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Coherent light is the electromagnetic realization of a bosonic coherent state. For one declared optical mode,

a^∣α⟩=α∣α⟩,α∈C.\hat a\lvert\alpha\rangle = \alpha\lvert\alpha\rangle, \qquad \alpha\in\mathbb C.

The complex amplitude α\alpha fixes the mean field relative to a phase reference, while

nˉ=⟨a^†a^⟩=∣α∣2\bar n = \langle\hat a^\dagger\hat a\rangle = \lvert\alpha\rvert^2

is the mean photon number in that mode. The state has Poisson number statistics, vacuum-level noise in every quadrature, and factorized normally ordered correlation functions. These properties make it the quantum state closest to an ideal deterministic classical wave.

“Coherent” has several meanings in optics. They must not be silently identified:

  • a coherent state is a specific quantum state ∣α⟩\lvert\alpha\rangle;
  • first-order coherence describes field-amplitude correlations and fringe visibility;
  • higher-order coherence describes factorization of photodetection correlations;
  • a laser is a driven, dissipative source whose output can approximate coherent light over specified modes and times.

A field may have excellent first-order coherence without being in a pure coherent state. Conversely, an ideal coherent pulse can be broadband. Spectral narrowness, phase stability, Poisson statistics, and coherent-state purity are related operational properties, not synonyms.

Required background. Quantized Electromagnetic Modes fixes field normalization, Photon Number States explains occupation statistics, Coherent States constructs displacement eigenstates, and Coherent States in Phase Space explains their phase-plane geometry.

A propagating laser beam has spatial, polarization, spectral, and temporal structure. A continuous output requires finite temporal packets or a continuum description; it cannot occupy one finite-energy mode for all time.

For a normalized mode ff, let

[a^f,a^f†]=1.[\hat a_f,\hat a_f^\dagger]=1.

Its coherent state satisfies

a^f∣αf⟩=αf∣αf⟩.\hat a_f\lvert\alpha_f\rangle = \alpha_f\lvert\alpha_f\rangle.

Equivalently,

∣αf⟩=D^f(αf)∣0f⟩,\lvert\alpha_f\rangle = \hat D_f(\alpha_f)\lvert0_f\rangle,

where

D^f(α)=exp⁡(αa^f†−α∗a^f).\hat D_f(\alpha) = \exp\left( \alpha\hat a_f^\dagger - \alpha^*\hat a_f \right).

The displacement operator translates the vacuum in phase space without changing its covariance matrix.

The coherent state expands as

∣α⟩=e−∣α∣2/2∑n=0∞αnn!∣n⟩.\lvert\alpha\rangle = e^{-\lvert\alpha\rvert^2/2} \sum_{n=0}^{\infty} \frac{\alpha^n}{\sqrt{n!}} \lvert n\rangle.

It is therefore not a state of definite photon number unless α=0\alpha=0, in which case it is the vacuum. The phase of α\alpha appears in the relative phases between neighboring number amplitudes:

α=nˉ eiϕ.\alpha = \sqrt{\bar n}\,e^{i\phi}.

Changing ϕ\phi rotates the state in optical phase space.

The overlap of two coherent states is

⟨β∣α⟩=exp⁡[−12∣β∣2−12∣α∣2+β∗α].\langle\beta\vert\alpha\rangle = \exp\left[ -\frac12\lvert\beta\rvert^2 -\frac12\lvert\alpha\rvert^2 +\beta^*\alpha \right].

Thus

∣⟨β∣α⟩∣2=e−∣α−β∣2.\lvert\langle\beta\vert\alpha\rangle\rvert^2 = e^{-\lvert\alpha-\beta\rvert^2}.

Distinct amplitudes are never exactly orthogonal at finite separation. This fact matters in optical communication, state discrimination, and the interpretation of a “classical amplitude alphabet.”

For a collection of orthonormal radiation modes labeled by μ\mu, a multimode coherent state is the simultaneous annihilation-operator eigenstate

a^μ∣{α}⟩=αμ∣{α}⟩\hat a_\mu \lvert\{\alpha\}\rangle = \alpha_\mu \lvert\{\alpha\}\rangle

for every μ\mu. It factorizes in that mode basis:

∣{α}⟩=⨂μ∣αμ⟩.\lvert\{\alpha\}\rangle = \bigotimes_\mu \lvert\alpha_\mu\rangle.

Equivalently,

∣{α}⟩=D^[α]∣0⟩,\lvert\{\alpha\}\rangle = \hat D[\alpha]\lvert0\rangle,

with

D^[α]=exp⁡[∑μ(αμa^μ†−αμ∗a^μ)].\hat D[\alpha] = \exp\left[ \sum_\mu \left( \alpha_\mu\hat a_\mu^\dagger - \alpha_\mu^*\hat a_\mu \right) \right].

The mean total photon number is

Nˉ=∑μ∣αμ∣2.\bar N = \sum_\mu\lvert\alpha_\mu\rvert^2.

For continuum-normalized modes, the sum becomes an integral and the amplitude must satisfy ∫∣αμ∣2dμ<∞\int|\alpha_\mu|^2d\mu<\infty for a normalizable Fock-space coherent vector with finite mean number. Finite energy also requires the distinct weighted condition ∫ℏωμ∣αμ∣2dμ<∞\int\hbar\omega_\mu|\alpha_\mu|^2d\mu<\infty. One condition does not imply the other without frequency-band assumptions.

Suppose a normalized packet mode is

a^f=∑μfμ∗a^μ,∑μ∣fμ∣2=1.\hat a_f = \sum_\mu f_\mu^*\hat a_\mu, \qquad \sum_\mu\lvert f_\mu\rvert^2=1.

A coherent state occupying only this packet mode has amplitudes

αμ=αfμ.\alpha_\mu = \alpha f_\mu.

Its total mean photon number is

∑μ∣αfμ∣2=∣α∣2.\sum_\mu \lvert\alpha f_\mu\rvert^2 = \lvert\alpha\rvert^2.

The packet envelope fμf_\mu determines where and when the pulse couples to an apparatus; α\alpha determines its overall complex amplitude.

If an experiment selects a different normalized mode gg, the measured coherent amplitude is the overlap projection

αg=⟨g∣f⟩α.\alpha_g = \langle g\vert f\rangle\alpha.

With all modes orthogonal to ff initially in vacuum, the selected quadrature sees the usual vacuum-loss channel of efficiency ∣⟨g∣f⟩∣2|\langle g|f\rangle|^2. If other modes contain light or noise, their projection must also be included. This is why local oscillator mode matching is part of a homodyne measurement, not a cosmetic alignment detail.

Write the positive-frequency electric-field operator as

E^(+)(x)=∑μEμ(x)a^μ,\hat{\mathbf E}^{(+)}(x) = \sum_\mu \boldsymbol{\mathcal E}_\mu(x) \hat a_\mu,

where x=(r,t)x=(\mathbf r,t) and the mode functions include the chosen normalization and free time dependence. In a multimode coherent state,

⟨E^(+)(x)⟩=∑μEμ(x)αμ.\langle \hat{\mathbf E}^{(+)}(x) \rangle = \sum_\mu \boldsymbol{\mathcal E}_\mu(x) \alpha_\mu.

Define

Ecl(+)(x)≡∑μEμ(x)αμ.\mathbf E_{\mathrm{cl}}^{(+)}(x) \equiv \sum_\mu \boldsymbol{\mathcal E}_\mu(x) \alpha_\mu.

Then

⟨E^(x)⟩=Ecl(+)(x)+Ecl(−)(x).\langle\hat{\mathbf E}(x)\rangle = \mathbf E_{\mathrm{cl}}^{(+)}(x) + \mathbf E_{\mathrm{cl}}^{(-)}(x).

Because expectation values respect the linear source-free Maxwell equations, this mean field evolves as a classical electromagnetic solution in a linear lossless medium. The quantum state also contains fluctuations that the mean field alone does not describe.

Choose the mode phase so that its local coefficient E0\mathcal E_0 is real and positive. For a one-mode field written as

E^(+)(t)=E0a^e−iωt,\hat E^{(+)}(t) = \mathcal E_0 \hat a e^{-i\omega t},

one has

⟨E^(t)⟩=2E0∣α∣cos⁡(ωt−ϕ),\langle\hat E(t)\rangle = 2\mathcal E_0 \lvert\alpha\rvert \cos\left( \omega t-\phi \right),

where ϕ=arg⁡α\phi=\arg\alpha. A different phase convention shifts the phase of the mode coefficient and α\alpha oppositely, leaving their product and the physical mean field unchanged.

The vacuum field scale E0\mathcal E_0 is fixed by mode normalization. Thus equal numerical values of α\alpha in two differently confined modes need not correspond to equal electric-field amplitudes.

Exact Poisson photon probabilities for coherent amplitude two and equal-width vacuum and displaced quadrature distributions

For real α=2\alpha=2, the upper panel shows the Poisson law with nˉ=4\bar n=4. The lower panel compares its XX distribution with vacuum: the mean shifts from 00 to 222\sqrt2, while both variances remain 1/21/2. The photon-number distribution changes under displacement; the quadrature width does not. The probability beyond the plotted photon numbers is small but nonzero.

Taking the modulus squared of the number-basis coefficients gives

P(n)=e−nˉnˉnn!,nˉ=∣α∣2.P(n) = e^{-\bar n} \frac{\bar n^n}{n!}, \qquad \bar n=\lvert\alpha\rvert^2.

This is a Poisson distribution. Its mean and variance are

⟨N^⟩=nˉ,(ΔN)2=nˉ.\langle\hat N\rangle=\bar n, \qquad (\Delta N)^2=\bar n.

Therefore

F=(ΔN)2⟨N^⟩=1,F = \frac{(\Delta N)^2}{\langle\hat N\rangle} = 1,

and the Mandel parameter is

Q=F−1=0.Q=F-1=0.

Poisson statistics lie between sub-Poissonian number squeezing and super-Poissonian excess noise. They do not mean “no noise.” The standard deviation is

ΔN=nˉ.\Delta N=\sqrt{\bar n}.

Only the relative number noise decreases:

ΔNnˉ=1nˉ.\frac{\Delta N}{\bar n} = \frac{1}{\sqrt{\bar n}}.

Because ∣α⟩\lvert\alpha\rangle is an annihilation-operator eigenstate,

⟨(a^†)ma^m⟩=∣α∣2m=nˉm.\left\langle (\hat a^\dagger)^m\hat a^m \right\rangle = \lvert\alpha\rvert^{2m} = \bar n^m.

Equivalently,

⟨N^(N^−1)⋯(N^−m+1)⟩=nˉm.\left\langle \hat N(\hat N-1)\cdots(\hat N-m+1) \right\rangle = \bar n^m.

Every normalized equal-mode correlation is therefore

g(m)(0)=1g^{(m)}(0)=1

where the normalization is defined and nˉ>0\bar n>0. In particular,

g(2)(0)=1.g^{(2)}(0)=1.

This is neither bunching nor antibunching. It is the correlation value of a Poisson process in the ideal single-mode model.

For ideal direct detection of a coherent mode during a gate that contains mean photon number nˉ\bar n, the count distribution is Poisson:

P(K=k)=e−nˉnˉkk!.P(K=k) = e^{-\bar n} \frac{\bar n^k}{k!}.

Independent detection efficiency η\eta thins a Poisson process into another Poisson process:

Pη(K=k)=e−ηnˉ(ηnˉ)kk!.P_\eta(K=k) = e^{-\eta\bar n} \frac{ (\eta\bar n)^k }{ k! }.

For an ideal on–off detector,

P(no click)=e−ηnˉ,P(\text{no click}) = e^{-\eta\bar n}, P(click)=1−e−ηnˉ.P(\text{click}) = 1-e^{-\eta\bar n}.

Technical intensity fluctuations, detector dead time, and saturation can spoil this law. Independent Poisson background counts instead preserve a Poisson distribution while shifting its mean; Poisson counting alone cannot separate that background from the signal. Summing deterministic independent coherent modes also remains Poisson.

Glauber photodetection theory uses normally ordered correlation functions. For mm detections,

G(m)(x1,…,xm;ym,…,y1)=⟨E^(−)(x1)⋯E^(−)(xm)×E^(+)(ym)⋯E^(+)(y1)⟩.G^{(m)} \left( x_1,\ldots,x_m; y_m,\ldots,y_1 \right) = \left\langle \hat E^{(-)}(x_1)\cdots \hat E^{(-)}(x_m) {}\times \hat E^{(+)}(y_m)\cdots \hat E^{(+)}(y_1) \right\rangle.

For a coherent state, each positive-frequency field operator acts by its classical eigenvalue. Therefore

G(m)=∏j=1mEcl(−)(xj)×∏j=1mEcl(+)(yj).G^{(m)} ={} \prod_{j=1}^{m} E_{\mathrm{cl}}^{(-)}(x_j) \times \prod_{j=1}^{m} E_{\mathrm{cl}}^{(+)}(y_j).

All normally ordered correlations factorize. This is the precise sense in which an ideal coherent state is fully coherent in Glauber’s hierarchy.

The first-order function is

G(1)(x,y)=⟨E^(−)(x)E^(+)(y)⟩.G^{(1)}(x,y) = \left\langle \hat E^{(-)}(x) \hat E^{(+)}(y) \right\rangle.

For coherent light,

G(1)(x,y)=Ecl(−)(x)Ecl(+)(y).G^{(1)}(x,y) = E_{\mathrm{cl}}^{(-)}(x) E_{\mathrm{cl}}^{(+)}(y).

This rank-one factorization gives ideal fringe visibility when the two sampled fields have matched polarization and intensity.

First-order coherence alone does not identify a coherent state. For example, a stationary one-mode number state can have perfect normalized first-order coherence while exhibiting

g(2)(0)=1−1n.g^{(2)}(0)=1-\frac1n.

The hierarchy matters.

For one stationary mode,

g(2)(τ)=⟨a^†(t)a^†(t+τ)a^(t+τ)a^(t)⟩⟨N^(t)⟩⟨N^(t+τ)⟩.g^{(2)}(\tau) = \frac{ \left\langle \hat a^\dagger(t) \hat a^\dagger(t+\tau) \hat a(t+\tau) \hat a(t) \right\rangle }{ \langle\hat N(t)\rangle \langle\hat N(t+\tau)\rangle }.

An ideal coherent state under linear harmonic evolution gives

g(2)(τ)=1g^{(2)}(\tau)=1

for every delay. A measured value near one is consistent with coherent light, but it is not sufficient evidence: many noncoherent states and noisy mixtures can share the same second-order value.

Adopt the dimensionless quadratures

X^=a^+a^†2,P^=a^−a^†i2.\hat X = \frac{ \hat a+\hat a^\dagger }{ \sqrt2 }, \qquad \hat P = \frac{ \hat a-\hat a^\dagger }{ i\sqrt2 }.

They satisfy

[X^,P^]=i.[\hat X,\hat P]=i.

In ∣α⟩\lvert\alpha\rangle,

⟨X^⟩=2 Re⁡α,\langle\hat X\rangle = \sqrt2\,\operatorname{Re}\alpha, ⟨P^⟩=2 Im⁡α.\langle\hat P\rangle = \sqrt2\,\operatorname{Im}\alpha.

The variances are

(ΔX)2=(ΔP)2=12,(\Delta X)^2 = (\Delta P)^2 = \frac12,

so

ΔX ΔP=12.\Delta X\,\Delta P = \frac12.

These are the vacuum variances in this convention. Some texts define quadratures with an extra factor of 2\sqrt2 or 22, changing every displayed variance. A quoted “shot-noise unit” is incomplete without the normalization.

The phase-referenced quadrature

X^θ=a^e−iθ+a^†eiθ2\hat X_\theta = \frac{ \hat a e^{-i\theta} + \hat a^\dagger e^{i\theta} }{ \sqrt2 }

has mean

⟨X^θ⟩=2 Re⁡(αe−iθ),\langle\hat X_\theta\rangle = \sqrt2\, \operatorname{Re} \left( \alpha e^{-i\theta} \right),

and variance

(ΔXθ)2=12(\Delta X_\theta)^2 = \frac12

for every θ\theta. The uncertainty disk is translated but not squeezed.

At the optimal phase, θ=arg⁡α\theta=\arg\alpha, the mean-to-noise ratio is

∣⟨Xθ⟩∣ΔXθ=2∣α∣=2nˉ.\frac{ \lvert\langle X_\theta\rangle\rvert }{ \Delta X_\theta } = 2\lvert\alpha\rvert = 2\sqrt{\bar n}.

The absolute quadrature noise remains fixed while the signal grows.

With complex phase-space coordinate β\beta, the one-mode Wigner function is

Wα(β)=2πexp⁡[−2∣β−α∣2].W_\alpha(\beta) = \frac{2}{\pi} \exp\left[ -2\lvert\beta-\alpha\rvert^2 \right].

It is a positive Gaussian centered at α\alpha with the same width as the vacuum. Positivity here is consistent with the coherent state lying at the classical boundary of the Glauber–Sudarshan description. The state remains fully quantum: it has irreducible noise, nonorthogonal alternatives, and measurement backaction.

Write

α=nˉ eiϕ.\alpha = \sqrt{\bar n}\,e^{i\phi}.

The angle ϕ\phi determines the mean field relative to a clock or local oscillator. Under an optical phase shift,

U^(ϑ)=e−iϑN^,\hat U(\vartheta) = e^{-i\vartheta\hat N},

the state transforms as

U^(ϑ)∣α⟩=∣αe−iϑ⟩.\hat U(\vartheta) \lvert\alpha\rangle = \lvert \alpha e^{-i\vartheta} \rangle.

Absolute phase is not read without a reference. Interference, homodyne, and heterodyne measurements compare the signal with another path or mode whose phase defines the coordinate system.

Unknown phase is a mixed-state description

Section titled “Unknown phase is a mixed-state description”

If the phase is uniformly unknown relative to the available reference frame, the appropriate phase-averaged state is

ρav=∫02πdϕ2π∣nˉeiϕ⟩⟨nˉeiϕ∣.\rho_{\mathrm{av}} = \int_0^{2\pi} \frac{d\phi}{2\pi} \lvert \sqrt{\bar n}e^{i\phi} \rangle \langle \sqrt{\bar n}e^{i\phi} \rvert.

Expanding in number states gives

ρav=e−nˉ∑n=0∞nˉnn!∣n⟩⟨n∣.\rho_{\mathrm{av}} = e^{-\bar n} \sum_{n=0}^{\infty} \frac{\bar n^n}{n!} \lvert n\rangle\langle n\rvert.

All off-diagonal number coherences vanish, and

Tr⁡(ρava^)=0.\operatorname{Tr} \left( \rho_{\mathrm{av}}\hat a \right) = 0.

Nevertheless,

⟨(a^†)ma^m⟩av=nˉm.\left\langle (\hat a^\dagger)^m\hat a^m \right\rangle_{\mathrm{av}} = \bar n^m.

Direct photon counting cannot distinguish this state from a pure coherent state of known amplitude and phase because both have the same Poisson number distribution. A phase-sensitive comparison with an external reference can.

Shared unknown phase is not independent random phase

Section titled “Shared unknown phase is not independent random phase”

Suppose several temporal packets are drawn from one phase-stable laser during a time shorter than its coherence time. A useful joint model is

ρshared=∫02πdϕ2π⨂j∣αjeiϕ⟩⟨αjeiϕ∣.\rho_{\mathrm{shared}} = \int_0^{2\pi} \frac{d\phi}{2\pi} \bigotimes_j \lvert \alpha_j e^{i\phi} \rangle \langle \alpha_j e^{i\phi} \rvert.

All packets share the same unknown phase. This state is not

⨂j[∫02πdϕj2π∣αjeiϕj⟩⟨αjeiϕj∣],\bigotimes_j \left[ \int_0^{2\pi} \frac{d\phi_j}{2\pi} \lvert \alpha_j e^{i\phi_j} \rangle \langle \alpha_j e^{i\phi_j} \rvert \right],

which assigns independent random phases to every packet. The first model retains relative phase coherence and predicts interference between packets; the second generally does not.

This distinction resolves many apparently contradictory claims about whether a free-running laser “really” emits a coherent state. The density operator depends on the chosen subsystem, reference frame, conditioning information, and time interval. Operational predictions, not a preferred ensemble decomposition, are decisive.

Let a passive interferometer transform annihilation operators as

b^j=∑kUjka^k,U†U=I.\hat b_j = \sum_k U_{jk}\hat a_k, \qquad U^\dagger U=I.

A product coherent input remains a product coherent output:

⨂k∣αk⟩⟼⨂j∣βj⟩,\bigotimes_k \lvert\alpha_k\rangle \longmapsto \bigotimes_j \lvert\beta_j\rangle,

where

βj=∑kUjkαk.\beta_j = \sum_k U_{jk}\alpha_k.

Thus passive linear optics acts on coherent amplitudes exactly as classical wave optics acts on complex field amplitudes.

For one common beam-splitter convention,

c^=ta^+rb^,d^=−r∗a^+t∗b^,\begin{aligned} \hat c &= t\hat a+r\hat b, \\ \hat d &= -r^*\hat a+t^*\hat b, \end{aligned}

with

∣t∣2+∣r∣2=1.\lvert t\rvert^2+\lvert r\rvert^2=1.

Then

∣α⟩a∣β⟩b⟼∣tα+rβ⟩c∣−r∗α+t∗β⟩d.\lvert\alpha\rangle_a \lvert\beta\rangle_b \longmapsto \lvert t\alpha+r\beta \rangle_c \lvert -r^*\alpha+t^*\beta \rangle_d.

No entanglement is generated between the outputs from product coherent inputs. This exceptional property is one reason coherent states are treated as classical optical inputs.

Model attenuation as a beam splitter coupling the signal to an environmental vacuum mode:

∣α⟩S∣0⟩E⟼∣η α⟩S∣1−η α⟩E.\lvert\alpha\rangle_S\lvert0\rangle_E \longmapsto \lvert\sqrt\eta\,\alpha\rangle_S \lvert\sqrt{1-\eta}\,\alpha\rangle_E.

After tracing out the environment,

ρS′=∣η α⟩⟨η α∣.\rho_S' = \lvert\sqrt\eta\,\alpha\rangle \langle\sqrt\eta\,\alpha\rvert.

An ideal coherent state remains pure and coherent under vacuum loss. Its mean photon number changes from nˉ\bar n to ηnˉ\eta\bar n, while its quadrature variance remains the vacuum value.

This stability is not generic. Number states become mixtures under loss, squeezed states lose squeezing, and phase-insensitive amplification must add noise.

A classical current or strong external drive couples linearly to a bosonic mode. In a rotating frame, a common driven damped-mode equation is

dαdt=−(κ2+iΔ)α+ε(t),\frac{d\alpha}{dt} = -\left( \frac{\kappa}{2}+i\Delta \right)\alpha + \varepsilon(t),

where κ>0\kappa>0 is the energy-decay rate, Δ=ωc−ωdrive\Delta=\omega_c-\omega_{\rm drive}, and ε\varepsilon has units of inverse time for dimensionless α\alpha.

For constant drive,

αss=εκ/2+iΔ.\alpha_{\mathrm{ss}} = \frac{ \varepsilon }{ \kappa/2+i\Delta }.

A linear oscillator driven coherently and coupled to a vacuum Markovian bath relaxes toward a coherent state. An initially coherent state follows the classical amplitude equation and retains vacuum covariance throughout. For a general initial state, excess noise and non-Gaussian structure can persist during the transient even though they decay asymptotically.

Nonlinearity changes this conclusion. Kerr interactions, saturation, parametric pair creation, and coupling to a saturable quantum emitter can shear, squeeze, antibunch, or entangle the field. Strong passive coupling between linear oscillators alone still preserves product coherent states. A nonzero mean amplitude does not guarantee a coherent state.

Coherent states make the classical limit transparent because their mean field is a classical solution and their relative fluctuations shrink with occupation.

For photon number,

ΔN⟨N⟩=1nˉ.\frac{\Delta N}{\langle N\rangle} = \frac1{\sqrt{\bar n}}.

For an optimally phased quadrature,

ΔXϕ∣⟨Xϕ⟩∣=12nˉ.\frac{ \Delta X_\phi }{ \lvert\langle X_\phi\rangle\rvert } = \frac1{2\sqrt{\bar n}}.

Therefore a large-amplitude coherent field supports deterministic classical predictions for coarse relative observables.

Fixed classical field as Planck’s constant changes

Section titled “Fixed classical field as Planck’s constant changes”

The single-photon electric-field scale behaves schematically as

E0∝ℏω.\mathcal E_0 \propto \sqrt{\hbar\omega}.

To hold a macroscopic classical field amplitude fixed while taking ℏ→0\hbar\to0, the coherent amplitude must scale as

∣α∣∝ℏ−1/2.\lvert\alpha\rvert \propto \hbar^{-1/2}.

Then

nˉ=∣α∣2∝ℏ−1.\bar n=\lvert\alpha\rvert^2 \propto \hbar^{-1}.

The classical limit is therefore a correlated scaling, not the statement that a fixed low-occupation state becomes classical merely by naming its mean field.

Even at large nˉ\bar n:

  • the quadrature variance does not vanish in absolute oscillator units;
  • coherent states with nearby amplitudes are nonorthogonal;
  • shot noise remains in finite measurements;
  • phase and amplitude are estimated relative to physical references;
  • nonlinear interactions can convert small fluctuations into visible nonclassical effects.

Classical electromagnetism emerges for selected observables and accuracy requirements. The underlying state does not stop obeying quantum mechanics.

The Glauber–Sudarshan representation writes a state as

ρ=∫d2α P(α)∣α⟩⟨α∣.\rho = \int d^2\alpha\, P(\alpha) \lvert\alpha\rangle\langle\alpha\rvert.

A coherent state has

P(β)=δ(2)(β−α).P(\beta) = \delta^{(2)}(\beta-\alpha).

It is therefore an extremal point of the set of states with a nonnegative classical PP probability measure; delta measures are allowed. Statistical mixtures with positive PP represent classical random amplitudes followed by quantum-limited photodetection.

This criterion is operationally powerful but representation specific. “Classical” here does not mean that the density operator can be replaced by a point in classical phase space for every purpose. It means its normally ordered moments admit a positive stochastic-amplitude model.

An ideal coherent state is a foundational model for laser-like light, but a real laser is an open, pumped, nonlinear device with spontaneous emission, gain saturation, output coupling, technical noise, and finite bandwidth. Whether its output is accurately described by ∣α⟩\lvert\alpha\rangle depends on the subsystem and timescale.

Well above threshold, gain saturation can stabilize the intracavity amplitude. A semiclassical description then has approximately fixed ∣α∣\lvert\alpha\rvert and an oscillating field. Quantum noise continuously perturbs both amplitude and phase.

Amplitude fluctuations are often damped back toward the steady value. Phase has no corresponding restoring force in a free-running laser with continuous phase symmetry, so it diffuses. The resulting finite coherence time produces a finite laser linewidth.

A free-running laser’s phase can diffuse even when gain saturation keeps its amplitude close to a steady value. That makes a coherent-state description conditional on mode, reference, and timescale. Linewidth and Coherence is the derivation of the stochastic phase equation, first-order coherence, Lorentzian Fourier pair, Schawlow–Townes scale, technical frequency noise, and linewidth measurement.

The conclusion needed here is qualitative: over delays short compared with the phase-diffusion time, phase-conditioned coherent wave packets can be an excellent model; over long unreferenced records, averaging over the diffusing phase becomes appropriate.

A continuous beam cannot be assigned one finite-energy amplitude α\alpha for all time. One may instead use:

  • finite temporal wave-packet modes;
  • a photon flux with units of inverse time;
  • input–output field operators satisfying delta-function commutators;
  • correlation functions over detector times.

For a constant-flux coherent beam whose envelope is flat over [0,T][0,T], the matched normalized temporal mode has nˉT=ΦT\bar n_T=\Phi T. With phase noise, ΦT\Phi T is still the total mean photon count in the interval, but need not occupy one fixed mode.

For example, in a carrier-rotating frame let ⟨b†(t)b(s)⟩=Φe−Dϕ∣t−s∣\langle b^\dagger(t)b(s)\rangle=\Phi e^{-D_\phi|t-s|} and aT=T−1/2∫0Tb(t)dta_T=T^{-1/2}\int_0^T b(t)dt. Then

⟨aT†aT⟩=2ΦTDϕ2[DϕT−1+e−DϕT].\langle a_T^\dagger a_T\rangle =\frac{2\Phi}{T D_\phi^2} \left[D_\phi T-1+e^{-D_\phi T}\right].

For DϕT≪1D_\phi T\ll1 this approaches ΦT\Phi T. For long bins it approaches 2Φ/Dϕ2\Phi/D_\phi; the remaining photons occupy orthogonal temporal modes. Thus averaging many short packets over a long record differs from treating one long, internally phase-diffusing packet as a single coherent mode.

Real laser output may differ from an ideal coherent state through:

  • excess intensity noise, especially near threshold or at low Fourier frequencies;
  • phase diffusion and technical frequency noise;
  • relaxation oscillations;
  • multimode competition;
  • polarization fluctuations;
  • amplified spontaneous emission;
  • non-Gaussian noise or intermittent mode hops;
  • imperfect spatial mode quality;
  • correlations introduced by stabilization loops and measurement.

Saying “laser light is coherent” is therefore a controlled approximation, not an exact universal theorem.

A Poisson histogram or g(2)=1g^{(2)}=1 alone does not identify a coherent state. Measurements answer complementary questions:

Property Representative measurement
mean field and phase interference or homodyne detection
first-order coherence delayed interferometry or spectrum
photon statistics number-resolved counting or calibrated click data
second-order coherence Hanbury Brown–Twiss measurement
quadrature covariance balanced homodyne detection
modal structure spatial, spectral, and temporal mode analysis
higher-order structure higher correlations or state tomography

Evidence consistent with an ideal coherent state includes:

g(m)≈1g^{(m)}\approx1

over the tested orders and delays,

Q≈0,Q\approx0,

vacuum-level quadrature variance in every phase, and a stable displacement after accounting for phase diffusion.

Within a trusted single-mode model, calibrated quadrature means and variances give a stronger exact statement. Put α=(⟨X⟩+i⟨P⟩)/2\alpha=(\langle X\rangle+i\langle P\rangle)/\sqrt2. The mean number after removing this displacement is

nˉres=Var⁡X+Var⁡P−12,⟨α∣ρ∣α⟩≥1−nˉres.\bar n_{\rm res}=\frac{\operatorname{Var}X+\operatorname{Var}P-1}{2}, \qquad \langle\alpha|\rho|\alpha\rangle\ge1-\bar n_{\rm res}.

The inequality follows from I−∣0⟩⟨0∣≤NI-|0\rangle\langle0|\le N in the displaced state. Exact vacuum variances in both conjugate quadratures force nˉres=0\bar n_{\rm res}=0 and hence the pure coherent state. Finite sampling, mode selection, phase-reference error, and calibration uncertainty must be included in a practical lower bound.

Each statement is bandwidth and mode dependent. Detector dark noise can mask sub-Poissonian statistics; classical technical noise can produce super-Poissonian counts; a narrow electronic analysis band can miss noise elsewhere.

Worked Example: A Dark Interferometer Port

Section titled “Worked Example: A Dark Interferometer Port”

Send coherent states into a balanced beam splitter with convention

c^=a^+b^2,d^=a^−b^2.\hat c = \frac{ \hat a+\hat b }{ \sqrt2 }, \qquad \hat d = \frac{ \hat a-\hat b }{ \sqrt2 }.

If

αa=αb=α,\alpha_a=\alpha_b=\alpha,

then the output amplitudes are

αc=2 α,αd=0.\alpha_c=\sqrt2\,\alpha, \qquad \alpha_d=0.

Thus

∣α⟩a∣α⟩b⟼∣2 α⟩c∣0⟩d.\lvert\alpha\rangle_a \lvert\alpha\rangle_b \longmapsto \lvert\sqrt2\,\alpha\rangle_c \lvert0\rangle_d.

The destructive-interference port is exactly vacuum in the ideal model, not a coherent state containing photons that later cancel at the detector. Relative phase error, amplitude or mode mismatch, unequal arm attenuation, and added light can populate the dark port. Equal pure loss in both arms reduces the bright output but leaves the ideally balanced dark output in vacuum; loss applied after the dark port also leaves vacuum unchanged.

Interferometers develops phase-estimation limits for coherent inputs. Phase-Space Distributions compares the delta PP measure, Wigner Gaussian, and heterodyne QQ density.

1. Separate finite photon number from finite energy

Section titled “1. Separate finite photon number from finite energy”

In a frequency-normalized channel, suppose ∣α(ω)∣2=A/ω2|\alpha(\omega)|^2=A/\omega^2 for ω≥ω0>0\omega\ge\omega_0>0 and zero otherwise. Calculate the mean number and ask whether the mean energy is finite. What physical condition removes the problem?

Solution

The mean number is ∫ω0∞Aω−2dω=A/ω0\int_{\omega_0}^\infty A\omega^{-2}d\omega=A/\omega_0. The energy is ℏA∫ω0∞ω−1dω\hbar A\int_{\omega_0}^\infty\omega^{-1}d\omega, which diverges logarithmically. The coherent vector is normalizable but has infinite mean free energy. A high-frequency cutoff, or sufficiently faster spectral decay, makes it a finite-energy pulse. Physical source bandwidth must be specified when applying continuum formulas.

Show that an ideal coherent state has

g(m)(0)=1g^{(m)}(0)=1

for every positive integer mm and nonzero α\alpha.

Solution

Repeated annihilation gives

a^m∣α⟩=αm∣α⟩.\hat a^m\lvert\alpha\rangle = \alpha^m\lvert\alpha\rangle.

Taking the adjoint relation on the bra,

⟨α∣(a^†)m=(α∗)m⟨α∣.\langle\alpha\vert (\hat a^\dagger)^m = (\alpha^*)^m \langle\alpha\vert.

Therefore

⟨(a^†)ma^m⟩=∣α∣2m.\left\langle (\hat a^\dagger)^m\hat a^m \right\rangle = \lvert\alpha\rvert^{2m}.

Since

⟨a^†a^⟩m=∣α∣2m,\langle\hat a^\dagger\hat a\rangle^m = \lvert\alpha\rvert^{2m},

the normalized correlation is

g(m)(0)=⟨(a^†)ma^m⟩⟨a^†a^⟩m=1.g^{(m)}(0) = \frac{ \langle(\hat a^\dagger)^m\hat a^m\rangle }{ \langle\hat a^\dagger\hat a\rangle^m } = 1.

At α=0\alpha=0, both numerator and denominator vanish, so this normalized expression is undefined even though the vacuum is a coherent state.

A coherent state ∣α⟩\lvert\alpha\rangle and vacuum enter a beam splitter with amplitude transmissivity tt and reflectivity rr. Show that the output is

∣tα⟩∣−r∗α⟩\lvert t\alpha\rangle \lvert-r^*\alpha\rangle

for the convention on this page. Are the output count records statistically independent in the ideal state?

Solution

The input amplitudes are the vector

(α0).\begin{pmatrix} \alpha\\ 0 \end{pmatrix}.

Applying the mode transformation gives

(βcβd)=(tr−r∗t∗)(α0)=(tα−r∗α).\begin{pmatrix} \beta_c\\ \beta_d \end{pmatrix} = \begin{pmatrix} t&r\\ -r^*&t^* \end{pmatrix} \begin{pmatrix} \alpha\\ 0 \end{pmatrix} = \begin{pmatrix} t\alpha\\ -r^*\alpha \end{pmatrix}.

A passive linear transformation maps a multimode coherent state to the coherent state with transformed amplitudes, so

∣α⟩a∣0⟩b⟼∣tα⟩c∣−r∗α⟩d.\lvert\alpha\rangle_a\lvert0\rangle_b \longmapsto \lvert t\alpha\rangle_c \lvert-r^*\alpha\rangle_d.

This is a product state. Ideal direct counts in the two output modes are independent Poisson variables with means

∣t∣2∣α∣2\lvert t\rvert^2\lvert\alpha\rvert^2

and

∣r∣2∣α∣2.\lvert r\rvert^2\lvert\alpha\rvert^2.

Conditioning on a fixed total count would introduce anticorrelation in the conditioned data, but the unconditional coherent-output counts factorize.

Evaluate

ρav=∫02πdϕ2π∣μeiϕ⟩⟨μeiϕ∣\rho_{\mathrm{av}} = \int_0^{2\pi} \frac{d\phi}{2\pi} \lvert \sqrt\mu e^{i\phi} \rangle \langle \sqrt\mu e^{i\phi} \rvert

in the number basis. Find ⟨a⟩\langle a\rangle and g(2)(0)g^{(2)}(0).

Solution

Expand the ket and bra:

ρav=e−μ∑m,n=0∞μ(m+n)/2m!n!×[∫02πdϕ2πei(m−n)ϕ]∣m⟩⟨n∣.\rho_{\mathrm{av}} ={} e^{-\mu} \sum_{m,n=0}^{\infty} \frac{ \mu^{(m+n)/2} }{ \sqrt{m!n!} } \times \left[ \int_0^{2\pi} \frac{d\phi}{2\pi} e^{i(m-n)\phi} \right] \lvert m\rangle\langle n\rvert.

The phase integral is δmn\delta_{mn}, so

ρav=e−μ∑n=0∞μnn!∣n⟩⟨n∣.\rho_{\mathrm{av}} = e^{-\mu} \sum_{n=0}^{\infty} \frac{\mu^n}{n!} \lvert n\rangle\langle n\rvert.

Because the state is number diagonal,

⟨a⟩=0.\langle a\rangle=0.

Its number distribution is Poisson, so

⟨N(N−1)⟩=μ2,⟨N⟩=μ.\langle N(N-1)\rangle=\mu^2, \qquad \langle N\rangle=\mu.

Therefore

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

for μ>0\mu>0. Direct counting cannot reveal the removed absolute phase coherence.

5. Bound fidelity using residual fluctuations

Section titled “5. Bound fidelity using residual fluctuations”

Calibrated measurements of one mode give arbitrary means and Var⁡X=0.53\operatorname{Var}X=0.53, Var⁡P=0.55\operatorname{Var}P=0.55, with [X,P]=i[X,P]=i. Ignoring statistical error for this exercise, lower-bound the overlap with the coherent state having those means. Is Gaussianity required?

Solution

After removing the measured displacement, nˉres=(0.53+0.55−1)/2=0.04\bar n_{\rm res}=(0.53+0.55-1)/2=0.04. Every nonvacuum component has at least one photon, so its total probability is at most 0.040.04. Therefore ⟨α∣ρ∣α⟩≥0.96\langle\alpha|\rho|\alpha\rangle\ge0.96. This argument uses number positivity and does not assume a Gaussian state. Experimental uncertainty would weaken the bound through an upper bound on the residual occupation.

Solve

dαdt=−(κ2+iΔ)α+ε\frac{d\alpha}{dt} = -\left( \frac{\kappa}{2}+i\Delta \right)\alpha + \varepsilon

for constant ε\varepsilon and initial amplitude α(0)=α0\alpha(0)=\alpha_0.

Solution

Define

γ=κ2+iΔ.\gamma = \frac{\kappa}{2}+i\Delta.

The steady amplitude is

αss=εγ.\alpha_{\mathrm{ss}} = \frac{\varepsilon}{\gamma}.

Subtracting the steady solution gives

ddt(α−αss)=−γ(α−αss).\frac{d}{dt} \left( \alpha-\alpha_{\mathrm{ss}} \right) = -\gamma \left( \alpha-\alpha_{\mathrm{ss}} \right).

Therefore

α(t)=αss+(α0−αss)e−γt.\alpha(t) = \alpha_{\mathrm{ss}} + \left( \alpha_0-\alpha_{\mathrm{ss}} \right) e^{-\gamma t}.

Explicitly,

α(t)=εκ/2+iΔ+[α0−εκ/2+iΔ]×e−(κ/2+iΔ)t.\alpha(t) ={} \frac{ \varepsilon }{ \kappa/2+i\Delta } + \left[ \alpha_0 - \frac{ \varepsilon }{ \kappa/2+i\Delta } \right] \times e^{-(\kappa/2+i\Delta)t}.

For a linear mode coupled to vacuum, an initial coherent state follows this amplitude trajectory while retaining vacuum quadrature covariance.

7. Count photons in a phase-diffusing temporal mode

Section titled “7. Count photons in a phase-diffusing temporal mode”

Derive the flat-mode occupation given above from ⟨b†(t)b(s)⟩=Φe−Dϕ∣t−s∣\langle b^\dagger(t)b(s)\rangle=\Phi e^{-D_\phi|t-s|}. At DϕT=2D_\phi T=2, what fraction of the interval’s mean photons occupies that one fixed mode?

Solution

Integrating the two triangular halves of the time square gives

⟨aT†aT⟩=2ΦT∫0T(T−τ)e−Dϕτdτ=2ΦTDϕ2(DϕT−1+e−DϕT).\langle a_T^\dagger a_T\rangle =\frac{2\Phi}{T}\int_0^T(T-\tau)e^{-D_\phi\tau}d\tau =\frac{2\Phi}{T D_\phi^2}(D_\phi T-1+e^{-D_\phi T}).

Dividing by ΦT\Phi T at DϕT=2D_\phi T=2 gives (1+e−2)/2≃0.568(1+e^{-2})/2\simeq0.568. Total direct counts still have mean ΦT\Phi T; a fixed flat-mode projection collects only about 57%57\%. Tracking the actual stochastic phase changes the selected mode and the conditioning information, so it is a different measurement.

A source has g(2)(0)=1.00±0.02g^{(2)}(0)=1.00\pm0.02, a narrow optical spectrum, and substantial excess amplitude noise below 10 kHz10\ \mathrm{kHz}. Which claims are supported?

  1. The field is an exact pure coherent state.
  2. The tested second-order statistics are consistent with coherent light.
  3. The source is shot-noise limited at every Fourier frequency.
  4. The field may still be a useful coherent-state approximation in a higher analysis band.
Solution

Claim 1 is not supported. One second-order number does not determine a density operator, and the measured excess noise already shows a departure in part of the spectrum.

Claim 2 is supported within the detector bandwidth, mode, delay bin, and uncertainty used for the g(2)g^{(2)} measurement.

Claim 3 is false. The stated low-frequency amplitude noise exceeds the coherent-state level. A spectrum-integrated or bandwidth-resolved noise measurement is required.

Claim 4 may be true. If technical noise is confined below 10 kHz10\ \mathrm{kHz}, the field can approximate a displaced vacuum in a higher analysis band, provided phase noise, modal purity, detector calibration, and other quadratures are also controlled. The approximation must be stated with that bandwidth.