image-20241124184248887


Mixed-Mode S-parameter

12 May 2021 Introduction to Mixed-Mode S-parameters [https://blog.teledynelecroy.com/2021/05/introduction-to-mixed-mode-s-parameters.html]

image-20251025193029645

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Bert Simonovich. A Guide for Single-Ended to Mixed-Mode S-parameter Conversions [https://www.signalintegrityjournal.com/articles/1832-a-guide-for-singleended-to-mixedmode-s-parameter-conversions]

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single-ended S-parameters

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Mixed-mode S-parameters

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Missing Term in KVL

Prof. Kolb/Whites. EE 382 Applied Electromagnetics Lecture 8: Maxwell's Equations and Electrical CIrcuits [http://montoya.sdsmt.edu/ee382/lectures/382Lecture8.pdf]

image-20250713101205684

Transmission-line

image-20250718223340699

Telegrapher’s equations

EECS 723- Microwave Engineering Spring 2.1 -The Lumped Element Circuit Model for Transmission Lines

1/20/2005 [https://www.ittc.ku.edu/~jstiles/723/handouts/2_1_Lumped_Element_Circuit_Model_package.pdf]

note [https://www.ittc.ku.edu/~jstiles/723/handouts/section_2_1_The_Lumped_Element_Circuit_Model_package.pdf]

present [https://www.ittc.ku.edu/~jstiles/723/handouts/section_2_1_The_Lumped_Element_Circuit_Model_present.pdf]

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Transmission Line Wave Equation

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Characteristic Impedance (\(Z_0\))

image-20250713112912199

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Remember, S-parameters don't mean much unless you know the value of the reference impedance (it's frequently called Z0).

simulator will read sp file's Z0 parameter

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The default Z0 exported by EMX is 50

Complex Propagation Constant \(\gamma\)

TODO 📅

Input impedance (Line Impedance)

image-20250718231905402

Reflection Coefficient

TODO 📅

image-20250719081121034

Steady-State Solution (DC voltage division)

Sam Palermo. [https://people.engr.tamu.edu/spalermo/ecen689/lecture3_ee689_tlines.pdf]

Kyoung-Jae Chung. Special Topics in Radiation Engineering (High-voltage pulsed power engineering) [https://ocw.snu.ac.kr/sites/default/files/NOTE/Lecture_03_Transmission%20line%20theory.pdf]

David R. Jackson. [https://courses.egr.uh.edu/ECE/ECE3317/SectionJackson/Class%20Notes/Notes%208%203317%20Transmission%20Lines%20(Bounce%20Diagram).pdf]

Shouri Chatterjee [https://web.iitd.ac.in/~shouri/ell112/material/txline.pdf]

How can I go from transmission line model to lumped elements model? [https://physics.stackexchange.com/a/386603]

image-20250713090925198

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E157 Introduction to Radio Frequency Circuit Design [https://pages.hmc.edu/mspencer/e157/fa24/]

Eric Bogatin. Pop Quiz: When is an Interconnect Not a Transmission Line? [https://www.signalintegrityjournal.com/blogs/4-eric-bogatin-signal-integrity-journal-technical-editor/post/265-pop-quiz-when-is-an-interconnect-not-a-transmission-line]

Shen Lin. On-Chip Inductance and Coupling Effects [http://eda.ee.ucla.edu/pub/asic.pdf]

A. Deutsch et al., "When are transmission-line effects important for on-chip interconnections?," in IEEE Transactions on Microwave Theory and Techniques, vol. 45, no. 10, pp. 1836-1846, Oct. 1997

Ho, Ron. “Chip Wires: Scaling and Efficiency.” (2003). [https://www-vlsi.stanford.edu/people/alum/pdf/0303_Ho_Wires.pdf]

—. ISSCC 2007 T3: Dealing with Issues in VLSI Interconnect Scaling, by Ron Ho

Tony Chan Carusone. ISSCC 2017 T6: Signal Integrity Analysis for Gb/s Links

Byungsub Kim ISSCC 2022 T11: "Basics of Equalization Techniques: Channels, Equalization, and Circuits"

Voltage scattering

image-20250719072111526

image-20241112201300108

transmitted voltage \[ V= \frac{2Z_l}{Z_l+R_0}\frac{V_s}{2}= \frac{Z_l}{Z_l+R_0}\cdot V_s \]


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CHAPTER 6 Transmission-Line Essentials for Digital Electronics [https://ws.engr.illinois.edu/sitemanager/getfile.asp?id=178]

CHAPTER 7 Transmission-Line Analysis [https://ws.engr.illinois.edu/sitemanager/getfile.asp?id=199]

Voltage Transfer Function

image-20241030220203806

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Reflection Coefficients

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Impulse Response From Sparameters

David Banas. A comparison of different techniques (i.e. - windowing, vector fitting, etc.) for extracting the impulse response from S-parameters. [https://github.com/capn-freako/ImpulseResponseFromSparameters/tree/main]

TODO 📅

Rational Fit

Matlab/rationalfit

To resolve the convergence problem of s-parameter in Spectre simulator - rationalfit and write Verilog-A

image-20220630224525565

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filename  = 'touchstone/ISI.S4P';
s4p = read(rfdata.data, filename);
sdd_params = s2sdd(s2p.S_Parameters, 2);
sdd21 = squeeze(sdd_params(2, 1, :)); % s21
freq = s4p.Freq;

% rational fitting
weight = ones(size(sdd21));
weight(floor(end*3/4):end) = 0.2;
weight(2:10) = 0;

[hfit, errb] = rationalfit(freq, sdd21, 'IterationLimit', [4, 16], 'Delayfactor', 0.98, ...
'Weight', weight, 'Tolerance', -38, 'NPoles', 32);
[sdd21_fit, ff] = freqresp(hfit, freq);

figure(1)
plot(freq/1e9, db(sdd21), 'b-'); hold on;
plot(ff/1e9, db(sdd21_fit), 'r-'); hold off; grid on;
legend('sdd21', 'sdd21\_fit');
xlabel('Freq (GHz)');
ylabel('magnitude (dB)');


ts = 1e-12;
n = 2^18;
trise = 4e-14;
[yout, tout] = stepresp(hfit, ts, n, trise);
figure(2)
plot(tout*1e12, yout, 'b-'); grid on;
xlabel('Time (ps)');
ylabel('V');
title('Step Response');


% write verilog-A
writeva(hfit, 'channel_32poles.va');

Using S Parameters to Estimate Q

TODO 📅

Jeff Walling. ECE 5984 Using S Parameters to Estimate Q [https://youtu.be/PXgM6pGIRvk?si=YDeh-COQEBXKUiw-]

Spar in Tran simulation

image-20250705210519145

Spar in AC simulation

image-20250816221249094

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reference

microwaves101, S-parameters (https://www.microwaves101.com/encyclopedias/s-parameters)

Pupalaikis, P. (2020). S-Parameters for Signal Integrity. Cambridge: Cambridge University Press. doi:10.1017/9781108784863

Coelho, C. P., Phillips, J. R., & Silveira, L. M. (n.d.). Robust rational function approximation algorithm for model generation. Proceedings 1999 Design Automation Conference (Cat. No. 99CH36361). doi:10.1109/dac.1999.781313

Cadence IEEE IMS 2023, Introducing the Spectre S-Parameter Quality Checker and Rational Fit Model Generator [https://support.cadence.com/apex/ArticleAttachmentPortal?id=a1O3w000009lplhEAA]

The Complex Art Of Handling S-Parameters: The importance of extraction and fitting to circuit simulation involving S-parameters [https://semiengineering.com/the-complex-art-of-handling-s-parameters]

Dr. John Choma. EE 541, Fall 2006: Course Notes #2 Scattering Parameters: Concept, Theory, and Applications [https://www.ieee.li/pdf/essay/scattering_parameters_concept_theory_applications.pdf]

Dr. Ray Kwok . Network Techniques: Conversion between Filter Transfer Function and Filter Scattering (SMatrix) Parameters [https://www.sjsu.edu/people/raymond.kwok/docs/project172/FTF%20to%20S-Matrix%20Spring%202011.pdf]

田庆诚教授 台湾中华大学 射频电路基础(公司培训)[https://www.bilibili.com/video/BV1LA41177wr/?p=3&share_source=copy_web&vd_source=5a095c2d604a5d4392ea78fa2bbc7249]

Three fast time-domain system simulation techniques:

  • single-bit response method
  • double-edge response method
  • multiple-edge response method

Single-Bit Response (SBR) Method

img

Overlapping portions of a pulse response from neighboring bits are referred to as intersymbol interference (ISI). A received waveform is formed by superimposing, in time, the pulse responses of each bit in the sequence, as illustrated in Figure 9, assuming symmetric positive and negative pulses are transmitted for 1s and 0s

image-20240824193208821

To avoid spurious glitches between consecutive ones, rising and falling edge responses shall be symmetric. This is the limitation of SBR method.

Let \(p(t)\) be the SBR of the channel, \(t_s\) be the data sampling phase, \(T\) be the bit time, \(N_c\) is the number of UI in stored pulse response and \(b_m\) be the \(m\)th transmitted symbol. The voltage seen by the receiver's data sampler at the \(m\)th data sample is determined by \[ y_m = \sum_{k=m-N_c+1}^{m}b_kp(t_s+(m-k)T) \] where \(b_k \in [0, 1]\) and \(p(t) \ge 0\)

We always prepend \(Nc-1\) 0s in random bit stream for consistency.

image-20220429112902281

For computation convenient, the pulse need to be positive. For differential signal and amplitude \(V_{peak}\), the peak to peak is \(-V_{peak}\) to \(+V_{peak}\). After pulse added by \(V_{peak}\), peak to peak is \(0\) to \(+2V_{peak}\).

image-20220429154336080

image-20220429154423247

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hold on;

yy_sum = zeros(OSR*Ns, Ns);
for idxBit = 1:Ns
bs_split = zeros(1, Ns+Nc-1);
bs_split(idxBit) = bs(idxBit);
yy = zeros(OSR, Ns);
for ii = Nc:Nc+Ns-1
bb = bs_split(ii:-1:ii-Nc+1);
yy(:,ii-Nc+1) = sum(bb.*yrps, 2);
end
yy_cont2 = reshape(yy, [], 1);
h = plot(yy_cont2);
h.Annotation.LegendInformation.IconDisplayStyle = 'off';
yy_sum(:, idxBit) = yy_cont2;
end
yy_sum = sum(yy_sum, 2); % merge
plot(yy_sum, 'k--');
plot(yy_cont, 'm-.');
grid on;
legend('sum', 'syn');
title('merge all single bit');
ylabel('mag');
xlabel('Time (\times Ts)');

The pulse response contain rising and falling edge. The 1 bit first rise from -1 to 1, then fall to -1; The 0 bit just do nothing for synthesized waveform with the help of falling edge of 1 bit.

The DC shift help deal with continuous 0 bits.

image-20220429174330324

another SBR example

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A = zeros(10,21);
n = [1:10];

% post cursor
for m = 1:3
A(m, 11+n(m)) = 0.5;
A(m, 11-n(m)) = 0.5;
end

% one
for m = 4:10
A(m, 11) = 1;
end

% h0 or main cursor
h0 = zeros(1, 21);
h0(1, 1) = 0.5;
h0(1, 21) = 0.5;
out = h0;

for m = 1:10
out = conv(out, A(m, :), "full");
end


stem(out)

143512636-0878e0fd-fe87-414c-9c73-52577eeb7593

143512677-ccefdf22-4e30-4e72-9220-bbe667671e79

S-Parameter to Single Bit Response (SBR)

Mike Li, "S-Parameter to Single Bit Response (SBR) Transformation and Convergence Study" [https://ieee802.org/3/bj/public/may12/li_01_0512.pdf]

TODO 📅

Double-Edge Response (DER) Method

To handle the more general cases, with asymmetric rising and falling edges, the system response can be constructed in terms of edge transitions instead of bit responses.

The DER method decomposes the input data pattern, in terms of rising and falling edge transitions. The system response can be calculated by superimposing the shifted versions of the rising and falling edge responses : \[ y_m = \sum_{k=m-N_c+1}^{m}(b_k-b_{k-1})s_k(t_s+(m-k)T) + y_{int} \] where

\[\begin{align} s_i(t) &= r(t) -V_{low} \quad \text{if} \: (b_i\gt b_{i-1}) \\ &= V_{high}-f(t) \quad \text{otherwise} \end{align}\]

\(r(t)\) and \(f(t)\) are the rising and falling edge responses,respectively. \(V_{high}\) and \(V_{low}\) are the steady state DC levels, in response to a constant stream of ones and zeros, respectively. \(y_{int}\) is the initial DC state (either \(V_{high}\) or \(V_{low}\) ).

We always prepend \(Nc\) 0s in random bit stream for consistency.

image-20220429191941805

der.drawio

image-20220430010336977

image-20220430013715680

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figure(1)
subplot(3, 1, 1)
plot(yrc);
hold on;
plot(yfc);
hold off;
legend('rising', 'falling')
grid on;
ylabel('mag');
xlabel('Time (\times Ts)');
title('step response');

subplot(3, 1, 2)
stem(bs, 'k'); grid on;
hold on;
stem((idxPreRspStart:idxPreRspEnd), bs(idxPreRspStart:idxPreRspEnd), "filled", 'r');
stem(idxPreRspStart, bs(idxPreRspStart), 'go');
stem(idxCurData, bs(idxCurData), "filled", 'm');
stem((idxPreRspStart:idxPreRspEnd)+0.5, 0.1.*bd(idxPreRspStart:idxPreRspEnd), 'bd-.');
hold off;
legend('', 'Nc bits', 'y_{int}', 'Current bit', 'Edge Transitions');
ylabel('mag');
xlabel('Time (\times UI)');
title('input stream');

subplot(3, 1, 3)
yy_cont = reshape(yy, [], 1); % continuous version
plot(yy_cont); grid on;
title('continuous yout')
ylabel('mag');
xlabel('Time (\times Ts)');

figure(2)
hold on;
for idx = idxPreRspStart+1-Nc:idxCurData+32-Nc
ys = yy(:, idx);
tt = ((idx-1)*OSR+1:idx*OSR);
h = plot(tt(:), ys(:), 'LineWidth',3);
h.Annotation.LegendInformation.IconDisplayStyle = 'off';
end
plot(yy_cont, 'm--', 'LineWidth',1);
hold off;
legend('syn')
ylabel('mag');
xlabel('Time (\times Ts)');
title('synthesize with step response');
grid on;

Reference

T. C. Carusone, "Introduction to Digital I/O: Constraining I/O Power Consumption in High-Performance Systems," in IEEE Solid-State Circuits Magazine, vol. 7, no. 4, pp. 14-22, Fall 2015

Oh, Kyung Suk Dan, and Xing Chao Chuck Yuan. High-Speed Signaling: Jitter Modeling, Analysis, and Budgeting. Prentice Hall, 2011.

Ren, Jihong and Kyung Suk Oh. “Multiple Edge Responses for Fast and Accurate System Simulations.” IEEE Transactions on Advanced Packaging 31 (2008): 741-748.

Shi, Rui. “Off-chip wire distribution and signal analysis.” (2008).

X. Chu, W. Guo, J. Wang, F. Wu, Y. Luo and Y. Li, "Fast and Accurate Estimation of Statistical Eye Diagram for Nonlinear High-Speed Links," in IEEE Transactions on Very Large Scale Integration (VLSI) Systems, vol. 29, no. 7, pp. 1370-1378, July 2021, doi: 10.1109/TVLSI.2021.3082208.

image-20250816004521416

image-20250816003816639

jitter variance vs. phase noise

Note that \(L(f )\) is defined over positive frequencies only \((f \ge 0)\)

image-20250902231037546


image-20250901224816795 \[\begin{align} S_{jACC(N)}(f) &= |1-z^{-N}|^2\cdot S_{jABS}(f) \\ &= |1-\cos\theta +j\sin\theta|^2\cdot S_{jABS}(f) = ((1-\cos\theta)^2 + \sin^2\theta)\cdot S_{jABS}(f) \\ &= 2(1-\cos\theta)\cdot S_{jABS}(f) = 4\sin^2(\theta/2)\cdot S_{jABS}(f) \end{align}\]

where \(\theta = 2\pi f N/f_0\)

image-20250901233055582

As EQ(3.44), EQ(3.45)

the autocorrelation is the inverse Fouer transform of the PSD

\[ R_{\varphi}(t) = \int_{-\infty}^{+\infty} S_{\varphi} (f) e^{j2\pi f t} df \]

Then, \[\begin{align} R_{\varphi}(0) &= \int_{-\infty}^{+\infty} S_{\varphi} (f) df \\ R_{\varphi}(NT_0) &= \int_{-\infty}^{+\infty} S_{\varphi} (f) e^{j2\pi f NT_0} df \end{align}\]

Thus, yield EQ(3.48)

image-20250903184827248


Simplified PLL Phase Noise Profile

Absolute Jitter

TODO 📅

Period Jitter

image-20250902233638588


image-20250901233626772

image-20250901233756765


a random-walk DCO - \(1/f^2\) Phase Noise Profile

L. Avallone, M. Mercandelli, A. Santiccioli, M. P. Kennedy, S. Levantino and C. Samori, "A Comprehensive Phase Noise Analysis of Bang-Bang Digital PLLs," in IEEE Transactions on Circuits and Systems I: Regular Papers, vol. 68, no. 7, pp. 2775-2786, July 2021 [https://sci-hub.st/10.1109/TCSI.2021.3072344]

image-20250902232230515

image-20250902231843251

Even-odd Jitter (EOJ)

Jitter measurement Description
F/2 F/2 is the peak-to-peak amplitude of the periodic jitter occurring at 1/2 of the data rate.

Even-odd jitter, also known as F/2 jitter, arises from a clock signal's duty cycle not being perfectly 50%

image-20250816130508935

Even-odd jitter has been referred to as duty cycle distortion by other Physical Layer specifications for operation over electrical backplane or twinaxial copper cable assemblies

image-20250816130650378


image-20250816181004878

Comparing DCD and F/2 Jitter Using a BERTScope® Bit Error Rate Testing Application Note [https://download.tek.com/document/65W_26040_0_Letter.pdf]

Pulse Width Jitter (PWJ)

image-20250816125512147

image-20250816125533070

Jeff Morriss Updated 10/25/07. Analysis of 8G PCIe Pulse Width Jitter (UI to UI Jitter_10_25.ppt)


image-20250816132730999

Duty Cycle Distortion – DCD

Jitter measurement Description
DCD Duty Cycle Distortion is the peak-to-peak amplitude of the component of the deterministic jitter correlated with the signal polarity.

image-20250816081711834

image-20250816081808897


Jitter fundamental & How Isolating Root Causes of Jitter [https://picture.iczhiku.com/resource/eetop/ShKgzTEiUfdFOcvn.pdf]

There are two primary causes of DCD jitter which are usually generated within a transmitter

  • If the data input to a transmitter is theoretically perfect, but if the transmitter sampling threshold is offset from its ideal level, then the output of transmitter will have duty cycle distortion as a function of the slew rate of the data signal
  • Another cause of duty cycle distortion can be a mismatch/asymmetry in rising and falling edge speeds

image-20250816085315710


Unfortunately, other sources such as ISI almost always exist making it sometimes difficult to isolate the DCD component. One technique to test for DCD is to stimulate your system/components with a repeating 1-0-1-0… data pattern. This technique will eliminate inter-symbol interference (ISI) jitter and make viewing the DCD within the spectrum display much easier

Why clock pattern? That's because all symbols experience same inter-symbol interference, which are canceled out


image-20250816103444976


image-20250816180338475

[https://scdn.rohde-schwarz.com/ur/pws/dl_downloads/dl_application/application_notes/1td03/1TD03_2e_RTO_Jitter_Analysis.pdf]

Correlated vs. Uncorrelated

If the PDF of one jitter source changes when the PDF of another source is changed, then those two sources are dependent or correlated

image-20250816080432083

Inter-Symbol Interference (ISI)

The primary cause of Data Dependent Jitter

image-20250816090326309

image-20250816090430513


Jitter measurements can be classified into three categories: cycle-to-cycle jitter, period jitter, and long-term jitter

Jitter is a key performance parameter. Need to know what matters in each case:

  • PJ for digital timing
  • LTJ for data converters and serial data
  • Phase noise for communications (not all bandwidths matter)

image-20240714095712249

The above Cycle-Cycle Jitter equation is wrong, \(\tau_1\) and \(\tau_2\) are not independent

Short Term Jitter

image-20230916235240675

image-20230916235314423

Period jitter, Jper is the short term variation in clock period compared to the average (mean) clock period.

Cycle-to-Cycle, Jcc is the time difference of two adjacent clock periods

Long Term Jitter (LTJ)

image-20230916235647723

image-20230916235709504

measuring LTJ

image-20230916235033464

Jitter Calculation Examples

image-20230917003028143

Jcc vs Jper

Estimating the RMS cycle-to-cycle jitter if all you have available is the RMS period jitter.

  • Cycle-to-cycle jitter - The short-term variation in clock period between adjacent clock cycles. This jitter measure, abbreviated here as \(J_{CC}\), may be specified as either an RMS or peak-to-peak quantity.
  • Period jitter - The short-term variation in clock period over all measured clock cycles, compared to the average clock period. This jitter measure, abbreviated here as \(J_{PER}\), may be specified as either an RMS or peak-to-peak quantity.

Let the variable below represent the variance of a single edge's timing jitter, i.e. the difference in time of a jittery edge versus an ideal edge, \(\sigma^2_j\)

If each edge's jitter is independent then the variance of the period jitter can be written as \[\begin{align} \sigma^2_\text{jper} &= (\sigma_\text{j(n+1)}-\sigma_\text{j(n)})^2 \\ &= \sigma_\text{j(n+1)}^2-2\sigma_\text{j(n+1)}\sigma_\text{j(n)})+\sigma_\text{j(n)})^2\\ &= \sigma_\text{j(n+1)}^2+\sigma_\text{j(n)})^2 \\ &=2\sigma^2_j \end{align}\]

In every cycle-to-cycle measurement we use one "interior" clock edge twice and therefore we must account for this

\[\begin{align} \sigma^2_\text{jcc} &= (\sigma_\text{jper(n+1)}-\sigma_\text{jper(n)})^2 \\ &=(\sigma_\text{j(n+2)}-2\sigma_\text{j(n+1)}+\sigma_\text{j(n)})^2 \end{align}\]

Since each edge's jitter is assumed to be independent and have the same statistical properties we can drop the cross correlation terms and write:

\[\begin{align} \sigma^2_\text{jcc} &=(\sigma_\text{j(n+2)}-2\sigma_\text{j(n+1)}+\sigma_\text{j(n)})^2 \\ &=\sigma_\text{j(n+2)}^2+4\sigma_\text{j(n+1)}^2+\sigma_\text{j(n)}^2 \\ &=6\sigma_\text{j}^2 \end{align}\]

The ratio of the variances is therefore \[ \frac{\sigma^2_\text{jcc}}{\sigma^2_\text{jper}} = \frac{6\sigma_\text{j}^2} {2\sigma_\text{j}^2}=3 \] Then \[ \sigma_\text{jcc} = \sqrt{3}\sigma_\text{per} \]

[Timing 101 #8: The Case of the Cycle-to-Cycle Jitter Rule of Thumb, Silicon Labs]

references

AN10007 Clock Jitter Definitions and Measurement Methods, SiTime [pdf]

SERDES Design and Simulation Using the Analog FastSPICE Platform, Silicon Creations [pdf]

Flexible clocking solutions in advanced processes from 180nm to 5nm, Silicon Creations [pdf]

One-size-fits-all PLLs for Advanced Samsung Foundry Processes, Silicon Creations [pdf]

Circuit Design and Verification of 7nm LowPower, Low-Jitter PLLs, Silicon Creations, [pdf]

Lecture 10: Jitter, ECEN720: High-Speed Links Circuits and Systems Spring 2023 [pdf]

Jitter 360° Knowledge Series [pdf, slides]

N. Da Dalt, "Tutorial: Jitter: Basic and Advanced Concepts, Statistics, and Applications," 2012 IEEE International Solid-State Circuits Conference, San Francisco, CA, USA, 2012 [slides, transcript ]

Loop Inductance is the sum of partial self-inductance and partial-mutual inductance


Magnetic Vector Potential (磁矢势)

Youjin Deng. 5-3 静磁场的基本规律 [http://staff.ustc.edu.cn/~yjdeng/EM2022/pdf/5-2(2022).pdf]

磁场不能用标量势描述

image-20250709195107708

image-20250709195217587

image-20250709200229266


image-20250708231822291

Partial Inductance

image-20250708230643776

self partial inductance

image-20250708233924675

mutual partial inductance

image-20250708234512418

Ex. two-wire

image-20250709001127400


image-20250602120913866

img

[https://www.oldfriend.url.tw/Q3D/ansys_ch_Partial_Loop_Inductance.html]

Current Return Path

image-20250705171613361

Current return paths are frequency dependent \(Z = R +j\omega L\)

  • Low frequency
    • \(R\) dominates - current use as many returns as possible to have parallel resistances
  • High frequency
    • \(j\omega L\)​ dominates - current use the closest possible return path to form the smallest possible loop inductance
  • Very high frequency
    • The current would be confined to the nearest possible return only at ultra-high frequencies (skin effect)

image-20250705170949035


skin effect & Dielectric loss

image-20250705170028485


EMX simulation

setup:

image-20250706004037966

frequency sweep:

image-20250706010943996

Cadence October 2020, Analysis of a Figure-Eight Inductor with EMX RAK

image-20250706010216105

proximity effect & skin effect

  • Skin effect concentrates current near the surface of a single conductor, while proximity effect concentrates current in specific regions of multiple conductors due to their interaction
  • Skin effect is caused by the conductor's own magnetic field, while proximity effect is caused by the magnetic field of a nearby conductor

proximity effect is a redistribution of electric current occurring in nearby parallel electrical conductors carrying alternating current (AC), caused by magnetic effects (eddy currents)

image-20250705163405433


skin effect is the tendency of AC current flow near the surface (or "skin") of a conductor, rather than throughout its cross-section, due to the magnetic field generated by the current itself

image-20250705165353751

Cause of skin effect

A main current \(I\) flowing through a conductor induces a magnetic field \(H\). If the current increases, as in this figure, the resulting increase in \(H\) induces separate, circulating eddy currents \(I_W\) which partially cancel the current flow in the center and reinforce it near the skin


Eddy current

By Lenz's law, an eddy current creates a magnetic field that opposes the change in the magnetic field that created it, and thus eddy currents react back on the source of the magnetic field

Electromagnetic coupling

Electric field coupling (also called capacitive coupling) occurs when energy is coupled from one circuit to another through an electric field

Two circuits above a signal return plane.

Magnetic field coupling (also called inductive coupling) occurs when energy is coupled from one circuit to another through a magnetic field

Two circuits above a signal return plane


For instance

  • magnetic coupling between multiple inductors
  • capacitive coupling between multiple transmission lines

Grounding

TODO 📅

Chapter 11 Layout and grounding [http://ieb-srv1.upc.es/gieb/tecniques/doc/EMC/pdfs/ScienceDirect_articles_27Jul2018_12-16-10.699/Chapter-11---Layout-and-grounding_2007_EMC-for-Product-Designers.pdf]

Decoupling Capacitor

image-20250705175343498

RLC network

[https://web.stanford.edu/class/archive/ee/ee371/ee371.1066/handouts/markChapt.pdf]

image-20250817105056325

image-20250817105203031image-20250817105308602

reference

ISSCC2002. Special Topic Evening Discussion Sessions SE1: Inductance: Implications and Solutions for High-Speed Digital Circuits [vSE1_Blaauw], [vSE1_Gauthier], [vSE1_Morton, [vSE1_Restle]]

Y. Massoud and Y. Ismail, "Gasping the impact of on-chip inductance," in IEEE Circuits and Devices Magazine, vol. 17, no. 4, pp. 14-21, July 2001 [https://sci-hub.se/10.1109/101.950046]

Clayton R. Paul, Partial Inductance [https://ewh.ieee.org/soc/emcs/acstrial/newsletters/summer10/PP_PartialInductance.pdf]

Cheung-Wei Lam. Common Misconceptions about Inductance & Current Return Path [https://ewh.ieee.org/r6/scv/emc/archive/022010Lam.pdf]

Randy Wolff. Signal Loop Inductance in [Pin] and [Package Model] [https://ibis.org/summits/feb10/wolff.pdf]

ANSYS Q3D Getting Started LE05. Module 5: Q3D Inductance Matrix Reduction [https://innovationspace.ansys.com/courses/wp-content/uploads/sites/5/2021/07/Q3D_GS_2020R1_EN_LE05_Ind_Matrix.pdf]


Paul, Clayton R. Inductance: Loop and Partial. Hoboken, N.J. : [Piscataway, N.J.]: Wiley ; IEEE, 2010.

Spartaco Caniggia. Signal Integrity and Radiated Emission of High‐Speed Digital Systems. Wiley 2008

Yuriy Shlepnev. How Interconnects Work: Characteristic Impedance and Reflections [https://www.linkedin.com/pulse/how-interconnects-work-characteristic-impedance-yuriy-shlepnev/]

-. How Interconnects Work: Bandwidth for Modeling and Measurements [https://www.linkedin.com/pulse/how-interconnects-work-bandwidth-modeling-yuriy-shlepnev/?trackingId=874kpm3XuNyV9D0eP6IioA%3D%3D]

Eric Bogatin. Pop Quiz: When is an Interconnect Not a Transmission Line? [https://www.signalintegrityjournal.com/blogs/4-eric-bogatin-signal-integrity-journal-technical-editor/post/265-pop-quiz-when-is-an-interconnect-not-a-transmission-line]

TeledyneLeCroy/SignalIntegrity Python tools for signal integrity applications [SignalIntegrityApp]

A Look at Transmission-Line Losses [http://blog.teledynelecroy.com/2018/06/a-look-at-transmission-line-losses.html]

How Much Transmission-Line Loss is Too Much? [http://blog.teledynelecroy.com/2018/06/how-much-transmission-line-loss-is-too.html]

Raymond Y. Chen, Raymond Y. Chen. Fundamentals of S Fundamentals of S-Parameter Parameter Modeling for Power Distribution Modeling for Power Distribution System (PDS) and SSO Analysis System (PDS) and SSO Analysis [https://ibis.org/summits/jun05/chen.pdf]

image-20250602155255711

image-20230709102848934

Transit frequency \(f_T\)

aka cut-off frequency

Gate (thermal) noise

image-20230709210517475

image-20230709211309265

image-20230709202930102

Two-Side Poly Contact & folding

image-20230709212015293

Both scheme yield a total distributed resistance of \(R_G/4\) for gate noise calculation

folding

finger 0 \[\begin{align} \overline{i_{tot,0}^2} &= \left(\frac{g_m}{2} \right)^2(4kT\frac{R_G/2}{3}) \\ &= g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{2^2\cdot 2} \end{align}\]

similarly finger 1 \[ \overline{i_{tot,1}^2} = g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{2^2\cdot 2} \] Assuming uncorrelated \[ \overline{i_{tot}^2} = \sum_{N=0}^1\overline{i_{tot,N}^2} =g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{2^2\cdot 2} \cdot 2 = g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{2^2} \] Generally \[ \overline{i_{tot}^2} = g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{N^2} \] where the gate is decomposed into \(N\) parallel fingers

two-side poly contact

No alt text provided for this image

We fracture Gate poly at the center point, then we obtain 2 segments, both have same \(\frac{g_m}{2}\) and \(R_G/2\).

The derivation procedure is same with folding structure, i.e. plug \(N=2\) into \(\overline{i_{tot}^2} = g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{N^2}\)

That is \[ \overline{i_{tot}^2} = g_m^2\left(4kT\frac{R_G}{12}\right) \] The input referred noise of gate resistance \[ \overline{V_{nRG}^2} = 4kT\frac{R_G}{12} \]

four equal gate fingers

image-20230709212818351

\[ \overline{i_{tot}^2} = g_m^2\left(4kT\frac{R_G}{3}\right)\frac{1}{4^2} \] Then \[ \overline{V_{nRG}^2} = \frac{\overline{i_{tot}^2}}{g_m^2} =4kT\frac{R_G}{48} \]

Gate resistance handling by parasitic extraction tools

They fracture the poly line at the intersection with the active (diffusion) layer, breaking it into "gate poly"(poly over active) and "field poly" (poly outside active)

gploy, fpoly

No alt text provided for this image

Gate poly is also fractured at the center point. Gate instance pin of the MOSFET (SPICE model) is connected to the center point of the gate poly. Gate poly is described by two parasitic resistors, connecting the fracture points.

image-20230709222642979

MOSFET extrinsic parasitic capacitance between gate poly and source / drain diffusion and contacts is calculated by parasitic extraction tools, and assigned to the nodes of the resistive networks.

Different extraction tools do this differently - some tools connect these parasitic capacitances to the center point of the gate poly, while some other tools connect them to the end points of the gate poly resistors.

\(\Delta\) gate model

This distributed network has a different AC and transient response than a simple lumped one-R and one-C circuit.

It was shown [B. Razavi] that such RC network behaves approximately the same as a network with one R and one C element, where C is the total capacitance, and R=1/3 * W/L rsh for single-side connected poly, and R=1/12 W/L * rsh for double-sided connected poly.

These coefficients - 1/3 and 1/12 - effectively enable an accurate reduced order model for the gate, reducing a large number of R and C elements to two (or three) resistors and one capacitor.

Gate Delta Model: where a gate is described by two positive and one negative resistors

image-20230709214200878

only applicable to contacts on gate overhangs

invalid for self-aligned gate contacts, where gate contact land directly on top of gate, not gate overhang

No alt text provided for this image

  1. 1-side gate contact \[ R_{eq,1side} =R_1 \parallel (R_2+R_1)= \frac{R_G}{6}\parallel (-\frac{R_G}{2}+\frac{R_G}{6})=\frac{R_G}{3} \]

  2. 2-side contact \[ R_{eq,2side}= R_1 \parallel R_1 = \frac{R_G}{6}\parallel \frac{R_G}{6} = \frac{R_G}{12} \]

Some SPICE simulators have problems handling negative resistors, that's possibly why this model did not get a wide adoption. Some foundries and PDKs support delta gate model, while some others don't.

Vertical component of gate resistance

In "old" technologies (pre-16nm), gate resistance was dominated by lateral resistance. However, in advanced technologies, multiple interfaces between gate material layers lead to a large vertical gate resistance.

No alt text provided for this image

It's very easy to check this in DSPF file - if gate instance pin is connected directly to the center of the gate poly - vertical resistance is not accounted for. If it is connected by a positive resistor to the center of the gate poly - that resistors represents the vertical gate resistance.

decap

decap-res.drawio

leakage current is determined by \(R_s + R_p\), and \(R_p \gg R_s\)

  • low freq: \(Z=R_s + R_p\)
  • high freq: \(Z=R_s\)

An example: \(R_s=200\space \Omega\), \(R_p = 8 \space M\Omega\) and \(C_\text{gate}=10\space fF\)

image-20240729205410196

reference

⭐ B. Razavi, Y. Ran, and K. F. Lee, “Impact of Distributed Gate Resistance on the Performance of MOS Devices,” IEEE Trans. Circuits and Systems, Part I, pp. 750–754, Nov. 1994.

⭐ Maxim Ershov, Diakopto. "Gate Resistance in IC design flow", [link, pdf]

A.J.Sholten et al., "FinFET compact modelling for analogue and RF applications", IEDM'2010 [https://sci-hub.se/10.1109/IEDM.2010.5703322]

Saha, Samar K.. “FinFET Devices for VLSI Circuits and Systems.” (2020).

Harpe, Pieter J. A., Andrea Baschirotto and Kofi A. A. Makinwa. “Hybrid ADCs, Smart sensors for the IoT, and Sub-1V and Advanced node analog circuit design: Advances in Analog Circuit Design 2017.” (2018).

Chauhan, Yogesh Singh. FinFET Modeling for IC Simulation and Design: Using the BSIM-CMG Standard. London, UK: Academic Press, 2015.

A.J.Sholten et al., "FinFET compact modelling for analogue and RF applications", IEDM'2010, p.190.

W. Wu and M. Chan, “Gate resistance modeling of multifin MOS devices,” IEEE Electron Device Letters, vol. 27, no. 1, pp. 68-70, Jan. 2006.

A. L. S. Loke, C. K. Lee and B. M. Leary, "Nanoscale CMOS Implications on Analog/Mixed-Signal Design," 2019 IEEE Custom Integrated Circuits Conference (CICC), Austin, TX, USA, 2019, pp. 1-57, doi: 10.1109/CICC.2019.8780267.

Nonzero FFT bins

everynanocounts. Memos on FFT With Windowing. [https://a2d2ic.wordpress.com/2018/02/01/memos-on-fft-with-windowing]

The problem with sine-wave scaling is that the noise power is, on average, evenly distributed over all FFT bins, whereas the sine-wave power is concentrated in only a few bins. With sine-wave scaling, the power of individual sine-wave components can be read directly from the spectral plot, but in order to determine the noise power, the powers of all the noise bins must be added together.

snr_final.drawio

We can't use Fourier transform of random signal

[https://raytroop.github.io/2023/11/10/random/#lti-systems-on-wss-processes]

\[\begin{align} \mathrm{SNR} &= \frac{X_\text{sig}^2}{X_\text{n}^2N} \\ &= \frac{X_\text{sig}^2\cdot \sum_k W_k^2}{X_\text{n}^2N\cdot \sum_k W_k^2} \\ &= \frac{\sum_\text{nb} X_\text{w,sig}^2}{N X_\text{w,n}^2} \end{align}\]

where \(\text{nb}\) is number of non-zero FFT bins

image-20250917184729018

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subplot(3,1,1);
for N = [16 256 1024]
wrect = rectwin(N);
Wrect = fftshift(fft(wrect));
Wrect_mag = abs(Wrect)/sum(wrect);
nb_rect = sum(Wrect_mag > 0.1);
fprintf('Number of nonzero FFT bin(rect window N=%d): %d\n', N, nb_rect);
stem(1:N, Wrect_mag, LineWidth=2)
hold on
end
grid on
legend('16', '256', '1024')
title('rect window')

subplot(3,1,2);
for N = [16 256 1024]
whann = hann(N);
Whann = fftshift(fft(whann));
Whann_mag = abs(Whann)/sum(whann);
nb_hann = sum(Whann_mag > 0.1);
fprintf('Number of nonzero FFT bin(hann window N=%d): %d\n', N, nb_hann);
stem(1:N, Whann_mag, LineWidth=2)
hold on
end
grid on
legend('16', '256', '1024')
title('Hanning window')

subplot(3,1,3);
for N = [16 256 1024]
whann2 = (1-cos(2*pi*(0:N-1)/N)).^2/2^2;
Whann2 = fftshift(fft(whann2));
Whann2_mag = abs(Whann2)/sum(whann2);
nb_hann2 = sum(Whann2_mag > 0.1);
fprintf('Number of nonzero FFT bin(hann2 window N=%d): %d\n', N, nb_hann2);
stem(1:N, Whann2_mag, LineWidth=2)
hold on
end
grid on
legend('16', '256', '1024')
title('Hann2 window')


% Number of nonzero FFT bin(rect window N=16): 1
% Number of nonzero FFT bin(rect window N=256): 1
% Number of nonzero FFT bin(rect window N=1024): 1
% Number of nonzero FFT bin(hann window N=16): 3
% Number of nonzero FFT bin(hann window N=256): 3
% Number of nonzero FFT bin(hann window N=1024): 3
% Number of nonzero FFT bin(hann2 window N=16): 5
% Number of nonzero FFT bin(hann2 window N=256): 5
% Number of nonzero FFT bin(hann2 window N=1024): 5

[https://web.engr.oregonstate.edu/~temes/ece627/Lecture_Notes/FFT_for_delta_sigma_spectrum_estimation.pdf]

image-20250913174821087

where \(\mathrm{NBW} = \frac{\sum_{n}|w[n]|^2}{ \left| \sum_{n} w[n] \right|^2}\)

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% excerpt of A.4 An Example in Pavan, Schreier and Temes, "Understanding Delta-Sigma Data Converters, Second Edition" ISBN 978-1-119-25827-8
%
% Compute modulator output and actual NTF
%
OSR = 32;
ntf0 = synthesizeNTF(5,OSR,1);
N = 64*OSR;
fbin = 11;
u = 1/2*sin(2*pi*fbin/N*[0:N-1]);
[v tmp1 tmp2 y] = simulateDSM(u,ntf0);
k = mean(abs(y)/mean(y.^2))
ntf = ntf0 / (k + (1-k)*ntf0);
%
% Compute windowed FFT and NBW
%
w = hann(N); % or ones(1,N) or hann(N).^2
nb = 3; % 1 for Rect; 5 for Hann^2
w1 = norm(w,1);
w2 = norm(w,2);
NBW = (w2/w1)^2
V = fft(w.*v)/(w1/2);
%
% Compute SNR
%
signal_bins = fbin + [-(nb-1)/2:(nb-1)/2];
inband_bins = 0:N/(2*OSR);
noise_bins = setdiff(inband_bins,signal_bins);
snr = dbp(sum(abs(V(signal_bins+1)).^2)/sum(abs(V(noise_bins+1)).^2))

Noise Floor

[http://individual.utoronto.ca/schreier/lectures/2015/1.pdf]

image-20241202212412428

General Formula

signal tone power \[ P_{\text{sig}} = 2 \frac{X_{w,sig}^2}{S_1^2} \]

noise power \[ P_n = \frac{X_{w,n}^2}{N\cdot S_2}N=\frac{X_{w,n}^2}{S_2} \]

where white noise, \(X_n(i) = X_n(j)\) for any \(i \neq j\)

Therefore, displayed SNR is obtained \[\begin{align} \mathrm{SNR} &= 10\log10\left(\frac{X_{w,sig}^2}{X_{w,n}^2}\right) \\ &= 10\log_{10}\left(\frac{P_{\text{sig}}}{P_n}\right) + 10\log_{10}\left(\frac{S_1^2}{2S_2}\right) \\ &= \mathrm{SNR}'-10\log_{10}\left(\frac{2S_2}{S_1^2}\right) \\ &= \mathrm{SNR}'-10\log_{10}(2\cdot\mathrm{NBW}) \end{align}\]

DFT's output \(\mathrm{SNR}\)


\[ \text{PS(k)} = \text{PSD(k)} \cdot \text{ENBW} \]

where Effective Noise BandWidth \(\text{ENBW} =f_{\text{res}} \cdot \frac{N S_2}{S_1^2}\)

yield \[ \text{PS(k)} = \text{PSD(k)} \cdot f_{\text{res}} \cdot \frac{N S_2}{S_1^2} = \left\{\text{PSD(k)} \cdot f_{\text{s}} \right\} \cdot \frac{S_2}{S_1^2} \] where \(\left\{\text{PSD(k)} \cdot f_{\text{s}} \right\} =\text{const}\), i.e. \(x_\text{n,rms}\)

image-20250826003933143

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ratio_list = [];
for len = 6:12
wnd = hanning(2^len);
S2 = sum(wnd.^2);
S1 = sum(wnd);
ratio = S2./S1.^2;
ratio_list(end+1) = ratio;
end

ratio_db = 10*log10(ratio_list);
plot(2.^[6:1:12], ratio_db, 'ro-', LineWidth=4)
grid on; grid minor;

xlabel('N'); ylabel("$10\log(S_2/S_1^2)$",'Interpreter', 'latex')

FFT Noise Floor

image-20250826010627757

image-20250826013036595

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N = 2048;
cycles = 67;
fs = 1000;
fx = fs*cycles/N;
LSB = 2/2^10;
%generate signal, quantize (mid-tread) and take FFT
x = cos(2*pi*fx/fs*[0:N-1]);
x = round(x/LSB)*LSB;
s = abs(fft(x));
s = s(1:end/2)/N*2;
% calculate SNR
sigbin = 1 + cycles;
noise = [s(1:sigbin-1), s(sigbin+1:end)];
snr = 10*log10( s(sigbin)^2/sum(noise.^2) );

sdb = 20*log10(s);

% How to plot a series of numbers which some of them are inf?
% https://www.mathworks.com/matlabcentral/answers/476643-how-to-plot-a-series-of-numbers-which-some-of-them-are-inf
plot([0:N/2-1]/N, max(sdb, -120), LineWidth=4)
hold on;
plot([0 0.5], [-61.9 -61.9], 'r--', LineWidth=2)
plot([0 0.5], [-92 -92], 'm--', LineWidth=2)
grid on; grid minor;
ylim([-120 0]); xlim([0 0.5]);
xlabel('Frequency [f/fs]'), ylabel('DFT Magnitude [dBFS]');
title('2048 point FFT, SNR=61.90dB')

Noise Spectral Density (NSD)

Understanding Key Parameters for RF-Sampling Data Converters White Paper (WP509) [https://docs.amd.com/v/u/en-US/wp509-rfsampling-data-converters]

Boris Murmann, ISSCC2022 SC1: Introduction to ADCs/DACs: Metrics, Topologies, Trade Space, and Applications [https://www.nishanchettri.com/isscc-slides/2022%20ISSCC/SHORT%20COURSE/SC1.pdf]

image-20250826005956497


image-20250902010512726

Rectangular Window

DFT bin's output noise standard deviation (rms) value is proportional to \(\sqrt{N}\), and the DFT's output magnitude for the bin containing the signal tone is proportional to \(N\)

signal tone power \[ P_{\text{sig}} = 2 \frac{X_{w,sig}^2}{N^2} \]

noise power \[ P_n = \frac{X_{w,n}^2}{N} \]

The displayed SNR \[ \mathrm{SNR} = \mathrm{SNR}' - 10\log_{10}(2/N) \] If we increase a DFT's size from \(N\) to \(2N\), the DFT's output SNR increased by 3dB. So we say that a DFT's processing gain increases by 3dB whenever \(N\) is doubled.


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for N=[2^6 2^8 2^10 2^12]
wd = rectwin(N);
nbw = enbw(wd)/N;
snr_shift = 10*log10(nbw * 2);
disp(snr_shift);
end

output:

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-15.0515

-21.0721

-27.0927

-33.1133

image-20241202212221239

image-20241202213152360

How spectrum analyzer work?

We tried to plot a power spectral density together with something that we want to interpret as a power spectrum

  • spectrum of a periodic signal
  • spectral density of a broadband signal such as noise

Sine-wave components are located in individual FFT bins, but broadband signals like noise have their power spread over all FFT bins!

The noise floor depends on the length of the FFT

PS and PSD

The spectral density format is appropriate for random or noise signals but inappropriate for discrete frequency components because the latter theoretically have zero bandwidth

Amplitude Correction

  1. A finite-duration window \(w[n]\)

    DTFT is \(W[e^{j\omega}]\) and the maximum magnitude is is at DC frequency, which \(\sum_n w_n\)

  2. Sinusoidal signal \(x[n]\)

    DFS is \(X_k\), and DTFT shall be \(\frac{2\pi}{N}X_k(e^{j\omega})\)

  3. the windowed sequence \(v[n] = x[n]w[n]\)

    with multiplication property, DTFT of \(v[n]\) shall be \(\frac{X_k(e^{j\omega})}{N}\sum_n w_n\)

    As we know, DFT of \(v[n]\) is samples of its DTFT, that is \[ \frac{X_k(e^{j\omega})}{N}\sum_n w_n = X_v[k] \] Therefore, \[ \frac{X_k(e^{j\omega})}{N} = \frac{X_v[k]}{\sum_n w_n} \]

Effective Noise BandWidth (ENBW)

General derivation

The relationship between a power spectrum (\(PS, V^2\)) and a power spectral density (\(PSD, V^2/Hz\)) is given by the effective noise bandwidth (ENBW), which can easily be determined at the time when the DFT is computed.

ENBW should always be recorded when a spectrum or spectral density is computed, such that the result can be converted to the other form at a later stage, when the information about the frequency resolution \(f_{res}\) and the window that was used is normally not easily available any more.

The normalized equivalent noise bandwidth (NENBW) of the window is given by

\[ \text{NENBW} = \frac{NS_2}{S_1^2} \] where \(S_1 = \sum _{k=0}^{N-1}w_k\) and \(S_2 = \sum _{k=0}^{N-1}w_k^2\)

The ENBW is given by

\[ \text{ENBW} = \text{NENBW}\cdot f_{res} = \text{NENBW}\cdot \frac{f_s}{N} = f_s\frac{S_2}{S_1^2} \]

Equivalent noise bandwidth (ENBW) compares a window to an ideal, rectangular time-window. It is the bandwidth of the rectangular window's frequency-domain shape that passes the same amount of white noise energy as the frequency-domain shape defined by the other window.

enbw

Therefore, the equivalent noise bandwidth \(B_{enbw}\) is given by

\[ B_{enbw} = \frac{\int_{-f}^{f} |W(f)|^2 df}{|W(f_0)|^2} \]

Translating to discrete domain, the equivalent noise bandwidth can be computed using DFT samples as

\[ B_{enbw} =\frac{\sum_{k=0}^{N-1}|W[k]|^2}{|W[k_0]|^2} \]

where \(k_0\) is the index at which the magnitude of FFT output is maximum and \(N\) is the window length, i.e. \(k_0=0\).

Applying Parseval's theorem and \(W[0]=\sum_{n}w[n]\), \(B_{enbw}\) can also be computed using time domain samples as

\[ B_{enbw} = N \frac{\sum_{n}|w[n]|^2}{ \left| \sum_{n} w[n] \right|^2} \]

scale \(w[n]\) don't change \(B_{enbw}\)

Noise power inside window: \(\int_{-f}^{f} |W(f)|^2 df \to N\cdot\sum_{n}|w[n]|^2\)

peak amplitude: \(|W(f_0)|^2 \to \left| \sum_{n} w[n] \right|^2\)

An alternative derivation

coherence-incoherence.drawio.svg

Assuming the windowed sequence \(v[n] = x[n]w[n]\)

  • \(W[k]\): Fourier Transform of finite sequence window

  • \(X_{sig}\): Fourier Transform of signal

  • \(X_{n}\): Fourier Transform of noise

  • \(X_{v,sig}\): Fourier Transform of windowed signal

  • \(X_{v,n}\): Fourier Transform of windowed noise

From Fig. 6,, we observe that the amplitude of the harmonic estimate at a given frequency is biased by the accumulated broad-band noise included in the bandwidth of the window.

image-20240517195407690

In this sense, the window behaves as a filter, gathering contributions for its estimate over its bandwidth

The Fourier Transform of windowed signal can be expressed as

\[\begin{align} X_{v,sig} &= W_{max}\cdot X_{sig} \\ &= W[0]\cdot X_{sig} \end{align}\]

For a typical window, \(W_{max}\) occurs at \(\omega = 0\)

And the Fourier Transform of windowed noise can be expressed as

\[ X_{v,n}^2 = \sum_k (W[k])^2 \cdot X_n^2 \]

divided by \((W[0])^2\) on both sides of the above equation

\[ \frac{X_{v,n}^2}{(W[0])^2} = \frac{\sum_k (W[k])^2}{(W[0])^2} \cdot X_n^2 \]

By Parseval's theorem

\[ \frac{X_{v,n}^2}{\left(\sum_n w[n]\right)^2} = \frac{N\sum_n w^2[n]}{\left(\sum_n w[n]\right)^2} \cdot X_n^2 \]

where \(X^2_n\) is what is deserved and

\[ X_n^2 = \frac{PS_{n}}{B_{enbw}} \]

where \(B_{enbw} = N \frac{\sum_{n}|w[n]|^2}{ \left| \sum_{n} w[n] \right|^2}\) and \(PS_{n}=\left| \frac{X_{v,n}}{\sum_n w[n]}\right|^2\)

example

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lw = 128;
win = hann(lw);
lt = 2048;
windft = fftshift(fft(win,lt));

ad = abs(windft).^2;
mg = max(ad);

fs = 1000;

bw = enbw(win,fs);

bdef = sum((win).^2)/sum(win)^2*fs;
fprintf("bw: %.3f\n", bw);
fprintf("bdef: %.3f\n", bdef);

freq = -fs/2:fs/lt:fs/2-fs/lt;

plot(freq,ad, bw/2*[-1 -1 1 1],mg*[0 1 1 0],'--')
xlim(bw*[-1 1])

Adiff = trapz(freq,ad)-bw*mg;
fprintf("Adiff: %.3e\n", Adiff);

Verify that the area of the rectangle contains the same total power as the window.

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Adiff = trapz(freq,ad)-bw*mg
output:
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bw: 11.811
bdef: 11.811
Adiff: 7.276e-12

image-20230530230434715


Unpingco, José. Python for Signal Processing: Featuring IPython Notebooks. Cham: Springer, 2013. [pdf]

[https://github.com/unpingco/Python-for-Signal-Processing/blob/master/Windowing_Part2.ipynb]

image-20250902002913214

demo

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%https://aaronscher.com/Course_materials/Communication_Systems/documents/PSD_Autocorrelation_Noise.pdf

%Clear variables. clear command window, close all figures:
clc;
clear all;
close all;
%%%Setup and define variables
f0=10; %frequency of sinusoidal signal (Hz)
fs=100; %sampling frequency (Hz)
Ts=1/fs; %sampling period (seconds)
N0=3000; %number of samples
t=[0:Ts:Ts*(N0-1)]; %Sample times
noise_PSD=.5; %This is the desired noise power spectral density in W/Hz.
variance=noise_PSD*fs;% Variance = sigma^2
sigma=sqrt(variance);
noise=transpose(sigma*randn(N0,1));%create sampled white Gaussian noise.
xsignal=20*sin(2*pi*f0*t); %create sampled sinusoidal signal
x=xsignal+noise; %Add signal to noise
figure(1)
histogram(noise,30) %plot histogram
set(gca,'FontSize',14) %set font size of axis tick labels to 18
xlabel('Noise amplitude','fontsize',14)
ylabel('Frequency of occurance','fontsize',14)
title('Simulated histogram of white Gaussian noise','fontsize',14)
SNR_try1=snr(xsignal,noise); %calculate SNR using built in "snr" function.
SNR_try2=10*log10(sum(xsignal.^2)/sum(noise.^2)); %manually calculate SNR.
%If everything is correct, the two SNR calculations above should agree.
%Plot noise in time-domain
figure(2)
plot(t,x)
set(gca,'FontSize',14) %set font size of axis tick labels to 18
xlabel('Time (s)','fontsize',14)
ylabel('Amplitude','fontsize',14)
title('Noisey sinusoid','fontsize',14)
grid on
%Plot power spectral density (PSD) of noise using three different methods:
%
%Method 1. Calcululate PSD from amplitude spectrum
N=2^16; %Number of discrete points in the FFT
y=fft(x,N)/fs; %fft of noise
z=fftshift(y);%center noise spectrum
f_vec=[0:1:N-1]*fs/N-fs/2; %designate sample frequencies
amplitude_spectrum=abs(z); %compute two-sided amplitude spectrum
ESD1=amplitude_spectrum.^2; %ESD = |F(w)|^2;
PSD1=ESD1/((N0-1)*Ts);% PSD=ESD/T where T = total time of sample
figure(3)
plot(f_vec,10*log10(PSD1));
xlabel('Frequency [Hz]','fontsize',14)
ylabel('dB/Hz','fontsize',14)
title('Power spectral density - method 1','fontsize',14)
grid on
set(gcf,'color','w'); %set background color from grey (default) to white
axis tight
%calculate average power using PSD calclated from method 1:
Average_power_method_1=sum(PSD1)*fs/N; % Pav=sum(PSD)*delta_f where delta_f=fs/N;
%
%Method 2 - Calculate PSD from autocorrelation
time_lag=((-length(x)+1):1:(length(x)-1))*Ts;
auto_cor=xcorr(x,x)/fs; %Use xcorr function to find PSD
y=1/fs*fft(auto_cor,N); %fft of auto correlation function
PSD2=abs(1/(N0-1)*fftshift(fft(auto_cor,N)));
figure(4)
plot(f_vec,10*log10(PSD2));%use convolution
xlabel('Frequency [Hz]','fontsize',14)
ylabel('dB/Hz','fontsize',14)
title('Power spectral density - method 2','fontsize',14)
grid on
set(gcf,'color','w'); %set background color from grey (default) to white
axis tight
%calculate average power using PSD calclated from method 1:
Average_power_method_2=sum(PSD2)*fs/N; %Pav=sum(PSD)*delta_f where delta_f=fs/N;
%
%Method 3 - Calculate PSD using built in pwelch function
figure(5)
PSD3=periodogram(x,[],N,fs,'centered');
plot(10*log10(PSD3))
xlabel('Frequency [Hz]','fontsize',14)
ylabel('dB/Hz','fontsize',14)
title('Power spectral density - method 3','fontsize',14)
grid on
set(gcf,'color','w'); %set background color from grey (default) to white
axis tight
Average_power_method_3=sum(PSD3)*fs/N; %Pav=sum(PSD)*delta_f where delta_f=fs/N;
%
%Calculate mean and average PSD of noise:
PSD_noise=periodogram(noise,[],N,fs,'centered');
Average_noise_PSD=mean(PSD_noise);
Mean_noise=mean(noise);

image-20230531004822838

image-20230531005008418

The power spectral density plots for methods 2 and 3 exactly match that for method 1 (shown above).

reference

enbw Matlab URL:https://www.mathworks.com/help/signal/ref/enbw.html

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N = 256;
wn = hanning(N);
s1 = sum(wn)^2;
s2 = sum(wn.^2);

(N*s2)/s1
enbw(wn)
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ans =

1.4942


ans =

1.4942

Schmid, H. (2012). How to use the FFT and Matlab's pwelch function for signal and noise simulations and measurements. URL:http://www.schmid-werren.ch/hanspeter/publications/2012fftnoise.pdf

Bonnie C.Baker. Reading and Using Fast Fourier Transforms (FFT) URL:http://ww1.microchip.com/downloads/en/appnotes/00681a.pdf

FFT analysis: SNR and Noise level vary with FFT Window size URL:https://www.virtins.com/forum/viewtopic.php?f=7&t=1382

Lyons, R. G. (2011). Understanding digital signal processing (3rd ed.). Prentice Hall

Stefan Scholl, "Exact Signal Measurements using FFT Analysis",Microelectronic Systems Design Research Group, TU Kaiserslautern, Germany. [pdf]

Aaron Scher. PSD, Autocorrelation, and Noise in MATLAB [pdf]

Aaron Scher. FFT, total energy, and energy spectral density computations in MATLAB [pdf]

Amplitude Estimation and Zero Padding URL:https://www.mathworks.com/help/signal/ug/amplitude-estimation-and-zero-padding.html

Harris, F. (1978). On the use of windows for harmonic analysis with the discrete Fourier transform. Proceedings of the IEEE, 66, 51-83. [pdf]

Harris, F. J. . (1976). Windows, harmonic analysis and the discrete fourier transform. [pdf]

Wang Hongwei. Virtins. Evaluation of Various Window Functions using Multi-Instrument [pdf]

Properties of FFT Windows Used in Stable32 [pdf]

Solomon, Jr, O M. PSD computations using Welch's method. [Power Spectral Density (PSD)]. United States. https://doi.org/10.2172/5688766 [pdf]

Measure Power of Deterministic Periodic Signals [https://www.mathworks.com/help/signal/ug/measuring-the-power-of-deterministic-periodic-signals.html]

Mathuranathan. Equivalent noise bandwidth (ENBW) of window functions. [https://www.gaussianwaves.com/2020/09/equivalent-noise-bandwidth-enbw-of-window-functions/]

recordingblogs, Equivalent noise bandwidth [https://www.recordingblogs.com/wiki/equivalent-noise-bandwidth]

unpingco, Python for Signal Processing [https://github.com/unpingco/Python-for-Signal-Processing/blob/master/Windowing_Part2.ipynb]

Pavan, Schreier and Temes, "Understanding Delta-Sigma Data Converters, Second Edition" ISBN 978-1-119-25827-8

A finite-length data record = an infinite record multiplied by a rectangular window

Windowing is unavoidable


Applying the Hanning window (or any window) to a periodic signal creates leakage.

leakage:

​ The component at one frequency leaks into the vicinity of another compnent owing to the spectral smearing introdued by window.

Notice side lobes adding out of phase can reduce the heights of the peaks

Windowed Signal

Short transient signals in the time domain produce high, broadband frequency content.

sharpTransient

To reduce leakage, a mathematical function called a window is applied to the data. Windows are designed to reduce the sharp transient in the re-created signal as much as possible.

windowedsignal

Because the sharp transients are reduced and smoothed, the broadband frequency of the spectral leakage is also reduced.

Periodic versus Non-Periodic Background

When performing a Fourier Transform on measurement data, a window affects periodic and non-periodic data differently:

  • Periodic (No Window needed): A signal captured in a periodic manner does not require a window, and a resulting Fourier Transform has no leakage. Applying a window alters the resulting Fourier transform, and even creates spectral leakage where there would have been no leakage otherwise.

  • Non-periodic (Window needed): Windows are used on signals that are captured in a non-periodic manner to reduce spectral leakage and get closer to the periodic results. A window can minimize the leakage present in a non-periodic signal, but cannot eliminate it.

The signal is repeated and appended mathematically because the measured data is assumed to be representative of the entire original signal

Periodic

When a measurement signal is captured in a periodic manner, the Fourier Transform of the captured signal will have no leakage in the frequency domain.

A window is not recommended for a periodic signal as it will distort the signal in an unnecessary manner, and actually creates spectral leakage.

captured-periodic


Maloberti, F. Data Converters. Dordrecht, Netherlands: Springer, 2007.

image-20250825231711883

image-20250825232155617

Non-periodic

The same sine wave, with a different measurement time, results in a non-periodic captured signal. Here, when the captured signal is repeated, the original sine wave signal is not re-created.

captured-nonperiodic

In fact, several broadband transient events (circled in red) are introduced. These transients create a broadband response, or leakage.

Windows are used to minimize this leakage effect in the frequency domain.

leakage-vs-nonleakage

Hanning

When doing operational noise and vibration measurements, the Hanning window is commonly used.

Random data has spectral leakage due to the abrupt cutoff at the beginning and end of the time block. It is non-periodic.

There is no way to ensure that the captured random signal is periodic by varying the measurement time.

Hanning windows are often used with random data because they have moderate impact on the frequency resolution and amplitude accuracy of the resulting frequency spectrum.

  • The maximum amplitude error of a Hanning window is 15%

    In the cited article, all spectral data had an amplitude correction factor applied.

  • while the frequency leakage is typically confined to 1.5 spectral lines to each side of the original sine wave signal

hanning.png

periodic signal

Applying the Hanning window (or any window) to a periodic signal creates leakage.

hanning-periodicsignal

The periodically captured sine wave with the Hanning window (blue) is wider in frequency than the original signal (red)

In the figure, the sine wave with the Hanning window (blue) is wider in frequency than the original signal (red).

non-periodic signal

When a Hanning window is applied to a non-periodic signal, the leakage is greatly reduced and the amplitude is higher.

hanning-nonperiodicsignal

A non-periodically captured sine wave (magenta) has a spectral leakage over the entire bandwidth, applying a Hanning window minimized the leakage (green)

RMS calculation

A RMS calculation sums up the energy within a frequency range.

rms-cal

  • both the RMS of the periodic and non-periodic signals with a Hanning window are equal to the RMS of the leakage-free sine wave.

  • Only the RMS of the non-periodic sine wave without a window applied is not equal to the others

With the leakage spread over a smaller frequency range, doing analysis calculations like RMS yields more accurate results.

Flattop

  • The Flattop window has a better amplitude accuracy in frequency domain compared to the Hanning window,

    The maximum amplitude error of a Flattop window is less than 0.01%. By contrast, the Hanning window maximum amplitude error is 15%.

  • A Flattop window confines leakage to 3.43 spectral lines to each side of the original signal.

amplitude errors

These maximum amplitude errors assume that amplitude correction factors are applied to the frequency spectrums. These amplitude correction factors compensate for any reduction caused by applying a window.

flattop-amplitude

leakage

The frequency accuracy of the Flattop window is more coarse compared to a Hanning window. As a result, the Flattop window is typically employed on data where frequency peaks are distinct and well separated from each other.

flattop-leakage

When the frequency peaks are not guaranteed to be well separated, the Hanning window is preferred because it is less likely to cause individual peaks to be lost in the spectrum

flattop-2tone

Spectrum of two periodically captured tones that are \(4Hz\) apart with a \(1Hz\) frequency resolution. The spectrum with a Hanning window (green) shows two peaks while the spectrum with a Flattop window (blue) shows one peak.

Note that at the original frequencies of the tones the amplitude is correct and equal to one for both windows.

One common application for a flattop window is performing calibration. For example, a sound pistonphone only produces one single and distinct frequency during microphone calibration.

Uniform

A Uniform window has a value of 1.0 across the entire measurement time. In reality, a Uniform window could be called no window.

Depending on the data acquisition system used, sometimes the term Rectangular window is also used.

  • A Uniform window creates no frequency or amplitude distortion when the measured signal is periodic.

  • When a measured signal is not periodic, the amplitude is reduced by a maximum of 36% and the frequency content is spread over the entire bandwidth of the measurement.

    This is due to sharp transients that are created by repeating and appending the measured signal.

Whenever a measurement signal is periodic, a Uniform window is preferred.

Applying a Hanning or Flattop window to a periodic signal will actually create amplitude and frequency distortion.

uniformwindow

Benefit of Reducing Leakage

The benefit is not that the captured signal is perfectly replicated.

The main benefit is that the leakage is now confined over a smaller frequency range, instead of affecting the entire frequency bandwidth of the measurement.

With the leakage spread over a smaller frequency range, doing analysis calculations like RMS yields more accurate results.

rms-windowed

It is impossible to calculate the proper RMS amplitude estimate over a limited frequency range of the un-windowed sine wave, since the leakage is over the full frequency range. Therefore the RMS amplitude is not correct.

Two tones

In the case of two closely spaced sine tones, without a window being applied, two tones frequencies would leak into each other, which make determining the true amplitude of individual peaks very difficult.

The window makes it easier to separate and distinguish each tone so a proper analysis could be performed.

windowed-2tone

window function in frequency domain

The transfer function \(a(f)\) of a window \(w_j, j \in [0, N-1]\) expresses the response of the window to a sinusoidal signal at an offset of \(f\) frequency bins, i.e. DFT .

real part: \[ a_r(f)=\sum_{j=0}^{N-1}w_j\cos (2\pi f j/N) \]

imaginary part: \[ a_i(f)=\sum_{j=0}^{N-1}w_j\sin (2\pi f j/N) \]

frequency response can be obtained as \[ a(f) = \frac{\sqrt{a_r^2+a_i^2}}{S_1} \] where \(S_1 = \sum _{k=0}^{N-1}w_k\)

Rectangular window example

aka. Uniform window, "Rectangular" window, "no window"

Whenever a measurement signal is periodic, a Uniform window is preferred. Applying a Hanning or Flattop window to a periodic signal will actually create amplitude and frequency distortion.

  1. When \(f=0\)

\[ a_r(f) + ja_i(f) = \sum_{k=0}^{N-1}w_k = N \]

  1. When \(f \neq 0\)

\[\begin{align} a_r(f) + ja_i(f) &= \sum_{k=0}^{N-1} e^{\frac{j2\pi k f}{N}} \\ &= \sum_{k=0}^{N/2} e^{\frac{j2\pi k f}{N}} + e^{\frac{j2\pi (k+N/2) f}{N}} \\ &= \sum_{k=0}^{N/2} e^{\frac{j2\pi k f}{N}} + e^{j\pi} e^{\frac{j2\pi k f}{N}} \\ &= \sum_{k=0}^{N/2} e^{\frac{j2\pi k f}{N}} - e^{\frac{j2\pi k f}{N}} \\ &= 0 \end{align}\]

A Uniform window creates no frequency or amplitude distortion when the measured signal is periodic.

However, if the signal cannot be guaranteed to be periodic, a Uniform window should be avoided.

Window Properties

There is no possibility of trade-off between main-lobe width and sied-lobe amplitude, since the window length is the only variable parameter.

The rectangular window has the narrowest main lobe for a given length, i.e. \(\Delta _{ml}=4\pi/L\)

Other windows include the Bartlett, Hann, and Hamming windows. The DTFTs of all these windows have main-lobe width \(\Delta _{ml}=8\pi/(L-1)\), which is approximately twice that of the rectangular window, but they have significantly smaller side-lobe amplitudes.

Demo

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clc;
clear all;

N = 512;
fs = 40*1e3; % 40kHz
fres = fs/N; % 78.125
tt = (0:N-1)*1/fs;
ff = (0:N/2)*fres;
fin = 390.625;

whan = hanning(N); % hanning window
wrect = rectwin(N); % rect window


% fin/fs = 5/N, periodically captured sine wave
wv = cos(2*pi*fin*tt);
power = periodogram(wv, whan, N, fs, 'power');
X = (power).^0.5*2^0.5;
psd = periodogram(wv, whan, N, fs, 'psd');
rms = sum(psd*fres)^0.5;
fprintf('RMS@periodic & hanning: %.5f\n', rms);

power_rect = periodogram(wv, wrect, N, fs, 'power');
X_rect = (power_rect).^0.5*2^0.5;
psd_rect = periodogram(wv, wrect, N, fs, 'psd');
rms_rect = sum(psd_rect*fres)^0.5;
fprintf('RMS@periodic & rect: %.5f\n', rms_rect);


figure(1)
plot(ff, X, 'r-o', ff, X_rect, 'b-s');
xlabel('Frequency(Hz)');
ylabel('|X|')
title('Amplitude spectrum of periodically captured sine wave');
legend('w/ hanning', 'w/ rect');
grid on
grid minor
% rectangular window provide higher frequency resolution
% hanning window induce leakage for the periodically captured sine wave



% fin - 0.5fres
fin_lkg0d5 = fin - 0.5*fres;
wv_lkg0d5 = cos(2*pi*fin_lkg0d5*tt);
power_lkg0d5 = periodogram(wv_lkg0d5, whan, N, fs, 'power');
X_lkg0d5 = (power_lkg0d5).^0.5*2^0.5;
psd_lkg0d5 = periodogram(wv_lkg0d5, whan, N, fs, 'psd');
rms_lkg0d5 = sum(psd_lkg0d5*fres)^0.5;
fprintf('RMS@-0.5fres & hanning: %.5f\n', rms_lkg0d5);

power_lkg0d5_rect = periodogram(wv_lkg0d5, wrect, N, fs, 'power');
X_lkg0d5_rect = (power_lkg0d5_rect).^0.5*2^0.5;
psd_lkg0d5_rect = periodogram(wv_lkg0d5, wrect, N, fs, 'psd');
rms_lkg0d5_rect = sum(psd_lkg0d5_rect*fres)^0.5;
fprintf('RMS@-0.5fres & rect: %.5f\n', rms_lkg0d5_rect);

figure(2)
plot(ff, X_lkg0d5, 'r-o', ff, X_lkg0d5_rect, 'b-s');
xlabel('Frequency(Hz)');
ylabel('|X|')
title('Amplitude spectrum of -0.5fres');
legend('w/ hanning', 'w/ rect');
grid on
grid minor
% hanning reduce leakage and max amplitude error 15%



% fin - 0.25fres
fin_lkg0d25 = fin - 0.25*fres;
wv_lkg0d25 = cos(2*pi*fin_lkg0d25*tt);
power_lkg0d25 = periodogram(wv_lkg0d25, whan, N, fs, 'power');
X_lkg0d25 = (power_lkg0d25).^0.5*2^0.5;
psd_lkg0d25 = periodogram(wv_lkg0d25, whan, N, fs, 'psd');
rms_lkg0d25 = sum(psd_lkg0d25*fres)^0.5;
fprintf('RMS@-0.25fres & hanning: %.5f\n', rms_lkg0d25);

power_lkg0d25_rect = periodogram(wv_lkg0d25, wrect, N, fs, 'power');
X_lkg0d25_rect = (power_lkg0d25_rect).^0.5*2^0.5;
psd_lkg0d25_rect = periodogram(wv_lkg0d25, wrect, N, fs, 'psd');
rms_lkg0d25_rect = sum(psd_lkg0d25_rect*fres)^0.5;
fprintf('RMS@-0.25fres & rect: %.5f\n', rms_lkg0d25_rect);

figure(3)
plot(ff, X_lkg0d25, 'r-o', ff, X_lkg0d25_rect, 'b-s');
xlabel('Frequency(Hz)');
ylabel('|X|')
title('Amplitude spectrum of -0.25fres');
legend('w/ hanning', 'w/ rect');
grid on
grid minor
% hanning reduce leakage

output

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RMS@periodic & hanning: 0.70711
RMS@periodic & rect: 0.70711
RMS@-0.5fres & hanning: 0.70711
RMS@-0.5fres & rect: 0.70711
RMS@-0.25fres & hanning: 0.70711
RMS@-0.25fres & rect: 0.70780

image-20230526005823613

rectangular window provide higher frequency resolution

image-20230526005934411

hanning reduce leakage and max amplitude error 15%

image-20230526010047826

hanning reduce leakage and reduce amplitude error

reference

Windows and Spectral Leakage. URL:https://community.sw.siemens.com/s/article/windows-and-spectral-leakage

Article (20416822) Title: How to Utilize a Windowing Technique for Accurate DFT URL: https://support.cadence.com/apex/ArticleAttachmentPortal?id=a1Od000000050UrEAI

B.P. Lathi, Roger Green. Linear Systems and Signals (The Oxford Series in Electrical and Computer Engineering) 3rd Edition

Window Types: Hanning, Flattop, Uniform, Tukey, and Exponential URL:https://community.sw.siemens.com/s/article/window-types-hanning-flattop-uniform-tukey-and-exponential

Window Correction Factors URL:https://community.sw.siemens.com/s/article/window-correction-factors

Root Mean Square (RMS) and Overall Level. URL:https://community.sw.siemens.com/s/article/root-mean-square-rms-and-overall-level

Alan V Oppenheim, Ronald W. Schafer. Discrete-Time Signal Processing, 3rd edition

Stefan Scholl, "Exact Signal Measurements using FFT Analysis",Microelectronic Systems Design Research Group, TU Kaiserslautern, Germany. [ pdf ]

Harris, F. (1978). On the use of windows for harmonic analysis with the discrete Fourier transform. Proceedings of the IEEE, 66, 51-83. [pdf]

Equivalent noise bandwidth (ENBW) of window functions URL:https://www.gaussianwaves.com/2020/09/equivalent-noise-bandwidth-enbw-of-window-functions/

Why should I zero-pad a signal before taking the Fourier transform? URL:https://dsp.stackexchange.com/q/741

enbw function in MATLAB URL:https://www.mathworks.com/help/signal/ref/enbw.html

Window function – figure of merits URL:https://www.gaussianwaves.com/2020/09/window-function-figure-of-merits/

Memos on FFT With Windowing URL:https://a2d2ic.wordpress.com/2018/02/01/memos-on-fft-with-windowing/

Jens Ahrens, "Some Notes on Windows in Spectral Analysis," Tech. Report, Chalmers Univeristy of Technology, 2020. URL:https://appliedacousticschalmers.github.io/scaling-of-the-dft/notes_on_windows/

Digital Delay Model

Akio Kitagawa, Analog layout design https://mixsignal.files.wordpress.com/2013/03/analog-layout.pdf

THE WIRE http://bwrcs.eecs.berkeley.edu/Classes/icdesign/ee141_f01/Notes/chapter4.pdf

Anoop Veliyath, Design Engineer, Cadence Design Systems. Accurately Modeling Transmission Line Behavior with an LC Network-based Approach [pdf]

Mark Horowitz. Lecture 2: Wires and Wire Models [pdf]

Neil Weste and David Harris. 2010. CMOS VLSI Design: A Circuits and Systems Perspective (4th. ed.). Addison-Wesley Publishing Company, USA.

Cheng-Kok Koh. EE695K Modeling and Optimization of High Performance Interconnect [lec3a_pdf]

Vishal Saxena. ECE 445 Intro to VLSI Design: Lectures for Spring 2019 https://www.eecis.udel.edu/~vsaxena/courses/ece445/s19/ECE445.htm

Effective Switching resistance

image-20231114001209252

https://www.eecis.udel.edu/~vsaxena/courses/ece445/s19/Lecture%20Notes/lec15_ece445.pdf

wire delay

Elmore Delay

image-20230624234813719

image-20230624234940864

image-20230625001756173

Basic idea: use of mean of \(v'(t)\) to approximate median of \(v'(t)\)

image-20230624235148246

image-20230625002239199

Elmore delay approximates the median of \(h(t)\) by the mean of \(h(t)\)

Distributed RC-Line

image-20230624224005736

Lumped approximations

\(rc\)-models

If your simulator does not support a distributed \(rc\)-model, or if the computational complexity of these models slows down your simulation too much, you can construct a simple yet accurate model yourself by approximating the distributed \(rc\) by a lumped RC network with a limited number of elements

image-20230624230057265

The accuracy of the model is determined by the number of stages. For instance, the error of the \(\Pi -3\) model is less than 3%, which is generally sufficient.


Why use "\(\Pi\) Model"

image-20230624230800255


examples

image-20230624224643487

image-20230624224923241

Wire Inductive Effect

  • RC delay increases quadratically with length
  • LC delay (speed of light flight time) increases linearly with length

Inductance will only be important to the delay of low-resistance signals such as wide clock lines


wave

Signal propagates over the wire as a wave (rather than diffusing as in \(rc\) only models)

Signal propagates by alternately transferring energy from capacitive to inductive modes

Glitches & Hazards

CPE166/EEE 270 Advanced Logic Design-Digital Design: Time Behavior of Combinational Networks: https://www.csus.edu/indiv/p/pangj/166/f/sram/Handout_Hazard.pdf

John Knight, ELEC3500 Glitches and Hazards in Digital Circuits http://www.doe.carleton.ca/~shams/ELEC3500/hazards.pdf

  • A glitch is an unwanted pulse at the output of a combinational logic network – a momentary change in an output that should not have changed
  • A circuit with the potential for a glitch is said to have a hazard
  • In other words a hazard is something intrinsic about a circuit; a circuit with hazard may or may not have a glitch depending on input patterns and the electric characteristics of the circuit.

When do circuits have hazards ?

Hazards are potential unwanted transients that occur in the output when different paths from input to output have different propagation delays

Types of Hazards (on an output)

static 1-hazard, static 0-hazard, dynamic hazard

image-20220508183800744

Hazard's Concern

  • Hazards do not hurt synchronous circuits
  • Hazards Kill Asynchronous Circuits
  • Glitches Increase Power Consumption

Isolation cells

Isolation cells and Level Shifter cells URL: https://vlsitutorials.com/isolation-cells-level-shifter-cells-low-power-vlsi/

Isolation cells are additional cells inserted by the synthesis tools for isolating the buses/wires crossing from power-gated domain of a circuit to its always-on domain (AON).

To prevent corruption of always-on domain, we clamp the nets crossing the power domains to a value depending upon the design.

A simple circuit having a switchable (or gated) power domain

isolation-cells-1-1

The circuit shown in Figure 1, after isolation cells are inserted

isolation-cells-2

Always-On Buffer

640?wx_fmt=png

image-20230211001607578

image-20230211001708189

image-20230211001849150

Clock Gating

The Ultimate Guide to Clock Gating https://anysilicon.com/the-ultimate-guide-to-clock-gating/

Clock Gating is defined as: "Clock gating is a technique/methodology to turn off the clock to certain parts of the digital design when not needed".

AND gate-based clock gating

In simplest form a clock gating can be achieved by using an AND gate as shown in picture below

clock gating

However, this simplest form of clock gating technique has some problem of generating glitches in the clock provide to the FF, which are not desirable.

img

Glitches in enable/gated clock

Latch based clock gating

These glitches can be removed by introducing a negative edge triggered FF (assuming downstream FFs are positive edge) or low-level sensitive latch at the output of the clock enable signal.

clock gating

This will make sure that any glitch in the clock enable signal will not be visible to the gated clock output. The Latch output will only be updated during the negative clock cycle and thus input to AND gate will be stable high.

clock gating

Glitch Free Gated Clock

OCV Derating With AOCV

Genus Attribute Reference 22.1

Innovus Text Command Reference 22.10

Article (20416394) Title: Analysis with Advanced On-chip Variation (AOCV) derating in EDI system and ETS URL: https://support.cadence.com/apex/ArticleAttachmentPortal?id=a1Od000000050NxEAI

timing_aocv_derate_mode

1
timing_aocv_derate_mode{aocv_multiplicative | aocv_additive}

Default: aocv_multiplicative

Controls the AOCV derating mode.

When set to aocv_multiplicative, the derating factor will be calculated as AOCV derating * OCV derating, which is set using the set_timing_derate command.

When set to aocv_additive, the derating factor will be calculated as AOCV derating + OCV derating values.

When you use this global variable, the report_timing command shows the total_derate column in the timing report output, which allows you to view and cross-check the calculated total derate factor.

To set this global variable, use the set_global command.

image-20221210143256639

preserve hand-instantiated cells

To preserve the hand-instantiated cells

1
set_dont_touch [get_cells -hierarchical *dont_touch_*]

The instances whose name contain "dont_touch_" shall be preserved during synthesis

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// no performace concerns, rest sync use sync3 is enough

module CN_resetb_sync_cell
(
input resetb_in,
input clkdst,
output resetb_out
);

`ifdef USE_VERILOG
reg [2:0] resetb_dly;
`else
wire [2:0] resetb_dly;
`endif

`ifdef USE_VERILOG
always @(posedge clkdst or negedge resetb_in)
if (~resetb_in) resetb_dly <= 3'b000;
else resetb_dly <= {resetb_dly[1:0], 1'b1};
`else
SDFCNQD4 dont_touch_sync_flop0 (
.SI(1'b0),
.SE(1'b0),
.CP(clkdst),
.CDN(resetb_in),
.D(1'b1),
.Q(resetb_dly[0])
);
SDFCNQD4 dont_touch_sync_flop1 (
.SI(1'b0),
.SE(1'b0),
.CP(clkdst),
.CDN(resetb_in),
.D(resetb_dly[0]),
.Q(resetb_dly[1])
);
SDFCNQD4 dont_touch_sync_flop2 (
.SI(1'b0),
.SE(1'b0),
.CP(clkdst),
.CDN(resetb_in),
.D(resetb_dly[1]),
.Q(resetb_dly[2])
);
`endif

assign resetb_out = resetb_dly[2];

endmodule

Gain-boosted cascode

TODO 📅

Zero-Value Time Constant Analysis

TODO 📅

Transmission Gate

Equivalent Resistance is defined by large signal

[https://www.ece.ucdavis.edu/~ramirtha/EEC116/F11/TGlecture.pdf]

CMRR (Common-Mode Properties)

image-20251029215920630


image-20251029215548157

MOSFET Thermal Noise

Legacy Long-Channel Model

image-20251028010509047 \[ \color{red} \overline{i^2_d} \propto \gamma \propto \eta \propto \frac{1}{V_{DS}} \]

image-20251028194916465


[https://www.eecg.toronto.edu/~johns/ece512/lecture_notes/04_noise_2_per_page.pdf]

image-20251027234644231


[https://people.engr.tamu.edu/spalermo/ecen474/lecture12_ee474_noise.pdf]

image-20251027235211591

Short-Channel Effects

Gildenblat, G. S. (2010). Compact modeling : principles, techniques and applications. Springer.

VDS Effect On Channel Noise

image-20251028193945932

\[ \color{red} \overline{i^2_d} \propto V_{DS} \] image-20251028194509372


K. Ohmori and S. Amakawa, "Direct White Noise Characterization of Short-Channel MOSFETs," in IEEE Transactions on Electron Devices, vol. 68, no. 4, pp. 1478-1482, April 2021 [pdf, slides]

image-20251028005749046

inverter capacitance simulation

inverter input

R-C, series equivalent circuit

invCap

inverter output

R-C, parallel equivalent circuit


AC simulation

image-20250628112910588

@vi = 0

image-20250628104042741

sweep vi from 0 to 800mV (vdd)

image-20250628105510374


SP simulation

image-20250628112857124

image-20250628112620876

EEStream. Cadence - How to find device capacitance - DC simulation, SP simulation and Large-signal SP simulation [https://www.youtube.com/watch?v=M3zP6eJnONk]

image-20250628114414562

50-ohm?

Why is 50-ohm characteristic impedance standardized in RF and Microwave systems? [link]

[https://www.microwaves101.com/encyclopedias/why-fifty-ohms]

It was a compromise made and a tradeoff between power handling (red curve) and losses (blue curve)

Gm Rout Lemma

\[ A_V = -G_m R_{out} \]

image-20231021092407849

Relative Sensitivity

Olivier de Weck, Karen Willcox. MIT, Gradient Calculation and Sensitivity Analysis [pdf]

Karti Mayaram, ECE 521 Fall 2016 Analog Circuit Simulation, Sensitivity and noise analyses [https://web.engr.oregonstate.edu/~karti/ece521/lec16_11_09.pdf]

Assuming Target \(T\) ( for example, the total resistance) is function of \(x_1,x_2,...,x_N\), then total variation can be expressed as

\[\begin{align} dT &= \sum_{n=1}^N\frac{\partial T}{\partial x_n}dx_n \\ &= \sum_{n=1}^N\frac{\partial T}{\partial x_n}x_n\cdot \frac{dx_n}{x_n} \end{align}\]

Then, we obtain relative variation \[\begin{align} \frac{dT}{T} &= \sum_{n=1}^N\frac{\partial T}{\partial x_n}\frac{x_n}{T}\cdot \frac{dx_n}{x_n} \\ &= \sum_{n=1}^N S_{x_n}^T \cdot \frac{dx_n}{x_n} \end{align}\]

⭐ where \(S_{x_n}^T=\frac{\partial T}{\partial x_n}\frac{x_n}{T}\) is relative sensitivity

relative sensitivity connect \(\frac{dx_n}{x_n}\) with total relative variation \(\frac{dT}{T}\)

And \(dT\) can be expressed as \[ dT =\sum_{n=1}^N S_{x_n}^T T\cdot \frac{dx_n}{x_n} = \sum_{n=1}^N x_n'\cdot \frac{dx_n}{x_n} \] ⭐ where \(x_n'= S_{x_n}^T T\) is the contribution of \(x_n\) in \(T\)

⭐ For parallel or series resistors, it can prove \(\sum_{n=1}^N S_{x_n}^T = 1\) and \(\sum_{n=1}^N x_n'=T\)


parallel_pgx.drawio

Here \(T= R_1 \parallel R_2 = \frac{R_1R_2}{R_1+R_2}\), and \(T|_{R_1=8000, R_2=2000} = 1600\)

We obtain relative sensitivity: \[\begin{align} S_{R_1}^T & = \frac{R_2}{R_1+R_2} \\ S_{R_2}^T & = \frac{R_1}{R_1+R_2} \end{align}\]

The contribution of \(R_1\) and \(R_2\) to \(T\) \[\begin{align} R_1' &= S_{R_1}^T T | _{R_1=8000, R_2=2000} = 320 \\ R_2' &= S_{R_2}^T T | _{R_1=8000, R_2=2000} = 1280 \end{align}\]


Normalized sensitivity captures relative sensitivity

change in objective per change in design variable

Normalized sensitivity

Device Current Components

image-20250101101419687

common gate amplifiers

No alt text provided for this image

[https://www.linkedin.com/posts/chembiyan-t-0b34b910_analog-analogdesign-rfdesign-activity-7126946716938878976-GeW6?utm_source=share&utm_medium=member_desktop]

Shot Noise

Any dc current flowing through a diode generates the so-called "shot noise" due to the random nature of the hole and electron transitions across the pn junction

Shot noise is not relevant in CMOS devices since it is only present in bipolar transistors and junction diodes

Level Shifter

image-20241003224949171

TIA

image-20240824111517140

\[\begin{align} I_{in} &= \frac{V_i}{R_S} + \frac{V_i - V_o}{R_F} \\ \frac{V_i - V_o}{R_F} &= g_m V_i \end{align}\]

Then

\[\begin{align} V_o &= \frac{I_{in}R_F}{\frac{R_S+R_F}{R_S}\frac{1}{1-g_mR_F}- 1} \\ V_i &= \frac{I_{in}R_F}{\frac{R_F}{R_S}+g_mR_F} \end{align}\] If \(R_S \gg R_F\) \[\begin{align} V_o &= \frac{I_{in}}{g_m}(1-g_mR_F) \\ V_i &= \frac{I_{in}}{g_m} \end{align}\]

linearity

TIA stage allows for improved gain with better linearity, as mostly signal current passes through \(R_F\) TODO 📅 ??? Quantitative analysis

Switched-Capacitor Resistor

\[ R_{eq} = \frac{1}{f_sC} \]

image-20240905202145206

[https://youtu.be/SL3-9ZMwdJQ?si=m_FSjnFQH4wjbZKH&t=1339]

Channel-Length Modulation & Pinched off

  • \(\lambda \propto \frac{1}{L_g}\)
  • \(\lambda \propto \frac{1}{V_{DS}}\)

image-20241116080122184

  • If \(V_{DS}\) is slightly greater than \(V_{GS} - V_{TH}\), then the inversion layer stops at \(x \leq L\), and we say the channel is "pinched off"
  • Upon passing the pinchoff point, the electrons simply shoot through the depletion region near the drain junction and arrive at the drain terminal

\(L^{'}\) is the function of \(V_{DS}\)

with \(\frac{1}{L^{'}} = \frac{1}{L-\Delta L}=\frac{L+\Delta L}{L^2-\Delta L^2}\approx \frac{1}{L}\left(1+\frac{\Delta L}{L}\right)\), we have \[ I_D \approx \frac{1}{2}\mu_n C_{ox}\frac{W}{L}\left(1+\frac{\Delta L}{L}\right)(V_{GS}-V_{TH})^2 = \frac{1}{2}\mu_n C_{ox}\frac{W}{L}(V_{GS}-V_{TH})^2 (1+\lambda V_{DS}) \] assuming \(\frac{\Delta L}{L} = \lambda V_{DS}\)

\(\lambda\) represents the relative variation in length for a given increment in \(V_{DS}\). Thus, for longer channels, \(\lambda\) is smaller


In reality, however, \(r_O\) varies with \(V_{DS}\). As \(V_{DS}\) increases and the pinch-off point moves toward the source, the rate at which the depletion region around the source becomes wider decreases, resulting in a higher incremental output impedance.

image-20241116084353713

Early Voltage indicator

\[ g_m r_o = \frac{g_m}{I_D}I_D \cdot \frac{V_A}{I_D} = \frac{g_m}{I_D} \cdot V_A \]

$g_m r_o $ is the indicator of \(V_A\), if \(\frac{g_m}{I_D}\) is same

Cgd of Common-Source Stage

Miller effect of Cgd during layout

Nonlinearity of Differential Circuits

image-20240804173949430

\[ \cos^3\omega t = \frac{3\cos \omega t + \cos(3\omega t)}{4} \]

image-20240804174042088

Zero in differential pair with active current mirror

image-20240629103021286

Noting the circuit consists of a "slow path" (M1, M3, M4) in parallel with a "fast path" (M2)

  • "slow path" \[ H_\text{slow}(s) = \frac{A_0}{(1+s/\omega _{pE})(1+s/\omega _{pO})} \]

  • "fast path" \[ H_\text{fast}(s) = \frac{A_0}{1+s/\omega _{pO}} \]

Then \[\begin{align} \frac{V_\text{out}}{V_\text{in}} &= H_\text{slow}(s) + H_\text{fast}(s) \\ &= \frac{A_0}{1+s/\omega _{pO}}\left(\frac{1}{1+s/\omega _{pE}} + 1 \right) \\ &= \frac{A_0(1+s/2\omega _{pE})}{(1+s/\omega _{pO})(1+s/\omega _{pE})} \end{align}\]

That is, the system exhibits a zero at \(2\omega_{pE}\)


signals traveling through two paths within an amplifier may cancel each other at one frequency, creating a zero in the transfer function

image-20240629104408168

\[ \omega_z = \frac{(A_1+A_2)\omega_{p1}\omega_{p2}}{A_1\omega_{p1}+A_2\omega_{p2}} \] noting \(\omega_{p1}\lt \omega_z \lt \omega_{p2}\)

"Zero" by Inspection

a method to predict the existence of "zero" by inspection, based on the concept of "Analog Phase Interpolation"

TODO 📅

Debashis Dhar, How to Recognize "Zero" by Inspection (Utilizing Analog Phase Interpolation) [https://www.linkedin.com/posts/debashis-dhar-12487024_how-to-recognize-zero-by-inspection-activity-7163364364329160704-9qOq?utm_source=share&utm_medium=member_desktop]

Random offset

The dependence of offset voltage and current mismatches upon the overdrive voltage is similar to our observations for corresponding noise quantities

differential pair

image-20240624222306837

In reality, since mismatches are independent statistical variables

image-20240624222417564

Above shows that the input transistors must be designed for high gain (\(g_mr_o = \frac{2}{V_{OV}\lambda}\)), which means they must be designed for small \(V_{GS}-V_{TH}\).

It is desirable to minimize \(V_{GS}-V_{TH}\) by lowering the tail current or increasing the transistor widths


For \(\frac{\Delta K}{K}\)

\[\begin{align} v_{os} g_m &= \Delta K \frac{W}{L}(V_{GS}-V_{TH})^2 \\ v_{os} 2K\frac{W}{L}(V_{GS}-V_{TH}) &= \Delta K \frac{W}{L}(V_{GS}-V_{TH})^2 \\ v_{os} &= \frac{V_{GS}-V_{TH}}{2} \frac{\Delta K}{K} \end{align}\]

The derivation for \(\frac{\Delta W/L}{W/L}\) is same with \(\frac{\Delta K}{K}\)


alternative derivation

\[\begin{align} \Delta V_\beta \cdot g_m &= \frac{\partial I_D}{\partial \beta} \Delta \beta \\ &= I_D \frac{\Delta \beta}{\beta} \end{align}\]

That is \(\Delta V_\beta = \frac{I_D}{g_m}\frac{\Delta \beta}{\beta}\)

\[ \Delta V_R \cdot g_m R = I_D \cdot \Delta R \]

That is \(\Delta V_R = \frac{I_D}{ g_m} \cdot \frac{\Delta R}{R}\)

[https://electronicengineering.phd.upc.edu/en/courses-and-seminars/courses-materials/2008-2009/slides-makinwa-1]


current mirror

image-20240624224944377

image-20240624225010443

To minimize current mismatch, the overdrive voltage must be maximized, a trend opposite to that in differential pair.

This is because as \(V_{GS}-V_{TH}\) increases, threshold mismatch has a lesser effect on the device currents

\(\Delta I_D= g_m \Delta V_{TH} = \frac{2I_D}{V_{OV}}\Delta V_{TH}\)

Effect of Feedback on Noise

Feedback does not improve the noise performance of circuits.

image-20240508205903213

The input-referred noise voltage and current remain the same if the feedback network introduces no noise.

RC charge & discharge

  • charge: \[ V_o(t) = V_{X}(1-e^{-\frac{t}{\tau}}) + V_{o,0}\cdot e^{\frac{-t}{\tau}} \]

  • discharge: \[ V_o(t) = V_{o,0}\cdot e^{-\frac{t}{\tau}} + V_{o,\infty}\cdot(1-e^{-\frac{t}{\tau}}) \]

  1. \(e^{-\frac{t}{\tau}}\) item determine the initial state
  2. \((1-e^{-\frac{t}{\tau}})\) item determine the final state

image-20231104231640290

image-20231104232000036

AC coupling

\(V_m=\frac{1}{4},\space \frac{3}{4}\) and its common voltage \(\frac{1}{2}\)

\(V_o=-\frac{1}{4},\space \frac{1}{4}\) and its common voltage \(0\)

image-20231121224940814

image-20231121225358509


\[ \tau = 200 \text{nF} \times (50+50)\text{ohm} = 20 \mu s \]

high level envelope:

image-20231121230155083

image-20231121230225895

Current mirror with source degeneration

image-20231103213308081

image-20231103213327501

degeneration

Razavi 2nd, problem 14.15

Monitored Analog Critical Parameters

monitor_parameters.drawio

Parameter Definition:

\[\begin{align} I_{\text{D,lin}} &= I_D \mid _{V_G=V_{DD},V_D=0.05V} \\ I_{\text{D,sat}} &= I_D \mid _{V_G=V_D=V_{DD}} \\ V_{\text{t,lin}} &= V_G \mid _{I_D=I_{\text{thx}}\cdot \frac{W}{L}@\{V_D=0.05V\}} \end{align}\]

\(I_{\text{thx}}\) could be different for technologies. (For N16, \(I_{\text{thx}}=10\)nA)


Constant Current Threshold Voltage

Extraction of constant current threshold voltage

gm-Maximum Method

Extraction of threshold voltage

[Inspect 4. Extracting Standard Parameters]

STB and PSTB in Spectre/RF

All credits to my colleague, Zhang Wenpian. > F. Wiedmann, "Loop gain simulation," Online:[https://sites.google.com/site/frankwiedmann/loopgain]

STB analysis

Spectre stb's "loopgain" is negative of "T" in paper[1] \[ T = \frac{2(AD-BC) - A + D}{2(AD-BC)-A+D-1} \]

AC simulation testbench, shown as below,

stb_pstb.drawio

  1. \(I_{inj}\) = 0, \(V_{inj}\) = 1

    B = if, D = ve

  2. \(I_{inj}\) = 1, \(V_{inj}\) = 0

    A = if, C = ve

PSTB analysis

Spectre pstb is similar to stb, just set pac as 1 instead of ac in current source and voltage source.

This analysis just use harmonic 0 transfer function in pac analysis, which has limitation.

Thevenin and Norton Equivalent Circuits

戴维南定理

image-20231021084850078

等效电阻的计算方法

image-20231021085151943

使用外加电源法时, 全部独立电源需要置零

诺顿定理

image-20231021090448282

Miller's Approximation: right-half-plane zero

image-20231021101204165

A quick inspection of this circuit reveals that a zero lies at a frequency where the current through \(C_{12}\) becomes equal to \(g_2V_1\).

When this occurs, the current through the parallel combination of \(C_2\) and \(R_2\) becomes zero, creating a zero in the transfer function.

In other words, we can write

\[\begin{align} g_2V_1 &= V_1sC_{12} \\ s &= \frac{g_2}{C_{12}} \end{align}\]

Nonoverlapping clock

Classical

image-20241016212042812

DWC

C2PHIa is important to ensure nonoverlapping and DelayA2B is due to level shifter

image-20241016212100040

Single ended Amplifier Offset Voltage

unity gain buffer

image-20220917115231508

\[\begin{align} V_o &= V_{o,dc}+A(V_p-V_m) \\ V_o' &= V_{o,dc}+A(V_p+V_{os}-V_m') \end{align}\]

Then, we get \[ V_{os}=\frac{V_o'-V_o}{A}+(V_m'-V_m) \] Due to \(V_o=V_m\) and \(V_o'=V_m'\) \[ V_{os}=(1/A+1)\Delta{V_m} \] or \[ V_{os}=(1/A+1)\Delta{V_o} \] if \(A \gg 1\) \[ V_{os}=\Delta{V_o} \]

non-inverting amplifier

image-20220917115308699 \[\begin{align} V_o &= V_{o,dc}+A(V_p-V_m) \\ V_o' &= V_{o,dc}+A(V_p+V_{os}-V_m') \\ V_m &= \beta V_o \\ V_m' &= \beta V_o' \end{align}\]

we get \[ V_{os}=\frac{V_o'-V_o}{A}+(V_m'-V_m) \] or \[ V_{os}=\frac{\Delta V_o}{A}+\beta \Delta V_o \] if \(A \gg 1\) \[ V_{os}=\beta \Delta V_o \] or \[ V_{os}=\Delta V_m \]


Lecture 22 Variability and Mismatch of Dr. Hesham A. Omran's Analog IC Design

image-20221022010448797

URL: https://www.master-micro.com/professional-courses/analog-ic-design/course-resources

Gotcha MOS ron

There is discrepancy between model operating point and \(V_{ds}/I_{ds}\)

I believe that the equation \(V_{ds}/I_{ds}\) is more appropriate where mos is used as switch, though \(V_{ds}=0\) is an outlier.

image-20230104230757729

image-20230104230837829

image-20230104230851475

Schmitt Inverter

image-20231021232912529

gm/ID Intuition

image-20230103220933081

small gm/ID for High ro, or high Early voltage \(V_A\)

Transit Frequency \(f_T\)

Defined as the frequency at which the small-signal current gain of a device is unity

image-20231213234524075


image-20240116233951006


image-20250701230019148

mag(Ids@ft) = Ig(1mA)

Aditya Varma Muppala. MMIC 08: High Frequency Device Characterization in Cadence - Fmax, Ft, NFmin vs Jd [https://youtu.be/kgEypIA8eus?si=sd4581x2hOuhsJ3P]


image-20250831165407595

MOSFET ZTC Condition Analysis

M. Coelho et al., "Is There a ZTC Biasing Point in the Leading-Edge FET Intrinsic Gain gmrDS?," 2025 9th International Young Engineers Forum on Electrical and Computer Engineering (YEF-ECE), Caparica / Lisbon, Portugal, 2025

zero temperature coefficient (ZTC)

image-20231212195536754

MOM cap of wo_mx

Monte Carlo model:

  • \(C_{pa}=C_{pa1}\), \(C_{pb}=C_{pb1}\) for each iteration during Process Variation
  • different variation is applied to \(C_{ab}\) and \(C_{a1b1}\) each iteration during Mismatch Variation, though \(C_{pa}\), \(C_{pb}\), \(C_{pa1}\) and \(C_{pb1}\) remain constant

image-20230220230434891

image-20230220230331505

Miller multiplication of Capacitor

Positive Cap

image-20231220225508580

image-20231220225450481

Negative Cap

image-20231220225910283

image-20231220230015868


gain has limited bandwidth

image-20231224212914366

image-20231224212541383

image-20231224212625409

\(V_o = V_i |A|e^{j\theta}\), and \(A_r = |A|\cos\theta\), \(A_i = |A|\sin\theta\)

Then \(I_i = (V_i - V_o)sC_f= V_i(1-|A|e^{j\theta})sC_f\), impedance is shown as below

\[\begin{align} Z &= \frac{V_i}{I_i} \\ &= \frac{1}{(1-|A|e^{j\theta})j\omega C_f} \\ &= -\frac{j}{\omega C_f\frac{1+|A|^2-2|A|\cos\theta}{1-|A|\cos\theta}} + \frac{|A|\sin\theta}{\omega C_f (1+|A|^2-2|A|\cos\theta)} \\ \end{align}\]

\(C_\text{eq}\) and \(R_\text{eq}\) are obtained \[\begin{align} C_\text{eq} &= \frac{1+|A|^2-2A_r}{1-A_r}\cdot C_f \\ R_\text{eq} &= \frac{A_i}{1+|A|^2-2A_r}\cdot \frac{1}{\omega C_f} \end{align}\]

D/S small signal model

image-20240106161059584

The Drain and Source of MOS are determined in DC operating point, i.e. large signal.

That is, top of \(M_2\) is drain and bottom is source, \[\begin{align} R_\text{eq2} &= \frac{r_\text{o2}+R_L}{1+g_\text{m2}r_\text{o2}} \\ & \simeq \frac{1}{g_\text{m2}} \end{align}\]

PMOS small signal model polarity

The small-signal models of NMOS and PMOS transistors are identical

A negative \(\Delta V_\text{GS}\) leads to a negative \(\Delta I_D\).

Recall that \(I_D\), in the direction shown here, is negative because the actual current of holes flows from the source to the drain.

image-20240106170315177

Conversely, a positive \(\Delta V_\text{GS}\) produces a positive \(\Delta I_D\), as is the case for an NMOS device.

image-20240106164923917

Leakage in MOS

image-20241109195527005

  • Subthreshold leakage
    • Drain-Induced Barrier Lowering (DIBL)
  • Reverse-bias Source/Drain junction leakages
  • Gate leakage
  • two other leakage mechanisms
    • Gate Induced Drain Leakage (GIDL)
    • Punchthrough

image-20241110001311117

W. M. Elgharbawy and M. A. Bayoumi, "Leakage sources and possible solutions in nanometer CMOS technologies," in IEEE Circuits and Systems Magazine, vol. 5, no. 4, pp. 6-17, Fourth Quarter 2005, doi: 10.1109/MCAS.2005.1550165.

X. Qi et al., "Efficient subthreshold leakage current optimization - Leakage current optimization and layout migration for 90- and 65- nm ASIC libraries," in IEEE Circuits and Devices Magazine, vol. 22, no. 5, pp. 39-47, Sept.-Oct. 2006, doi: 10.1109/MCD.2006.272999.

P. Monsurró, S. Pennisi, G. Scotti and A. Trifiletti, "Exploiting the Body of MOS Devices for High Performance Analog Design," in IEEE Circuits and Systems Magazine, vol. 11, no. 4, pp. 8-23, Fourthquarter 2011, doi: 10.1109/MCAS.2011.942751.

Andrea Baschirotto, ISSCC2015 "ADC Design in Scaled Technologies"

Joachim Assenmacher Infineon Technologies, "BSIM4 Modeling and Parameter Extraction" [https://ewh.ieee.org/r5/denver/sscs/References/2003_03_Assenmacher.pdf]

Stefan Rusu, Intel ISSCC 2008 Tutorial: "Leakage Reduction Techniques" [https://www.nishanchettri.com/isscc-slides/2008%20ISSCC/Tutorials/T06_Pres.pdf]

Drain-Induced Barrier Lowering (DIBL)

As a result of DIBL, threshold voltage is reduced with shorter channel lengths and, consequently, the subthreshold leakage current is increased

image-20240901231532412

impact on output impedance

The principal impact of DIBL on circuit design is the degraded output impedance.

In short-channel devices, as \(V_{DS}\) increases further, drain-induced barrier lowering becomes significant, reducing the threshold voltage and increasing the drain current

image-20240901232709711

Impact Ionization and GIDL are different, however both increase drain current, which flowing from the drain into the substrate

image-20241120210915254

Gate induced drain leakage (GIDL)

image-20241110001118250

Figure 4.3

The large current flows from the drain to bulk and this drain leakage current is named gate-induced drain leakage (GIDL) since it is due to a gate-induced high electric field present in the gate-to-drain overlap region

gate-induced drain leakage (GIDL) increases exponentially due to the reduced gate oxide thickness

image-20240902000820459

Chauhan, Yogesh Singh, et al. FinFET modeling for IC simulation and design: using the BSIM-CMG standard. Academic Press, 2015.


image-20240901225754731

\[ \frac{g_m}{I_D} = \frac{2}{V_{GS}-V_{TH}} \] Decrease of gm/Id results from decrease in VT.

GIDL (Gate induced drain leakage) as at weak inversion may results in a weak lateral electric field causing leakage current between drain and bulk, which degrade the efficiency of the transistor (gm/ID).

[https://www.linkedin.com/posts/master-micro_mastermicro-mastermicro-adt-activity-7214549962833989632-ZoV_?utm_source=share&utm_medium=member_desktop]

Voltage Dependence

image-20241111224955193

Temperature Dependence

image-20241111225025277


In advanced node, gate leakage is also a strong function of temperature

image-20241111230519009

signal detection circuit

sc_sigdet.drawio

phase I

\[\begin{align} Q_a &= (V_{a0} - 0.5*(V_{ip} + V_{im}))*C + (V_{a0} - V_{th})*C \\ Q_b &= (V_{b0} - 0.5*(V_{ip} + V_{im}))*C + V_{b0}*C \end{align}\]

Phase II

\[\begin{align} Q_a &= (V_{a} - V_{ip})*C + (V_{a} - V_{b})*0.5C \\ Q_b &= (V_{b} - V_{im})*C + (V_{b} - V_{a})*0.5C \end{align}\]

With the law of charge conservation, we get

\[\begin{equation} V_a - V_b = (V_{a0} - V_{b0}) + 0.5*(V_{ip} - V_{im} - V_{th}) \end{equation}\]

REF: D. A. Yokoyama-Martin et al., "A Multi-Standard Low Power 1.5-3.125 Gb/s Serial Transceiver in 90nm CMOS," IEEE Custom Integrated Circuits Conference 2006, 2006, pp. 401-404, doi: 10.1109/CICC.2006.320970.

Power/Ground and I/O Pins

Power / Ground Pin Information

In both digital and analog I/O, power and ground pins appear at the sub-circuit definiton, allowing user to use the I/O in voltage islands. They follow certain naming conventions.

  1. digital I/O sub-circuit
  • VDD: pre-driver core voltage (supplied by PVDD1CDGM)
  • VSS: pre-driver ground and also global ground (supplied by PVDD1CDGM)
  • VDDPST: I/O post-driver voltage, i.e. 1.8V (supplied by PVDD2CDGM or PVDD2POCM)
  • VSSPOST: I/O post-driver ground (supplied by PVDD2CDGM or PVDD2POCM)
  • POCCTRL: POCCTRL signal (supplied by PVDD2POCM)
  1. analog I/O placed in a core voltage domain, the convention is
  • TACVDD: analog core voltage (supplied by PVDD3ACM)
  • TACVSS: analog core ground (supplied by PVDD3ACM)
  • VSS: global core ground
  1. analog I/O placed in an I/O voltage domain, the convention is:
  • TAVDD: analog I/O voltage, i.e. 1.8V (supplied by PVDD3AM)
  • TAVSS: analog I/O ground (supplied by PVDD3AM)
  • VSS: global core ground

Power/Ground Combo Cells

power/ground combo pad cell pins to be connected to bump to core side pin name
PVDD1CDGM VDD VSS VDD VSS
PVDD2CDGM PVDD2POCM VDDPST VSSPST N/A
PVDD3AM TAVDD TAVSS AVDD AVSS
PVDD3ACM TACVDD TACVSS AVDD AVSS

Note for the retention mode

  1. At initial state, IRTE must be 0 when VDD is off.
  2. IRTE must be kept >= 10us after VDD turns on again (from the retention mode to the normal operation mode).
  3. IRTE can be switched only when both VDD and VDDPST are on.

rention_seq.drawio

When the rention function is needed, IRTE signal must come from an "always-on" core power domain. If you don't need the rention function, it is required to tie IRTE to ground. In other words, no matter the rention feature is needed or not, it is required to have PCBRTE in each domain.

PCBRTE_in_digital_domain.drawio

Note: PCBRTE does not need PAD connection.

Internal Pins

There are 3 internal global pins, i.e. ESD, POCCTRL, RTE, in all digital domain cells.

In real application,

  • ESD pin is an internal signal and active in ESD event happening
  • POCCTRL is an internal signal and active in Power-on-control event.

However, these special events (i.e. ESD event and Power-on-control event) are not modeled in NLDM kit (.lib), only normal function is covered, so ESD and POCCTRL pins are simply defined as ground in NLDM kit (.lib).

These 3 global pins will be connected automatically after cell-to-cell abutting in physical layout.

Power-Up sequence in Digital Domain

Power up the I/O power (VDDPST) first, then the core power (VDD)

pocctrl_seq.drawio

  1. PVDDD2POCM cell would generate Power-On-Control signal (POCCTRL) to have the post-driver NMOS and PMOS off, so that the crowbar current would not occur in the post-driver fingers when the I/O voltage is on while the core voltage remains off. As such, I/O cell would be in the Hi-Z state. when POCCTRL is on, the pll-up/down resistor is disabled and C is 0.
  2. The POCCTRL signal is transmitted to I/O cells through cell abutment. There is no need to have routing for POCCTTRL nor give a control signal to the POCCTRL pin any of I/O cells. Note that the POCCTRL signal would be cut if inserting a power-cut (PRCUT) cell.

power-on-control-ciruit.drawio

Power-Down sequence in Digital Domain

It's the reverse of power-up sequence.

Use model in Innovus

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set init_gnd_net "vss_core vss DUMMY_ESD DUMMY_POCCTRL"

addInst -moduleBased u_io -ori R270 -physical -status fixed -loc 135 994 -inst u_io/VDDIO_1 -cell PVDD2CDGM_H

addNet u_io_RTE
attachTerm FILLER_6 RTE u_io_RTE
attachTerm VDDIO_1 RTE u_right_RTE
setAttribute -skip_routing true -net u_io_RTE

clearGlobalNets
globalNetConnect DUMMY_POCCTRL -type pgpin -pin POCCTRL -singleInstance u_io/VDDDIO_1 -override
globalNetConnect DUMMY_ESD -type pgpin -pin ESD -singleInstance u_io/VDDDIO_1 -override
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set pins [get_object_name [get_ports *]]
foreach pin $pins {
set netPtr [dbGetNetByName $pin]
if { $netPtr == "0x0" } {
puts "INFO: can't find the port: $pin"
} else {
setAttribute -net $pin -skip_routing true
}
}

foreach net [get_object_name [get_nets -of_objects [get_pins */RTE -hierarchical]]] {
setAttribute -net $net -skip_routing true
dbSet [dbGetNetByName $net].dontTouch true
}

reference

M. Tian, V. Visvanathan, J. Hantgan and K. Kundert, "Striving for small-signal stability," in IEEE Circuits and Devices Magazine, vol. 17, no. 1, pp. 31-41, Jan. 2001, doi: 10.1109/101.900125.

Open loop gain analysis and "STB" method [https://www.linkedin.com/pulse/open-loop-gain-analysis-stb-method-jean-francois-debroux]

The Analog Designer's Toolbox (ADT) | Invited Talk by IEEE Santa Clara Valley Section CAS Society, https://youtu.be/FT6kKC5OdE0

ESSCIRC2023 Circuit Insights Ali Sheikholeslami [https://youtu.be/2xFIZM5_FPw?si=XWwSzDgKWZGB0rX1]

Ali Sheikholeslami, Circuit Intuitions: Thevenin and Norton Equivalent Circuits, Part 3 IEEE Solid-State Circuits Magazine, Vol. 10, Issue 4, pp. 7-8, Fall 2018.

—, Circuit Intuitions: Thevenin and Norton Equivalent Circuits, Part 2 IEEE Solid-State Circuits Magazine, Vol. 10, Issue 3, pp. 7-8, Summer 2018.

—, Circuit Intuitions: Thevenin and Norton Equivalent Circuits, Part 1 IEEE Solid-State Circuits Magazine, Vol. 10, Issue 2, pp. 7-8, Spring 2018.

—, Circuit Intuitions: Miller's Approximation IEEE Solid-State Circuits Magazine, Vol. 7, Issue 4, pp. 7-8, Fall 2015.

—, Circuit Intuitions: Miller's Theorem IEEE Solid-State Circuits Magazine, Vol. 7, Issue 3, pp. 8-10, Summer 2015.

Shanthi Pavan, "Demystifying Linear Time Varying Circuits"

ecircuitcenter. Switched-Capacitor Resistor [http://www.ecircuitcenter.com/Circuits/SWCap/SWCap.htm]

Jørgen Andreas Michaelsen. INF4420 Switched-Capacitor Circuits. [https://www.uio.no/studier/emner/matnat/ifi/INF4420/v13/undervisningsmateriale/inf4420_v13_07_switchedcapacitor_print.pdf]

chembiyan T. OC Lecture 10: A very basic introduction to switched capacitor circuits [https://youtu.be/SaYtemYp4rQ?si=q2qovTKJrLy65pnu

Robert Bogdan Staszewski, Poras T. Balsara. "All‐Digital Frequency Synthesizer in Deep‐Submicron CMOS"

Mayank Parasrampuria, Sandeep Jain, Burn-in 101 [link]


Kevin Zheng. Circuit Artists [https://circuit-artists.com/posts/]

image-20250730172648857


image-20231106232135180

Terminology

The most accurate method to calculate the degradation of transistors is the SPICE-level simulation of the whole netlist with application programming interface (API) and industry-standard stress process models

MOSRA: MOSFET reliability analysis Synopsys

RelXpert: Cadence

TMI: TSMC Model Interface, TSMC

OMI: Open Model Interface, Si2 standard,

The Silicon Integration Initiative (Si2) Compact Model Coalition has released the Open Model Interface, an Si2 standard, C-language application programming interface that supports SPICE compact model extensions.OMI allows circuit designers to simulate and analyze such important physical effects as self-heating and aging, and perform extended design optimizations. It is based on TMI2, the TSMC Model Interface, which was donated to Si2 by TSMC in 2014.

  • TDDB: Time-Dependent Dielectric Breakdown
  • HCI: Hot Carrier injection
  • BTI: Bias Temperature Instability
    • NBTI: Negative Bias Temperature Instability
    • PBTI: Positive Bias Temperature Instability
  • SHE: Self-Heating Effect

4645.reliability.png

Aging & SHE in FinFET

image-20230513215602865

SHE

image-20221214001912093

image-20230513110032603

image-20221214001940656

Self-Heating & EM

image-20230513220047241

Heat Sink (HS)

  1. guard ring

    closer OD help reduce dT

  2. extended gate

  3. source/drain metal stack

Bias Temperature Instability (BTI)

image-20250105132044116


img

BTI occurs predominantly in PMOS (or p-type or p channel) transistors and causes an increase in the transistor's absolute threshold voltage.

Stress in the case of NBTI means that the PMOS transistor is in inversion; that means that its gate to body potential is substantially below 0 V for analogue circuits or at VGB = −VDD for digital circuits

Higher voltages and higher temperatures both have an exponential impact onto the degradation, induced by NBTI.

NBTI will be accelaerated with thinner gate oxide, at a high temperature and at a high electric field across the oxide region.

During recovery phase where the gate voltage of pMOS is high and stress is removed, the H atoms in the gate oxiede diffuse back to Si-SiO2 interface and the recombination of Si-H bonds reduces the threshold voltage of pMOS.

image-20230513111525657

image-20230513111657285

The net result is an increase in the magnitude of the device threshold voltage |Vt|, and a degradation of the channel carrier mobility.

Caution: The aging model provided by fab may NOT contain recovry effect

image-20230513104621962

image-20230513104654501

PBTI

image-20250730180359480

image-20250730180302668

Hot Carrier Degradation (HCI)

Short-channel MOSFETs may exprience high lateral electric fields if the drain-source voltage is large. while the average velocity of carriers saturate at high fields, the instantaneous velocity and hence the kinetic energy of the carriers continue to increase, especially as they accelerate toward the drain. These are called hot carriers.

In nanometer technologies, hot carrier effects have subsided. This is because the energy required to create an electron-hole pair, \(E_g \simeq 1.12 eV\), is simply not available if the supply voltage is around 1V.

\[ F_E= E \cdot q \]

\[\begin{align} E_k &= F_E \cdot s \\ &= E \cdot q \cdot s \end{align}\]

Electrons and holes gaining high kinetic energies in the electric field (hot carriers) may be injected into the gate oxide and cause permanent changes in the oxide-interface charge distribution, degrading the current-voltage characteristics of the MOSFET.

The channel hot-electron (CHE) effect is caused by electons flowing in the channel region, from the source to the drain. This effect is more pronounced at large drain-to-source voltage, at which the lateral electric field in the drain end of the channel accelerates the electrons.

Four different hot carrier injectoin mechanisms can be distinguished: - channel hot electron (CHE) injection - drain avalanche hot carrier (DAHC) injection - secondary generated hot electron (SGHE) injection - substrate hot electron (SHE) injection

HCI is more of a drain-localized mechanism, and is primarily a carrier mobility degradation (and a Vt degradation if the device is operated bi-directionally).

image-20230512213236023

For smaller transistor dimensions, CHE dominates the hot carrier degradation effect

The hot-carrier induced damage in nMOS transistors has been found to result in either trapping of carriers on defect sites in the oxide or the creation of interface states at the silicon-oxide interface, or both.

The damage caused by hot-carrier injection affects the transistor characteristics by causing a degradation in transconductance, a shift in the threshold voltage, and a general decrease in the drain current capability.

HCI seems to have just a weak temperature dependency. Unlike BTI, it seems to be no or just little recovery. As holes are much "cooler" (i.e. heavier) than electrons, the channel hot carrier effect in nMOS devices is shown to be more significant than in pMOS devices.

image-20231106224938502

Degradation saturation effect

HCI model can reproduce the saturation effect if stress time is long enough

image-20230513112108262

Gate Oxide Integrity (GOI)

image-20250730180005931

Time dependent dielectric breakdown (TDDB)

image-20250730175415143

Scaling drive more concerns in TDDB

image-20250730175201502


img

M. A. Alam, ECE 695A Reliability Physics of Nanotransistors [link], [https://nanohub.org/resources/17208/download/2013.03.01-ECE695A-L21.pdf]

K. Yang, R. Zhang, T. Liu, D. -H. Kim and L. Milor, "Optimal Accelerated Test Regions for Time- Dependent Dielectric Breakdown Lifetime Parameters Estimation in FinFET Technology," 2018 Conference on Design of Circuits and Integrated Systems (DCIS), Lyon, France, 2018 [https://par.nsf.gov/servlets/purl/10104486]

waveform-dependent nature

The figure below illustrates the waveform-dependent nature of these mechanisms – as described earlier, BTI and HCI depend upon the region of active device operation. The slew rate of the circuit inputs and output will have a significant impact upon these mechanisms, especially HCI.

  • Negative bias temperature instability (NBTI). This is caused by constant electric fields degrading the dielectric, which in turn causes the threshold voltage of the transistor to degrade. That leads to lower switching speeds. This effect depends on the activity level of the circuits, with heavier impact on parts of the design that don’t switch as often, such as gated clocks, control logic, and reset, programming and test circuitry.
  • Hot carrier injection (HCI). This is caused by fast-moving electrons inserting themselves into the gate and degrading performance. It primarily occurs on higher-voltage modes and fast switching signals.

image-20230513110202915

  • longer channel length help both BTI and HCI
  • larger \(V_{ds}\) help BTI, but hurt HCI
  • lower temperature help BTI of core device, but hurt that of IO device for 7nm FinFET

MOSRA

MOSRA is a 2-step simulation: 1) Age computation, 2) Post-age analysis

TMI

BTI recovery effect NOT included for N7

Stochastic Nature of Reliability Mechanisms

A fraction of devices will fail

img

img

Circuit Simulations

image-20231106230145351

image-20231106230226203

Heat transfer, thermal resistance

image-20241120222920258


image-20241120221254833

image-20241120221405337

image-20241120223053280

Burn-in & High-temperature operating life (HTOL)

  • HTOL:
    • characterization test
    • characterize the life expectancy
  • Burn-in:
    • production test
    • weed out defective products

HTOL and Burn-in Testing capture the two ends of the reliability characterization graph known as the "bathtub curve"

importance-of-htol-figure-1

[https://arworld.us/the-importance-of-htol-and-burn-in-testing-methods/]

reference

Phillip Allen. Reliability of Analog Circuits [https://aicdesign.org/wp-content/uploads/2021/04/Reliability_Theory210224-1.pdf]

M. A. Alam. ECE 695A Reliability Physics of Nanotransistors [https://nanohub.org/groups/ece695alam]


Tanya Nigam and Andreas Kerber. Global Foundaries. CICC2014 Session 15 - Challenges for Analog Nanoscale Technologies: Reliability challenges and modeling of HK MG Technologies

Spectre Tech Tips: Device Aging? Yes, even Silicon wears out - Analog/Custom Design (Analog/Custom design) - Cadence Blogs - Cadence Community https://shar.es/afd31p

S. Liao, C. Huang, and A. C. J. X. T. Guo, "New Generation Reliability Model," Dec 2016. [Online]. Available: http://www.mos-ak.org/berkeley_2016/publications/T11_Xie_MOS-AK_Berkeley_2016.pdf. [Accessed Aug 2018]

Tianlei Guo, Jushan Xie, "A Complete Reliability Solution: Reliability Modeling, Applications, and Integration in Analog Design Environment" [https://mos-ak.org/beijing_2018/presentations/Tianlei_Guo_MOS-AK_Beijing_2018.pdf]

FinFET Reliability Analysis with Device Self-Heating via @DanielNenni https://semiwiki.com/eda/synopsys/5085-finfet-reliability-analysis-with-device-self-heating/

Chris Changze Liu 刘长泽,Hisilicon, Huawei, "Reliability Challenges in Advanced Technology Node" https://www.tek.com.cn/sites/default/files/2018-09/reliability-challenges-in-advanced-technology-node.pdf

Ben Kaczer, imec. FEOL reliability: from essentials to advanced and emerging devices and circuits. 2016 IRPS Tutorial

Ben Kaczer, imec. Present and Future of FEOL Reliability—from Dielectric Trap Properties to Reliable Circuit Operation. 2016 IEDM 2016 [link]

Kang, Sung-Mo Steve, Yusuf Leblebici and Chulwoo Kim. “CMOS Digital Integrated Circuits: Analysis & Design, 4th Edition.” (2014).

Behzad Razavi. "Design of Analog CMOS Integrated Circuits" (2016)

Basel Halak. Ageing of Integrated Circuits : Causes, Effects and Mitigation Techniques. Cham, Switzerland: Springer, 2020. ‌

Elie Maricau, and Georges Gielen. Analog IC Reliability in Nanometer CMOS. Springer Science & Business Media, 2013. ‌

Transistor Aging Intensifies At 10/7nm And Below https://semiengineering.com/transistor-aging-intensifies-10nm/

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