT S-parameters and Noise Measurement
DUT
Noise Tuner
Meas S-parametersPout(i) @ each Γnt(i)
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 44
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Measurement System With On-Wafer Probes
Noise Tuner
4
Noise Source
FULL 2-port Cal
1-port Cal
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 45
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
60 µm FET
0 5 10 15 20 25
Frequency (GHz)
F (1
dB
per
div
isio
n)
corrected
cold
Y-factor
N8975Data sets offset by 1dB
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 46
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Measurements Compared
0
2
4
6
8
10
1 2 3 4 5 6
Frequency (GHz)
NF
(dB
)
0
2
4
6
8
10
12
14
16
18
20
Gai
n (d
B)
NFA
PNA/NF
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 47
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Uncertainty Example (ATE Setup)
2.000
2.500
3.000
3.500
4.000
4.500
0.5 2.5 4.5 6.5 8.5 10.5 12.5 14.5 16.5 18.5 20.5 22.5 24.5 26.5
GHz
NF (d
B)
PNA-X
Y-factor with noise source connected to DUT via switch
matrix
Amplifier:Gain = 15 dBInput/output match = 10 dBNF = 3 dBGamma opt = 0.268 ∠ 0o
Fmin = 1.87 dBRn = 12 – 33
0.2 dB
0.75 dB
0.5 dBY-factor with noise source
directly at DUT input
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 48
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise Figure Uncertainty Example (Wafer Setup)
PNA-X
Y-factor with noise source connected to DUT input
Y-factor with noise source connected to DUT via switch matrix
Amplifier:Gain = 15 dBInput/output match = 10 dBNF = 3 dBGamma opt = 0.268 ∠ 0o
Fmin = 1.87 dBRn = 12 – 33Wave model correlation = 50%
2.000
2.500
3.000
3.500
4.000
4.500
0.5 2.5 4.5 6.5 8.5 10.5 12.5 14.5 16.5 18.5 20.5 22.5 24.5 26.5
GHz
NF (d
B)
PNA-X
Y-factor with noise source connected to probe input
Y-factor with noise source connected to probe via switch matrix
Amplifier:Gain = 15 dBInput/output match = 10 dBNF = 3 dBGamma opt = 0.268 ∠ 0o
Fmin = 1.87 dBRn = 12 – 33
0.3 dB
1.1 dB
0.75 dB
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 49
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Verification approach
Need To Avoid Using An Active Device– Cannot Guarantee Behavior Over Time– Dependence On Temperature– Noise May Be Injected Through Bias Supply
Use Mismatched Transmission Line, Passive Device– Noise Parameters, Noise Figure Are Calculated From S-
parameters– Can Cascade With Any Amplifier And De-embed
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 50
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Mismatch Transmission Line Characteristics
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 51
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Noise wave representations
a1L
b1L a2L
b2L[TL]anL
bnL
a1A
b1A a2A
b2A[TA]anA
bnA
50 Ω 25 Ω 50 Ω AMP
[TL], [CL] [TA], [CA]
2 2* *
2 2* *;C C
⎛ ⎞ ⎛ ⎞⎜ ⎟ ⎜ ⎟= =⎜ ⎟ ⎜ ⎟⎝ ⎠ ⎝ ⎠
nL nL nL nA nA nAtL tA
nL nL nL nA nA nA
a a b a a b
b a b b a b
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 52
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Measured S-parameters of Amplifier
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 53
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calculated vs. Measured Combined |S11|
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 54
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calculated vs. Measured Combined Gain
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 55
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Calculated vs. Measured Combined Noise Figure
Uncertainty Bark=2
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 56
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Additional References:
[1] D. Vondran, “Noise Figure Measurement: Corrections Related to Match and Gain,” Microwave J., pp 22-38, Mar. 1999[2] Collantes, J. M., R. D. Pollard, et al. (2002). "Effects of DUT mismatch on the noise figure characterization: a comparative analysis of two Y-factor techniques." Instrumentation and Measurement, IEEE Transactions on 51(6): 1150-1156.[3] “Fundamentals of RF and Microwave Noise Figure Measurements,” Hewlett-Packard Application Note 57-1, Palo Alto, CA July 1983[4] IRE Subcommittee 7.9 On Noise: “Representation Of Noise In Linear Two-ports,” Proc. IRE, Vol. 48, Pp. 69-74, Jan. 1960[4] A. C. Davidson, B. W. Leake, et al. (1989). "Accuracy improvements in microwave noise parameter measurements." Microwave Theory and Techniques, IEEE Transactions on 37(12): 1973-1978.[5] R.Q. Lane, “The Determination of Device Noise Parameters,” Proceedings of the IEEE, Aug. 1969, pp. 1461-1462[6] P. Penfield, Jr "Wave Representation of Amplifier Noise." IRE Transactions On Circuit Theory: Mach (1962) pp. 84-86[7] K. Hartmann, “Noise Characterization of Linear Circuits,” IEEE Transactions on Circuits and Systems, Vol. cAS-23, No. 10, Oct. 1976, pp. 581-590[8] R.P. Meys, “A Wave Approach to the Noise Properties of Linar Microwave Devices,” IEEE Transactions on Microwave Theory and Techniques, Vol. MTT-26, No. 1, Jan. 1978, pp 34-37[9] S. W. Wedg ,and D. B. Rutledge (1992). "Wave techniques for noise modeling and measurement." Microwave Theory and Techniques, IEEE Transactions on 40(11): 2004-2012.[10] J. Randa, W. Wiatr, “Conte Carlo Estimation of Noise Parameter Uncertainties,” IEE Proc. Sci. Meas. Technology, Vol. 149, No. 6, Nov. 2002, pp. 333-337[11] E.C. Valk, D. Routledge, J.F. Vaneldik, T.L. Landecker, “De-Embedding Two-Port Noise Parameters Using a Noise Wave Model,” IEEE Transactions on Instrumentation and Measurement, vol. 37, no. 2, June 1988, pp 195-200
IEEE IMS SCV Chapter Mtg
May 21, 2008Page 57
Aerospace and Defense Symposium 2007EuMw 2007 Agilent Workshop
By Ken WongAdvancements in Noise Measurement
Test port 1
R1
Source 1
OUT 1OUT 2
Source 2
OUT 1 OUT 2
Test port 2
R2
35 dB
65 dB
65 dB
Rear panel
A
35 dB
B
Source 2 Output 1
Source 2 Output 2
Noise receivers
10 MHz -3 GHz
3 - 26.5 GHz
DUT
Noise Source
24V DC
Noise Option Block Diagram