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Laser Modes

A laser mode is a self-reproducing electromagnetic field pattern of the complete active resonator. Its label can contain independent longitudinal, transverse, polarization, propagation-direction, and frequency indices. A claim that a laser is “single mode” is therefore incomplete unless it says which of those degrees of freedom has been selected.

The passive cavity supplies candidate modes. Pump overlap, gain dispersion, loss, saturation, and nonlinear coupling decide which candidates actually oscillate. This distinction matters:

passive-cavity eigenmode  ≠  lasing steady state\text{passive-cavity eigenmode} \;\ne\; \text{lasing steady state}

in general. Near threshold, one passive mode may be an excellent starting point. Far above threshold, thermal lensing, gain guiding, spatial hole burning, nonlinear index changes, or coherent coupling can alter the mode itself.

This page owns:

  1. longitudinal standing-wave and traveling-wave mode structure;
  2. mode spacing and transverse-order degeneracy;
  3. the scalar paraxial equation and normalized fundamental Gaussian mode;
  4. Hermite–Gaussian modes in Cartesian geometry;
  5. Laguerre–Gaussian modes in cylindrical geometry;
  6. the relation between HG and LG bases inside a degenerate mode subspace;
  7. second-moment beam quality and the meaning of M2M^2;
  8. intensity, phase, spectral, and modal measurements;
  9. multimode gain saturation, spatial and spectral hole burning, and two-mode stability;
  10. practical mode-selection strategies and their failure modes.

Optical Cavities owns resonance, free spectral range, Gaussian waist design, stability, finesse, linewidth, and quality factor. Gain and Threshold owns modal gain overlap and the onset condition. Rate-Equation Lasers owns the single-mode population–photon dynamics after one spatial mode has been chosen. Quantized Electromagnetic Modes owns field quantization and photon normalization. Linewidth and Coherence owns the temporal spectrum and phase noise of a selected lasing mode.

Unless stated otherwise:

  • the physical field is Re⁡[E(r)e−iωt]\operatorname{Re}[\mathcal E(\mathbf r)e^{-i\omega t}];
  • E(r)=u(x,y,z)eikz\mathcal E(\mathbf r)=u(x,y,z)e^{ikz}, with uu a slowly varying scalar envelope;
  • k=2π/λk=2\pi/\lambda uses the wavelength in the propagation medium;
  • w(z)w(z) is the field-amplitude radius, so the fundamental intensity falls to e−2e^{-2} at r=w(z)r=w(z);
  • w0=w(0)w_0=w(0) is the waist radius;
  • zR=πw02/λz_R=\pi w_0^2/\lambda is the Rayleigh range;
  • R(z)R(z) is the wavefront radius of curvature;
  • ζ(z)=arctan⁡(z/zR)\zeta(z)=\arctan(z/z_R) is the Gouy phase;
  • transverse modes obey ∫∣uμ(x,y;z)∣2 dx dy=1\int |u_\mu(x,y;z)|^2\,dx\,dy=1 at every zz;
  • qq labels longitudinal resonance;
  • m,n=0,1,2,…m,n=0,1,2,\ldots label Cartesian mode order;
  • p=0,1,2,…p=0,1,2,\ldots and ℓ∈Z\ell\in\mathbb Z label radial and azimuthal cylindrical mode order.

The sign of every propagation phase changes if the opposite phasor convention is adopted. Intensities, nodal sets, frequency splittings, and mode orthogonality do not.

Let R(ω)\mathcal R(\omega) represent one complete circuit through propagation, mirrors, apertures, lenses, polarization elements, gain, and loss. A self-reproducing field satisfies

R(ωμ)uμ=λμ(ωμ)uμ.\mathcal R(\omega_\mu)u_\mu = \lambda_\mu(\omega_\mu)u_\mu.

The eigenvalue has three jobs:

λμ=∣λμ∣eiϕμ.\lambda_\mu = |\lambda_\mu| e^{i\phi_\mu}.
  • ϕμ=2πq\phi_\mu=2\pi q supplies the resonance condition;
  • ∣λμ∣|\lambda_\mu| records round-trip amplitude survival or growth;
  • the eigenfunction uμu_\mu records the spatial and polarization pattern.

For a passive lossy resonator, ∣λμ∣<1|\lambda_\mu|<1. At laser threshold, the active round-trip eigenvalue of the leading mode reaches unit magnitude. Above threshold, saturation changes R\mathcal R until the occupied steady-state modes have zero net growth.

This operator definition is more general than the familiar HG and LG families. Finite apertures produce diffractive Fox–Li modes; waveguides produce guided modes; open non-Hermitian resonators can have nonorthogonal right and left eigenmodes; unstable resonators deliberately magnify their field every pass. HG and LG functions are exact scalar paraxial solutions in idealized quadratic optical systems, not a universal taxonomy for every laser.

In a linear two-mirror cavity, counterpropagating waves at one resonance combine into a standing pattern. Suppressing the slowly varying transverse factor,

Eq(z)∝sin⁡(kqz+φq).\mathcal E_q(z) \propto \sin(k_q z+\varphi_q).

For ideal mirrors and a uniform nondispersive cavity of length LL,

kqL≃qπ,νq≃qc2nL.k_qL \simeq q\pi, \qquad \nu_q \simeq \frac{qc}{2nL}.

The integer qq counts half wavelengths in the optical path. Optical values of qq are usually so large that experiments identify frequency differences rather than the absolute integer.

The standing-wave intensity,

Iq(z)∝sin⁡2(kqz+φq),I_q(z) \propto \sin^2(k_qz+\varphi_q),

contains fixed nodes and antinodes. Saturation depletes inversion near the antinodes while leaving more inversion near the nodes. That spatial hole burning weakens competition between longitudinal modes whose standing-wave patterns are displaced from one another.

An ideal unidirectional ring supports a traveling pattern,

Eq(z)∝eikqz,\mathcal E_q(z) \propto e^{ik_qz},

whose intensity is uniform along a lossless uniform path. It therefore avoids the fixed longitudinal holes of a single standing wave. Real rings may still support clockwise and counterclockwise modes; backscattering can couple them into standing-wave doublets.

For one fixed transverse and polarization family, adjacent longitudinal resonances obey

νq+1−νq≃νFSR.\nu_{q+1}-\nu_q \simeq \nu_{\mathrm{FSR}}.

The general local result is

νFSR=1trt,\nu_{\mathrm{FSR}} = \frac{1}{t_{\mathrm{rt}}},

where trt=dΦrt/dωt_{\mathrm{rt}}=d\Phi_{\mathrm{rt}}/d\omega is the round-trip group delay. The common c/(2nL)c/(2nL) expression for a linear cavity is a nondispersive approximation. Mirror phase, material dispersion, and frequency-dependent mode shape shift the spacing.

If a gain profile has useful width Δνg\Delta\nu_g, the rough count

Nlong∼ΔνgνFSRN_{\mathrm{long}} \sim \frac{\Delta\nu_g}{\nu_{\mathrm{FSR}}}

estimates how many longitudinal resonances sample it. It does not predict how many lase: each mode has its own loss, pump overlap, detuning, and cross-saturation.

For an ideal stable spherical-mirror cavity, define

gi=1−LRi,0<g1g2<1,g_i = 1-\frac{L}{R_i}, \qquad 0<g_1g_2<1,

and

α=arccos⁡g1g2.\alpha = \arccos\sqrt{g_1g_2}.

One conventional indexing of the resonance frequencies is

νqmn=νFSR[q+m+n+1πα].\nu_{qmn} = \nu_{\mathrm{FSR}} \left[ q + \frac{m+n+1}{\pi}\alpha \right].

Changing the branch convention can shift qq by an integer, but observable frequency differences are unchanged. Adjacent longitudinal modes of fixed m,nm,n differ by νFSR\nu_{\mathrm{FSR}}. Adjacent transverse orders N=m+nN=m+n differ by

Δν⊥=απνFSR.\Delta\nu_{\perp} = \frac{\alpha}{\pi} \nu_{\mathrm{FSR}}.

When α/π\alpha/\pi is rational, different pairs (q,N)(q,N) can be degenerate. Small mirror astigmatism, apertures, gain gradients, thermal lenses, or polarization-dependent phase usually lift that ideal degeneracy.

For an astigmatic cavity, the two transverse axes can have different Gouy increments:

νqmn=νFSR[q+m+12παx+n+12παy].\begin{aligned} \nu_{qmn} = \nu_{\mathrm{FSR}} \bigg[ q &+ \frac{m+\tfrac12}{\pi}\alpha_x \\ &+ \frac{n+\tfrac12}{\pi}\alpha_y \bigg]. \end{aligned}

The splitting between HG10\mathrm{HG}_{10} and HG01\mathrm{HG}_{01} is then

νq10−νq01=αx−αyπνFSR.\nu_{q10}-\nu_{q01} = \frac{\alpha_x-\alpha_y}{\pi} \nu_{\mathrm{FSR}}.

These formulas describe passive resonances. Gain pulling and nonlinear index changes can move an operating laser away from them.

Start with the scalar Helmholtz equation in a uniform medium:

(∇2+k2)E=0.\left( \nabla^2+k^2 \right) \mathcal E = 0.

Insert

E(x,y,z)=u(x,y,z)eikz.\mathcal E(x,y,z) = u(x,y,z)e^{ikz}.

The envelope obeys

∇⊥2u+2ik∂u∂z+∂2u∂z2=0.\nabla_\perp^2u + 2ik\frac{\partial u}{\partial z} + \frac{\partial^2u}{\partial z^2} = 0.

If uu changes over an axial distance much longer than one wavelength, then

∣∂2u∂z2∣≪∣2k∂u∂z∣.\left| \frac{\partial^2u}{\partial z^2} \right| \ll \left| 2k\frac{\partial u}{\partial z} \right|.

Neglecting the second axial derivative gives

(∇⊥2+2ik∂z)u=0.\left( \nabla_\perp^2 + 2ik\partial_z \right)u = 0.

This paraxial equation has the same mathematical structure as a two-dimensional free-particle Schrödinger equation with zz playing the role of time. Quadratic lenses and mirror curvature generate the oscillator-like HG and LG eigenfamilies.

The approximation fails for large divergence, wavelength-scale focusing, strong longitudinal field components, sharp apertures, or strongly inhomogeneous media. In those regimes, scalar mode labels may remain useful shorthand, but a vector Maxwell solution is the authoritative object.

A normalized fundamental solution is

u00(r,z)=2π1w(z)exp⁡[−r2w2(z)]×exp⁡[ikr22R(z)−iζ(z)],\begin{aligned} u_{00}(r,z) =& \sqrt{\frac{2}{\pi}} \frac{1}{w(z)} \exp \left[ -\frac{r^2}{w^2(z)} \right] \\ &\times \exp \left[ i\frac{kr^2}{2R(z)} -i\zeta(z) \right], \end{aligned}

where

w(z)=w01+(zzR)2,R(z)=z[1+(zRz)2],ζ(z)=arctan⁡(zzR),zR=πw02λ.\begin{aligned} w(z) &= w_0 \sqrt{ 1+\left(\frac{z}{z_R}\right)^2 }, \\ R(z) &= z \left[ 1+\left(\frac{z_R}{z}\right)^2 \right], \\ \zeta(z) &= \arctan \left( \frac{z}{z_R} \right), \\ z_R &= \frac{\pi w_0^2}{\lambda}. \end{aligned}

At the waist, R→∞R\to\infty. Far from the waist,

w(z)≃θ0∣z∣,θ0=λπw0.w(z) \simeq \theta_0|z|, \qquad \theta_0 = \frac{\lambda}{\pi w_0}.

The normalized intensity is

∣u00(r,z)∣2=2πw2(z)exp⁡[−2r2w2(z)].|u_{00}(r,z)|^2 = \frac{2}{\pi w^2(z)} \exp \left[ -\frac{2r^2}{w^2(z)} \right].

Thus ww is not an rms radius and not a diameter. It is the radius at which the intensity has fallen to e−2e^{-2} of its on-axis value.

The Gouy phase contributes an extra phase advance of π\pi as the fundamental beam passes from z=−∞z=-\infty to +∞+\infty. Higher-order modes accumulate a larger multiple of the same phase, which is why transverse order shifts cavity resonance frequency.

Rectangularly separable paraxial systems use the physicists’ Hermite polynomials HmH_m. With

N=m+n,N=m+n,

a normalized mode is

umnHG(x,y,z)=1w(z)2π 2m+nm!n!×Hm(2 xw)Hn(2 yw)×exp⁡[−x2+y2w2]×exp⁡[ik(x2+y2)2R]×exp⁡[−i(N+1)ζ].\begin{aligned} u_{mn}^{\mathrm{HG}} (x,y,z) =& \frac{1}{w(z)} \sqrt{ \frac{2}{ \pi\,2^{m+n}m!n! } } \\ &\times H_m \left( \frac{\sqrt2\,x}{w} \right) H_n \left( \frac{\sqrt2\,y}{w} \right) \\ &\times \exp \left[ -\frac{x^2+y^2}{w^2} \right] \\ &\times \exp \left[ i\frac{k(x^2+y^2)}{2R} \right] \\ &\times \exp \left[ -i(N+1)\zeta \right]. \end{aligned}

The omitted zz arguments on ww, RR, and ζ\zeta are understood.

HmH_m has mm real zeros, so HGmn\mathrm{HG}_{mn} has:

  • mm nodal lines parallel to the yy axis;
  • nn nodal lines parallel to the xx axis;
  • (m+1)(n+1)(m+1)(n+1) intensity lobes in the ideal mode;
  • parity (−1)m(-1)^m under x↦−xx\mapsto-x;
  • parity (−1)n(-1)^n under y↦−yy\mapsto-y.

The signs of neighboring field lobes alternate. An ordinary camera measures ∣u∣2|u|^2 and erases those signs. Interference with a phase reference or a mode-selective projection is needed to recover them.

At any transverse plane,

∫(umnHG)∗um′n′HG dx dy=δmm′δnn′.\int \left( u_{mn}^{\mathrm{HG}} \right)^* u_{m'n'}^{\mathrm{HG}} \,dx\,dy = \delta_{mm'}\delta_{nn'}.

An arbitrary square-integrable scalar paraxial field can therefore be expanded as

u(x,y,z)=∑m,ncmnumnHG(x,y,z),u(x,y,z) = \sum_{m,n} c_{mn} u_{mn}^{\mathrm{HG}}(x,y,z),

provided all basis functions use a consistent waist, axis, and reference plane. A poor basis choice may require many coefficients even when the beam is physically simple.

All ideal HG modes with equal N=m+nN=m+n acquire the same Gouy phase. In a rotationally symmetric spherical cavity they are frequency-degenerate.

For a pure ideal mode, the second-moment beam-quality factors are

Mx2=2m+1,My2=2n+1.M_x^2 = 2m+1, \qquad M_y^2 = 2n+1.

Only HG00\mathrm{HG}_{00} reaches unity on both axes.

Cylindrically symmetric systems use associated Laguerre polynomials Lp∣ℓ∣L_p^{|\ell|}. In polar coordinates (r,ϕ)(r,\phi), define

N=2p+∣ℓ∣.N = 2p+|\ell|.

A normalized scalar mode is

upℓLG(r,ϕ,z)=1w(z)2p!π(p+∣ℓ∣)!×(2 rw)∣ℓ∣Lp∣ℓ∣(2r2w2)×exp⁡[−r2w2]eiℓϕ×exp⁡[ikr22R]×exp⁡[−i(N+1)ζ].\begin{aligned} u_{p\ell}^{\mathrm{LG}} (r,\phi,z) =& \frac{1}{w(z)} \sqrt{ \frac{2p!}{ \pi(p+|\ell|)! } } \\ &\times \left( \frac{\sqrt2\,r}{w} \right)^{|\ell|} L_p^{|\ell|} \left( \frac{2r^2}{w^2} \right) \\ &\times \exp \left[ -\frac{r^2}{w^2} \right] e^{i\ell\phi} \\ &\times \exp \left[ i\frac{kr^2}{2R} \right] \\ &\times \exp \left[ -i(N+1)\zeta \right]. \end{aligned}
  • pp counts radial nodes.
  • ∣ℓ∣|\ell| sets the order of the axial zero.
  • ℓ\ell sets the sign and number of azimuthal phase windings.
  • 2p+∣ℓ∣+12p+|\ell|+1 multiplies the Gouy phase.

For ℓ≠0\ell\ne0, the phase changes by

Δarg⁡u=2πℓ\Delta\arg u = 2\pi\ell

around a closed loop enclosing the axis. A single-valued field must vanish at the phase singularity, producing the familiar dark center. An annular intensity profile alone does not prove a nonzero winding: incoherent mixtures, obscurations, and radial modes can also make rings.

Within the usual scalar paraxial treatment,

L^z=−iℏ∂∂ϕ.\hat L_z = -i\hbar\frac{\partial}{\partial\phi}.

Therefore

L^zupℓLG=ℓℏupℓLG.\hat L_z u_{p\ell}^{\mathrm{LG}} = \ell\hbar u_{p\ell}^{\mathrm{LG}}.

A photon in a pure LG mode carries canonical axial orbital angular momentum ℓℏ\ell\hbar in this approximation. The statement must be qualified for nonparaxial focusing, spatially varying polarization, material media, and gauge-dependent decompositions of electromagnetic angular momentum.

Modes with +ℓ+\ell and −ℓ-\ell have identical ideal intensity but opposite phase winding. Their second-moment beam quality is

M2=2p+∣ℓ∣+1.M^2 = 2p+|\ell|+1.

Six representative transverse laser modes: four Hermite–Gaussian patterns and two Laguerre–Gaussian patterns, with field-sign labels and nodal boundaries.

Representative scalar transverse modes at one plane. Gray lobes suggest intensity envelopes, while the ++ and −- labels retain field phase information that an intensity image loses. LG0+1\mathrm{LG}_{0}^{+1} has an axial zero and one positive phase winding; LG10\mathrm{LG}_{1}^{0} has one radial node but no azimuthal winding.

The labels describe ideal basis functions. A measured pattern can be a coherent superposition, an incoherent spectral mixture, a clipped beam, or a distorted eigenmode. Visual resemblance is evidence, not a complete modal decomposition.

For one ideal isotropic paraxial system, all modes of total order

N=m+n=2p+∣ℓ∣N = m+n = 2p+|\ell|

span the same (N+1)(N+1)-dimensional degenerate subspace. HG and LG modes are different orthonormal bases for that subspace.

For example, first-order modes can be combined schematically as

u0,+1LG∝u10HG+iu01HG,u_{0,+1}^{\mathrm{LG}} \propto u_{10}^{\mathrm{HG}} + i u_{01}^{\mathrm{HG}},

and

u0,−1LG∝u10HG−iu01HG.u_{0,-1}^{\mathrm{LG}} \propto u_{10}^{\mathrm{HG}} - i u_{01}^{\mathrm{HG}}.

The relative phase of ±π/2\pm\pi/2 turns two Cartesian lobed modes into a vortex mode. An astigmatic mode converter implements this transformation by giving the two axes different Gouy phases.

Geometry determines which basis is convenient:

Symmetry or perturbationNatural description
rectangular aperture or astigmatismHG-like modes
cylindrical symmetryLG-like modes
elliptic coordinatesInce–Gaussian modes
strong aperture or aberrationnumerical round-trip modes
waveguide confinementguided vector modes

Degeneracy means that any coherent superposition inside the subspace is also an eigenmode of the ideal symmetric problem. A small perturbation can select a different basis by diagonalizing the perturbation within that subspace.

No single instrument measures every part of a laser-mode label.

A beam profiler measures a spatially sampled intensity,

I(x,y)∝∣∑μaμuμ(x,y)∣2I(x,y) \propto \left| \sum_\mu a_\mu u_\mu(x,y) \right|^2

if the fields remain mutually coherent during the exposure. Cross terms then depend on relative phase.

If frequency separations are large compared with the detector bandwidth, the exposure averages those terms:

I‾(x,y)≃∑μ∣aμ∣2∣uμ(x,y)∣2.\overline I(x,y) \simeq \sum_\mu |a_\mu|^2 |u_\mu(x,y)|^2.

The same camera image can therefore arise from a coherent superposition or an incoherent mixture. Background subtraction, finite sensor area, clipping, and saturation can further distort second moments and weak outer lobes.

A scanning Fabry–Pérot resonator or optical spectrum analyzer can resolve longitudinal frequencies if its resolution and free spectral range are appropriate. A fast photodetector can reveal intermode beat notes at

νbeat=∣νμ−νν∣.\nu_{\mathrm{beat}} = |\nu_\mu-\nu_\nu|.

Integrated detection can miss beats between orthogonal transverse modes because

∫uμ∗uν dx dy=0.\int u_\mu^*u_\nu\,dx\,dy = 0.

A local detector, aperture, or deliberate spatial projection prevents that orthogonality cancellation.

Interferometry with a known reference reveals wavefront curvature, lobe signs, and phase singularities. Modal decomposition instead projects the complex field onto a chosen basis:

cμ=∫uμ∗(x,y)u(x,y) dx dy.c_\mu = \int u_\mu^*(x,y) u(x,y) \,dx\,dy.

Intensity-only projections generally recover ∣cμ∣2|c_\mu|^2, not all relative phases. Full reconstruction requires additional phase diversity, interferometry, wavefront sensing, or a tomographically complete set of measurements.

A defensible report distinguishes:

Degree of freedomExample evidence
longitudinal frequencyresolved optical spectrum or beat measurement
transverse fieldphase-sensitive modal decomposition
polarizationStokes parameters or polarization tomography
direction in a ringseparate clockwise and counterclockwise outputs
temporal statecoherence or photon-statistics measurement

A beam can be HG00\mathrm{HG}_{00} in space and still contain many longitudinal frequencies. It can be single-frequency but occupy two polarizations. It can also have M2M^2 near one while carrying technical phase and amplitude noise.

M2M^2 is a propagation measure, not a complete mode label. Define centered second moments in one transverse direction,

σx2=⟨(x−⟨x⟩)2⟩,σθx2=⟨(θx−⟨θx⟩)2⟩,Cxθ=⟨(x−⟨x⟩)(θx−⟨θx⟩)⟩.\begin{aligned} \sigma_x^2 &= \left\langle (x-\langle x\rangle)^2 \right\rangle, \\ \sigma_{\theta_x}^2 &= \left\langle (\theta_x-\langle\theta_x\rangle)^2 \right\rangle, \\ C_{x\theta} &= \left\langle (x-\langle x\rangle) (\theta_x-\langle\theta_x\rangle) \right\rangle. \end{aligned}

Then a scalar paraxial second-moment definition is

Mx2=4πλσx2σθx2−Cxθ2.M_x^2 = \frac{4\pi}{\lambda} \sqrt{ \sigma_x^2\sigma_{\theta_x}^2 - C_{x\theta}^2 }.

The corresponding uncertainty inequality gives

Mx2≥1.M_x^2 \ge 1.

At a principal waist, an equivalent propagation law can be written

wx2(z)=w0x2+[Mx2λπw0x]2(z−z0)2,w_x^2(z) = w_{0x}^2 + \left[ \frac{M_x^2\lambda}{ \pi w_{0x} } \right]^2 (z-z_0)^2,

where wx=2σxw_x=2\sigma_x is the second-moment radius.

For an ideal fundamental Gaussian, Mx2=My2=1M_x^2=M_y^2=1. Larger values indicate a larger waist–divergence product, but do not uniquely identify the underlying mode mixture. Important limitations are:

  • M2M^2 does not determine optical linewidth, polarization, or coherence;
  • one transverse image cannot determine M2M^2;
  • sensor noise at large radius can dominate a second moment;
  • aperture clipping can make a measured beam appear deceptively narrow;
  • strongly astigmatic beams need a full two-axis or four-dimensional moment treatment;
  • a good M2M^2 fit does not prove that the field is an exact cavity eigenmode.

Let nμn_\mu be the photon number or a proportional modal intensity. A generic multimode rate equation is

dnμdt=[Gμ({nν})−κμ]nμ+Sμ.\frac{dn_\mu}{dt} = \left[ G_\mu(\{n_\nu\}) - \kappa_\mu \right] n_\mu + S_\mu.

GμG_\mu is saturated modal gain, κμ\kappa_\mu is modal loss, and SμS_\mu represents spontaneous or other source terms. Near a stationary operating point, a useful expansion is

Gμ−κμ≃aμ−∑νbμνnν.G_\mu-\kappa_\mu \simeq a_\mu - \sum_\nu b_{\mu\nu}n_\nu.

Here:

  • aμa_\mu is the unsaturated excess gain;
  • bμμb_{\mu\mu} is self-saturation;
  • bμνb_{\mu\nu} with μ≠ν\mu\ne\nu is cross-saturation.

Ignoring source terms well above threshold gives

dnμdt=[aμ−∑νbμνnν]nμ.\frac{dn_\mu}{dt} = \left[ a_\mu - \sum_\nu b_{\mu\nu}n_\nu \right] n_\mu.

The first mode to cross threshold need not remain the only mode. Pump redistribution, thermal lensing, or weaker cross-saturation can let a second mode turn on later and suppress, coexist with, or destabilize the first.

For two modes,

n˙1=(a1−b11n1−b12n2)n1,n˙2=(a2−b21n1−b22n2)n2.\begin{aligned} \dot n_1 &= \left( a_1 - b_{11}n_1 - b_{12}n_2 \right)n_1, \\ \dot n_2 &= \left( a_2 - b_{21}n_1 - b_{22}n_2 \right)n_2. \end{aligned}

Besides the off state and the two single-mode states, a coexistence solution has

n1∗=a1b22−a2b12D,n2∗=a2b11−a1b21D,D=b11b22−b12b21.\begin{aligned} n_1^* &= \frac{ a_1b_{22}-a_2b_{12} }{ D }, \\ n_2^* &= \frac{ a_2b_{11}-a_1b_{21} }{ D }, \\ D &= b_{11}b_{22} - b_{12}b_{21}. \end{aligned}

Physical coexistence requires both numerators and DD to give positive populations. A useful dimensionless coupling is

C=b12b21b11b22.C = \frac{ b_{12}b_{21} }{ b_{11}b_{22} }.

For the symmetric case, C<1C<1 permits stable coexistence: self-saturation is stronger than the combined cross-saturation. When C>1C>1, the coexistence fixed point is unstable and one single-mode branch tends to exclude the other. Unequal excess gains decide which branch is reached; hysteresis or noise-driven switching can occur in suitable parameter ranges.

The model is local to a regime where mode shapes and saturation coefficients are fixed. It does not capture coherent population oscillations, beating near a material relaxation rate, four-wave mixing, or a mode basis that changes with pump.

For a local saturable gain medium, a schematic overlap is

bμν∝∫gainW(r)∣uμ(r)∣2∣uν(r)∣2 d3r,b_{\mu\nu} \propto \int_{\mathrm{gain}} W(\mathbf r) |u_\mu(\mathbf r)|^2 |u_\nu(\mathbf r)|^2 \,d^3r,

where WW includes pump distribution, material density, and local saturation physics. Modes occupying different pumped regions interact weakly; modes sampling the same inversion interact strongly.

In a homogeneously broadened ensemble, each emitter contributes across the same line. Spectrally nearby modes then draw on nearly the same population, so cross-saturation can be comparable to self-saturation. This often favors a small number of oscillating frequencies.

In an inhomogeneously broadened ensemble, different frequency classes respond at different detunings. Two sufficiently separated modes can saturate partly distinct subensembles. Cross-saturation is then weaker and multifrequency oscillation is easier.

This contrast is not absolute. Velocity-changing collisions, spectral diffusion, population transport, power broadening, and coherent effects can reconnect nominally separate classes.

Spatial hole burning is nonuniform depletion in position. Spectral hole burning is nonuniform depletion across an inhomogeneous frequency distribution. Both leave unsaturated resources that another mode can use. They should not be conflated:

  • a standing-wave cavity can exhibit spatial holes even in a homogeneous line;
  • a traveling-wave cavity can exhibit spectral holes in an inhomogeneous line;
  • a real gain medium can exhibit both simultaneously.

Diffusion, ballistic motion, carrier transport, and collisions refill holes. Fast transport makes the reservoir more nearly uniform and strengthens competition. Slow transport preserves local depletion and supports more independent modal reservoirs.

Mode selection works by changing excess gain aμa_\mu, saturation bμνb_{\mu\nu}, or both.

  • Shorten the cavity so νFSR\nu_{\mathrm{FSR}} exceeds the usable gain width.
  • Add an etalon, grating, distributed reflector, or frequency-selective external cavity.
  • Use a unidirectional ring to reduce standing-wave spatial hole burning.
  • Seed the desired mode strongly enough to capture the available gain.
  • Stabilize cavity length and gain-medium temperature to prevent hopping.

An intracavity filter does not merely “pick a frequency.” It changes loss, dispersion, group delay, and often spatial mode matching.

  • Match the pumped region to the desired fundamental mode.
  • Use an aperture where higher-order modes have more intensity.
  • Choose mirror curvature and cavity geometry with adequate mode discrimination.
  • Reduce aberration, thermal lens asymmetry, and gain guiding.
  • Couple into a single-mode waveguide or fiber when appropriate.

Apertures trade discrimination against diffraction loss and power handling. At high power, deliberately larger or higher-order modes can reduce intensity on optics; lowest order is not automatically optimal.

Birefringent elements, anisotropic gain, Brewster surfaces, wave plates, and polarizers split polarization modes. Faraday rotators or other nonreciprocal elements can favor one ring direction. Backscattering and polarization coupling must still be measured rather than assumed absent.

Consider an empty symmetric linear cavity with

L=0.100 m,R1=R2=0.200 m.L = 0.100\ \mathrm{m}, \qquad R_1=R_2 = 0.200\ \mathrm{m}.

Then

g1=g2=1−LRi=12,g_1=g_2 = 1-\frac{L}{R_i} = \frac12,

so

α=arccos⁡(12)=π3.\alpha = \arccos \left( \frac12 \right) = \frac{\pi}{3}.

Using c=2.99792458×108 m s−1c=2.99792458\times10^8\ \mathrm{m\,s^{-1}},

νFSR=c2L≃1.499 GHz.\nu_{\mathrm{FSR}} = \frac{c}{2L} \simeq 1.499\ \mathrm{GHz}.

One transverse-order step is

Δν⊥=13νFSR≃0.500 GHz.\Delta\nu_\perp = \frac13 \nu_{\mathrm{FSR}} \simeq 0.500\ \mathrm{GHz}.

The frequency factor for total order NN is

q+N+13.q+\frac{N+1}{3}.

Therefore

νq,N=3=νq+1,N=0.\nu_{q,N=3} = \nu_{q+1,N=0}.

The third-order transverse manifold is degenerate with the next longitudinal fundamental resonance in the ideal model. A small astigmatism splits the HG members; finite apertures give them different losses; pump overlap gives them different gains. The observed lasing spectrum is thus the perturbed active problem, not merely the ideal frequency table.

  1. Calling every bright central spot TEM₀₀. A camera image lacks phase, and unresolved mixtures can look nearly Gaussian.
  2. Using TEM without declaring the convention. In open optical resonators the fields are approximately transverse; exact vector modes can contain longitudinal components.
  3. Confusing longitudinal and transverse single-mode operation. These are independent claims.
  4. Treating LG+ℓ\mathrm{LG}_{+\ell} and LG−ℓ\mathrm{LG}_{-\ell} as distinguishable by intensity. Their ideal intensities are identical.
  5. Equating a donut with orbital angular momentum. Phase winding, not annular intensity alone, establishes ℓ\ell.
  6. Reading field signs from intensity lobes. Squaring removes the sign.
  7. Using M2M^2 as a complete mode decomposition. It is one second-moment propagation metric.
  8. Applying spherical-cavity formulas to a thermally distorted laser. The active mode and Gouy phase can depend on pump.
  9. Assuming the lowest-loss mode always wins far above threshold. Nonlinear cross-saturation and mode reshaping can reorder the branches.
  10. Calling all holes spatial hole burning. Frequency-selective depletion is spectral hole burning.

For an unfamiliar laser:

  1. Specify whether the question concerns frequency, transverse field, polarization, direction, or temporal statistics.
  2. Compute or measure passive resonances and losses before adding gain.
  3. Choose a basis matched to the actual symmetry and waist.
  4. Record transverse profiles at several axial planes with calibrated background and sensor area.
  5. Resolve optical frequencies or beat notes on the relevant bandwidth.
  6. Add phase-sensitive or projective measurements if modal coefficients are required.
  7. Vary pump and alignment to distinguish a fixed passive mode from an active, pump-dependent mode.
  8. Fit a multimode saturation model only after checking whether its mode shapes remain approximately fixed.

The result should state both the inferred mode content and the evidence that rules out plausible alternatives.

At a fixed plane, let

u00(r)=Aexp⁡(−r2w2).u_{00}(r) = A \exp \left( -\frac{r^2}{w^2} \right).

Find A>0A>0 from

∫R2∣u00∣2 d2r=1.\int_{\mathbb R^2} |u_{00}|^2\,d^2r = 1.

Verify that r=wr=w is the e−2e^{-2} intensity radius.

Solution

Using polar coordinates,

1=2πA2∫0∞rexp⁡(−2r2w2)dr=2πA2w24.\begin{aligned} 1 &= 2\pi A^2 \int_0^\infty r \exp \left( -\frac{2r^2}{w^2} \right) dr \\ &= 2\pi A^2 \frac{w^2}{4}. \end{aligned}

Therefore

A=2π1w.A = \sqrt{\frac{2}{\pi}} \frac{1}{w}.

The intensity ratio is

I(r)I(0)=exp⁡(−2r2w2).\frac{I(r)}{I(0)} = \exp \left( -\frac{2r^2}{w^2} \right).

At r=wr=w this equals e−2e^{-2}. The rms radius and diameter are different quantities.

For the ideal mode HG20\mathrm{HG}_{20}:

  1. find its total transverse order;
  2. locate its nodal lines at the waist;
  3. state its parity under x↦−xx\mapsto-x and y↦−yy\mapsto-y;
  4. find Mx2M_x^2 and My2M_y^2.

Use H2(ξ)=4ξ2−2H_2(\xi)=4\xi^2-2.

Solution

The total order is

N=m+n=2.N = m+n = 2.

The Hermite argument is

ξ=2 xw0.\xi = \frac{\sqrt2\,x}{w_0}.

H2(ξ)=0H_2(\xi)=0 at ξ=±1/2\xi=\pm1/\sqrt2, so the vertical nodal lines are

x=±w02.x = \pm\frac{w_0}{2}.

There is no horizontal nodal line because n=0n=0. H2H_2 is even and H0=1H_0=1, so the field is even under both reflections. Finally,

Mx2=2m+1=5,My2=2n+1=1.M_x^2 = 2m+1 = 5, \qquad M_y^2 = 2n+1 = 1.

The mode is diffraction-limited in the yy direction but not in the xx direction.

Consider LG1−2\mathrm{LG}_{1}^{-2}.

  1. How many radial nodes does it have?
  2. What happens to its intensity on the axis?
  3. What is its total transverse order?
  4. What is its paraxial axial orbital angular momentum per photon?
  5. Can an ideal intensity image distinguish it from LG1+2\mathrm{LG}_{1}^{+2}?
Solution

p=1p=1 gives one radial node. Because ∣ℓ∣=2|\ell|=2, the amplitude contains r2r^2 and vanishes quadratically on the axis; the intensity vanishes as r4r^4.

The total order and beam quality are

N=2p+∣ℓ∣=4,N = 2p+|\ell| = 4,

and

M2=N+1=5.M^2 = N+1 = 5.

The azimuthal factor is e−2iϕe^{-2i\phi}, so

Lz=−2ℏL_z = -2\hbar

per photon in the scalar paraxial description. Changing ℓ\ell from −2-2 to +2+2 complex-conjugates the azimuthal phase but leaves ∣u∣2|u|^2 unchanged. An ideal intensity image cannot determine the sign. Interference or another phase-sensitive measurement is required.

For the symmetric cavity in the worked example,

α=π3.\alpha = \frac{\pi}{3}.

Show that every increase of three in total transverse order can be offset by one longitudinal free spectral range. Give one HG mode of order three that is degenerate with a neighboring fundamental mode.

Solution

The dimensionless resonance factor is

q+N+13.q+\frac{N+1}{3}.

Increasing NN by three adds one:

q+N+43=(q+1)+N+13.q+\frac{N+4}{3} = (q+1)+\frac{N+1}{3}.

For N=0N=0 and N=3N=3,

νq,3=νq+1,0.\nu_{q,3} = \nu_{q+1,0}.

The order-three HG modes are

HG30,HG21,HG12,HG03.\mathrm{HG}_{30}, \quad \mathrm{HG}_{21}, \quad \mathrm{HG}_{12}, \quad \mathrm{HG}_{03}.

Thus, for example, HG30\mathrm{HG}_{30} with longitudinal index qq is degenerate with HG00\mathrm{HG}_{00} at q+1q+1 in the ideal cavity. Apertures, astigmatism, gain overlap, and aberration generally split their thresholds even when their ideal frequencies coincide.

An astigmatic cavity has

αx=π3,αy=π4,νFSR=1.50 GHz.\alpha_x = \frac{\pi}{3}, \qquad \alpha_y = \frac{\pi}{4}, \qquad \nu_{\mathrm{FSR}} = 1.50\ \mathrm{GHz}.

Find νq10−νq01\nu_{q10}-\nu_{q01}.

Solution

Using the axis-resolved spectrum,

νq10−νq01=αx−αyπνFSR=(13−14)(1.50 GHz)=0.125 GHz.\begin{aligned} \nu_{q10}-\nu_{q01} &= \frac{\alpha_x-\alpha_y}{\pi} \nu_{\mathrm{FSR}} \\ &= \left( \frac13-\frac14 \right) (1.50\ \mathrm{GHz}) \\ &= 0.125\ \mathrm{GHz}. \end{aligned}

Therefore

νq10−νq01=125 MHz.\nu_{q10}-\nu_{q01} = 125\ \mathrm{MHz}.

The sign says that the xx-excited mode lies higher for the stated branch convention.

Take

a1=a2=a>0,b11=b22=b>0,b12=b21=cb.a_1=a_2=a>0, \qquad b_{11}=b_{22}=b>0, \qquad b_{12}=b_{21}=cb.

Find the coexistence fixed point and determine its linear stability for c<1c<1 and c>1c>1.

Solution

Symmetry gives

n1∗=n2∗=n∗.n_1^* = n_2^* = n^*.

The zero-growth condition is

a−bn∗−cbn∗=0,a-bn^*-cbn^* = 0,

so

n∗=ab(1+c).n^* = \frac{a}{b(1+c)}.

At this point, the Jacobian is

J=−bn∗(1cc1).J = -bn^* \begin{pmatrix} 1 & c\\ c & 1 \end{pmatrix}.

Its symmetric and antisymmetric eigenvalues are

λ+=−a,\lambda_+ = -a,

and

λ−=−a1−c1+c.\lambda_- = -a \frac{1-c}{1+c}.

The symmetric perturbation always decays. If c<1c<1, the antisymmetric perturbation also decays and coexistence is stable. If c>1c>1, the antisymmetric perturbation grows: one mode rises while the other falls.

The single-mode state (a/b,0)(a/b,0) gives the absent second mode a small-signal growth rate

a−cbab=a(1−c).a-cb\frac{a}{b} = a(1-c).

It is stable against invasion when c>1c>1. The equivalent statement holds for the other single-mode branch.

7. Quantify standing-wave spatial hole burning

Section titled “7. Quantify standing-wave spatial hole burning”

Define normalized longitudinal intensity patterns on 0<z<L0<z<L by

fq(z)=2sin⁡2(qπzL),f_q(z) = 2 \sin^2 \left( \frac{q\pi z}{L} \right),

so that their spatial average is one. Compute the self-overlap

⟨fq2⟩\left\langle f_q^2 \right\rangle

and the cross-overlap

⟨fqfr⟩\left\langle f_qf_r \right\rangle

for distinct positive integers q≠rq\ne r. Compare the cross-overlap with the self-overlap.

Solution

Using

⟨sin⁡4⟩=38,\left\langle \sin^4 \right\rangle = \frac38,

the self-overlap is

⟨fq2⟩=4⟨sin⁡4⟩=32.\left\langle f_q^2 \right\rangle = 4 \left\langle \sin^4 \right\rangle = \frac32.

For distinct integer harmonics, all oscillatory cross terms average to zero:

⟨sin⁡2(qπzL)sin⁡2(rπzL)⟩=14.\left\langle \sin^2 \left( \frac{q\pi z}{L} \right) \sin^2 \left( \frac{r\pi z}{L} \right) \right\rangle = \frac14.

Hence

⟨fqfr⟩=1.\left\langle f_qf_r \right\rangle = 1.

Relative to self-saturation, the cross-saturation from this ideal longitudinal overlap is

⟨fqfr⟩⟨fq2⟩=23.\frac{ \langle f_qf_r\rangle }{ \langle f_q^2\rangle } = \frac23.

Different standing waves therefore compete less strongly than a mode competes with itself. In an ideal uniform traveling wave, f=1f=1 and both self- and cross-overlaps equal one. This calculation isolates the spatial effect; spectral and transverse overlaps can change the full coefficient.

8. Decide when a beat note survives detection

Section titled “8. Decide when a beat note survives detection”

Two fields are

E=a1u1(x,y)e−iω1t+a2u2(x,y)e−iω2t.\mathcal E = a_1u_1(x,y)e^{-i\omega_1t} + a_2u_2(x,y)e^{-i\omega_2t}.

Derive the interference term in the intensity. Explain when it disappears because of detector bandwidth and when it disappears because of spatial integration.

Solution

The intensity contains

I(x,y,t)∝∣a1∣2∣u1∣2+∣a2∣2∣u2∣2+2Re⁡[a1a2∗u1u2∗e−i(ω1−ω2)t].\begin{aligned} I(x,y,t) \propto& |a_1|^2|u_1|^2 + |a_2|^2|u_2|^2 \\ &+ 2\operatorname{Re} \left[ a_1a_2^* u_1u_2^* e^{-i(\omega_1-\omega_2)t} \right]. \end{aligned}

The last line oscillates at

Ω=∣ω1−ω2∣.\Omega = |\omega_1-\omega_2|.

A detector whose integration time is much longer than 2π/Ω2\pi/\Omega averages that term to zero. A sufficiently fast local detector can retain it.

Even a fast detector that integrates the complete transverse plane gives a cross term proportional to

∫u1u2∗ dx dy.\int u_1u_2^* \,dx\,dy.

This vanishes for exactly orthogonal modes. A finite aperture, local detector, deliberate mode projection, or imperfect orthogonality can restore the beat. Detector bandwidth and spatial orthogonality are therefore independent reasons for a missing signal.

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