Path 08 · Module 04

Vector Network Analysis,
Calibration & Fixtures

A smooth trace is easy to trust. Move the vector reference plane deliberately, then use independent evidence to decide whether the result deserves that trust.

01 / 10

Smooth traces can still fail verification

The antenna looks better through a cable, and every calibration standard remeasures perfectly. What has actually improved?

The fictional 2.450 GHz condition-monitoring node needs two different port measurements: an antenna-feed impedance and a PCB filter’s two-port response. In one investigation the engineer adds a lossy cable and sees return loss improve from 6.021 to 8.021 dB. In another, a calibration with the wrong load definition still draws beautifully smooth curves. Neither observation alone establishes the DUT response.

Think about itWould an unused verification load necessarily agree if the three calibration standards agree?
Answer

No. The wrong-load example below fits the standards exactly but misses an independent load by 0.019123505976 in absolute complex reflection. That exceeds this lesson’s local 0.01 criterion.

This lesson follows measurement uncertainty and stable lab connections. We replace the portfolio’s generic QPSK stimulus with the explicitly named SYN-VNA-CW-v1 stepped continuous-wave variant. All numerical data are Illustrative / Derived, noiseless calculations at a frozen evaluation date of 2026-09-09 UTC. They are not hardware captures, a wireless-standard waveform or a calibration certificate.

The two misleading improvements · pinned synthetic results
ObservationTempting conclusionDiscriminating evidence
Cable-input return loss 8.020599913280 dBAntenna match improvedAt R2-FEED, Γ = 0.5 and return loss remains 6.020599913280 dB.
Wrong SOL standard fit ≈ 0 residualCalibration is accurateUnused Γv = −0.2 recovers as −0.219123505976.
Common misconceptionCalibration is a button that makes subsequent measurements true.

Calibration estimates corrections under defined models and conditions. Its validity can be lost, and its residual uncertainty remains. Independent verification asks whether different evidence supports using those corrections now.

Engineering decision → record update

Open M08-04-FILTER-PLAN-A and M08-04-FEED-PLAN-A. Record DUT change, wrong standard definition and changed fixture as competing hypotheses. Keep the earlier raw IDs unchanged; reserve “inspect,” “blocked” and “invalid” outcomes.

02 / 10

Measure complex wave ratios at named planes

What does a VNA receiver ratio know about the plane you want?

A source excites one port. A reference receiver samples the incident wave; test receivers sample reflected and transmitted waves. Ratios retain amplitude and relative phase while reducing common source variation. Couplers, switches and receivers are imperfect, so a raw normalized ratio is not yet the DUT’s scattering parameter. The naming of receiver channels varies by instrument. [VNA-ERROR]

Sij=biaj(ak=0 for kj)S_{ij}=\frac{b_i}{a_j}\qquad(a_k=0\text{ for }k\ne j)Definition: a and b are incident and outgoing power waves at named ports, normalized to a real positive Zref = 50 Ω. With the other port matched, Sij = bi/aj. Use the e^(+jωt) phasor convention; reflection Γ and receiver ratio m are dimensionless complex quantities.
Original illustrative reference-plane mapIncident wave travels left to right; reflected wave returns. Calibration stops at M-CAL; fixture removal requires its own model.M-CALF-INCable / launchF-OUTR2-FEEDForward wave a → · exp(−γl)← Return wave b · reflection traverses each line twiceReal Zref = 50 Ω · e^(+jωt) · illustrative, not a wiring instruction
With a fixture, M-CAL coincides with F-IN; F-OUT coincides with R2-FEED. Calibrating at F-OUT would already include the cable: never remove it twice.

M-CAL is the instrument calibration plane. With a fixture present it coincides with F-IN; F-OUT coincides with the product’s R2-FEED. For the two-port filter, its ports are R1-DUT port 1 and port 2, bounded by separately named left and right fixtures. R3 remains the receiver decision boundary; S0 remains the spatial/OTA boundary. Neither is another name for a VNA connector.

Think about itCan a raw open observation of 1.02 prove that the open delivers gain?
Answer

No. Directivity and tracking errors can make raw m exceed one. Passivity concerns corrected network waves at the declared reference plane, not an uncorrected receiver ratio.

Go deeperKeep the network conventions with the data

Revisit two-port networks and S-parameters for wave normalization and chain conversion. This lesson retains the real 50 Ω convention throughout; a file normalized to another impedance requires an explicit compatible transformation before comparison.

Engineering decision → record update

Name every port and plane in the raw-data header, including direction, reference impedance, terminations, fixture order and whether instrument correction was already applied.

03 / 10

Separate systematic, random, and drift errors

Which errors can a fitted correction remove, and which change after you fit it?

Systematic errors are reproducible within the model and state. Random receiver noise and connection variation need statistical evidence. Drift changes the system with time or environment. A calibration can estimate systematic terms; it does not freeze a moving cable or eliminate all uncertainty. [VNA-ERROR]

Orientation of a conventional two-direction error model · informative
ContributionForward excitation at port 1Reverse excitation at port 2
DirectivityLeakage in reflection at port 1Leakage in reflection at port 2
Source matchIncident-wave interaction at port 1Incident-wave interaction at port 2
Load matchImperfect receiving termination at port 2Imperfect receiving termination at port 1
Reflection trackingReflection amplitude/phase path at port 1Reflection amplitude/phase path at port 2
Transmission trackingForward ratio path, 1 → 2Reverse ratio path, 2 → 1
IsolationForward leakage bypassing DUT pathReverse leakage bypassing DUT path

The numerical one-port witness uses only three terms: directivity leakage d, reflection tracking t and source match s. They are complex functions of frequency in real equipment; this bounded fixture holds their supplied values constant across its grid.

m=d+tΓ1sΓΓ^=mdt+s(md)\begin{aligned}m &= d + \frac{t\Gamma }{1 - s\Gamma} \\ \hat{\Gamma} &= \frac{m - d}{t + s(m - d)}\end{aligned}Illustrative three-term receiver model at M-CAL. Γ is the true reflection at this plane, m the observed ratio. The inverse is valid only with identified coefficients and a sufficiently separated denominator.
Think about itIf you average the same biased ratio 64 times, does the bias shrink by eight?
Answer

No. An average of identical biased values is the same value. A square-root averaging law requires a specified random process and independence assumptions. This explorer has no stochastic noise model.

Correct SOL anchor · 2.450 GHz, fixture-free M-CAL = R2-FEED
QuantityTrue Γ or termRaw observation m
Directivity / tracking / source matchd = 0.02; t = 0.9; s = 0.1All real; dimensionless
Open+1 + j01.020000000000 + j0
Short−1 + j0−0.798181818182 + j0
Load0 + j00.020000000000 + j0
Separate DUT0.5 + j00.493684210526 + j0
Unused verification−0.2 + j0−0.156470588235 + j0
Engineering decision → record update

Separate error mechanism, fitted correction and residual uncertainty in the record. Receiver noise, standard uncertainty, connector repeatability and drift are different contributors, even if all affect the same S11 trace.

04 / 10

Choose what the calibration can solve

Do your standards provide the independent information your correction needs?

One open gives one complex response constraint. Three distinct, characterized reflection standards can identify the three-term one-port model. A two-port measurement needs additional information about transmission, both excitation directions and the receiving-port match. Choose the method from accessible interfaces and credible standard models before acquiring the DUT.

mi=d+qΓi+smiΓi[1,Γi,miΓi][d,q,s]T=mi\begin{aligned}m_{i} &= d + q\Gamma _{i} + s m_{i}\Gamma _{i} \\ [1, \Gamma _{i}, m_{i}\Gamma _{i}] \cdot [d,q,s]^{T} &= m_{i}\end{aligned}Derived: define q = t − ds, then solve the complex 3×3 linear system with rows [1, Γi, miΓi] for [d,q,s]. Recover t = q + ds. The independent NumPy solve gives d = .02, t = .9, s = .1 for the pinned SOL data.
Method capability and what must be supplied
MethodInformation and applicabilityCoverage / numerical implementation here
ResponseA known through or reflection response supplies tracking normalization for that measurement.Here only m/m_open. Does not independently solve directivity/source match; matched-load residual .019607843137.
One-port SOLThree distinct complex reflection standards at one plane, with their frequency-dependent models.Solves d,t,s for that reflection port. Implemented here; not a two-port solution.
Full two-port SOLTCharacterized SOL at both interfaces, a suitable characterized/solvable thru, both source directions and load-match information. Isolation handling follows the selected procedure.Complete applicable error correction requires all selected observations and model assumptions. Taught; numeric solver not implemented.
TRL / multiline TRLCompatible thru and lines; common high reflection with enough phase information to resolve ambiguity. Line impedance establishes the reference; lengths must distinguish the standards.Both directions with method-specific error-box assumptions. Multiple line lengths extend useful coverage. Taught; numeric solver not implemented.
LRM / LRL variantsLine/thru, reflect and match (or second line); the chosen method determines known quantities and symmetry assumptions. Match quality/model matters.Useful when realizable standards differ from ideal coaxial SOL. Taught; numeric solver not implemented.
Known fixture inverseIndependently known, stable left/right networks and compatible already calibrated exterior S-data.Removes those networks. Implemented here; supplies no missing unknown analyzer calibration observations.

The distinctions above are informative method planning, grounded in the accessible TRL and LRM descriptions. Exact standard classes and algorithm assumptions belong to the selected instrument/method. [VNA-TRL] [VNA-LRM]

Give a TRL line enough distinction

For a separate ideal line-separation example, Δτ = 100 ps and Δφ = 360° fΔτ. Its one-way separation is 88.2° at 2.450 GHz, 0° at DC and 180° at 5 GHz. Near integer multiples of 180°, the ideal distinction degenerates. A 20°–160° interior guideline suggests 0.556–4.444 GHz for this first branch, but that alone cannot establish a valid band: loss, dispersion, impedance, phase branch, model assumptions and uncertainty still matter. [VNA-TRL]

Common misconceptionTRL means the reference impedance is automatically exactly 50 Ω.

The line establishes the reference under the method’s assumptions. Its characteristic impedance needs characterization or justified renormalization if a 50 Ω result is required. A convenient line length does not determine that impedance.

Engineering decision → record update

Record the method, standard IDs, model versions, frequency coverage, branch choice and both-direction requirements. Mark an unavailable commercial solve as unimplemented; do not relabel a known-box inverse.

05 / 10

Standards are models with physical interfaces

What if the calibration load is repeatable but its model is wrong?

An open has fringing capacitance, a short has inductance, and each standard can have offset delay, loss and a defined connector reference plane. A kit definition binds those quantities to frequency limits and standard classes. Its coefficients have specific units: an open polynomial C(f) = C0 + C1f + C2f² + C3f³ uses coefficients in F/Hzⁿ when f is in Hz; an inductance polynomial uses H/Hzⁿ. Do not paste values from another unit convention. [VNA-KIT]

Think about itIf actual load Γ = .02 but the fit assumes zero, will remeasuring that load expose the error?
Answer

The solver maps it back to its assumed zero. Use a separate reference. In this example the fitted directivity shifts to .038036072144 and the DUT becomes .484848484848 instead of .5.

Wrong-load model · independent solver, all entries real + j0
QuantityCorrect SOLActual load .02, assumed 0
Raw load observation0.02 + j00.038036072144 + j0
Estimated d0.02 + j00.038036072144 + j0
Estimated t0.9 + j00.903249384541 + j0
Estimated s0.1 + j00.080160320641 + j0
Recovered DUT Γ0.5 + j00.484848484848 + j0
Recovered unused Γv-0.2 + j0-0.219123505976 + j0
Unused reference residual≈ 00.019123505976 > 0.01
Calibration-standard residual≈ 0≈ 0 · fit to incorrect definitions

Connector gender, pin depth, cleanliness, mating torque and adapters are part of the physical model boundary. Use the actual compatible hardware’s inspection and handling procedure. An adapter inserted after calibration adds a network; treating it as zero length or redefining a kit class does not characterize it. Offset loss in the cited kit help uses its own convention; it is not the explorer’s total matched dB loss parameter. [VNA-KIT]

Go deeperSeparate a standard definition from its uncertainty

Knowing nominal coefficients is not knowing them exactly. Record characterization evidence, covariance where available, connector repeatability and applicable frequency range. Correlated standard errors can move several corrected S-parameters together. The supplied ideal SOL values are synthetic choices, not a borrowed commercial kit.

Engineering decision → record update

Preserve actual standard identities and assumed model files separately. A corrected model creates a new derived calibration version linked to immutable raw standard observations; it never rewrites those observations.

06 / 10

Move the reference plane deliberately

Does your operation remove phase, loss, mismatch, or an already removed cable?

For e^(+jωt), forward propagation is exp(−γl), with γ = α + jβ. One-way physical length l and velocity v give τ = l/v. A matched line’s one-way power insertion loss LdB corresponds to voltage-wave factor 10^(−LdB/20). A reflection travels out and back.

S21=S12=10LdB/20ej2πfτΓin=ΓDUT102LdB/20ej4πfτ\begin{aligned}S_{21}=S_{12}&=10^{-L_{\mathrm{dB}}/20}e^{-j2\pi f\tau}\\\Gamma_{\mathrm{in}}&=\Gamma_{\mathrm{DUT}}10^{-2L_{\mathrm{dB}}/20}e^{-j4\pi f\tau}\end{aligned}Derived, real matched 50 Ω line. LdB is a positive one-way loss in dB, f is in Hz, τ in seconds. Removing this known propagation uses the inverse with positive phase; applying the forward factor again adds cable.
One cable, three plane operations · 2.450 GHz, l = 20 mm, v = 2×10⁸ m/s, τ = 100 ps
Stage / operationComplex ΓMagnitude / return loss
Actual R2-FEED load.500000000000 + j0.5 / 6.020599913280 dB
M-CAL before 1 dB one-way cable−.396380404700 − j.024938141268.397164117362 / 8.020599913280 dB; phase −176.4°
Phase-only extension to feed delay.397164117362 + j0Same magnitude; loss remains
Matched loss-and-phase removal.500000000000 + j0.5 restored when the line model is valid

Port extension can include a loss model on some instruments; this lesson names its phase-only operation explicitly. A cable-end calibration already includes that cable in the calibration error network. Do not remove it again. A mismatched launch generally requires a full network model, beyond a scalar electrical delay. [VNA-EXT]

Remove the actual two-port network in the actual order

Tmeasured=TleftTDUTTrightTDUT,recovered=Tleft1TmeasuredTright1\begin{aligned}T_{\mathrm{measured}}&=T_{\mathrm{left}}T_{\mathrm{DUT}}T_{\mathrm{right}}\\T_{\mathrm{DUT,recovered}}&=T_{\mathrm{left}}^{-1}T_{\mathrm{measured}}T_{\mathrm{right}}^{-1}\end{aligned}Definition: [V1,I1]ᵀ = T[V2,−I2]ᵀ, currents into both ports. Uniform fixture: A = D = cosh(γl), B = Zc sinh(γl), C = sinh(γl)/Zc. B has Ω units and C siemens; Zc is the fixture’s characteristic impedance.

The filter proxy is a series impedance Zs = 10 Ω + j(ω·10 nH − 1/(ωC)), with C = 1/((2π·2.45 GHz)²·10 nH) = 0.421995766940 pF. At resonance its S11 = S22 = 1/11, S21 = S12 = 10/11 and transmission is −0.827853703165 dB. The antenna-load proxy uses 150 Ω plus the same reactance, giving Γ = (Z−50)/(Z+50). Both are passive lumped models; neither is a measured commercial device.

Two 55 Ω fixtures around the filter · 2.450 GHz · independently checked cascade
OperationRecovered S21Largest independent verification residual / status
Exact full fixture inverse0.909090909091 − j00 / supported
Wrong matched 50 Ω inverse0.921475475313 + j0.0005062428810.067586382995 / blocked
Phase-only approximation0.731953987647 + j0.0004021230140.166983085403 / blocked
Common misconceptionMultiplying S matrices cascades two-port networks.

Reflections between networks require a compatible network interconnection calculation. Use the stated chain convention or a wave/nodal connection. The independent oracle here solves the connected nodal network without using the production S↔ABCD conversion.

Go deeperConditioning is part of whether an inverse is usable

Normalize a chain to [[A,B/50],[50C,D]] before comparing conditioning. The implementation uses κF = ‖A‖F‖A⁻¹‖F, an independently tested conservative bound: κ2 ≤ κF ≤ nκ2 for an n×n matrix. Local rules warn above 10⁸ and reject at or above 10¹² or singularity. This can reject earlier than κ2. A one-port inverse also rejects a denominator no larger than 10⁻¹² times the sum of its constituent magnitudes. Exact zero is handled explicitly. Undefined chain conversion at vanishing transmission leaves available S-data visible and the cascade unavailable; it is not an invitation to divide by a tiny number.

Engineering decision → record update

Record calibration plane, each fixture ID, propagation convention, left/right order, reference impedance and every operation once. Retain the original exterior S-data and link the derived DUT-plane dataset to its model.

07 / 10

Acquire in a valid DUT and receiver state

Can cleaner averaging compensate for the wrong power state or insufficient frequency coverage?

Choose source power to preserve the DUT’s intended small-signal state and receiver linearity, with adequate observable signal. Lower IF bandwidth or more averaging can reduce applicable random contributions but cost acquisition time. They cannot correct deterministic standard bias, and longer sweeps can expose more drift. Actual safe levels, settling and coupling depend on the selected hardware and settings. [VNA-ERROR]

The explorer’s source power is context from −40 to +10 dBm; −10 dBm is the default. Its fictional small-signal ceiling is 0 dBm, inclusive. Exceeding it marks the inference invalid. IFBW choices are 10, 100, 1000 and 10000 Hz; averaging choices are 1, 4, 16 and 64. These controls do not modify the noiseless curves. A real power sweep and receiver checks must establish the appropriate region; the synthetic ceiling is not a safe equipment rating.

A time trace inherits the frequency experiment

The fixed grid has 101 points from 2.0 to 3.0 GHz at Δf = 10 MHz. Its span B = 1 GHz gives an inverse-span scale 1/B = 1 ns; periodic delay extent is 1/Δf = 100 ns. Neither is a promise to distinguish any two responses. For reflection at v = 2×10⁸ m/s, 100 ns round-trip corresponds to 10 m one-way before periodic ambiguity, subject to loss and observability.

Two close reflections and a window tradeoffSchematic, not sampled VNA data: impulses at 2 and 2.8 nanoseconds become overlapping finite-band responses. Tapering lowers sidelobes and broadens each response. Heights and drawn widths are not quantitative.Ideal delays · 2 ns and 2.8 ns (illustrative)22.8 nsSchematic finite-band response · vertical scale arbitrarySolid: rectangular frequency windowDashed: tapered window, broader response
Original qualitative sketch. The two delays are 0.8 ns apart; the lesson’s 1 GHz span supplies an inverse-span scale of 1 ns, not a guaranteed separation threshold. Curves illustrate window behavior and are not a computed transform or a gate preview.
Think about itIf a narrow gate hides the launch reflection, have you recovered a launch-free antenna measurement?
Answer

Not necessarily. Finite-band responses overlap; removing part of one may remove part of another. A prior mismatch also changes energy delivered downstream. Keep ungated data and verify the gated result independently.

A transform record needs actual frequency samples, bandpass or lowpass interpretation, start/stop values, DC extrapolation, interpolation, window and normalization. This grid contains no DC: a lowpass response would require additional assumptions. Tapering lowers sidelobes while broadening responses. Multiplication by a time gate convolves frequency data and can alter broadband magnitude and phase. It does not repair the discontinuity or establish absolute accuracy. [VNA-TIME]

Engineering decision → record update

Save the grid, power, IFBW, averaging, settling sequence, DUT bias/temperature and all transform settings. Give gated data a derived ID; preserve the full complex ungated sweep. Unknown ratings and residual uncertainty stay unknown.

08 / 10

Track what changes after calibration

What still belongs to the calibration after a connector is remated or the cable moves?

A successful calibration describes a particular bench state. Rerouting a cable, changing torque, adding an adapter, altering bias, warming the fixture or switching an instrument path can change that state. Define the expected validity conditions and review triggers in advance; repeatability of an unchanged setup cannot estimate the variability of remating it. [VNA-ERROR]

Think about itOur drift example still clears the numerical 0.01 verification tolerance. Does that make the unchanged-state condition true?
Answer

No. The supplied state changed after calibration, so the dataset is blocked until reviewed and reverified or recalibrated under a justified procedure. A tolerance and a state-validity condition answer different questions.

Post-calibration drift · add +0.005 real to actual d, retain old fitted terms
QuantityPinned result at 2.450 GHz
New raw DUT m0.498684210526 + j0
New raw verification mv−0.151470588235 + j0
Recovered DUT0.505011244066 + j0
Recovered unused verification-0.194223273478 + j0
Absolute verification residual0.005776726522
Averages 1 / 4 / 16 / 64Identical deterministic bias; unchanged-state gate remains blocked

Plan a repeat acquisition before and after the intended change, an independent check device, and a return-to-baseline measurement when feasible. Keep cable route and thermal state with timestamps. If evidence cannot distinguish DUT drift from fixture drift, the honest next step is a discriminating measurement, not an automatic correction.

Common misconceptionThe calibration is valid until a universal number of hours expires.

Elapsed time is only one influence. A single changed connection can matter immediately; a stable bench can behave differently. Use evidence and the selected procedure’s validity conditions, not a made-up universal interval.

Engineering decision → record update

Create a new configuration/state ID after each consequential change. Preserve the old calibration and raw sweeps, document the trigger, and identify the verification needed before reusing a DUT inference.

09 / 10

Verify with evidence independent of the fit

What evidence could disagree with your correction without sharing its assumptions?

An unused, independently characterized device challenges the fitted correction. It needs a compatible reference value and uncertainty at the same planes and state. Reusing standards can detect changes but can also reproduce shared model error. A verification residual is valuable evidence; it is not itself the complete uncertainty of the DUT result. [VNA-VERIFY]

Γ^vΓv0.01|\hat{\Gamma}_{v} - \Gamma _{v}| \le 0.01Local illustrative criterion only, inclusive equality. The one-port reference Γv = −0.2 is never fitted. The two-port reference has S11=S22=0 and S12=S21=.8, independent of the fixture fit; its maximum entry residual is checked across all 101 points.
Eligibility is a sequence of different questions
GateWhen it prevents use
Schema and compatibilityInvalid draft is not committed. Wrong plane, port order, Zref, grid or calibration identity blocks inference.
Identification and numericsSingular standards, unstable inverse or unsupported transformation is invalid.
Measurement statePower outside the supplied small-signal limit is invalid. Changed connections/drift block reuse.
Independent evidenceUnknown standard/verification evidence means inspect. Failed residual means blocked.
Network plausibilityCheck sampled passivity and reciprocity separately; neither proves calibration accuracy.
Residual uncertaintyStandard models, connections, fixture characterization, drift and receiver correlations still need evidence. No physical DUT acceptance is supplied.

For a real-reference two-port, passivity requires the largest singular value σmax(S) ≤ 1 + 10⁻¹⁰ in this numerical check. Four separate |Sij| ≤ 1 tests are insufficient because coherent incident waves can combine. Reciprocity is a separate |S12−S21| ≤ 10⁻¹⁰ check; a passive nonreciprocal device is possible. Do not clip reflection to one or normalize a failing network to make it look passive.

At exact match, Γ = 0 has undefined phase and infinite return loss; the explorer labels those analytic limits. Checks cover sampled frequencies and the declared small-signal state. Real uncertainty requires a model of residual errors and their correlations; first-order propagation has conditions, developed in 08.1. [MET-NIST]

Engineering decision → record update

Retain the unused reference’s provenance, raw observations, comparison residuals and uncertainty. A supported synthetic criterion permits only the stated synthetic inference. It supplies no accreditation, radiation conclusion or conformity decision.

10 / 10

Defend two calibration and fixture plans

Can another engineer reproduce the calibration and explain why the resulting plane is defensible?

Start with correct SOL and reveal the unused load. Save a baseline, choose the wrong load model, and compare the perfect standard fit with the failed independent residual. Next choose the lossy line: predict the result of phase-only extension, then apply matched loss-and-phase removal. Finally choose the mismatched filter fixtures and compare the exact model with an assumed matched 50 Ω model. Keep the resulting warning with the data.

Interactive · Class 1 · illustrative vector evidence

VNA Error & Plane Explorer

Fit SOL, test an unused load, then move a lossy fixture plane. Compare the standard fit with independent evidence before using the result.

Presets restore all model inputs and evidence atomically; default correct SOL.
1 · DUT and reference-plane operation
Closed choices; default: One-port antenna-load proxy. Reset restores this default.
Closed choices; default: Three-term one-port SOL solve. Reset restores this default.
Closed choices; default: Absent · calibration at DUT. Reset restores this default.
Closed choices; default: None. Reset restores this default.
Closed choices; default: Exact actual fixture model. Reset restores this default.

Line/filter use already calibrated exterior S-data and known boxes. The numerical calibration selector and error terms belong only to the one-port branch. Match-only corrections on mismatched fixtures remain approximations with warnings.

2 · One-port standards and complex receiver errors
0…0.1 dimensionless; step 0.001; default 0.02. Reset restores this default.
-180…180 degrees; step 1; default 0. Reset restores this default.
0.5…1.5 dimensionless; step 0.001; default 0.9. Reset restores this default.
-180…180 degrees; step 1; default 0. Reset restores this default.
0…0.3 dimensionless; step 0.001; default 0.1. Reset restores this default.
-180…180 degrees; step 1; default 0. Reset restores this default.
-0.9…0.9 dimensionless; step 0.001; default 0. Reset restores this default.
-0.9…0.9 dimensionless; step 0.001; default 0. Reset restores this default.
Closed choices; default: Off. Reset restores this default.
Closed choices; default: Known synthetic reference. Reset restores this default.
3 · Fixture dimensions and acquisition context
0…0.1 m; step 0.001; default 0.02. Reset restores this default.
100000000…300000000 m/s; step 1000000; default 200000000. Reset restores this default.
0…10 dB; step 0.1; default 1. Reset restores this default.
25…100 Ω, real; step 1; default 50. Reset restores this default.
-40…10 dBm; step 1; default -10. Reset restores this default.
Closed choices; default: 1000. Reset restores this default.
Closed choices; default: 1. Reset restores this default.

Loss is total one-way matched power insertion loss, independent of length in this bounded parameterization. Zero length with nonzero loss is a lumped-loss limit. The line DUT itself stays fixed at 20 mm, 2×10⁸ m/s, 1 dB. Source power above the local 0 dBm small-signal limit invalidates inference; it is not a real safe rating. Averaging cannot remove deterministic bias.

4 · Evidence eligibility
Closed choices; default: Known synthetic reference. Reset restores this default.
Closed choices; default: Unchanged. Reset restores this default.
Closed choices; default: Compatible 50 Ω / planes / grid. Reset restores this default.

Arrow keys: 10 MHz; Home/End: 2/3 GHz. View only; default 2.450 GHz.

Correct one-port SOL · committed result

Supported synthetic criterion

The supplied synthetic reference criterion clears on all 101 points under unchanged, compatible conditions. Real residual uncertainty remains unknown.

Output plane: M-CAL = R2-FEED. Three-term SOL receiver correction precedes any fixture transformation; residual standard-model and state errors can remain. Acquisition context: -10 dBm CW, 1000 Hz IFBW, 1 averages. IFBW and averaging have no numerical effect in this noiseless model.

Original illustrative reference-plane mapSource and ratio receivers establish the one-port M-CAL plane, coincident with the fixture-free antenna-load proxy.Source / couplerTest portM-CALR2-FEEDLoad proxyForward wave a → · exp(−γl)← Return wave b · reflection traverses each line twiceReal Zref = 50 Ω · e^(+jωt) · illustrative, not a wiring instruction
No external fixture is present: the calibration planes coincide with the DUT ports. Reference/test receivers sample the waves through couplers; they are not series elements in this RF path.
Synthetic amplitude at the declared planesMagnitude is dimensionless. Raw m is a receiver ratio and can exceed one. Dashes identify stages. The cursor table gives exact complex values, phase and units.Dimensionless amplitude · Γ and receiver m00.5122.252.52.753Frequency / GHzTruth · synthetic onlyRaw receiver |m|SOL at M-CALAfter plane operation
vna-error-plane-explorer/2.0. Fixed 101-point grid, 2.0–3.0 GHz, 10 MHz steps; no interpolation in decisions. Phase is wrapped in the cursor table. All curves are noiseless illustrative calculations; invalid evidence stays visible with its status.
Cursor 2.45 GHz · Γ / m · dimensionless complex values
StageReal + j imaginaryMagnitudePhase (wrapped)Reading
Synthetic truth at DUT0.5 + j00.56.020599913 dB
Raw at exterior plane0.493684210526 + j00.4936842105266.131015251 dB
SOL-calibrated at M-CAL0.5 + j00.56.020599913 dB
After selected plane operation0.5 + j00.56.020599913 dB
Residual, conditioning and sampled properties
CheckResult and meaning
DUT truth residual at cursor0
Largest verification residual, all 101 points0; criterion ≤ 0.01 (inclusive)
Standard-system conditioningκF = 4.720696; κ2 ≤ κF ≤ 3κ2
Normalized fixture conditioningκF = 2; [[A,B/50],[50C,D]]
Passivity at cursor|Γ| = 0.5; within 1 + 10⁻¹⁰
Reciprocity at cursorNot a one-port property
UncertaintyActual standard, connection, drift, fixture and receiver covariance unknown; tolerance is not an accuracy specification.
Independent verification and complete SOL witness

Independent load Γv = −0.2 real at R2-FEED; never fitted as a SOL standard. Values are conditional synthetic references; unknown evidence withholds a verification conclusion.

Independent verification at cursor
QuantityValue
Reference Γv−0.2 + j0
Raw verification receiver mv-0.156470588235 + j0
SOL-calibrated at M-CAL · verification-0.2 + j0
Recovered Γv-0.2 + j0
Absolute DUT-plane residual0
Calibration-plane residual before fixture removal0
Three complex standards · raw observations never rewritten
StandardActual ΓAssumed ΓObserved mSOL re-fit Γ
Open1 + j01 + j01.02 + j01 + j0
Short-1 + j0-1 + j0-0.798181818182 + j0-1 + j0
Load0 + j00 + j00.02 + j00 + j0
Actual versus estimated one-port coefficients (not a two-port solver)
TermActual at calibrationEstimated from standards
d0.02 + j00.02 + j0
t0.9 + j00.9 + j0
s0.1 + j00.1 + j0

Fit residual: 0. Three fitted standards can match their assumed definitions exactly even when those definitions are wrong. Post-fit drift changes actual d by +0.005 only, without re-fitting.

Committed configuration and evidence snapshot (included in print)
Correct one-port SOL · reproducible inputs
InputCommitted value
Directivity magnitude |d|0.02 dimensionless
Directivity phase0 degrees
Tracking magnitude |t|0.9 dimensionless
Tracking phase0 degrees
Source match magnitude |s|0.1 dimensionless
Source match phase0 degrees
Actual load Γ (real)0 dimensionless
Assumed load Γ (real)0 dimensionless
Fixture one-way length0.02 m
Fixture phase velocity200000000 m/s
Fixture one-way matched loss1 dB
Actual fixture characteristic impedance50 Ω, real
Source available CW power at M-CAL-10 dBm
Analytic DUTantenna
One-port numerical calibrationsol
Fixture in signal pathabsent
Plane operationnone
Removal modelactual
Post-calibration directivity changeoff
Standard evidenceknown
Independent verification evidenceknown
Connections after calibrationunchanged
Dataset compatibilitycompatible
IF bandwidth (Hz; context only)1000
Sweep averaging (count; context only)1

vna-error-plane-explorer/2.0 · p08-m04-one-port-v1 · p08-m04-fixture-cascade-v1 · p08-m04-verification-rules-v1. SYN-VNA-CW-v1; fixed evaluation 2026-09-09 UTC; M-CAL-50-v1; no physical acquisition. Parent raw fixture remains immutable. Connection: unchanged; standard evidence: known; verification: known; compatibility: compatible. Apply each correction once. Numeric tolerances describe computation, not measured uncertainty.

Method planning · separate from numeric recovery

Default SOLT. Planning view only; no numeric solve for any of these methods.

SOLT · numeric solver not implemented. Require characterized SOL at both ports, the applicable thru, both source directions and source/load-match information. Known-box inversion cannot supply these missing analyzer calibration observations.

Plan A · PCB filter in a two-port fixture

Planes and method. Define R1-DUT ports 1/2 and both exterior M-CAL planes. Plan full two-port SOLT at accessible connectors with characterized kit models and thru, both source directions and match information. For a suitable planar coupon, investigate TRL/multiline TRL directly at the DUT planes with line impedance, branch and band evidence. Select one documented procedure; the explorer implements neither commercial solve.

Fixtures and acquisition. Characterize left and right launches independently, retaining raw exterior 50 Ω complex S-data and actual port order. The local RLC fixture uses 2–3 GHz, 101 points, −10 dBm CW, 1000 Hz IFBW and one sweep average. Establish the actual small-signal range, receiver reserve, bias, settling, thermal equilibrium and connector state before a physical run. Take ten complete repeat sweeps and a separate controlled remating series; do not confuse the populations.

Verification and decision. Use an unused characterized attenuator/line appropriate to both directions before and after DUT acquisition, including the fixture operation. Quantify standard, thru/line, match, receiver, remating and fixture-model covariance. Reject incompatible metadata and unstable inverses. Reverify after cable, connector, power-state or thermal changes. No actual DUT limit or complete uncertainty is supplied; the plan cannot close product acceptance.

Plan B · Antenna feed through a cable and launch

Planes and method. Prefer a feasible characterized SOL at R2-FEED. If calibration ends at M-CAL/F-IN instead, use an independently characterized cable/launch ending at F-OUT/R2-FEED. Apply its removal once. Verify standard gender, offsets, loading and actual access; do not silently replace a launch with a matched line.

Fixtures and acquisition. Freeze antenna mounting, enclosure, nearby objects, cable route and any common-mode suppression, plus supply and thermal state. The local 150 Ω resonant load proxy uses the same stepped CW grid and context as Plan A. Begin with an unused reflection reference at the intended feed plane, preserve ungated complex sweeps, and collect ten stable repeats plus separately labelled remating/route perturbations.

Verification and decision. Compare the independent reference before/after correction, then a direct feed-plane calibration when practicable. Include standard, mismatch, loss/delay, launch, drift and connection uncertainty. Cable-loss improvement alone cannot establish antenna improvement. Hand qualified R2 impedance evidence to the antenna evidence architecture; radiation efficiency, pattern and S0/OTA claims require their own measurements.

Complete static measurement records

These two p08-measurement-record-v1 snapshots are illustrative plans, independent of previous visits and custom explorer edits. “Unknown” fields require evidence; they do not mean zero or pass. Raw IDs remain immutable.

M08-04-FILTER-PLAN-A · full record
p08-measurement-record-v1 · M08-04-FILTER-PLAN-A
Record fieldFixed illustrative snapshot
idM08-04-FILTER-PLAN-A
parentIdsM08-03-SPUR-PLAN-A · M08-02-TX-PLAN-B · M08-01-RAW-A
owner08.4 · fictional RF measurement engineer
questionDoes a shift in the node filter response belong to the component or its launch fixtures?
hypothesesH1: component resonance changed. H2: incorrect fixture model. H3: calibration/connector drift. H4: receiver or DUT is outside its small-signal state.
requirementREQ-VNA-EVIDENCE-v1: coherent four-Sij data at R1-DUT over 2.0–3.0 GHz; synthetic independent max |ΔSij| ≤ 0.01, all 101 samples. No product insertion-loss limit supplied.
decisionRulep08-m04-verification-rules-v1: compatible identity, planes, ports, Zref and grid; valid state; invertible model; independent verification ≤0.01 inclusive. Unknown actual uncertainty prevents real acceptance.
specimenSYN-FILTER-RLC-v1 / p08-m04-fixture-cascade-v1; R=10 Ω, L=10 nH, C=1/[(2π·2.45 GHz)²L]; one analytic network, not a commercial filter.
configurationCFG-VNA-FILTER-A; HW-SYN-A1; FW-SYN-1.0 retained as parent identity; radio transmit disabled, unpowered passive component test. New local swept-CW mode, not portfolio QPSK or a named wireless standard.
stateUnbiased passive RLC, 3.300 V parent node supply disconnected from RF path, illustrative 298.15 K; fixed left/right 20 mm fixtures, supported cables, stable enclosure state.
timestampFrozen illustrative plan 2026-09-09T00:00:00Z; no physical acquisition timestamp.
environmentStable 25 °C assumption; actual temperature record, humidity and external coupling unknown.
stimulusSYN-VNA-CW-v1: stepped coherent CW from 2e9 to 3e9 Hz, 1e7 Hz spacing, 101 points; forward and reverse source directions. No PRBS/seed applies to CW.
statisticComplex normalized wave ratios, real positive 50 Ω at both ports. Source available CW mean −10 dBm at exterior M-CAL, not accepted DUT power, PSD, dBc, PEP or a burst-period average.
populationOne synthetic specimen/state, one deterministic sweep each direction; practical plan takes 10 unchanged complete sweeps and 5 separately labelled disconnect/reconnect sequences, with before/after verification. No synthetic repeatability variance supplied.
acquisitionConfigure band, source power, IFBW and bias first; warm up per selected manual; inspect interfaces; calibrate; verify unused device; DUT forward/reverse; verification again. Actual settling and duration unknown until measured.
planesM-CAL1 = left F-IN → left F-OUT = R1-DUT port1 → component → R1-DUT port2 = right F-IN → right F-OUT = M-CAL2. Currents into ports. R2 antenna feed, S0 OTA and R3 decision boundary not measured.
chainTwo independent known uniform fixtures: each l=.020 m, v=2e8 m/s, one-way matched loss 1 dB, Zc=50 Ω baseline /55 Ω named mismatch variant; no protection pad, bias tee or external loss silently inherited. All unused RF ports terminated in stated 50 Ω.
instrumentSYN-VNA-04 / SIM-004 / firmware SIM-1, two source directions and reference/test receivers. Actual make/model/options/firmware and safe ratings unknown; teaching sources do not supply a physical operating authorization.
settings−10 dBm source available CW, 1000 Hz IFBW, averaging1, linear 101-point grid. Plan power repeat at −20 dBm and confirm unchanged S within evaluated uncertainty; settle bias/thermal state independently.
calibrationPlan full two-port SOLT at coax M-CAL with characterized connector-compatible SOL and thru, both directions/load match; independently characterize fixture models. If same-stackup TRL standards at DUT planes exist, compare that alternative over validated line bands instead of removing those launches twice. Commercial solve not implemented.
rawEvidenceSYN-VNA-FILTER-RAW-v1: immutable analytic exterior S from left × DUT × right; SYN-VNA-VERIFY-2P-v1: independent matched device S12=S21=.8, S11=S22=0. Parent raw and fixture IDs retained. Actual Touchstone files/certificates absent.
processingvna-error-plane-explorer/2.0; p08-m04-fixture-cascade-v1: T_DUT=T_left⁻¹ T_exterior T_right⁻¹; no raw rewrite, smoothing, gating or renormalization. Derived record M08-04-FILTER-DERIVED-A refers to raw and both box IDs.
uncertaintyReal standard-model, connection, drift, source/load match, receiver noise, fixture-parameter covariance, bias and thermal contributions unknown. κF and 1e−10 tests are numerical checks, not measurement uncertainty or confidence.
resultExact known models recover S11=S22=1/11, S21=S12=10/11 at 2.450 GHz; transmission −0.827853703165 dB. Synthetic verification residual is roundoff. A wrong 50 Ω removal model for the 55 Ω fixture fails independent verification.
inferenceSupported only for the named synthetic inverse problem; passive-looking recovered curves cannot override failed verification. No real filter pass, commercial SOLT/TRL solve, accredited calibration or radiation claim.
unresolvedActual standards/fixtures, method covariance, reference-device characterization, connector repeatability, instrument limits and state evidence are required before using hardware data.
nextMeasurement engineer: acquire a connector-compatible unused attenuator/line and check four complex Sij across the band; compare independent fixture characterization. Hand qualified vector data and residual uncertainty to planned 08.5.
reviewInvalidate on cable movement, reconnect, changed fixture/port mapping, power/gain switching, bias, temperature, firmware or frequency grid; reverify and recalibrate as the cause requires.
M08-04-FEED-PLAN-A · full record
p08-measurement-record-v1 · M08-04-FEED-PLAN-A
Record fieldFixed illustrative snapshot
idM08-04-FEED-PLAN-A
parentIdsM08-03-BURST-PLAN-A · M08-02-TX-PLAN-B · M06-E1
owner08.4 · fictional RF measurement engineer
questionIs the apparent antenna-feed match a load property or round-trip cable attenuation?
hypothesesH1: feed impedance changed. H2: cable loss hides reflection. H3: wrong standard model. H4: common-mode cable coupling invalidates a two-port line model.
requirementREQ-FEED-EVIDENCE-v1: complex Γ at R2-FEED, same product state, 2.0–3.0 GHz; synthetic independent |ΔΓv|≤.01. No antenna efficiency or product return-loss limit supplied.
decisionRulep08-m04-verification-rules-v1: compatible one-port identity, plane, real 50 Ω and grid; valid state and inverse; unused reflection reference residual ≤.01 inclusive. Actual residual uncertainty is unknown; no real DUT acceptance.
specimenSYN-ANT-LOAD-RLC-v1 / p08-m04-one-port-v1: Z=150+j(ω·10 nH−1/(ωC)) Ω; C shares 2.450 GHz resonance; impedance-only proxy.
configurationCFG-VNA-FEED-A; parent HW-SYN-A1/FW-SYN-1.0; radio disabled for passive swept-CW feed test. Physical plan names enclosure, mounting, cable support and antenna tune state before comparison.
statePassive unbiased load; parent 3.300 V supply disabled for RF test; 298.15 K teaching state; no spatial/OTA model. Connector mating/torque follows actual interface procedure.
timestampFrozen illustrative plan 2026-09-09T00:00:00Z; no physical acquisition timestamp.
environmentStable 25 °C assumption; actual temperature record, humidity and external coupling unknown.
stimulusSYN-VNA-CW-v1: one-port stepped CW, 2e9–3e9 Hz in 1e7 Hz steps, 101 samples. No PRBS/seed applies; no transmission-direction observation is inferred.
statisticComplex incident/reflected wave ratio Γ at real positive 50 Ω R2-FEED after correction. Source available CW mean −10 dBm at M-CAL; actual power delivered to the mismatched load is not assumed equal to that available power.
populationOne synthetic load/state and deterministic sweep. Physical plan: 10 fixed-setup sweeps, then 5 separately identified controlled remating/route sequences; independent verification before/after. No statistical confidence from the synthetic repeats.
acquisitionFreeze mounting, enclosure, route and thermal state; establish actual safe/linear source level; calibrate SOL at named plane; check unused reference; acquire one-port DUT sweep; recheck reference; retain route/remating controls separately. Actual settling and duration unknown.
planesM-CAL = F-IN before cable; F-OUT = R2-FEED. Fixture-free anchor calibrates directly at R2-FEED. R1 component port and R3 decision boundary retain their portfolio meanings.
chainOne cable/launch, 20 mm, 100 ps one-way, 1 dB one-way matched loss, Zc50 Ω baseline; full known fixture transformation required for mismatch. No pad or protection network from TX-PWR-A is copied into this new topology.
instrumentSYN-VNA-04 / SIM-004 / firmware SIM-1, two source directions and reference/test receivers. Actual make/model/options/firmware and safe ratings unknown; teaching sources do not supply a physical operating authorization.
settings−10 dBm source available CW, 1000 Hz IFBW, averaging1, linear 101-point grid. Plan power repeat at −20 dBm and confirm unchanged S within evaluated uncertainty; settle bias/thermal state independently.
calibrationPlan one-port SOL at feed if compatible standards can physically reach it. Otherwise SOL at M-CAL using correct open/short/load definitions, then remove independently characterized cable/launch once. Independent Γv=−.2 load is excluded from fit; repeat it before and after each controlled reconnect.
rawEvidenceSYN-VNA-SOL-RAW-v1; SYN-VNA-WRONG-LOAD-RAW-v1 preserves actual load Γ=.02 and assumed0; SYN-VNA-FEED-RAW-v1; SYN-VNA-VERIFY-1P-v1 Γv=−.2. These immutable simulated definitions are not measurements.
processingvna-error-plane-explorer/2.0; p08-m04-one-port-v1: solve [1,Γi,miΓi]·[d,q,s]=mi, t=q+ds; Γ=(m−d)/(t+s(m−d)); then inverse fixture transformation. M08-04-FEED-DERIVED-A references raw and cable model; no double correction.
uncertaintyReal standard-model, connection, drift, source/load match, receiver noise, fixture-parameter covariance, bias and thermal contributions unknown. κF and 1e−10 tests are numerical checks, not measurement uncertainty or confidence.
resultAt 2.450 GHz actual ΓDUT=.5. Cable input −.396380404700−j.024938141268; phase-only .397164117362; exact loss-and-phase removal .5. Wrong-load calibration alone yields Γhat=.484848484848 and unused-load residual .019123505976, failing the .01 local criterion.
inferenceAn apparently improved match behind loss is not improved antenna performance. S11 supplies port evidence only; radiation efficiency, pattern, TRP/TIS and packet behavior require their own evidence.
unresolvedActual standards/fixtures, method covariance, reference-device characterization, connector repeatability, instrument limits and state evidence are required before using hardware data.
nextMeasurement engineer: check unused load through the same fixture, then compare direct feed-plane calibration if possible. Control cable route/choke effects; send qualified R2 impedance evidence to 08.5 and the Path06 spatial investigation.
reviewInvalidate on cable movement, reconnect, changed fixture/port mapping, power/gain switching, bias, temperature, firmware or frequency grid; reverify and recalibrate as the cause requires.
Engineering decision → record update

Hand both qualified port-measurement records to 08.5 Modulated Transmitter & Receiver Measurements. Preserve remaining uncertainty and validity conditions when moving from small-signal CW evidence to a modulated operating state.

Ungraded review

Check your understanding

Answer each question in your own words, then reveal the model answer.

  1. 01What information does a three-term one-port solve add to open-response scaling?
    Model answer

    Three independent known complex standards identify directivity d, reflection tracking t and source match s at each frequency. Scaling m by one open observation fixes one response but cannot identify three independent terms. Repeated standards make the solve singular; a complete two-port calibration also needs both source directions and load-match information.

  2. 02Why can the wrong load model produce a perfect calibration-standard fit?
    Model answer

    The solve matches the assumed standard definitions. An actual Γ = 0.02 load called zero changes the fitted terms. It maps all three fitted standards to those assumptions but recovers the separate −0.2 verification load as −0.219123505976. A small fit residual tests the equations, not the truth of the models.

  3. 03Does remeasuring the calibration load provide independent verification?
    Model answer

    It checks repeatability and some changes, but shares the definition and interface errors used in the fit. Use an unused, independently characterized device with reference values and uncertainty. Keep its observations out of the calibration solve; compare at compatible planes, ports, reference impedance, grid and state.

  4. 04Why does phase-only extension leave the cable example at |Γ| = 0.397164117362?
    Model answer

    It reverses the −176.4° round-trip phase, but leaves 2 dB of round-trip attenuation. The DUT is still Γ = 0.5. A justified matched loss-and-phase inverse restores it; a mismatched launch needs the full network model. Removing an already calibrated cable a second time is also wrong.

  5. 05Can a time gate prove a discontinuity no longer affects the DUT?
    Model answer

    No. It changes the finite-band transformed dataset. Windowing trades sidelobes for impulse width, close reflections overlap, and early reflections can mask later energy. Gating does not repair the hardware, recover missing frequencies or establish absolute calibration accuracy. Retain the ungated data and all transform/gate settings.

  6. 06A passive-looking trace clears the residual tolerance after a connection changed. Is the DUT result accepted?
    Model answer

    No. The unchanged-state validity condition failed. The local residual criterion is only one gate and does not replace uncertainty. Unknown verification is inspect; incompatible or changed evidence is blocked; a singular model or invalid small-signal state is invalid. None is a product pass.

References and further study

Primary-source access: 2026-09-09. vna-error-plane-explorer/2.0; p08-m04-one-port-v1; p08-m04-fixture-cascade-v1; p08-m04-verification-rules-v1. Numerical validation uses 10⁻¹⁰ absolute complex error, 10⁻⁸ dB, 10⁻⁸ degrees for nonzero phase, and 10⁻⁹ relative normalized chain recovery. These are computation tolerances, not measurement uncertainty. IEEE 370 catalogue scope and its 2022 erratum were inspected; the full standard was not available. The two Keysight application-note URLs supplied asset introductions, not readable full PDFs. No unavailable clauses or normative thresholds are asserted.

  1. VNA-TIME · Keysight. Time Domain · M9485A help. Living documentation; no displayed revision/date. Consulted: Response resolution; alias responses; transform modes; gating and masking; window settings. Informative finite-band transform and gating limits; the original delay/window sketch is qualitative, not a computed transform.
  2. VNA-ERROR · Keysight. Measurement Errors · PXI VNA help. Living documentation; no displayed revision/date. Consulted: Random Errors; Systematic Errors; individual directivity, match, tracking and isolation descriptions. Informative instrument error orientation; not a complete implementation or specification.
  3. VNA-APP · Keysight. Applying Error Correction to Vector Network Analyzer Measurements · 5965-7709. Asset identity verified; PDF edition unavailable. Consulted: Accessible asset introduction only. Catalogue/introduction: SOLT, TRL and adapter scope. Full PDF was unavailable; no clause claims.
  4. VNA-KIT · Keysight. Calibration Standards · M9485A help. Living documentation; no displayed revision/date. Consulted: Standard Definitions; capacitance/inductance models; class assignments. Informative standard/offset model fields. No actual kit coefficients are assumed.
  5. VNA-KIT-APP · Keysight. Specifying Calibration Standards and Kits · 5989-4840. Asset identity verified; PDF edition unavailable. Consulted: Accessible asset introduction only. Document scope only. Accessible help supplies teaching; full PDF and kit-specific definitions remain unresolved.
  6. VNA-TRL · Keysight. TRL Calibration · PNA help. Living documentation; no displayed revision/date. Consulted: Cal Standards Used in TRL: THRU, REFLECT, LINE, MATCH. Method-specific line impedance, phase selection and band planning; not a universal phase-only validity rule.
  7. VNA-LRM · Anritsu. LRL/LRM Calibration Theory and Methodology · 11410-00492. Rev. C, printed January 2017, ©2016. Consulted: pp.1–4: algorithm choices, LRM, line lengths; p.10 revision. Historical informative method distinctions, match assumptions and line separation; not current option availability.
  8. VNA-EXT · Keysight. Port Extensions · PNA help. Living documentation; no displayed revision/date. Consulted: Why/How to use Port Extensions; data-flow note. Electrical plane motion and optional loss; this lesson explicitly distinguishes its phase-only operation.
  9. VNA-VERIFY · NIST authors / IEEE Microwave Magazine. Electronic Vector-Network-Analyzer Verification. Williams, Lewandowski, LeGolvan and Ginley; October 2009, pp.119–123. Consulted: Calibration comparison; quantifying verification; uncertainty/covariance discussion. Independent reference comparisons and residual uncertainty; no claim about current service/software availability.
  10. IEEE370 · IEEE SA. IEEE 370-2020 · Electrical Characterization of PCB and Related Interconnects up to 50 GHz. Active at access; published 2021-01-08. Consulted: Official catalogue identity, scope and errata link. Catalogue only. Full normative text not read; does not prescribe every antenna calibration.
  11. IEEE370-ERR · IEEE SA. IEEE 370-2020 correction sheet. 21 January 2022. Consulted: Complete two-page erratum; correction to Annex G equation G.1. Erratum identity reviewed; no normative algorithm implemented from the unavailable base text.
  12. MET-NIST · NIST. TN 1297 · §5 Combined Standard Uncertainty. 1994 guidance; web page updated 2023-03-01. Consulted: 5.1–5.5; combination, correlation and coverage conditions. Uncertainty is distinct from calibration residual and numerical tolerance; no uncertainty budget fabricated.
  13. MET-INDEX · BIPM / JCGM. Guides in Metrology publication index. Live listing: JCGM 100:2008 and Amd.1:2026. Consulted: GUM, nonlinearity amendment and GUM-6 listings. Current source identity only; inherited 08.1 owns detailed propagation.