Skip to content

Line Shapes and Broadening

An ideal transition has a definite frequency

ω0=Eu−Elℏ,\omega_0 = \frac{E_u-E_l}{\hbar},

but a measured spectral line has a center, area, width, shape, and wing structure. These features answer different physical questions. The area can track transition strength and population; the width can encode coherence loss, motion, collisions, drive strength, static disorder, or instrumental resolution; the wings can distinguish models that look nearly identical at the peak.

Write an isolated line schematically as

S(ω)=AL(ω−ωc),∫−∞∞L(δω) dδω=1.\begin{aligned} S(\omega) &= \mathcal A L(\omega-\omega_c), \\ \int_{-\infty}^{\infty} L(\delta\omega)\,d\delta\omega &=1. \end{aligned}

Here A\mathcal A is the integrated area on an angular-frequency axis and LL is a normalized profile. Broadening can lower the peak while leaving A\mathcal A unchanged. Conversely, a process that changes populations or oscillator strength can change the area as well as the shape.

The central lesson is that a linewidth is not a mechanism. It is a fitted or derived parameter whose physical meaning depends on the profile, coordinate, preparation, propagation model, and instrument.

This page owns the spectroscopy-facing derivation and use of natural, lifetime, Doppler, collisional, power, and inhomogeneous broadening. It also owns the Lorentzian-Gaussian-Voigt dictionary, the separation of intrinsic and instrumental widths, and the fitting cautions needed to extract physical parameters from measured lines.

Nearby pages retain narrower responsibilities:

This article treats mostly isolated lines. Overlapping resonances, interference profiles, line mixing, thresholds, and strongly non-Markovian dynamics can require a matrix response or a more specialized theory.

The page uses:

  • δω=ω−ωc\delta\omega=\omega-\omega_c for angular-frequency detuning;
  • γL\gamma_{\mathrm L} for a Lorentzian half width at half maximum;
  • σG\sigma_{\mathrm G} for a Gaussian standard deviation;
  • Γ1\Gamma_1 for a population-decay rate;
  • Γ2\Gamma_2 for a coherence-decay rate;
  • T1=1/Γ1T_1=1/\Gamma_1 and T2=1/Γ2T_2=1/\Gamma_2;
  • wL=2γLw_{\mathrm L}=2\gamma_{\mathrm L} for Lorentzian FWHM;
  • wG=22ln⁡2 σGw_{\mathrm G}=2\sqrt{2\ln2}\,\sigma_{\mathrm G} for Gaussian FWHM; and
  • R(ω)R(\omega) for a normalized instrumental response.

Rates such as Γ1\Gamma_1 have units of inverse seconds. When they set an angular-frequency width, the numerical unit is rad s−1\mathrm{rad\,s^{-1}}, with radians dimensionless. Convert to ordinary-frequency width using

Δν=Δω2π.\Delta\nu = \frac{\Delta\omega}{2\pi}.

An energy width is

ΔE=ℏΔω=hΔν.\Delta E = \hbar\Delta\omega = h\Delta\nu.

The symbol Γ\Gamma is used elsewhere for a decay rate, an angular-frequency HWHM, an angular-frequency FWHM, or an energy width. Never compare quoted values until the units and width convention are explicit.

For a normalized line L(δω)L(\delta\omega):

  • the center estimates a transition frequency after shifts are modeled;
  • the area carries integrated spectral weight;
  • the width specifies a scale only after naming HWHM, FWHM, standard deviation, or another convention;
  • the shape describes the core, symmetry, and tails; and
  • the wings can dominate weak neighboring features and radiative-transfer errors even when the line center fits well.

The peak value is not independent. At fixed area, a normalized Lorentzian has

LL(0)=1πγL,L_{\mathrm L}(0) = \frac{1}{\pi\gamma_{\mathrm L}},

whereas a normalized Gaussian has

LG(0)=1σG2π.L_{\mathrm G}(0) = \frac{1} {\sigma_{\mathrm G}\sqrt{2\pi}}.

A narrower line is therefore taller at fixed area.

Homogeneous broadening gives every member of the selected ensemble the same dynamical profile. Markovian lifetime decay, pure dephasing, and impact- limit collisions are standard examples. A narrow subensemble does not remove the width.

Inhomogeneous broadening averages over members with different static or slowly varying centers. Thermal Doppler broadening, unresolved site shifts, and shot-to-shot detuning disorder are examples. Selecting a narrower class or refocusing slow offsets can reduce the width.

The distinction is operational. Spectral diffusion that is static during one measurement but changes between scans looks inhomogeneous; the same noise can look like homogeneous dephasing when it fluctuates rapidly during each coherence interval.

If two statistically independent, shift-invariant broadening stages act sequentially, their profiles convolve:

L12(ω)=∫−∞∞L1(ω−ω′)L2(ω′) dω′.L_{12}(\omega) = \int_{-\infty}^{\infty} L_1(\omega-\omega') L_2(\omega')\,d\omega'.

Static distributions also produce a convolution when the homogeneous shape does not depend on the shifted center. Correlated mechanisms, state-dependent widths, line mixing, nonlinear propagation, and saturation generally require a joint model rather than a blind convolution.

An excited level uu with radiative branches u→lu\rightarrow l has total radiative population-decay rate

Γurad=∑lAul.\Gamma_u^{\mathrm{rad}} = \sum_l A_{ul}.

If this is the only loss, its population decays as

Pu(t)=Pu(0)e−Γuradt.P_u(t) = P_u(0)e^{-\Gamma_u^{\mathrm{rad}}t}.

The state amplitude decays at half that rate. For a stable lower state and no additional dephasing, the transition has Lorentzian angular-frequency FWHM

wnat=Γurad,w_{\mathrm{nat}} = \Gamma_u^{\mathrm{rad}},

ordinary-frequency FWHM

Δνnat=Γurad2π,\Delta\nu_{\mathrm{nat}} = \frac{\Gamma_u^{\mathrm{rad}}}{2\pi},

and energy FWHM

ΔEnat=ℏΓurad.\Delta E_{\mathrm{nat}} = \hbar\Gamma_u^{\mathrm{rad}}.

This is the natural radiative width in the simplest free-space Markov model. It is not necessarily the observed width.

Let the upper and lower levels lose population at rates Γu\Gamma_u and Γl\Gamma_l, and let γϕ\gamma_\phi be additional pure dephasing of the optical coherence. Under independent Markovian decay,

Γ2=Γu+Γl2+γϕ.\Gamma_2 = \frac{\Gamma_u+\Gamma_l}{2} + \gamma_\phi.

The Lorentzian profile has

γL=Γ2,wL=2Γ2=Γu+Γl+2γϕ.\begin{aligned} \gamma_{\mathrm L} &= \Gamma_2, \\ w_{\mathrm L} &= 2\Gamma_2 = \Gamma_u+\Gamma_l+2\gamma_\phi. \end{aligned}

The transition width contains the sum of level decay contributions. Using only the upper lifetime is justified only when the lower level is stable and pure dephasing is negligible.

The radiative rate depends on the electromagnetic mode density. Cavities, interfaces, photonic crystals, and strong coupling can modify decay or split the response. Nonradiative loss adds lifetime broadening, while structured reservoirs can produce nonexponential decay and non-Lorentzian spectra.

Accordingly, “natural linewidth” should name the environment and model. A free-space Einstein AA coefficient is not a universal property of the bare matter Hamiltonian independent of its radiation field.

Suppose a transition coherence for t≥0t\ge0 behaves as

C(t)=C(0)e−Γ2te−iωct.C(t) = C(0) e^{-\Gamma_2t} e^{-i\omega_ct}.

Its one-sided Fourier response contains

∫0∞e−Γ2teiδωt dt=1Γ2−iδω.\int_0^\infty e^{-\Gamma_2t} e^{i\delta\omega t} \,dt = \frac{1} {\Gamma_2-i\delta\omega}.

The absorptive part, or the squared amplitude under the matching emission model, has a Lorentzian denominator:

LL(δω)=1πΓ2δω2+Γ22.L_{\mathrm L}(\delta\omega) = \frac{1}{\pi} \frac{\Gamma_2} {\delta\omega^2+\Gamma_2^2}.

Thus T2T_2 sets the angular-frequency HWHM,

γL=1T2,wL=2T2.\gamma_{\mathrm L} = \frac{1}{T_2}, \qquad w_{\mathrm L} = \frac{2}{T_2}.

For a stable lower state with population lifetime T1T_1 and pure-dephasing time TϕT_\phi,

1T2=12T1+1Tϕ.\frac{1}{T_2} = \frac{1}{2T_1} + \frac{1}{T_\phi}.

No pure dephasing gives T2=2T1T_2=2T_1 and wL=1/T1w_{\mathrm L}=1/T_1.

An upper population can disappear through radiative decay, quenching, predissociation, autoionization, chemical reaction, or escape:

Γutot=Γurad+Γunr.\Gamma_u^{\mathrm{tot}} = \Gamma_u^{\mathrm{rad}} + \Gamma_u^{\mathrm{nr}}.

All irreversible loss from the selected upper state contributes to its survival amplitude in the stated model. Only the radiative branches produce the photons assigned to fluorescence. A broadened line and a reduced quantum yield can therefore have the same nonradiative origin.

The reciprocal relation assumes an exponential over the time interval that controls the line. It can fail or become approximate for:

  • short-time quadratic survival;
  • long-time nonexponential tails;
  • coherent recurrences in a discrete spectrum;
  • strong coupling and resolved dressed states;
  • thresholds and energy-dependent continua;
  • non-Markovian spectral diffusion; and
  • several unresolved transitions with different centers.

Finite observation time and transit time can also broaden a line, but they do not necessarily define an intrinsic excited-state lifetime.

For a wave propagating along zz, a nonrelativistic absorber with velocity vzv_z sees a first-order Doppler shift

δω≃−k0vz,k0=ω0c.\delta\omega \simeq -k_0v_z, \qquad k_0 = \frac{\omega_0}{c}.

For a thermal gas, one velocity component follows

p(vz)=m2πkBTexp⁡ ⁣(−mvz22kBT).p(v_z) = \sqrt{ \frac{m}{2\pi k_{\mathrm B}T} } \exp\!\left( -\frac{mv_z^2} {2k_{\mathrm B}T} \right).

Mapping velocity to detuning produces a Gaussian line with standard deviation

σD=ω0ckBTm.\sigma_{\mathrm D} = \frac{\omega_0}{c} \sqrt{ \frac{k_{\mathrm B}T}{m} }.

Its angular-frequency FWHM is

wD=22ln⁡2 ω0ckBTm,w_{\mathrm D} = 2\sqrt{2\ln2}\, \frac{\omega_0}{c} \sqrt{ \frac{k_{\mathrm B}T}{m} },

or, in fractional form,

ΔνDν0=8kBTln⁡2mc2.\frac{\Delta\nu_{\mathrm D}} {\nu_0} = \sqrt{ \frac{8k_{\mathrm B}T\ln2} {mc^2} }.

The fractional first-order Doppler FWHM is the same on frequency and angular- frequency axes. A wavelength-domain profile is only approximately Gaussian for a narrow line because the frequency-wavelength map is nonlinear.

The formula measures the velocity variance along the optical wavevector. It returns a translational temperature only for a Maxwellian distribution. Atomic beams, expanding gases, trapped particles, plasmas with unequal ion and electron temperatures, and laser-cooled clouds can be nonthermal or anisotropic.

A fitted Gaussian width can also contain laser jitter, unresolved isotope structure, static fields, or instrumental resolution. Calling every Gaussian width a Doppler temperature is therefore unsafe.

Counterpropagating-beam methods, saturated absorption, two-photon geometries, and trapped-particle spectroscopy can suppress first-order Doppler broadening. Natural width, transit time, recoil, collisions, laser frequency noise, power broadening, and second-order Doppler shifts can remain.

In the impact approximation, many short, statistically independent collisions interrupt the optical phase. A simple coherence model is

C(t)∝exp⁡ ⁣[−(Γ2(0)+γcol)t]×exp⁡ ⁣[−i(ω0+Δcol)t].\begin{aligned} C(t) &\propto \exp\!\left[- (\Gamma_2^{(0)}+\gamma_{\mathrm{col}})t \right] \\ &\quad\times \exp\!\left[-i (\omega_0+\Delta_{\mathrm{col}})t \right]. \end{aligned}

The collision-induced HWHM γcol\gamma_{\mathrm{col}} adds to other homogeneous Lorentzian HWHMs, while Δcol\Delta_{\mathrm{col}} shifts the center. At low perturber density,

γcol∼np⟨vrelσbroad⟩.\gamma_{\mathrm{col}} \sim n_{\mathrm p} \left\langle v_{\mathrm{rel}} \sigma_{\mathrm{broad}} \right\rangle.

The broadening cross section is a phase-changing collision quantity, not generally the same as an elastic or momentum-transfer cross section.

Molecular databases often tabulate a Lorentzian HWHM at reference pressure and temperature. A common empirical form is

γL(p,T)=(TrefT)n[γairpair+γselfpself],\gamma_{\mathrm L}(p,T) = \left( \frac{T_{\mathrm{ref}}}{T} \right)^n \left[ \gamma_{\mathrm{air}}p_{\mathrm{air}} + \gamma_{\mathrm{self}}p_{\mathrm{self}} \right],

with pressure units matched to the tabulated coefficients. A pressure shift is parameterized separately. The exponent nn is line- and perturber- dependent; it is not a universal kinetic-theory constant.

“Pressure broadening” covers several mechanisms:

  • resonance or self-broadening between identical radiators;
  • van der Waals broadening by neutral perturbers;
  • Stark broadening by charged particles and fluctuating electric fields;
  • state-changing and quenching collisions;
  • velocity-changing collisions; and
  • line mixing among coupled transitions.

Impact-limit cores are often approximately Lorentzian. Quasistatic fields can produce non-Lorentzian wings, asymmetry, and density scalings that differ from the simple linear-pressure picture.

Collisions do not only broaden. Frequent velocity-changing collisions can confine the phase-accumulating motion and narrow the Doppler contribution, an effect commonly called Dicke narrowing. Collisional width and shift can also depend on molecular speed.

The ordinary Voigt model omits these effects. High-resolution gas spectra can require speed-dependent profiles, hard- or soft-collision narrowing models, correlations between velocity- and state-changing collisions, and line mixing.

Consider a Markovian two-level system driven with Rabi frequency Ω\Omega and detuning Δ\Delta. Let Γ1\Gamma_1 be population decay and Γ2\Gamma_2 coherence decay. The steady excited-state population is

ρeess=Ω2Γ22[Γ1(Δ2+Γ22)+Ω2Γ2].\rho_{ee}^{\mathrm{ss}} = \frac{ \Omega^2\Gamma_2 }{ 2\left[ \Gamma_1 (\Delta^2+\Gamma_2^2) + \Omega^2\Gamma_2 \right] }.

As a function of detuning, the denominator contains

Δ2+Γ22(1+s0),s0=Ω2Γ1Γ2.\Delta^2 + \Gamma_2^2 \left(1+s_0\right), \qquad s_0 = \frac{\Omega^2} {\Gamma_1\Gamma_2}.

The ideal two-level Lorentzian HWHM is therefore

γpow=Γ21+s0,\gamma_{\mathrm{pow}} = \Gamma_2 \sqrt{1+s_0},

and the FWHM is

wpow=2Γ21+s0.w_{\mathrm{pow}} = 2\Gamma_2 \sqrt{1+s_0}.

At weak drive, s0≪1s_0\ll1, the width tends to 2Γ22\Gamma_2. Stronger drive flattens the population response and broadens its detuning dependence.

If pure dephasing is absent, Γ2=Γ1/2\Gamma_2=\Gamma_1/2, so

s0=2Ω2Γ12.s_0 = \frac{2\Omega^2} {\Gamma_1^2}.

Some authors define the Rabi frequency or saturation parameter with different factors of two. The invariant procedure is to derive the line from the stated Hamiltonian and master equation, then read off the half-maximum detuning.

Power broadening is not an intrinsic property of the unilluminated transition. It depends on local intensity, polarization, detuning convention, and level structure. In multilevel systems, strong light can also cause optical pumping, AC Stark shifts, Autler–Townes splitting, coherent dark states, and spatially varying saturation.

Once resolved dressed-state peaks or coherent Rabi dynamics appear, one broad Lorentzian is no longer the right description.

Let each microscopic member have homogeneous profile Lhom(ω−Ω)L_{\mathrm{hom}}(\omega-\Omega) but a center Ω\Omega drawn from p(Ω)p(\Omega). The ensemble profile is

Lens(ω)=∫−∞∞p(Ω)Lhom(ω−Ω) dΩ.L_{\mathrm{ens}}(\omega) = \int_{-\infty}^{\infty} p(\Omega) L_{\mathrm{hom}}(\omega-\Omega) \,d\Omega.

If pp is Gaussian and LhomL_{\mathrm{hom}} is Lorentzian, the result is a Voigt profile. If both are Gaussian, their variances add.

Sources of static or slow center variation include:

  • Doppler shifts;
  • isotope or unresolved hyperfine structure;
  • strain, site, solvent, or local-field distributions;
  • spatially varying Zeeman, Stark, or trapping fields;
  • laser-frequency drift between shots; and
  • slow spectral diffusion.

Unresolved structure is sometimes called broadening, but it can be a sum of several sharp lines rather than one broadened transition.

Quasi-static detuning noise causes ensemble coherence to decay on a time T2∗T_2^* that can be much shorter than the homogeneous T2T_2. A spin echo or photon echo can refocus sufficiently slow, reversible offsets, revealing a longer coherence time.

An echo cannot undo population loss, fast Markovian dephasing, or every form of spectral diffusion. The difference between T2∗T_2^* and T2T_2 is a useful diagnostic, not a universal partition into Gaussian and Lorentzian widths.

An inhomogeneous ensemble can contain narrow spectral classes. State selection, spectral hole burning, or sufficiently narrow excitation can probe a subset whose width is closer to the homogeneous line. The measured hole still includes pump power, population dynamics, diffusion, and probe resolution.

The normalized Lorentzian is

LL(δω;γL)=1πγLδω2+γL2.L_{\mathrm L} (\delta\omega;\gamma_{\mathrm L}) = \frac{1}{\pi} \frac{\gamma_{\mathrm L}} {\delta\omega^2+\gamma_{\mathrm L}^2}.

It has HWHM γL\gamma_{\mathrm L}, FWHM wL=2γLw_{\mathrm L}=2\gamma_{\mathrm L}, and algebraic wings LL∼δω−2L_{\mathrm L}\sim\delta\omega^{-2}. Its ordinary variance does not exist on an infinite domain.

Lorentzians arise from ideal exponential coherence, impact-limit phase interruptions, and isolated weakly damped poles. They should not be assigned automatically to every broadened peak.

The normalized Gaussian is

LG(δω;σG)=1σG2πexp⁡ ⁣[−δω22σG2].L_{\mathrm G} (\delta\omega;\sigma_{\mathrm G}) = \frac{1} {\sigma_{\mathrm G}\sqrt{2\pi}} \exp\!\left[ -\frac{\delta\omega^2} {2\sigma_{\mathrm G}^2} \right].

Its FWHM is

wG=22ln⁡2 σG.w_{\mathrm G} = 2\sqrt{2\ln2}\, \sigma_{\mathrm G}.

Gaussians arise from normal distributions of shifts and from several independent Gaussian resolution sources. Their tails fall much faster than Lorentzian wings.

The Voigt profile is the convolution

LV(δω;σG,γL)=∫−∞∞LG(x;σG)×LL(δω−x;γL) dx.\begin{aligned} L_{\mathrm V} (\delta\omega;\sigma_{\mathrm G},\gamma_{\mathrm L}) &= \int_{-\infty}^{\infty} L_{\mathrm G}(x;\sigma_{\mathrm G}) \\ &\quad\times L_{\mathrm L} (\delta\omega-x;\gamma_{\mathrm L}) \,dx. \end{aligned}

Using the Faddeeva function

w(z)=e−z2erfc⁡(−iz),w(z) = e^{-z^2} \operatorname{erfc}(-iz),

one may write

LV=Re⁡w(z)σG2π,z=δω+iγLσG2.L_{\mathrm V} = \frac{\operatorname{Re}w(z)} {\sigma_{\mathrm G}\sqrt{2\pi}}, \qquad z = \frac{\delta\omega+i\gamma_{\mathrm L}} {\sigma_{\mathrm G}\sqrt2}.

The Voigt profile is normalized. Its core can be Gaussian-dominated, but any nonzero Lorentzian component controls the far-wing asymptote.

Linear and logarithmic comparisons of normalized Lorentzian and Gaussian line profiles with equal FWHM

Normalized Lorentzian and Gaussian profiles with the same FWHM can look similar near half maximum while differing strongly in peak height and wings. A Voigt convolution inherits Lorentzian far wings whenever γL>0\gamma_{\mathrm L}>0.

Two Lorentzian convolutions add HWHMs:

γL,tot=γL,1+γL,2.\gamma_{\mathrm L,tot} = \gamma_{\mathrm L,1} + \gamma_{\mathrm L,2}.

Two Gaussian convolutions add variances:

σG,tot2=σG,12+σG,22.\sigma_{\mathrm G,tot}^2 = \sigma_{\mathrm G,1}^2 + \sigma_{\mathrm G,2}^2.

Therefore Gaussian FWHMs add in quadrature, not linearly. A Gaussian and a Lorentzian form a Voigt profile, whose FWHM has no elementary exact formula. A useful approximation is

wV≃0.5346wL+0.2166wL2+wG2.w_{\mathrm V} \simeq 0.5346w_{\mathrm L} + \sqrt{ 0.2166w_{\mathrm L}^2 + w_{\mathrm G}^2 }.

This estimates the total FWHM; it does not separate mechanisms from one measured number.

The Voigt profile assumes a Gaussian distribution of Doppler shifts convolved with a velocity-independent Lorentzian collision width and shift. Precision gas spectroscopy can resolve omitted physics such as speed-dependent collisions, velocity-changing collisions, Dicke narrowing, correlations, and line mixing.

An IUPAC task group recommended the Hartmann-Tran profile in 2014 as a beyond-Voigt isolated-line model. The current HITRAN2024 framework, published in 2026, recommends a modified Hartmann-Tran profile for cases in which beyond-Voigt effects matter. This mHT representation uses a quadratic speed-dependent hard-collision profile with double-power-law temperature dependences and replaces HITRAN’s earlier preferred HT parameterization.

This is a database and high-resolution modeling recommendation, not a claim that every spectrum needs the most elaborate profile. The simplest model that leaves statistically and physically acceptable residuals is often the most identifiable.

A spectrometer records a response-convolved signal:

Smeas(ω)=∫−∞∞R(ω−ω′)Strue(ω′) dω′,S_{\mathrm{meas}}(\omega) = \int_{-\infty}^{\infty} R(\omega-\omega') S_{\mathrm{true}}(\omega') \,d\omega',

with

∫R(ω) dω=1\int R(\omega)\,d\omega =1

when the apparatus function preserves area. Slit functions, diffraction, detector pixels, interferometer windows, laser linewidth, and frequency noise can all contribute.

Resolving power is commonly quoted as

R=νΔν,\mathcal R = \frac{\nu}{\Delta\nu},

but Δν\Delta\nu must still be tied to an instrument-profile convention. Two features separated by one quoted FWHM are not automatically resolved under every criterion.

A rectangular observation of duration TT produces a sinc-like amplitude window and sinc-squared intensity response. A Gaussian pulse produces a Gaussian transform-limited envelope. Apodization changes sidelobes and width.

This Fourier width is a property of preparation or observation. It should not be added to a lifetime rate unless the full temporal model shows that the corresponding kernels convolve or decay rates add.

Fast white frequency noise can resemble homogeneous dephasing. Slow drift can produce an inhomogeneous distribution between scans. Intermediate colored noise produces profile shapes that depend on acquisition time and scan protocol. Quoting only the laser’s nominal linewidth can be insufficient.

For sampled data yky_k, a defensible model has the form

yk=[R∗Sphys](ωk)+b(ωk)+ϵk,y_k = \left[ R*S_{\mathrm{phys}} \right](\omega_k) + b(\omega_k) + \epsilon_k,

where SphysS_{\mathrm{phys}} contains all resolved lines, RR is the calibrated instrument response, bb is a baseline or background, and ϵk\epsilon_k is a noise model.

Fit this forward-convolved model to the data. Deconvolving first and fitting later usually creates correlated noise and unstable artifacts.

Why direct deconvolution is ill conditioned

Section titled “Why direct deconvolution is ill conditioned”

In Fourier space,

S~meas(t)=R~(t)S~true(t).\widetilde S_{\mathrm{meas}}(t) = \widetilde R(t) \widetilde S_{\mathrm{true}}(t).

Formal inversion divides by R~(t)\widetilde R(t). Where the transfer function is small, noise is amplified:

S~true(t)=S~meas(t)R~(t).\widetilde S_{\mathrm{true}}(t) = \frac{ \widetilde S_{\mathrm{meas}}(t) }{ \widetilde R(t) }.

Regularization imposes prior smoothness or sparsity and therefore changes the estimator. A deconvolved line should be reported with the regularization, resolution, uncertainty, and validation tests.

A useful progression is:

  1. calibrate the frequency axis and instrumental response;
  2. fit a physically justified Lorentzian or Gaussian limit;
  3. fit a Voigt profile if independent Gaussian and Lorentzian mechanisms are plausible;
  4. add neighboring lines, asymmetry, or pressure shifts when residuals demand them;
  5. use speed-dependent, narrowing, line-mixing, or mHT models only with data capable of constraining the added parameters; and
  6. compare residual structure, parameter stability, and predictive behavior across pressures, powers, or temperatures.

More parameters always reduce an unconstrained least-squares residual. They do not automatically improve the physical inference.

Line wings can trade off strongly against polynomial baselines and neighboring features. A fit window that is too narrow cannot determine Lorentzian tails; a window that is too broad may require a more realistic continuum model.

Integrated area is conserved by a normalized convolution only on the full axis. Finite windows, clipped detector ranges, variable throughput, and nonlinear transmittance can spoil apparent area conservation.

Profiles are densities. Under

ω=2πcλ,\omega = \frac{2\pi c}{\lambda},

one must transform

Lλ(λ)=Lω(ω)2πcλ2.L_\lambda(\lambda) = L_\omega(\omega) \frac{2\pi c}{\lambda^2}.

A symmetric line in frequency is not exactly symmetric in wavelength. Fit in the coordinate for which the physical and instrumental model is defined, then transform the final density with its Jacobian.

Worked Example: Natural and Doppler Widths

Section titled “Worked Example: Natural and Doppler Widths”

Consider an optical transition at

λ0=500 nm\lambda_0 = 500\ \mathrm{nm}

in an atom of mass m=40 um=40\,u at T=300 KT=300\ \mathrm K. Let the upper population lifetime be T1=10 nsT_1=10\ \mathrm{ns}, with a stable lower level and no pure dephasing.

The ordinary-frequency natural FWHM is

Δνnat=12πT1≃15.9 MHz.\Delta\nu_{\mathrm{nat}} = \frac{1}{2\pi T_1} \simeq 15.9\ \mathrm{MHz}.

The line frequency is

ν0=cλ0≃5.996×1014 Hz.\nu_0 = \frac{c}{\lambda_0} \simeq 5.996\times10^{14}\ \mathrm{Hz}.

The Doppler FWHM is

ΔνD=ν08kBTln⁡2mc2≃1.18 GHz.\Delta\nu_{\mathrm D} = \nu_0 \sqrt{ \frac{8k_{\mathrm B}T\ln2} {mc^2} } \simeq 1.18\ \mathrm{GHz}.

The Doppler core is roughly 7474 times wider than the natural FWHM. Using the Voigt approximation with

wL=15.9 MHz,wG=1.18 GHz,w_{\mathrm L}=15.9\ \mathrm{MHz}, \qquad w_{\mathrm G}=1.18\ \mathrm{GHz},

gives

wV≃1.19 GHz.w_{\mathrm V} \simeq 1.19\ \mathrm{GHz}.

The FWHM is almost Doppler limited, yet the natural Lorentzian component still controls sufficiently remote wings. A Gaussian-only fit can therefore recover the core width while underpredicting wing absorption.

  1. Name the spectral coordinate. Frequency, angular frequency, wavenumber, wavelength, and energy densities require Jacobians.
  2. Separate center, area, and width. Do not use peak height as a proxy for all three.
  3. Declare width conventions. Record HWHM, FWHM, standard deviation, and whether the number is angular frequency, hertz, or energy.
  4. List candidate mechanisms. Include lifetimes, dephasing, motion, collisions, drive, static distributions, transit time, and apparatus.
  5. Estimate scales before fitting. Compare expected natural, Doppler, pressure, power, and resolution widths.
  6. Use a forward model. Convolve the physical spectrum with a calibrated response and include baseline and neighboring lines.
  7. Vary control parameters. Pressure, temperature, power, beam geometry, and observation time help separate mechanisms.
  8. Inspect residuals and covariance. Structured residuals reveal model failure; strong covariance reveals weak identifiability.
  9. Test fit-window stability. Centers, areas, and widths should not drift without physical explanation.
  10. Report provenance. State whether widths were observed, fitted, calculated, deconvolved, or taken from a database.

Writing linewidth equals inverse lifetime without conventions

Section titled “Writing linewidth equals inverse lifetime without conventions”

The relation depends on whether the lifetime describes population or coherence and whether the width is HWHM, FWHM, angular frequency, ordinary frequency, or energy.

Treating natural and observed widths as identical

Section titled “Treating natural and observed widths as identical”

Doppler motion, collisions, drive, static disorder, unresolved structure, laser noise, and instrument response can all dominate the radiative width.

Lorentzian HWHMs add under convolution. Gaussian variances add. Voigt and more general profiles require their own forward calculation.

Calling every Gaussian width Doppler broadening

Section titled “Calling every Gaussian width Doppler broadening”

Static fields, isotope mixtures, laser jitter, and Gaussian instrument functions can produce the same elementary shape.

Impact collisions, laser phase diffusion, a chosen numerical regulator, and some instrument functions can be Lorentzian without measuring the target’s population lifetime.

Treating power broadening as a material constant

Section titled “Treating power broadening as a material constant”

It depends on local Rabi frequency and relaxation. Spatial intensity variation can itself make the ensemble profile non-Lorentzian.

Assuming a Voigt fit proves two mechanisms

Section titled “Assuming a Voigt fit proves two mechanisms”

A Voigt curve can be an effective fit to unresolved structure or other physics. Parameter plausibility and control-variable scaling are needed.

Interpreting unresolved splitting as one decay width

Section titled “Interpreting unresolved splitting as one decay width”

Several narrow transitions can mimic one broad line. Better resolution, field dependence, polarization, or a constrained multiplet model may reveal the components.

Linear subtraction works only for Lorentzian FWHMs under the matching convolution model. Gaussian widths subtract in quadrature. A Voigt instrument requires a Voigt-aware fit.

Collisions, AC Stark effects, recoil, and calibration errors can move the center. Width and shift parameters can be correlated.

Trusting a small fit error under a wrong profile

Section titled “Trusting a small fit error under a wrong profile”

Statistical covariance assumes the model family is adequate. It does not include model discrepancy, baseline error, calibration drift, or omitted neighbors.

Gaussian and Lorentzian profiles with similar cores can differ by orders of magnitude in the wings. Radiative transfer and weak-line retrievals are often wing sensitive.

  1. A linewidth becomes meaningful only after the spectral coordinate, units, profile, and width convention are specified.
  2. Exponential coherence gives a Lorentzian whose angular-frequency HWHM is 1/T21/T_2; a stable lower state without pure dephasing gives FWHM 1/T11/T_1.
  3. Maxwellian first-order Doppler broadening is Gaussian with width proportional to ω0T/m\omega_0\sqrt{T/m}.
  4. Impact-limit collisions often add Lorentzian width and a pressure shift, but velocity changes, quasistatic fields, and line mixing can produce more complex profiles.
  5. Ideal two-level power broadening increases the homogeneous width by 1+s0\sqrt{1+s_0} and is not intrinsic to the undriven transition.
  6. Inhomogeneous broadening averages over a distribution of centers and can sometimes be reduced by selection or refocusing.
  7. Lorentzian widths add, Gaussian variances add, and their convolution is Voigt; none of these rules is universal beyond its assumptions.
  8. Precision work should fit a physical spectrum convolved with the instrument response and should validate the profile through residuals and control-parameter scaling.

Exercise 1: Translate lifetimes into a width

Section titled “Exercise 1: Translate lifetimes into a width”

An upper level decays at Γu=5.0×107 s−1\Gamma_u=5.0\times10^7\ \mathrm{s}^{-1}, a lower level at Γl=2.0×107 s−1\Gamma_l=2.0\times10^7\ \mathrm{s}^{-1}, and pure dephasing occurs at γϕ=1.0×107 s−1\gamma_\phi=1.0\times10^7\ \mathrm{s}^{-1}. Find the Lorentzian angular- frequency HWHM, angular-frequency FWHM, and ordinary-frequency FWHM.

Solution

The coherence-decay rate is

Γ2=Γu+Γl2+γϕ=4.5×107 s−1.\begin{aligned} \Gamma_2 &= \frac{\Gamma_u+\Gamma_l}{2} + \gamma_\phi \\ &= 4.5\times10^7\ \mathrm{s}^{-1}. \end{aligned}

Thus

γL=4.5×107 rad s−1,\gamma_{\mathrm L} = 4.5\times10^7\ \mathrm{rad\,s}^{-1},

and

wL=9.0×107 rad s−1.w_{\mathrm L} = 9.0\times10^7\ \mathrm{rad\,s}^{-1}.

The ordinary-frequency FWHM is

ΔνFWHM=wL2π≃14.3 MHz.\Delta\nu_{\mathrm{FWHM}} = \frac{w_{\mathrm L}}{2\pi} \simeq 14.3\ \mathrm{MHz}.

A line at ν0=3.00×1014 Hz\nu_0=3.00\times10^{14}\ \mathrm{Hz} from particles of mass m=20 um=20\,u has Gaussian FWHM ΔνD=9.00×108 Hz\Delta\nu_{\mathrm D}=9.00\times10^8\ \mathrm{Hz}. Assuming a Maxwellian gas and pure Doppler broadening, find the temperature.

Solution

Invert the fractional Doppler-width formula:

T=mc28kBln⁡2(ΔνDν0)2.T = \frac{mc^2}{8k_{\mathrm B}\ln2} \left( \frac{\Delta\nu_{\mathrm D}}{\nu_0} \right)^2.

With m=20um=20u and ΔνD/ν0=3.00×10−6\Delta\nu_{\mathrm D}/\nu_0=3.00\times10^{-6},

T≃3.51×102 K.T \simeq 3.51\times10^2\ \mathrm K.

The result is a translational temperature only under the Maxwellian and single-mechanism assumptions.

Two independent Lorentzian mechanisms have HWHMs 1212 and 8 MHz8\ \mathrm{MHz}. Two independent Gaussian mechanisms have standard deviations 1212 and 8 MHz8\ \mathrm{MHz}. Find the total Lorentzian HWHM and total Gaussian standard deviation.

Solution

Lorentzian HWHMs add:

γL,tot=12+8=20 MHz.\gamma_{\mathrm L,tot} = 12+8 = 20\ \mathrm{MHz}.

Gaussian variances add:

σG,tot=122+82 MHz≃14.4 MHz.\begin{aligned} \sigma_{\mathrm G,tot} &= \sqrt{12^2+8^2}\ \mathrm{MHz} \\ &\simeq 14.4\ \mathrm{MHz}. \end{aligned}

Adding the Gaussian standard deviations linearly would overestimate the width.

An ideal two-level system has no pure dephasing, so Γ2=Γ1/2\Gamma_2=\Gamma_1/2. It is driven with Ω=Γ1\Omega=\Gamma_1. Find the on- resonance saturation parameter s0s_0 and the ratio of power-broadened FWHM to the weak-drive FWHM.

Solution

The saturation parameter is

s0=Ω2Γ1Γ2=Γ12Γ1(Γ1/2)=2.s_0 = \frac{\Omega^2} {\Gamma_1\Gamma_2} = \frac{\Gamma_1^2} {\Gamma_1(\Gamma_1/2)} =2.

The width ratio is

wpowwweak=1+s0=3≃1.73.\frac{w_{\mathrm{pow}}} {w_{\mathrm{weak}}} = \sqrt{1+s_0} = \sqrt3 \simeq 1.73.

A Voigt line has Gaussian FWHM wG=500 MHzw_{\mathrm G}=500\ \mathrm{MHz} and Lorentzian FWHM wL=100 MHzw_{\mathrm L}=100\ \mathrm{MHz}. Use the stated approximation to estimate wVw_{\mathrm V}.

Solution

Substitution gives

wV≃0.5346(100)+0.2166(100)2+(500)2≃556 MHz.\begin{aligned} w_{\mathrm V} &\simeq 0.5346(100) \\ &\quad+ \sqrt{ 0.2166(100)^2 + (500)^2 } \\ &\simeq 556\ \mathrm{MHz}. \end{aligned}

The result is not 600 MHz600\ \mathrm{MHz} because Gaussian and Lorentzian FWHMs do not simply add.

Exercise 6: Remove a Gaussian instrument width

Section titled “Exercise 6: Remove a Gaussian instrument width”

A measured Gaussian line has FWHM 120 MHz120\ \mathrm{MHz}. The calibrated instrument response is Gaussian with FWHM 90 MHz90\ \mathrm{MHz}. Assuming the intrinsic line is also Gaussian and the two are independent, find its FWHM.

Solution

Gaussian variances, and therefore squared Gaussian FWHMs, add:

wmeas2=wint2+winst2.w_{\mathrm{meas}}^2 = w_{\mathrm{int}}^2 + w_{\mathrm{inst}}^2.

Hence

wint=1202−902 MHz≃79.4 MHz.\begin{aligned} w_{\mathrm{int}} &= \sqrt{120^2-90^2}\ \mathrm{MHz} \\ &\simeq 79.4\ \mathrm{MHz}. \end{aligned}

This quadrature subtraction would be wrong for Lorentzian or Voigt profiles.

A spin ensemble has a free-induction decay time T2∗=2 μsT_2^*=2\ \mu\mathrm s. A spin echo yields T2=40 μsT_2=40\ \mu\mathrm s, while the population lifetime is T1=5 msT_1=5\ \mathrm{ms}. What does this hierarchy imply, and what does it not prove?

Solution

The large improvement from T2∗T_2^* to T2T_2 shows that slow, reversible frequency offsets dominate the free-induction decay. The remaining 40 μs40\ \mu\mathrm s coherence time is far shorter than the relaxation-limited value 2T1=10 ms2T_1=10\ \mathrm{ms}, so additional homogeneous dephasing or spectral noise remains.

The result does not prove that the static distribution is exactly Gaussian, that the residual decay is exactly exponential, or that one microscopic noise source is responsible. Echo-pulse errors and spectral diffusion also need to be checked.

A high-resolution gas spectrum is fitted by a Voigt profile. The residuals show an antisymmetric pattern that reverses with pressure, and the fitted Gaussian width drifts with pressure even though temperature is fixed. Give at least four checks before reporting a Doppler temperature.

Solution

A defensible audit should include at least:

  1. test a pressure-dependent line shift and verify frequency calibration;
  2. test speed-dependent and velocity-changing-collision profiles;
  3. examine Dicke narrowing and possible line mixing;
  4. include neighboring transitions and baseline uncertainty;
  5. fit several pressures jointly with physically constrained scaling;
  6. convolve every candidate with the measured instrument response;
  7. inspect parameter covariance and fit-window stability; and
  8. compare a current mHT implementation when HITRAN parameters are available.

The structured residual and pressure-dependent Gaussian width show that the Voigt decomposition is not stable. Its Gaussian parameter cannot yet be identified with a Doppler width or temperature.

  • P. F. Bernath, Spectra of Atoms and Molecules, 5th ed., Oxford University Press, 2025, doi:10.1093/oso/9780197754498.001.0001.
  • W. Demtröder, Laser Spectroscopy 1: Basic Principles, 5th ed., Springer, 2014, doi:10.1007/978-3-642-53859-9.
  • C. J. Foot, Atomic Physics, Oxford University Press, 2005.
  • G. B. Rybicki and A. P. Lightman, Radiative Processes in Astrophysics, Wiley, 1979.
  • H. R. Griem, Principles of Plasma Spectroscopy, Cambridge University Press, 1997, doi:10.1017/CBO9780511524578.
  • W. C. Martin, W. L. Wiese, and A. Kramida, “Spectral Line Shapes, Widths, and Shifts”, in Atomic Spectroscopy: An Introduction, National Institute of Standards and Technology, updated 2025, accessed 2026-07-22.
  • NIST Digital Library of Mathematical Functions, “Voigt Functions” and “Physical Applications”, accessed 2026-07-22.
  • HITRAN, Definitions and Units, including Doppler, pressure, and Voigt conventions, accessed 2026-07-22.
  • J. Tennyson et al., “Recommended isolated-line profile for representing high-resolution spectroscopic transitions,” Pure and Applied Chemistry 86, 1931-1943 (2014), doi:10.1515/pac-2014-0208.
  • P. Wcisło et al., “New beyond-Voigt line-shape profile recommended for the HITRAN database,” Journal of Quantitative Spectroscopy and Radiative Transfer 347, 109596 (2025), doi:10.1016/j.jqsrt.2025.109596.
  • I. E. Gordon et al., “The HITRAN2024 molecular spectroscopic database,” Journal of Quantitative Spectroscopy and Radiative Transfer 353, 109807 (2026), official PDF.
  • J. J. Olivero and R. L. Longbothum, “Empirical fits to the Voigt line width: A brief review,” Journal of Quantitative Spectroscopy and Radiative Transfer 17, 233-236 (1977), doi:10.1016/0022-4073(77)90161-3.