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T. Lee, Stanford University Center for Integrated Systems
Linearity, Time-Variation, Phase Modulation and Oscillator Phase
Linearity, Time-Variation, Phase Modulation and Oscillator Phase Noise
Prof. Thomas H. LeeStanford University
[email protected]://www-smirc.stanford.edu
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Preliminaries (to refresh dormant neurons...)
A system is linear as long as superposition holds.
Scaling of a single input is included, since scaling may al-ways be viewed as the result of summing.
The response to an impulse then yields sufficient informa-tion to deduce the response to any arbitrary input.
All real systems may be made to act nonlinearly for some in-puts (e.g., the response to 1mV may differ in shape and odor from the response to a gigavolt).
Linearity thus holds only over some restricted range of excita-tions, in practice.
A system is time-invariant if the only result of time-shifting any input is to shift the response by precisely the same amount.
If a system is LTI, it may be shown that excitation at
f
produces a response only at
f
.
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Preliminaries
If a system is LTV, it is no longer generally true that an excitation at
f
produces a response at the same frequen-cy.
Superposition still holds, however, so the response to the sum of two inputs may be deduced from the response to each.
If a system is nonlinear, the response may also contain spectral components not present in the excitation.
Dependency of output on combination of inputs not neces-sarily linear; this difference can be used as a basis for deter-mining whether spectral shaping is due to time-variation or nonlinearity.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Oscillator with Input Noise Sources
i n1 t( )
i n2 t( )
i nM t( )
V out t( ) A t( ) f ω0t φ t( )+[ ]⋅=
t
Vout
Oscillator
Non-ideal waveform
Ideal waveform
V out t( ) A ω0t φ0+( )cos⋅=
Noise current
v n1 t( )
v n2 t( )
v nN t( )
sources.
Noise voltagesources.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Desired SignalStrong Adjacent Channel
Desired Signal
RF
LO
IF
The desired signal is buried under the phase noise of an adjacent strong channel.
Phase Noise in RF Applications
f
f
f
fRF
fLO
fIF
RF
LO
IF
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Units of Phase Noise
log(∆ω)=log(ω-ω0)
L ∆ω 1
f 3------
1
f 2------
Measured in dB below carrier per unit bandwidth.
(-20dB/dec)
(-30dB/dec)
Sv ω( )
ω
∆ω
ω0
dBc Hz⁄[ ]
ω1 f 3⁄
dBc
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Isubstrate
Vsupply
Isupply
Substrate and Supply Noise
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Phase Noise: General Considerations
Consider simple oscillator:
RLC
+
noiseless
negative
R
:
Can show that noise-to-signal power ratio is
Negative-
R
must cancel the tank loss in steady state.
Noise current sees pure
LC
impedance.
G C LNoiselessV
4kTG
EnergyRestorer
NS
Vn
2
Vsig
2
kTE
stored
ωkTQP
diss
= = =
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
General Considerations
Practical oscillators operate in one of two regimes:
Current-limited
, in which the oscillation amplitude is linear-ly proportional to
I
bias
R
tank
.
Voltage-limited
, in which the oscillation amplitude is large-ly independent of bias current.
Ibias
Vosc
Current-limited
Voltage-limited
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
General Considerations
In the voltage-limited regime, increases in bias current do not increase carrier power.
Additional dissipation only increases noise power, so CNR degrades (decreases).
In the current-limited regime, increases in bias current increase signal power faster than noise power.
CNR increases until boundary with voltage-limited region is approached.
Best oscillator performance is typically achieved near the transition point between current- and voltage-limit-ed modes of operation.
T. Lee, Stanford University Center for Integrated Systems
Short Course: CMOS RF IC Design
Oscillator Phase Noise
An expression for noise-to-carrier ratio reveals important optimization objectives:
Vcarrier∝ IbiasRtank==> Pcarrier ∝ (Ibias)2Rtank in the current-lim-ited regime of oscillation.
Pnoise = kT/C = kTω2L, if dominated by tank loss.
So, N/C ∝ kTω2L/(Ibias)2Rtank to an approximation.
Generally want to minimize L/R to optimize oscillator for a given oscillation frequency and power consumption. This result contradicts much published advice, which advocates
maximizing tank inductance.
N/C is important, but also need to know noise spectrum.
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
General Considerations
Assuming all noise comes from tank loss, PSD of tank voltage is given approximately by
.
Noise power splits evenly between phase and ampli-tude domains. Then, we finally have
.
Funny units: Some dBc/hertz at a certain offset frequency. Example: –110dBc/Hz @ 600kHz offset, at 1.8GHz.
vn
2
∆f
in
2
∆fZ
2⋅ =4kTG 1
G
ω0
2Q∆ω⋅
2
=4kTRω
02Q∆ω
2
=
L ∆ω =10 logv
n
2∆f⁄
vsig
2⋅ =10 log 2kT
Psig
ω0
2Q∆ω
2
⋅⋅
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Simple LTI Model vs. Reality
Previous expression doesn’t quite describe real phase noise spectra:
log ∆ω
L(∆ω)
2−
3−
∆ω1 f
3⁄
ωc
RealityOur LTI eqn.
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Leeson Model
Leeson provided empirical
fix to remove discrepancies:
.
Factor
F
accounts for excess noise in all regions.
∆ω
1/
f
3
accounts for 1/
f
3
region close to carrier.
First additive factor of 1 accounts for noise floor.
Problem: Can’t compute these fudge factors
a priori
; they are basically
post hoc
fitting parameters.
Need to revisit unstated assumptions.
Is an oscillator truly a linear, time-invariant system?
L ∆ω =10 log 2FkTP
sig
1ω
02Q∆ω
+
2
1
∆ω1 f
3⁄
∆ω+
⋅ ⋅⋅
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
C Li(t)δ t τ–( )
t
i(t)
t
Vout
t
Vout
Oscillators Are Time-Variant Systems
τ
Impulse injected at the peak of amplitude.
∆V
∆V
Even for an ideal LC oscillator, the phase response is Time Variant.
Impulse injected at zero crossing.τ
τ
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Once Introduced, phase error persists indefinitely.
Non-linearity quenches amplitude changes over time.
θ
∆θ
V
dVdt--------
LimitCycle
a
b
∆V
Active Device
C Lδ t τ–( )
t
i(t)
τ
G -G(A)
Amplitude Restoring Mechanism
i(t)
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
Phase Impulse Response
φ t( )hφ t τ,( )
0 t
i(t)
τ 0 τ
hφ t τ,( )Γ ωoτ( )
qmax-------------------u t τ–( )=
t
i t( )
The unit impulse response is:
Γ x( ) is a dimensionless function periodic in 2π, describing how much
phase change results from applying an impulse at time: t Tx
2π------=
The phase impulse response of an arbitrary oscillator is a time varying step.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
t
t
t
t
V out t( ) V out t( )
Γ ω0t( ) Γ ω0t( )
LC Oscillator Ring Oscillator
Impulse Sensitivity Function (ISF)
The ISF quantifies the sensitivity of every point in the waveform to perturbations.
Waveform
ISF
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
φ t( ) hφ t τ,( )i τ( )dτ∞–
∞
∫1
qmax---------------- Γ ω0τ( )i τ( )dτ
∞–
t
∫= =
φ t( )i t( )hφ t τ,( )
Γ ω0τ( )
qmax-------------------u t τ–( )=
Superposition Integral:
Phase Response to an Arbitrary Source
Γ ω0t( )
∞–t
∫ ω0t φ t( )+[ ]cosi t( )
qmax----------------
φ t( )ψ t( ) V t( )
IdealIntegration
PhaseModulation
Equivalent representation:
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
i t( ) φ t( ) V t( )hφ t τ,( ) ω0t φ t( )+[ ]cos
LTV system Nonlinear system
Phase Noise Due to White Noise
i n2
∆f---------
L ∆ω Γrms
2
qmax2
----------------in
2 ∆f⁄
2∆ω2-------------------⋅=
For a white input noise current with the spectral density of
The phase noise sideband power below carrier at an offset of ∆ω is:
Γrms is the rms value of the ISF.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
ISF is a periodic function:
cn nω0t θn+( )cos
c0
c1 ω0t θ1+( )cos
Σ ω0t φ t( )+[ ]cos
i t( )qmax-------------
φ t( )
∞–t
∫
∞–t
∫
∞–t
∫
V t( )
ISF Decomposition
Phase can be written as:
φ t( ) 1qmax------------- c0 i τ( )dτ
∞–
t
∫ cn i τ( ) nω0τ( )cos dτ∞–
t
∫n 1=
∞
∑+=
Γ ωot( ) c0 cn nω0τ θn+( )cosn 1=
∞
∑+=
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
c0c1 c2 c3
2ω0ω0 3ω0ω
Sφ ω( )
i n2
∆f------- ω( )
1f--- Noise
Sv ω( )
2ω0ω0 3ω0ω
ω
PM∆ω
∆ω ∆ω ∆ω
∆ω
Noise Contributions from nωo
φ t( ) 1qmax------------- c0 i τ( )dτ
∞–
t
∫ cn i τ( ) nωτ( )cos dτ∞–
t
∫n 1=
∞
∑+=
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
c012π------ Γ x( )dx
0
2π
∫=
t
t
V out t( )
Γ ωt( )
Symmetric rise and fall time
t
t
V out t( )
Γ ωt( )
Asymmetric rise and fall time
Effect of Symmetry
The dc value of the ISF is governed by rise and fall time symmetry, and
controls the contribution of low frequency noise to the phase noise.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
1/f 3 Corner of Phase Noise Spectrum
ω1 f
3⁄ω1 f⁄
c0Γrms--------------
2
=
The 1/f3 corner of phase noise is NOT the same as 1/f corner of device noise
log(ω-ωo)
L ∆ω( )
1f 2-----
c0
c1
c2
c3
ω1f---
ω 1
f 3----
By designing for a symmetric waveform, the performancedegradation due to low frequency noise can be minimized.
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
0.5 1.0 1.5 2.0 2.5Wp to Wn ratio
-80.0
-70.0
-60.0
-50.0
-40.0
-30.0
Sid
eban
d po
wer
bel
ow c
arrie
r (d
Bc)
Sidebands Due to Low Frequency Injection
Effect of Rise and Fall Time Symmetry
WN/L
WP/L
fo=1GHzfoff=50MHz
i t( )
1 2 3 4 5Analytical ExpressionSimulation
http://smirc.stanford.edu/papers/CICC98s-ali.pdf Email: [email protected]
t
V out t( ) V out t( )
t
i t( )
t
i t( ) i t( )
A low frequency current induces a frequency change for the asymmetric waveform.
C
Effect of Symmetry
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
10kHz 100kHz 1MHzOffset from Multiple Integer of Carrier (fm)
-50.0
-40.0
-30.0
-20.0
-10.0
Sid
eban
d P
ower
bel
ow C
arrie
r (d
Bc)
Injection at Integer Multiples of f0
f=fmf=f0+fmf=2f0+fmf=3f0+fmf=4f0+fm
1 2 3 4 5
i t( ) I n f 0 f m+( )sin=
fm dBc
f0
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
1µA 10µΑ 100µΑ 1mAInjected Current (amperes)
-80.0
-60.0
-40.0
-20.0
Sid
eban
d P
ower
bel
ow C
arrie
r (d
Bc)
f=fmf=f0+fmf=2f0+fmf=3f0+fm
Sideband Power vs. Injection Current
i t( ) I n f 0 f m+( )sin=
1 2 3 4 5
fm dBc
f0
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
100kHz 1MHzFrequency of Injection (Hz)
-55
-45
-35
Sid
eban
d P
ower
bel
ow C
arrie
r (d
Bc)
Symmetric, n1
Symmetric, n4
Asymmetric, n1
Asymmetric, n4
Symmetric vs. Asymmetric Ring Oscillator
i1 t( )
1 2 3 4 5
i4 t( )
fm dBc
f0
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
0
5
10
15
20
Col
lect
or V
olta
ge (
Vol
ts)
0 5ns 10ns 15nsTime
0
1mA
2mA
3mA
Col
lect
or C
urre
nt
Time Varying Current in Colpitts Oscillator
10kΩ
40pF
200pF500µA
200nH
Gnd
Gnd
Vcc
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
i n t( ) i n0 t( ) α ω0t( )=
i n0 t( )
α ω0t( )
Cyclostationary Properties, Time Domain
φ t( ) in τ( )Γ ω0τ( )
qmax------------------dτ
∞–
t
∫=
in0 τ( )α ω0τ( )Γ ω0τ( )
qmax-------------------------------------dτ
∞–
t
∫=
Γeff x( ) Γ x( ) α x( )⋅=
Effective ISF:
A cyclostationary source can be modeled as stationary with a new ISF.
Noise Modulating Function (NMF)
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
0.0 2.0 4.0 6.0x (radians)
-1.5
-0.5
0.5
1.5
Colpitts Oscillator
Γeff x( ) Γ x( )α x( )=
Γ x( )
α x( )
Effective ISF
ISFNMF α x( )
Γ x( )
Γeff x( )
Gnd
Vcc
T. Lee, Stanford University Center for Integrated Systems
Short Course: Phase Noise in Oscillators
Plus ça change...
To exploit cyclostationary effects, arrange to supply energy to the tank impulsively, where the ISF is a minimum.
This idea is actually very old; mechanical clocks use an es-capement to deliver energy from a spring, to a pendulum in impulses.
Coupled topendulum
Drivenby spring
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Phase Noise
In the best implementations, impulses are delivered at or near the pendulum’s velocity maxima. The escape-ment thus restores energy without disturbing the period of oscillation. [Airy, 1826]
See: www.database.com/~lemur/dmh-airy-1826.html (my thanks to Byron Blanchard for finding this reference.)
Similarly, the optimal moments for an
LC
oscillator are near the voltage maxima.
L/2
C
Vdd
A Symmetric LC Oscillator
Uses the same current twice for high transconductance.
WN/L
WP/L
WN/L
WP/L
Adjust ratiosto fine tune
[Also appears in: J.Craninckx, et al, Proceedings of CICC 97.]
symmetry
L/2
L
C
VDD
Itail
Itail
Itail
Tank Voltage Amplitude
Itail
-Itail
t
i(t)
Assuming fast switching of the
differential pair, the current can
be approximated as:
ReqLCi(t)
Itail
-Itail
t
i(t)
Tank Voltage Amplitude
Assuming rectangular waveform:
Vmax4π--- I tailReq=
Effectively, the current waveform
is closer to sinusoidal, therefore:
Vmax I tailReq≈
“Current limited” mode .
2 4 6 8 10 12 14 16 18 20
Tail current (mA)
0.5
1.0
1.5
2.0
2.5
3.0
3.5
Tan
k vo
ltage
sw
ing
(vol
t)
Vdd=1.5V
Vdd=2.5V
Vdd=3.0V
Modes of Amplitude Limiting
Voltage Limited
Current Limited
Complementary cross-coupled LC oscillator
i p12 i p2
2
in12
in22
i tail2
L
C
VDD
bias
vrs2 rs
Major Noise Sources
Different noise sources affect
phase noise differently.
in2
∆f------ 4kTγµCox
WL----- VGS VT–( )=
Valid in both long and short
channel regimes.
Inductor Noise:
vn2
∆f------ 4kT rs=
C
L
i1 t( )
i2 t( )r r
R
C
L
i2 t( ) i1– t( )
2---------------------------
2r
Equivalent Circuit for Differential Sources
DifferentialEquivalent
in2
∆f------
diff pair–
14---
in12
∆f--------
in22
∆f--------
i p12
∆f--------
i p22
∆f--------+ + +
12---
in2
∆f------
i p2
∆f------+
= =
0.5
1.0
1.5
2.0
2.5
Nod
e V
olta
ge (
V)
0.0 1.0 2.0 3.0 4.0 5.0 6.0x (radians)
-1.5
-1.0
-0.5
0.0
0.5
1.0
1.5
ISF
V+V-
Vtail
NMOS ISF
PMOS ISF
Tail ISF
Waveform and ISF
Effect of Tail Current Source
L
C
VDD
2ω0ω0
ω
i n2
∆f------- ω( )
1f--- Noise
i tail2
For the tail current source, only
in the vicinity of even harmonics
of the tail current source affect
phase noise.
low frequency noise and noise
Die Photo of the Complementary Oscillator
700µm x 800µm
L L
C
Active
Bypass Bypass
Driver
Pad limited
0.25µm process
103
104
105
106
107
Offset from carrier (Hz)
-140
-130
-120
-110
-100
-90
-80
-70
-60
-50P
hase
noi
se b
elow
car
rier
(dB
c/H
z)
Complementary cross coupled LC oscillatorf0=1.8GHz, Pdiss=6mWatt
106 107103 104 105
Phase Noise vs. Offset from Carrier
2 4 6 8 10 12 14 16Tail Current (mA)
-126
-124
-122
-120
-118
-116
-114
-112
Pha
se n
oise
at 6
00K
Hz
offs
et (
dBc/
Hz)
f0=1.8GHz, 0.25µm Process (VDD =3V)
Measurement
Complementary Cross-Coupled LC Oscillator
C
L
Vdd
bias
Gnd
Itail
Γ2rms=0.5
Simulated ISF
Complementary Cross-Coupled VCO
1.5
2
2.5
3
24
68
1012
1416
x 10−3
−126
−124
−122
−120
−118
−116
−114
−112
f0=1.8GHz, 0.25µm Process
Pha
se n
oise
bel
ow c
arrie
r at
600
kHz
offs
et
Vdd Itail (mA)
-121dBc/Hz@600kHz
f0=1.8GHz
P=6mW
CL
Vdd
bias
Gnd
Itail
Complementary vs. NMOS-Only VCO
Vdd
C
bias
Gnd
L/2 L/2
Itail
CL
Vdd
bias
Gnd
Itail
11.5
22.5
3
2 4 6 8 10 12 14 16
x 10−3
−126
−124
−122
−120
−118
−116
−114
−112
f0=1.8GHz, 0.25µm Process
VddItail (mA)
Pha
se n
oise
bel
ow c
arrie
r at
600
kHz
offs
et
NMOS-Only
Complementary
T. Lee, Stanford University Center for Integrated Systems
Another example (Margarit et al.)
Gnd
Bias
VCC
Bias
L2 L1
R2 R1C2
C1
C4 C3
1.6 mA1.2 mA0.8 mA0.4 mA
0
227ns 228ns 229ns 230ns 231ns
227ns 228ns 229ns 230ns 231ns
Col
lect
or c
urre
nth φφ
(°/p
C)
20
10
0
–10
–20h φφef
f (°/
pC) (
dash
ed)
227ns 228ns 229ns 230ns 231ns
227ns 228ns 229ns 230ns 231ns
VCO
outp
ut vo
ltage 500 mV
–500 mV
h φφ (°
/pC)
4
2
0
–2
–4
T. Lee, Stanford University Center for Integrated Systems
Predicted vs. measured
LTV model
Spectre
Offset frequency (Hz)102 103 104 105 106
0
–10
–20
–30
–40
–50
–60
–70
–80
–90
–100
–110
–120
–130
–140
–150
dBc/Hz
http://smirc.stanford.edu/papers/CICC98s-ali.pdf Email: [email protected]
Approximate ISF for Ring Oscillators
2π
2f 'max------------
1f 'max------------
Γ x( )
x
2π x
f 'max
f x( )
f– 'max
1
1f 'max------------
2f 'max------------
The peak of the ISF is inversely proportional to the maximum slope of the normalized waveform.
Γrms2 1
2π------ Γ2 x( ) xd0
2π∫
42π------ x 2 xd
0
1 f 'max⁄
∫2
3π------1
f 'max-------------
3= = =
http://smirc.stanford.edu/papers/CICC98s-ali.pdf Email: [email protected]
Γrms2 2π2
3η3--------- 1
N3
------=
t Dη
f 'max-------------=
Risetime and Delay Relationship
2π x
f 'max
f x( )
f– 'max
1
1f 'max------------
ηf 'max------------
ηf 'max------------
2π 2Nt D2Nηf 'max-------------= =Period:
Stage Delay:
1f 'max-------------
πNη--------=⇒
ISF RMS:
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
102 103 104 105 106
Offset from the Carrier (Hz)
-130
-80
-30
Sid
eban
d be
low
Car
rier
per
Hz
(dB
c/H
z)
f0=232MHz, 2µm Technology
L ∆f 10 0.84 ∆f2⁄( )log=
L 500kHz 114.7dBcHz----------–=
ω 1
f 3-----
75kHz=
L 500kHz 114.5dBcHz----------–=
ω 1
f 3-----
80kHz=
Predicted:
Measured:
5-Stage Single-Ended Ring Oscillator
http://smirc.stanford.edu/papers/Orals98s-ali.pdf Email: [email protected]
102 103 104 105 106-130
-80
-30
Sid
eban
d P
ower
bel
ow C
arrie
r pe
r H
z (d
Bc/
Hz)
f0=115MHz, 2µm Process
Offset from the Carrier (Hz)
L ∆f 10 0.152 ∆f2⁄( )log=
L 500kHz 122.1dBcHz----------–=
ω 1
f 3-----
43kHz=
L 500kHz 122.5dBcHz----------–=
ω 1
f 3-----
45kHz=
Predicted:
Measured:
11-Stage Single-Ended Ring Oscillator
http://smirc.stanford.edu/papers/CICC98s-ali.pdf Email: [email protected]
10Number of Stages, N
0.1
1.0
RM
S V
alue
of I
SF
ISF RMS vs. Number of Stages
2 3
+: Fixed Frequency, 5V Supplyo: Fixed Drive, Similar Invertersx: Fixed Frequency, 3V Supply
Inverter Chain CMOS Ring Oscillator
__: 4/N1.5 (η=0.75)
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10Number of Stages, N
0.1
RM
S v
alue
of I
SF
3 4
0.2
0.3
+: Fixed Power, Fixed Swingo: Fixed Power, Fixed Load Resistancex: Fixed Tail Current, Fixed Load Resistance
ISF RMS vs. Number of Stages
Differential MOS Ring Oscillator
__: 3/N1.5 (η=0.9)
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VDD
bias
Gnd
RL RL
Itail
W/L W/Lin2
∆f------
N
in2
∆f------
Load
P NItailVDD=
f 01
2NtD------------- 1
2ηNtr---------------
I tail
2ηNqmax-----------------------≈ ≈=
in2
∆f------
in2
∆f------
N
in2
∆f------
Load
+ 4kT Itail1
Vchar------------- 1
RLI tail----------------+
= =
L min ∆f 83η------ N⋅ kT
P------
VDD
Vchar-------------
VDD
RLI tail----------------+
f 0
∆f------
2
⋅ ⋅ ⋅≈
Vchar VGS VT–( ) γ⁄=
Vchar EcL γ⁄=
N Stages
Power Dissipation:
Frequency:
Noise:
Short channel:
Long channel:
Phase Noise in Differential Ring Oscillator
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L min ∆f 83η------ N⋅ kT
P------
VDD
Vchar-------------
VDD
RLI tail----------------+
f 02
∆ f2
---------⋅ ⋅ ⋅≈
For a given power and frequency, phase noise degrades
with number of stages, N, in differential ring oscillators.
Doubling the number of stages:
VDD
bias
Gnd
RL/2 RL/2
Itail /2
W/L W/L
RL is divided by 2 to keep the frequency constant,
Itail is divided by 2 to keep the power constant,
Therefore:Maximum charge swing, qmax, is 4 times smaller.
This is NOT the case for single-ended ring, since the swing is constant.
Effect of Number of Stages on Phase Noise
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VDD
bias
Gnd
RL RL
Itail
Control
W/L W/L
Differential Ring Oscillators
Effective channel length: Leff=0.25µm.
Unsilicided poly load resistors.
N Stages
Maximum frequency of 5.4GHz.
http://smirc.stanford.edu/papers/CICC98s-ali.pdf Email: [email protected]
0 10 20 30 40 50 60 70 80NMOS width (µm)
-104
-102
-100
-98
-96
-94
-92
-90
Pha
se N
oise
at 1
MH
z of
fset
(dB
c/H
z)
Predicted and Measured Phase Noise
Differential Ring Oscillators; RL=1kΩ, Leff=0.25µm
4.47GHz
3.39GHz
2.24GHz1.19GHz
Measured
Predicted
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Die Photo of 12-Stage Differential Ring Osc.
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W/LNtail
W/LNinv
W/LPtail
W/LPinv
Nbias
Pbias
0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0Symmetry Voltage (VPbias+VNbias) [V]
200kHz
400kHz
600kHz
800kHz
1.0MHz
1.2MHz
1/f3
Cor
ner
Fre
quen
cy
9-Stage Current-Starved Single-Ended VCO
Vsym=VPbias+VNbias
f0=600MHz, 0.25µm Process
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Amplitude Noise
Phase noise generally dominates close-in spectrum. Amplitude noise typically dominates far-out spectrum.
Effect of amplitude noise may be accommodated with the same general approach: Investigate impulse re-sponse.
If amplitude control mechanism acts as a first-order system (e.g., if it is well damped), amplitude impulse response will die out with a time constant equal to the inverse bandwidth of the control loop.
For an
LC
tank, this bandwidth is the tank bandwidth,
ω
0
/Q.
Corresponding contribution to noise spectrum is flat to frequency offset equal to that bandwidth, then rolls off; produces pedestal in overall response.
If amplitude control is underdamped (e.g., behaves as 2nd order), can get peaking in the spectrum.
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Amplitude Response
Possible responses corresponding to these control dy-namics look roughly as follows:
log ∆ω
L(∆ω)
2−
From amplitude noise
From phase noise
Underdamped
Well-damped
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Summary and Conclusions
LTI theories say:
Maximize signal power and resonator
Q
and operate at edge of current-limited regime, with minimum ratio
L
/
R
consis-tent with oscillation.
Can’t do anything about 1/
f
3
corner frequency.
Corner frequency is strictly technology-limited.
LTV theory says:
Continue to maximize signal power, resonator
Q
, and
R
/
L.
Use tapped tanks (à la Clapp, e.g.).
Maximize symmetry (in the ISF sense) to reduce 1/
f
3
corner frequency.
Choose topologies and bias conditions so that energy is re-turned to tank impulsively.
Tom Lee, Stanford University Center for Integrated Systems
A Phase Noise Tutorial
Acknowledgments
Prof. Ali Hajimiri of Caltech, who developed this theory while a Ph.D. student at Stanford.
David Leeson, for graciously encouraging us to build on his theory.
Web URL is, again: http://www-smirc.stanford.edu