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Correlation Functions

Optical coherence is not one number and not a synonym for narrow linewidth. It is a hierarchy of correlation functions that predicts how field samples at different positions, times, polarizations, and detector channels interfere or produce joint photoevents. First-order coherence controls amplitude interference. Second-order coherence controls ideal coincidence statistics. Higher orders control increasingly detailed multiphoton records.

The hierarchy is operational. In Glauber photodetection theory, an absorbing detector selects a positive-frequency field operator at each event, and an nn-fold coincidence samples a normally ordered 2n2n-operator expectation value. The ordering is part of the physics, not decorative notation. Symmetrized noise, time-ordered Green functions, and retarded response functions answer different questions.

A trustworthy correlation statement identifies:

  • every space-time, polarization, and mode argument;
  • the operator ordering and state;
  • whether the field is stationary, pulsed, or explicitly time dependent;
  • normalization and treatment of zero intensity;
  • filtering, finite gates, loss, background, and detector timing response;
  • whether the result is raw, corrected, inferred, or model predicted.

Without these declarations, a value such as g(2)(0)=1g^{(2)}(0)=1 does not identify a state or even a unique experiment.

This page is the canonical home for optical coherence functions:

  • the first-order kernel G(1)G^{(1)} and degree of coherence g(1)g^{(1)};
  • the second-order photodetection function G(2)G^{(2)} and normalized coincidence function g(2)g^{(2)};
  • the general normally ordered Glauber hierarchy;
  • coherent, thermal, and number-state examples;
  • the relation between gated count factorial moments and continuous-time correlations;
  • classical Cauchy–Schwarz bounds and sufficient nonclassicality tests;
  • stationarity, spectral coherence, multimode averaging, filtering, and detector convolution.

Photon Counting owns the calibrated detector response, efficiency, dark counts, dead time, and response matrices. Hanbury Brown–Twiss Interferometry owns the detailed intensity-interferometer geometry and data normalization, while Photon Antibunching owns the single-emitter signature and its experimental pitfalls. Coherent Light, Thermal Light, and Photon Number States own those source states.

Generic connected, retarded, many-body, and spectral correlators belong to Correlation Functions Overview. Environmental memory, KMS relations, and bath ordering belong to Bath Correlation Functions.

Write

x=(r,t,λ),x=(\mathbf r,t,\lambda),

where λ\lambda abbreviates polarization, detector channel, spectral filter, or other resolved labels. Let

E^(+)(x)\hat E^{(+)}(x)

be the scalar positive-frequency field after projection onto the detector response. Its adjoint is

E^(−)(x)=[E^(+)(x)]†.\hat E^{(-)}(x) = \left[ \hat E^{(+)}(x) \right]^\dagger.

Vector fields require polarization contractions or a coherence matrix. The scalar notation below assumes that those choices have already been made.

Constants containing detector responsivity can be restored when absolute rates are needed. Correlation ratios often cancel a common constant, but they do not cancel mode mismatch or channel-dependent response automatically.

The normally ordered optical intensity operator at xx is proportional to

I^(x)=E^(−)(x)E^(+)(x).\hat I(x) = \hat E^{(-)}(x)\hat E^{(+)}(x).

Its expectation,

I(x)=⟨I^(x)⟩,I(x) = \left\langle\hat I(x)\right\rangle,

sets the ideal first-order absorption rate. The symbol II below denotes this normally ordered mean unless stated otherwise.

Vacuum has a nonzero symmetrized field variance but

⟨0∣E^(−)(x)E^(+)(x)∣0⟩=0\langle0| \hat E^{(-)}(x)\hat E^{(+)}(x) |0\rangle = 0

in an ideal empty mode. This is one reason ordering conventions cannot be interchanged casually.

The first-order optical correlation is

G(1)(x1,x2)=⟨E^(−)(x1)E^(+)(x2)⟩.G^{(1)}(x_1,x_2) = \left\langle \hat E^{(-)}(x_1) \hat E^{(+)}(x_2) \right\rangle.

Its diagonal is the mean intensity:

G(1)(x,x)=I(x).G^{(1)}(x,x)=I(x).

The kernel is Hermitian,

G(1)(x2,x1)=[G(1)(x1,x2)]∗,G^{(1)}(x_2,x_1) = \left[ G^{(1)}(x_1,x_2) \right]^*,

and positive semidefinite. For arbitrary complex coefficients cjc_j,

∑j,kcj∗ckG(1)(xj,xk)≥0.\sum_{j,k} c_j^*c_k G^{(1)}(x_j,x_k) \ge0.

This follows because the left side is

⟨A^†A^⟩,A^=∑kckE^(+)(xk).\left\langle \hat A^\dagger\hat A \right\rangle, \qquad \hat A = \sum_k c_k\hat E^{(+)}(x_k).

When both local intensities are nonzero, define

g(1)(x1,x2)=G(1)(x1,x2)I(x1)I(x2).g^{(1)}(x_1,x_2) = \frac{ G^{(1)}(x_1,x_2) }{ \sqrt{I(x_1)I(x_2)} }.

The Cauchy–Schwarz inequality gives

∣g(1)(x1,x2)∣≤1.\left| g^{(1)}(x_1,x_2) \right| \le1.

The magnitude measures normalized amplitude coherence between the two samples; the argument gives their correlation phase. If either intensity vanishes, the normalized ratio is undefined even though the unnormalized kernel is well defined.

Suppose two sampled fields are recombined with a controllable phase ϕ\phi. After absorbing fixed transmission factors into I1I_1 and I2I_2, the mean output intensity is

I(ϕ)=I1+I2+2I1I2 Re⁡[eiϕg12(1)].\begin{aligned} I(\phi) ={}& I_1+I_2 \\ &+ 2\sqrt{I_1I_2}\, \operatorname{Re} \left[ e^{i\phi}g_{12}^{(1)} \right]. \end{aligned}

The fringe visibility

V≡Imax⁡−Imin⁡Imax⁡+Imin⁡\mathcal V \equiv \frac{I_{\max}-I_{\min}} {I_{\max}+I_{\min}}

is therefore

V=2I1I2I1+I2∣g12(1)∣.\mathcal V = \frac{ 2\sqrt{I_1I_2} }{ I_1+I_2 } \left|g_{12}^{(1)}\right|.

For balanced intensities,

V=∣g12(1)∣.\mathcal V = \left|g_{12}^{(1)}\right|.

Unequal intensity lowers visibility even for perfect mutual coherence. Conversely, high visibility establishes first-order coherence for the selected samples but does not establish Poisson statistics or a coherent quantum state.

For several polarization or spatial components, define

Γμν(1)(x1,x2)=⟨E^μ(−)(x1)E^ν(+)(x2)⟩.\Gamma_{\mu\nu}^{(1)}(x_1,x_2) = \left\langle \hat E_\mu^{(-)}(x_1) \hat E_\nu^{(+)}(x_2) \right\rangle.

This matrix carries intensity, polarization, and mutual coherence together. Tracing over unresolved components can reduce measured visibility. A scalar g(1)g^{(1)} is meaningful only after specifying the projections or contractions used by the optical system and detector.

Operational hierarchy of optical coherence: first-order field interference, second-order intensity coincidences, and higher-order event correlations with coherent, thermal, and number-state benchmarks.

The optical hierarchy associates order one with field-amplitude interference, order two with joint intensity events, and order mm with mm-fold photodetection. The familiar equal-mode values 11, m!m!, and n!/[nm(n−m)!]n!/[n^m(n-m)!] summarize different states but do not replace the full space-time functions; the number-state expression applies for m≤nm\leq n and vanishes for m>nm>n.

For a stationary field,

G(1)(t1,t2)=G(1)(t2−t1).G^{(1)}(t_1,t_2) = G^{(1)}(t_2-t_1).

With the convention

G(1)(τ)=⟨E^(−)(t)E^(+)(t+τ)⟩,G^{(1)}(\tau) = \left\langle \hat E^{(-)}(t) \hat E^{(+)}(t+\tau) \right\rangle,

stationarity implies

G(1)(−τ)=[G(1)(τ)]∗.G^{(1)}(-\tau) = \left[ G^{(1)}(\tau) \right]^*.

Stationarity is an ensemble property. A finite record can drift, blink, age, or mix several operating points even when a time-averaged plot appears smooth.

Choose the spectral convention

S(ω)=12π∫−∞∞dτ eiωτG(1)(τ).S(\omega) = \frac1{2\pi} \int_{-\infty}^{\infty} d\tau\, e^{i\omega\tau} G^{(1)}(\tau).

Then

G(1)(τ)=∫−∞∞dω e−iωτS(ω).G^{(1)}(\tau) = \int_{-\infty}^{\infty} d\omega\, e^{-i\omega\tau}S(\omega).

For a stationary physical field, S(ω)S(\omega) is nonnegative in the relevant analytic-signal convention. The spectral width and temporal decay of g(1)g^{(1)} are Fourier related, but “coherence time” has several definitions.

A common integral convention is

τc=∫−∞∞dτ ∣g(1)(τ)∣2.\tau_c = \int_{-\infty}^{\infty} d\tau\, \left|g^{(1)}(\tau)\right|^2.

Other conventions use a 1/e1/e width, half width at half maximum, or integral of ∣g(1)∣|g^{(1)}|. Numerical coherence times should therefore be accompanied by their definition. Linewidth and Coherence applies these alternatives to laser phase diffusion, frequency-noise PSDs, and measured cw line shapes.

For a Lorentzian spectrum centered at ω0\omega_0 with field-correlation decay rate γ\gamma,

g(1)(τ)=e−iω0τe−γ∣τ∣.g^{(1)}(\tau) = e^{-i\omega_0\tau} e^{-\gamma|\tau|}.

For a Gaussian spectrum with rms width σω\sigma_\omega,

g(1)(τ)=e−iω0τe−σω2τ2/2.g^{(1)}(\tau) = e^{-i\omega_0\tau} e^{-\sigma_\omega^2\tau^2/2}.

The oscillatory carrier and decaying envelope contain different information. Removing a carrier in a rotating frame does not lengthen the physical coherence envelope.

The normally ordered second-order function is

G(2)(x1,x2)=⟨E^(−)(x1)E^(−)(x2)×E^(+)(x2)E^(+)(x1)⟩.\begin{aligned} G^{(2)}(x_1,x_2) ={}& \bigl\langle \hat E^{(-)}(x_1) \hat E^{(-)}(x_2) \\ &\quad\times \hat E^{(+)}(x_2) \hat E^{(+)}(x_1) \bigr\rangle. \end{aligned}

It is nonnegative because it has the form

G(2)(x1,x2)=⟨A^†A^⟩,G^{(2)}(x_1,x_2) = \left\langle \hat A^\dagger\hat A \right\rangle,

with

A^=E^(+)(x2)E^(+)(x1).\hat A = \hat E^{(+)}(x_2) \hat E^{(+)}(x_1).

For ideal weak absorbers, G(2)G^{(2)} is proportional to the joint density for two photoevents at the declared coordinates. Detector response and finite gates turn this density into integrated probabilities.

When I(x1)I(x2)≠0I(x_1)I(x_2)\ne0, define

g(2)(x1,x2)=G(2)(x1,x2)I(x1)I(x2).g^{(2)}(x_1,x_2) = \frac{ G^{(2)}(x_1,x_2) }{ I(x_1)I(x_2) }.

For one stationary channel,

g(2)(τ)=G(2)(τ)I2,g^{(2)}(\tau) = \frac{G^{(2)}(\tau)}{I^2},

where

G(2)(τ)=⟨E^(−)(t)E^(−)(t+τ)×E^(+)(t+τ)E^(+)(t)⟩.\begin{aligned} G^{(2)}(\tau) ={}& \bigl\langle \hat E^{(-)}(t) \hat E^{(-)}(t+\tau) \\ &\quad\times \hat E^{(+)}(t+\tau) \hat E^{(+)}(t) \bigr\rangle. \end{aligned}

At large delays, independent stationary samples often give

g(2)(τ)⟶1,g^{(2)}(\tau)\longrightarrow1,

but this limit can fail for nonergodic mixtures, blinking, periodic driving, long memory, or conditioning.

For a stationary ideal point process with mean detection rate Rˉ\bar R,

Rˉ g(2)(τ)\bar R\,g^{(2)}(\tau)

is the conditional event rate at delay τ\tau given an event at the origin, under the standard weak-detection assumptions. Thus:

  • g(2)(τ)>1g^{(2)}(\tau)>1 means enhanced conditional detection;
  • g(2)(τ)<1g^{(2)}(\tau)<1 means suppressed conditional detection;
  • g(2)(τ)=1g^{(2)}(\tau)=1 means no second-order excess at that delay.

This interpretation concerns events in the selected channel. It does not imply a force between photons, a literal packet size, or a complete description of the field state.

At one point,

G(2)(x,x)=⟨:I^(x)2:⟩,G^{(2)}(x,x) = \left\langle : \hat I(x)^2 : \right\rangle,

not the unordered ⟨I^2⟩\langle\hat I^2\rangle. For one mode,

a^†a^†a^a^=N^(N^−1).\hat a^\dagger\hat a^\dagger\hat a\hat a = \hat N(\hat N-1).

The falling factorial excludes pairing one registered event with itself. When ordinary count variance is reconstructed, the missing diagonal returns as the Poisson shot-noise term.

For a pulse described by one selected mode with number operator N^\hat N, the zero-delay pulsed quantity is

gp(2)[0]=⟨N^(N^−1)⟩⟨N^⟩2.g_{\mathrm p}^{(2)}[0] = \frac{ \langle\hat N(\hat N-1)\rangle }{ \langle\hat N\rangle^2 }.

Square brackets emphasize a discrete pulse lag. This quantity is not automatically the same as an infinitesimal continuous-time g(2)(0)g^{(2)}(0). It integrates all temporal structure accepted within the pulse and detection gate.

Let NGN_G be the ideal count in a gate GG. Under linear photodetection,

⟨(NG)m⟩=∫Gdx1⋯∫Gdxm×G(m)(x1,…,xm),\begin{aligned} \left\langle (N_G)_m \right\rangle ={}& \int_G dx_1\cdots \int_G dx_m \\ &\times G^{(m)}(x_1,\ldots,x_m), \end{aligned}

up to the declared responsivity factors. Here

(NG)m=NG(NG−1)⋯(NG−m+1).(N_G)_m = N_G(N_G-1)\cdots(N_G-m+1).

Changing the gate changes the measured mode mixture and therefore can change the normalized correlation even when the source is unchanged.

For one stationary stream with mean ideal rate Rˉ\bar R and a gate of duration TT,

⟨NT⟩=RˉT.\langle N_T\rangle = \bar R T.

The general factorial second moment is

⟨NT(NT−1)⟩=Rˉ2∫0Tdt∫0Tdt′×g(2)(t′−t).\begin{aligned} \langle N_T(N_T-1)\rangle ={}& \bar R^2 \int_0^Tdt \int_0^Tdt' \\ &\times g^{(2)}(t'-t). \end{aligned}

When the same-channel stationary correlation is even in delay,

CT:=∫0Tdτ (T−τ)[g(2)(τ)−1].\mathcal C_T := \int_0^T d\tau\, (T-\tau) \left[ g^{(2)}(\tau)-1 \right].

The count variance is then

Var⁡(NT)=RˉT+2Rˉ2CT.\operatorname{Var}(N_T) = \bar R T + 2\bar R^2\mathcal C_T.

The first term is shot noise. Positive integrated excess produces super-Poissonian count variance; negative integrated excess can produce sub-Poissonian variance. A local dip at zero delay does not by itself fix the long-gate Fano factor because the complete correlation area matters.

For mm detection coordinates, define the ordered absorption product

A^m(x):=E^(+)(xm)⋯E^(+)(x1),\hat A_m(\mathbf x) := \hat E^{(+)}(x_m)\cdots \hat E^{(+)}(x_1),

where x=(x1,…,xm)\mathbf x=(x_1,\ldots,x_m). The detection-diagonal correlation is

G(m)(x):=⟨A^m†(x)A^m(x)⟩≥0.G^{(m)}(\mathbf x) := \left\langle \hat A_m^\dagger(\mathbf x) \hat A_m(\mathbf x) \right\rangle \geq 0.

Expanding A^m†A^m\hat A_m^\dagger\hat A_m reverses the positive-frequency factors relative to the negative-frequency factors. The positive-operator form also makes the nonnegativity of an ideal joint photodetection rate explicit.

The normalized detection-diagonal function is

g(m)(x1,…,xm)=G(m)(x1,…,xm)∏j=1mI(xj),g^{(m)}(x_1,\ldots,x_m) = \frac{ G^{(m)}(x_1,\ldots,x_m) }{ \prod_{j=1}^{m}I(x_j) },

when every denominator is nonzero.

The more general coherence kernel keeps separate negative- and positive-frequency coordinates:

G(m)(x;y):=⟨A^m†(x)A^m(y)⟩.G^{(m)}(\mathbf x;\mathbf y) := \left\langle \hat A_m^\dagger(\mathbf x) \hat A_m(\mathbf y) \right\rangle.

Here y=(y1,…,ym)\mathbf y=(y_1,\ldots,y_m). Expanding the compact notation gives negative-frequency factors at x\mathbf x followed by the reversed positive-frequency factors at y\mathbf y. The detection-diagonal function sets yj=xjy_j=x_j. Keeping the full kernel is important in coherence theory, propagation, and interferometric transformations.

A field is first-order coherent over a domain when its first-order kernel factorizes there:

G(1)(x,y)=E∗(x)E(y).G^{(1)}(x,y) = \mathcal E^*(x)\mathcal E(y).

Full Glauber coherence requires factorization of the entire normally ordered hierarchy:

G(m)(x;y)=∏j=1mE∗(xj)×∏j=1mE(yj)\begin{aligned} G^{(m)}(\mathbf x;\mathbf y) ={}& \prod_{j=1}^{m} \mathcal E^*(x_j) \\ &\times \prod_{j=1}^{m} \mathcal E(y_j) \end{aligned}

for all relevant orders and coordinates. An ideal multimode coherent state satisfies this condition. Demonstrating one value such as g(2)(0)=1g^{(2)}(0)=1 does not demonstrate full coherence.

Correlation hierarchy is not always state tomography

Section titled “Correlation hierarchy is not always state tomography”

Photodetection correlations are invariant under a global optical phase. A coherent state with unknown uniformly distributed global phase can reproduce the same phase-insensitive normally ordered number correlations as a fixed coherent amplitude. Low-order correlation data also leave many distinct states compatible with the observations.

The complete state requires an informationally complete measurement, often using a phase reference. Phase-Space Distributions and homodyne tomography address that larger reconstruction problem.

For a coherent state, each positive-frequency field annihilation operator acts by its classical complex amplitude. Therefore all normally ordered correlations factorize. Wherever the intensity is nonzero,

gcoh(m)=1.g_{\mathrm{coh}}^{(m)} = 1.

The result holds across coordinates for an ideal coherent field after deterministic linear propagation. Technical amplitude or phase fluctuations can produce a mixture whose measured coherence is lower or whose intensity correlations differ from one.

For zero-mean circular Gaussian thermal light, Gaussian moment factorization gives the Siegert relation

gth(2)(x1,x2)=1+∣gth(1)(x1,x2)∣2.g_{\mathrm{th}}^{(2)}(x_1,x_2) = 1+ \left| g_{\mathrm{th}}^{(1)}(x_1,x_2) \right|^2.

At one coordinate,

gth(2)(0)=2.g_{\mathrm{th}}^{(2)}(0)=2.

More generally, for one thermal mode,

gth(m)(0)=m!.g_{\mathrm{th}}^{(m)}(0)=m!.

The Siegert relation requires Gaussian chaotic statistics. It is not a definition of thermal light and need not hold for arbitrary bunched, non-Gaussian, displaced, or technically noisy fields.

For ∣n⟩|n\rangle and m≤nm\le n,

⟨(a^†)ma^m⟩=n!(n−m)!.\left\langle (\hat a^\dagger)^m\hat a^m \right\rangle = \frac{n!}{(n-m)!}.

Thus

g∣n⟩(m)(0)=n!nm(n−m)!,g_{|n\rangle}^{(m)}(0) = \frac{n!} {n^m(n-m)!},

and the correlation vanishes for m>nm>n. In particular,

g∣n⟩(2)(0)=1−1n.g_{|n\rangle}^{(2)}(0) = 1-\frac1n.

A freely evolving one-mode number state can nevertheless have ∣g(1)(τ)∣=1|g^{(1)}(\tau)|=1. Perfect first-order coherence therefore does not imply coherent-state number statistics.

For MM independent thermal modes with equal mean occupation and a detector that sums their intensities,

g(2)(0)=1+1M.g^{(2)}(0) = 1+\frac1M.

As more unresolved modes are collected, the bunching excess decreases. This approach toward one is mode averaging, not proof that the light became a coherent state.

For unequal modal means μj\mu_j, define

Meff=(∑jμj)2∑jμj2.M_{\mathrm{eff}} = \frac{ \left(\sum_j\mu_j\right)^2 }{ \sum_j\mu_j^2 }.

Then

g(2)(0)=1+1Meffg^{(2)}(0) = 1+\frac1{M_{\mathrm{eff}}}

for independent thermal modes.

Number Statistics and the Mandel Parameter

Section titled “Number Statistics and the Mandel Parameter”

For one selected mode with finite nonzero mean,

g(2)(0)=⟨N(N−1)⟩⟨N⟩2.g^{(2)}(0) = \frac{ \langle N(N-1)\rangle }{ \langle N\rangle^2 }.

Using

N2=N(N−1)+N,N^2=N(N-1)+N,

one obtains

g(2)(0)=1+Var⁡(N)−⟨N⟩⟨N⟩2.g^{(2)}(0) = 1+ \frac{ \operatorname{Var}(N)-\langle N\rangle }{ \langle N\rangle^2 }.

The Mandel parameter

Q=Var⁡(N)−⟨N⟩⟨N⟩Q = \frac{ \operatorname{Var}(N)-\langle N\rangle }{ \langle N\rangle }

therefore satisfies

Q=⟨N⟩[g(2)(0)−1].Q = \langle N\rangle \left[ g^{(2)}(0)-1 \right].

For this one-mode, one-gate setting:

  • g(2)(0)<1g^{(2)}(0)<1 is equivalent to sub-Poissonian number variance;
  • g(2)(0)=1g^{(2)}(0)=1 gives Poisson variance, but not necessarily a Poisson distribution;
  • g(2)(0)>1g^{(2)}(0)>1 gives super-Poissonian variance.

For continuous-time light, a point value g(2)(0)g^{(2)}(0) and a finite-window Fano factor are not equivalent unless the gate and temporal correlation structure are included.

Positive Glauber–Sudarshan representation

Section titled “Positive Glauber–Sudarshan representation”

A field is classical in the standard optical coherence sense if its density operator has a nonnegative, sufficiently regular Glauber–Sudarshan distribution:

ρ=∫d2Mα P(α)∣α⟩⟨α∣,\rho = \int d^{2M}\boldsymbol{\alpha}\, P(\boldsymbol{\alpha}) |\boldsymbol{\alpha}\rangle \langle\boldsymbol{\alpha}|,

with

P(α)≥0.P(\boldsymbol{\alpha})\ge0.

Normally ordered moments then become ordinary classical averages over complex amplitudes. This gives useful inequalities. Violation proves that no such positive classical mixture explains the selected-mode correlations.

For classical random intensity I≥0I\ge0,

gcl(2)(0)=E[I2]E[I]2=1+Var⁡(I)E[I]2≥1.g_{\mathrm{cl}}^{(2)}(0) = \frac{\mathbb E[I^2]}{\mathbb E[I]^2} = 1+ \frac{\operatorname{Var}(I)} {\mathbb E[I]^2} \ge1.

Therefore

g(2)(0)<1g^{(2)}(0)<1

is a sufficient nonclassicality witness under the standard calibrated photodetection assumptions.

The converse is false. Squeezed vacuum, entangled light, and other nonclassical states can have g(2)(0)>1g^{(2)}(0)>1.

For a stationary classical intensity process, Cauchy–Schwarz gives

∣E[I(t)I(t+τ)]∣≤E[I(t)2].\left| \mathbb E[I(t)I(t+\tau)] \right| \le \mathbb E[I(t)^2].

After normalization,

gcl(2)(τ)≤gcl(2)(0).g_{\mathrm{cl}}^{(2)}(\tau) \le g_{\mathrm{cl}}^{(2)}(0).

An observed rise away from zero delay,

g(2)(τ)>g(2)(0)g^{(2)}(\tau)>g^{(2)}(0)

for some τ\tau, is the operational antibunching pattern when stationarity and detector artifacts have been controlled. This criterion is distinct from the stronger but more commonly quoted g(2)(0)<1g^{(2)}(0)<1.

For classical intensities IaI_a and IbI_b at equal time,

[gab(2)]2≤gaa(2)gbb(2).\left[ g_{ab}^{(2)} \right]^2 \le g_{aa}^{(2)} g_{bb}^{(2)}.

Violation is a nonclassical cross-correlation witness. The auto- and cross-correlations must use compatible gates, modes, backgrounds, and normalizations. Comparing differently filtered channels can manufacture an apparent violation of an inapplicable inequality.

The universal first-order inequality

∣g(1)∣≤1|g^{(1)}|\le1

follows from quantum positivity as well as classical Cauchy–Schwarz. It is not a classicality criterion.

For any state with nonzero intensity,

g(2)(0)≥0,g^{(2)}(0)\ge0,

because the numerator is an expectation of A^†A^\hat A^\dagger\hat A. There is no state-independent finite upper bound: rare bright events can make the normalized correlation arbitrarily large.

Absorptive direct photodetection produces products with all negative-frequency operators to the left of all positive-frequency operators. For one mode,

⟨(a^†)ma^m⟩=⟨:N^m:⟩.\left\langle (\hat a^\dagger)^m\hat a^m \right\rangle = \left\langle : \hat N^m : \right\rangle.

This is a factorial moment. It differs from the ordinary power ⟨N^m⟩\langle\hat N^m\rangle by commutator terms.

Quadrature detectors and phase-space representations often involve symmetrically ordered moments. For example,

12⟨a^a^†+a^†a^⟩=⟨N^⟩+12.\frac12 \left\langle \hat a\hat a^\dagger + \hat a^\dagger\hat a \right\rangle = \langle\hat N\rangle+\frac12.

The extra 1/21/2 is the vacuum contribution in this quadrature convention. It does not imply that an ideal absorption counter clicks in vacuum.

A time-ordered propagator has the structure

⟨TE^(x1)E^(x2)⟩,\left\langle \mathcal T \hat E(x_1)\hat E(x_2) \right\rangle,

while a retarded response involves a causal commutator. Neither is generally equal to G(1)G^{(1)} or G(2)G^{(2)}. Green Functions in Many-Body QM and Retarded and Advanced Response own those orderings.

An experiment fixes an ordering through its coupling, detection, and signal processing. Reordering operators after the fact changes the predicted observable.

A deterministic linear optical system maps an input field to

E^out(+)(x)=∫dy h(x,y)E^in(+)(y).\hat E_{\mathrm{out}}^{(+)}(x) = \int dy\, h(x,y)\hat E_{\mathrm{in}}^{(+)}(y).

The first-order kernel propagates bilinearly:

Gout(1)(x,x′)=∫dy∫dy′ h∗(x,y)h(x′,y′)×Gin(1)(y,y′).\begin{aligned} G_{\mathrm{out}}^{(1)}(x,x') ={}& \int dy \int dy'\, h^*(x,y)h(x',y') \\ &\times G_{\mathrm{in}}^{(1)}(y,y'). \end{aligned}

The second-order function carries four copies of the transfer kernel, and the mmth-order function carries 2m2m. Apertures, dispersion, polarization elements, spectral filters, fibers, and interferometers therefore reshape the arguments and mode weights of measured correlations.

Beam Splitters and Interferometers own the corresponding two-mode transformations and phase conventions.

For one selected channel with uniform efficiency η\eta,

Gdet(m)=ηmGin(m),G_{\mathrm{det}}^{(m)} = \eta^mG_{\mathrm{in}}^{(m)},

while each intensity in the denominator contributes one factor of η\eta. Therefore

gdet(m)=gin(m).g_{\mathrm{det}}^{(m)} = g_{\mathrm{in}}^{(m)}.

This useful invariance assumes linear independent loss, no additive background, no saturation, and the same efficiency weighting in numerator and denominator. Loss still reduces sample size and increases uncertainty.

Mode-dependent loss can change a correlation by changing the mixture of accepted modes. A spectral filter that selects one thermal mode from many can increase g(2)(0)g^{(2)}(0) toward 22 even while reducing the total count rate.

Let a signal of mean rate SS have second-order function gs(2)(τ)g_{\mathrm s}^{(2)}(\tau), and let independent Poisson background of rate BB have gb(2)=1g_{\mathrm b}^{(2)}=1. The observed correlation is

gobs(2)(τ)−1=ρ2[gs(2)(τ)−1],ρ=SS+B.\begin{aligned} g_{\mathrm{obs}}^{(2)}(\tau)-1 ={}& \rho^2 \left[ g_{\mathrm s}^{(2)}(\tau)-1 \right], \\ \rho ={}& \frac{S}{S+B}. \end{aligned}

Background pulls both bunching peaks and antibunching dips toward one. A background-corrected value inherits uncertainty from SS, BB, and any assumption that the background is Poisson and independent.

Let hrel(τ)h_{\mathrm{rel}}(\tau) be the normalized relative-time response of two detector channels. In a stationary approximation,

gobs(2)(τ)−1=∫dτ′ hrel(τ−τ′)×[gtrue(2)(τ′)−1].\begin{aligned} g_{\mathrm{obs}}^{(2)}(\tau)-1 ={}& \int d\tau'\, h_{\mathrm{rel}}(\tau-\tau') \\ &\times \left[ g_{\mathrm{true}}^{(2)}(\tau')-1 \right]. \end{aligned}

Jitter broadens a narrow feature and lowers its extremum while preserving its area when the assumptions and integration range hold. Finite histogram bins apply an additional average. A displayed bin width is not the detector timing resolution.

Dead time suppresses nearby same-channel events and can create a false dip. Afterpulsing creates excess events following a click. Cross-talk creates short-delay or neighboring-channel excess. These are correlations of the detector record, not necessarily of the incident field. The response models belong to Photon Counting.

Time tags, pulse indices, detector labels, and live-time intervals should be retained whenever possible. A histogram is a derived statistic. Once events are irreversibly binned or detector labels are discarded, later analyses cannot recover the lost timing or channel information.

For a stationary two-detector record, a coincidence histogram estimates the pair density as a function of delay. Normalization divides by the pair exposure expected from independent streams, including acquisition duration, bin width, and detector live time. The exact estimator depends on whether the source is continuous, pulsed, triggered, periodic, or nonstationary.

In a continuous stationary measurement, large delays can provide an independent-event baseline if the record is long compared with every source correlation time. In a pulsed experiment, side peaks correspond to different pulse pairs and the zero-pulse peak to the same pulse. Pulse-to-pulse drift, missing triggers, and unequal gate acceptance can bias a simple peak-area ratio.

Uncertainty is not independent-bin Poisson by default

Section titled “Uncertainty is not independent-bin Poisson by default”

One event contributes to several delay pairs, normalization is estimated from the same record, and blinking creates long-range dependence. Histogram bins can therefore be correlated. Suitable uncertainty methods include:

  • likelihoods for the underlying time-tag or count process;
  • block bootstrap with blocks longer than relevant memory;
  • repeated independent acquisitions;
  • propagation of background and timing calibrations;
  • model comparison using held-out time intervals.

The measurement should be repeated at several bin widths and normalization windows. A physical feature should transform according to the convolved model, not disappear unpredictably under modest analysis choices.

For a Markovian system coupled to one traveling output channel,

b^out(t)=b^in(t)+L^(t).\hat b_{\mathrm{out}}(t) = \hat b_{\mathrm{in}}(t)+\hat L(t).

Input–Output Theory owns the boundary relation, normalization, coherent drives, and multiport extensions. With vacuum input and normally ordered output detection, the source contribution often reduces to correlations of the system coupling operator L^\hat L.

Let the system obey a time-independent Markov master equation

ρ˙=Lρ\dot\rho = \mathcal L\rho

with steady state ρss\rho_{\mathrm{ss}}. For τ≥0\tau\ge0, the quantum regression construction gives

G(1)(τ)=Tr⁡[L^eLτ(ρssL^†)],\begin{aligned} G^{(1)}(\tau) ={}& \operatorname{Tr} \left[ \hat L e^{\mathcal L\tau} \left( \rho_{\mathrm{ss}}\hat L^\dagger \right) \right], \end{aligned}

and

G(2)(τ)=Tr⁡[L^†L^ eLτ(L^ρssL^†)].\begin{aligned} G^{(2)}(\tau) ={}& \operatorname{Tr} \left[ \hat L^\dagger\hat L\, e^{\mathcal L\tau} \left( \hat L\rho_{\mathrm{ss}}\hat L^\dagger \right) \right]. \end{aligned}

The second formula has a transparent conditional structure:

  1. a detection applies L^\hat L at the origin;
  2. the unnormalized conditional state evolves for time τ\tau;
  3. L^†L^\hat L^\dagger\hat L evaluates the later emission rate.

Normalize by

Rˉ=Tr⁡(L^†L^ρss)\bar R = \operatorname{Tr} \left( \hat L^\dagger\hat L\rho_{\mathrm{ss}} \right)

to obtain

g(2)(τ)=G(2)(τ)Rˉ2.g^{(2)}(\tau) = \frac{G^{(2)}(\tau)}{\bar R^2}.

These formulas assume Markovian reduced dynamics, the relevant regression conditions, a stationary state, vacuum input after coherent amplitudes are handled, and ideal output detection. Structured reservoirs, feedback, propagation delay, nonstationary driving, or coherent input interference require the larger model.

For a two-level emitter with

L^=Γ σ^−,\hat L=\sqrt{\Gamma}\,\hat\sigma_-,

a detected emission prepares the emitter in its ground state in the ideal model. Because

σ^−2=0,\hat\sigma_-^2=0,

the immediate second emission is forbidden and the ideal source has

g(2)(0)=0.g^{(2)}(0)=0.

Driving must repopulate the excited state before another photon can be emitted. The complete resonance-fluorescence shape and experimental qualification belong to the Antibunching page.

A value ∣g(1)∣≈1|g^{(1)}|\approx1 says the selected field samples have a stable normalized amplitude relation. It does not determine number statistics, state purity, absolute phase, or higher-order coherence.

A value g(2)≈1g^{(2)}\approx1 says there is little second-order excess or deficit under the declared averaging. It is compatible with ideal coherent light, phase-randomized Poisson light, some mixtures, large-number Fock states to limited precision, multimode thermal light with many modes, or a source whose features were washed out by background and timing response.

A peak with g(2)(0)>1g^{(2)}(0)>1 means detections cluster relative to the chosen baseline. Thermal Gaussian light gives a classical wave-fluctuation interpretation. Bunching by itself is not a nonclassicality witness.

A stationary dip satisfying

g(2)(0)<g(2)(τ)g^{(2)}(0)<g^{(2)}(\tau)

for some delay violates the classical stationary-intensity bound under the standard assumptions. The value g(2)(0)<1g^{(2)}(0)<1 is a particularly strong sub-Poissonian witness. Detector dead time and background correction must be controlled before either claim is made.

Two sources can share g(1)g^{(1)} and g(2)g^{(2)} while differing at third or higher order. Multiphoton contamination, non-Gaussian tails, and rare bright events can be invisible to low-order summaries. Match the measured order to the scientific claim.

Linewidth constrains first-order temporal coherence only after a line-shape and stationarity model are specified. It says nothing by itself about g(2)g^{(2)} or higher orders.

g(2)(0)g^{(2)}(0) can mean one spatial mode at equal time, a pulse-integrated factorial moment, two detector channels at zero electronic delay, or an extrapolated deconvolved value. Write the actual definition.

Replacing normal ordering with ordinary intensity products

Section titled “Replacing normal ordering with ordinary intensity products”

Photodetection factorial moments exclude self-pairing. Ordinary powers include commutator or shot-noise terms. The difference is essential near the single-photon level.

One second-order value cannot establish the infinite factorization hierarchy or identify a coherent state. Use phase-sensitive and higher-order measurements when the stronger claim matters.

Blinking, pair production, technical modulation, rare bursts, detector afterpulsing, and non-Gaussian states can all give g(2)>1g^{(2)}>1. The Siegert relation requires Gaussian chaotic statistics.

Jitter and binning average a correlation feature; they do not merely add an error bar. Compare a convolved physical model with raw data.

Using a stationary inequality on nonstationary data

Section titled “Using a stationary inequality on nonstationary data”

Drift, pulsed driving, and postselection can invalidate delay-translation arguments. Segment the data and state the ensemble before invoking classical bounds.

Confusing loss invariance with experimental immunity

Section titled “Confusing loss invariance with experimental immunity”

Uniform ideal loss cancels from normalized g(m)g^{(m)}, but reduces precision. Mode-dependent loss, background, saturation, dead time, and threshold coarse graining do not generally cancel.

  1. Define the field samples. State spatial, temporal, spectral, polarization, and detector-channel labels.
  2. Choose the order. Match G(1)G^{(1)}, G(2)G^{(2)}, or a higher function to interference, pair, or multiphoton information.
  3. Declare stationarity and gates. Separate continuous delay, pulse lag, and integrated pulse-mode definitions.
  4. Write the forward model. Include propagation, filtering, detector efficiency, background, timing response, and recovery.
  5. Estimate raw correlations. Preserve time tags and report the normalization and live-time treatment.
  6. Test robustness. Vary bins, windows, segmentation, and reasonable nuisance parameters.
  7. State only the supported inference. Distinguish first-order coherence, bunching, antibunching, sub-Poissonian statistics, and full state reconstruction.

Prove

∣G(1)(x1,x2)∣2≤I(x1)I(x2)\left| G^{(1)}(x_1,x_2) \right|^2 \le I(x_1)I(x_2)

and hence ∣g(1)∣≤1|g^{(1)}|\le1.

Solution

Define vectors in the Hilbert–Schmidt inner-product space by

∣vj)=E^(+)(xj)ρ.|v_j) = \hat E^{(+)}(x_j)\sqrt{\rho}.

Their inner product is

(v1∣v2)=Tr⁡[ρ E^(−)(x1)E^(+)(x2)ρ]=G(1)(x1,x2).\begin{aligned} (v_1|v_2) &= \operatorname{Tr} \left[ \sqrt{\rho}\, \hat E^{(-)}(x_1) \hat E^{(+)}(x_2) \sqrt{\rho} \right] \\ &= G^{(1)}(x_1,x_2). \end{aligned}

Their squared norms are

(vj∣vj)=I(xj).(v_j|v_j) = I(x_j).

Hilbert-space Cauchy–Schwarz therefore gives

∣G(1)(x1,x2)∣2≤I(x1)I(x2).|G^{(1)}(x_1,x_2)|^2 \le I(x_1)I(x_2).

Dividing by the positive denominator proves ∣g(1)∣≤1|g^{(1)}|\le1. Equality means the two detector-projected field vectors are linearly dependent in the state, which is the rank-one condition behind perfect normalized fringe contrast.

Two interferometer arms have

I2=4I1I_2=4I_1

and

∣g12(1)∣=0.90.|g_{12}^{(1)}|=0.90.

Find the fringe visibility. Would balancing the intensities change the intrinsic ∣g(1)∣|g^{(1)}|?

Solution

Use

V=2I1I2I1+I2∣g12(1)∣.\mathcal V = \frac{2\sqrt{I_1I_2}}{I_1+I_2} |g_{12}^{(1)}|.

Since I1I2=2I1\sqrt{I_1I_2}=2I_1,

V=4I15I1(0.90)=0.72.\begin{aligned} \mathcal V &= \frac{4I_1}{5I_1}(0.90) \\ &= 0.72. \end{aligned}

Balancing the detected intensities would raise the measured visibility to 0.900.90, but it would not change the intrinsic normalized mutual coherence if the balancing attenuation were uniform over the accepted modes. The original visibility was limited by both imbalance and imperfect coherence.

3. Higher-order correlations of a three-photon state

Section titled “3. Higher-order correlations of a three-photon state”

For the one-mode state ∣3⟩|3\rangle, calculate

g(2)(0),g(3)(0),g(4)(0).g^{(2)}(0), \qquad g^{(3)}(0), \qquad g^{(4)}(0).
Solution

For m≤nm\le n,

g∣n⟩(m)(0)=n!nm(n−m)!.g_{|n\rangle}^{(m)}(0) = \frac{n!}{n^m(n-m)!}.

Thus

g(2)(0)=3⋅232=23,g^{(2)}(0) = \frac{3\cdot2}{3^2} = \frac23,

and

g(3)(0)=3!33=29.g^{(3)}(0) = \frac{3!}{3^3} = \frac29.

Four annihilations acting on ∣3⟩|3\rangle give zero, so

g(4)(0)=0.g^{(4)}(0)=0.

The hierarchy records the finite occupation cutoff in a way that g(2)g^{(2)} alone cannot.

4. Thermal correlations and long-gate count noise

Section titled “4. Thermal correlations and long-gate count noise”

A stationary thermal field has

g(2)(τ)=1+e−2γ∣τ∣g^{(2)}(\tau) = 1+e^{-2\gamma|\tau|}

and mean ideal rate Rˉ\bar R. Derive the count Fano factor for a gate TT and its limit for γT≫1\gamma T\gg1.

Solution

Insert the excess correlation into

CT:=∫0Tdτ (T−τ)e−2γτ.\mathcal C_T := \int_0^T d\tau\, (T-\tau)e^{-2\gamma\tau}.

Then

Var⁡(NT)=RˉT+2Rˉ2CT.\operatorname{Var}(N_T) = \bar RT + 2\bar R^2\mathcal C_T.

For a=2γa=2\gamma,

∫0Tdτ (T−τ)e−aτ=Ta−1−e−aTa2.\int_0^T d\tau\, (T-\tau)e^{-a\tau} = \frac{T}{a} - \frac{1-e^{-aT}}{a^2}.

Because ⟨NT⟩=RˉT\langle N_T\rangle=\bar RT, the Fano factor is

FT=1+Rˉγ−Rˉ2γ2T(1−e−2γT).\begin{aligned} F_T ={}& 1+ \frac{\bar R}{\gamma} \\ &- \frac{\bar R} {2\gamma^2T} \left( 1-e^{-2\gamma T} \right). \end{aligned}

For γT≫1\gamma T\gg1,

FT⟶1+Rˉγ.F_T \longrightarrow 1+\frac{\bar R}{\gamma}.

The long gate contains many coherence intervals, but each interval contributes thermal excess noise. The normalized variance depends on the count rate per coherence time.

Three independent thermal modes have mean occupations

μ1=2,μ2=1,μ3=1.\mu_1=2, \qquad \mu_2=1, \qquad \mu_3=1.

Find MeffM_{\mathrm{eff}} and the summed zero-delay g(2)(0)g^{(2)}(0).

Solution

The total mean is 44, and the sum of squared modal means is

∑jμj2=4+1+1=6.\sum_j\mu_j^2 = 4+1+1 = 6.

Therefore

Meff=426=83.M_{\mathrm{eff}} = \frac{4^2}{6} = \frac83.

The correlation is

g(2)(0)=1+1Meff=1+38=118.\begin{aligned} g^{(2)}(0) &= 1+\frac1{M_{\mathrm{eff}}} \\ &= 1+\frac38 = \frac{11}{8}. \end{aligned}

The effective mode number need not be an integer because unequal modal weights interpolate continuously between equal-mode cases.

6. Classical bounds from intensity fluctuations

Section titled “6. Classical bounds from intensity fluctuations”

Let I(t)≥0I(t)\ge0 be a stationary classical random intensity. Prove both

g(2)(0)≥1g^{(2)}(0)\ge1

and

g(2)(τ)≤g(2)(0).g^{(2)}(\tau)\le g^{(2)}(0).
Solution

At equal time,

g(2)(0)−1=E[I2]−E[I]2E[I]2=Var⁡(I)E[I]2≥0.\begin{aligned} g^{(2)}(0)-1 &= \frac{ \mathbb E[I^2]-\mathbb E[I]^2 }{ \mathbb E[I]^2 } \\ &= \frac{\operatorname{Var}(I)} {\mathbb E[I]^2} \ge0. \end{aligned}

For separated times, Cauchy–Schwarz gives

∣E[I(t)I(t+τ)]∣2≤E[I(t)2]×E[I(t+τ)2].\begin{aligned} \left| \mathbb E[I(t)I(t+\tau)] \right|^2 \le{}& \mathbb E[I(t)^2] \\ &\times \mathbb E[I(t+\tau)^2]. \end{aligned}

Stationarity makes the two factors on the right equal. Since the intensities are nonnegative,

E[I(t)I(t+τ)]≤E[I2].\mathbb E[I(t)I(t+\tau)] \le \mathbb E[I^2].

Dividing by E[I]2\mathbb E[I]^2 proves the delay bound. A calibrated stationary record whose correlation rises away from zero cannot be represented by this classical random-intensity model.

A signal has

gs(2)(0)=0.20.g_{\mathrm s}^{(2)}(0)=0.20.

Independent Poisson background is present, and the signal fraction of the total mean rate is ρ=0.80\rho=0.80. Find the raw observed gobs(2)(0)g_{\mathrm{obs}}^{(2)}(0). Does uniform signal loss alone change the ideal signal correlation?

Solution

Use

gobs(2)(0)−1=ρ2[gs(2)(0)−1].g_{\mathrm{obs}}^{(2)}(0)-1 = \rho^2 \left[ g_{\mathrm s}^{(2)}(0)-1 \right].

Therefore

gobs(2)(0)=1+(0.80)2(0.20−1)=1−0.512=0.488.\begin{aligned} g_{\mathrm{obs}}^{(2)}(0) &= 1+(0.80)^2(0.20-1) \\ &= 1-0.512 \\ &= 0.488. \end{aligned}

The background substantially fills the dip. Uniform independent signal loss by itself multiplies the signal numerator and denominator by the same η2\eta^2 and leaves its ideal normalized g(2)g^{(2)} unchanged. In practice, loss lowers the signal fraction relative to fixed background and can indirectly worsen the raw value.

8. Immediate correlation after a two-level emission

Section titled “8. Immediate correlation after a two-level emission”

A Markovian two-level emitter has output coupling

L^=Γ σ^−.\hat L=\sqrt{\Gamma}\,\hat\sigma_-.

Use the conditional form of G(2)(0)G^{(2)}(0) to show that the ideal zero-delay correlation vanishes whenever the steady emission rate is nonzero.

Solution

At zero delay,

G(2)(0)=Tr⁡[L^†L^L^ρssL^†].G^{(2)}(0) = \operatorname{Tr} \left[ \hat L^\dagger\hat L \hat L\rho_{\mathrm{ss}}\hat L^\dagger \right].

By cyclicity of the trace,

G(2)(0)=Tr⁡[L^†L^†L^L^ρss].\begin{aligned} G^{(2)}(0) &= \operatorname{Tr} \left[ \hat L^\dagger\hat L^\dagger \hat L\hat L \rho_{\mathrm{ss}} \right]. \end{aligned}

For a two-level lowering operator,

L^2=Γσ^−2=0.\hat L^2 = \Gamma\hat\sigma_-^2 = 0.

Hence

G(2)(0)=0.G^{(2)}(0)=0.

If

Rˉ=Tr⁡(L^†L^ρss)>0,\bar R = \operatorname{Tr} \left( \hat L^\dagger\hat L\rho_{\mathrm{ss}} \right) >0,

then normalization gives

g(2)(0)=0.g^{(2)}(0)=0.

The result expresses the finite excitation capacity of one ideal two-level emitter. Background, timing averaging, multiple emitters, and detector artifacts raise the measured minimum.

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