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The AC Stark shift, or light shift, is the displacement of a quantum energy level caused by an oscillating electromagnetic field. In its simplest form, an off-resonant drive couples two bare states without transferring much population. The coupling nevertheless changes the eigenvalues:

δEg≃−ℏ∣Ω∣24Δ,δEe≃+ℏ∣Ω∣24Δ.\delta E_g \simeq - \frac{ \hbar|\Omega|^2 }{ 4\Delta }, \qquad \delta E_e \simeq + \frac{ \hbar|\Omega|^2 }{ 4\Delta }.

Here

Δ=ω0−ωL\Delta = \omega_0-\omega_L

is the atom-minus-laser detuning, and Ω\Omega is the resonant Rabi-frequency coefficient in the Hamiltonian convention stated below. A red-detuned field has Δ>0\Delta>0: it shifts the ground state downward and the excited state upward in this ideal two-level model.

The shift moves spectroscopic resonances, accumulates coherent phase, creates state-dependent optical potentials, and supplies both a control resource and a systematic error.

Required background. Two-Level Atom defines the Hamiltonian, Rabi Oscillations explains coherent mixing, Dipole Approximation supplies the interaction, and Harmonic Perturbations introduces the two frequency denominators.

The full multilevel response and magic-frequency calculation are developed in Dynamic Polarizability.

Use two bare states satisfying

H0∣g⟩=Eg∣g⟩,H0∣e⟩=Ee∣e⟩,H_0|g\rangle = E_g|g\rangle, \qquad H_0|e\rangle = E_e|e\rangle,

with

ℏω0=Ee−Eg>0.\hbar\omega_0 = E_e-E_g > 0.

The applied electric field is

E(t)=E0ϵcos⁡(ωLt+ϕ),\mathbf E(t) = E_0 \boldsymbol\epsilon \cos \left( \omega_Lt+\phi \right),

where:

  • E0E_0 is a peak amplitude;
  • ϵ\boldsymbol\epsilon is a real unit polarization for the basic two-level derivation;
  • Δ=ω0−ωL\Delta=\omega_0-\omega_L;
  • red detuning means Δ>0\Delta>0;
  • blue detuning means Δ<0\Delta<0;
  • Ω\Omega is chosen nonnegative after absorbing any sign into ϕ\phi;
  • frequency variables are angular frequencies unless stated otherwise; decay rates are inverse times, not oscillation frequencies.

For a polarization-selected electric-dipole matrix element,

deg=⟨e∣d⋅ϵ∣g⟩,d_{eg} = \langle e| \mathbf d\mathbin{\cdot}\boldsymbol\epsilon |g\rangle,

the Rabi-frequency magnitude is

Ω=E0∣deg∣ℏ.\Omega = \frac{ E_0|d_{eg}| }{ \hbar }.

Because E0E_0 is a peak amplitude, a vacuum plane wave has cycle-averaged intensity

I=12ϵ0cE02.I = \frac12 \epsilon_0cE_0^2.

Using an RMS electric field in a peak-amplitude formula creates a factor-of-two error.

In the electric-dipole approximation,

V(t)=−d⋅E(t).V(t) = - \mathbf d\mathbin{\cdot}\mathbf E(t).

Within the selected two-state subspace and after a convenient phase choice, the interaction contains

ℏΩcos⁡(ωLt+ϕ)(σ++σ−),\hbar\Omega \cos \left( \omega_Lt+\phi \right) \left( \sigma_++\sigma_- \right),

up to an overall sign that can be absorbed into ϕ\phi. Expanding the cosine produces co-rotating terms near the slow mismatch

ω0−ωL=Δ\omega_0-\omega_L = \Delta

and counter-rotating terms near the fast sum

ω0+ωL.\omega_0+\omega_L.

The RWA drops the fast pair. This is a dynamical approximation separate from the two-level and electric-dipole approximations.

In the ordered basis (∣e⟩,∣g⟩)(|e\rangle,|g\rangle), remove an irrelevant common energy and choose ϕ=0\phi=0. The retained Hamiltonian is

HRWA=ℏ2(ΔΩΩ−Δ).H_{\mathrm{RWA}} = \frac{\hbar}{2} \begin{pmatrix} \Delta & \Omega \\ \Omega & -\Delta \end{pmatrix}.

Equivalently,

HRWA=ℏ2(Δσz+Ωσx).H_{\mathrm{RWA}} = \frac{\hbar}{2} \left( \Delta\sigma_z + \Omega\sigma_x \right).

The generalized Rabi frequency is

ΩR=Δ2+Ω2.\Omega_R = \sqrt{ \Delta^2+\Omega^2 }.

The eigenvalues are

ε±=±ℏΩR2.\varepsilon_\pm = \pm \frac{\hbar\Omega_R}{2}.

These are rotating-frame quasienergies up to an arbitrary common offset and integer shifts of ℏωL\hbar\omega_L. Their differences and their adiabatic connection to the bare levels carry the observable content.

Avoided crossing of detuned two-level dressed energies and the far-detuned light-shift limit

The detuned rotating-wave Hamiltonian converts the bare crossing into an avoided crossing of gap ℏΩ\hbar\Omega. Far from resonance, each bare-connected branch is displaced by a second-order amount proportional to Ω2/Δ\Omega^2/\Delta. At resonance the bare-state shift language fails and the appropriate description is dressed-state splitting.

Following the ground-like and excited-like branches

Section titled “Following the ground-like and excited-like branches”

At Ω=0\Omega=0, the rotating-frame bare energies are

εe(0)=+ℏΔ2,εg(0)=−ℏΔ2.\varepsilon_e^{(0)} = + \frac{\hbar\Delta}{2}, \qquad \varepsilon_g^{(0)} = - \frac{\hbar\Delta}{2}.

When Δ>0\Delta>0, ∣g⟩|g\rangle connects to the lower dressed branch. When Δ<0\Delta<0, it connects to the upper branch. The ground-connected quasienergy can therefore be written

εg,ad=−sgn⁡(Δ)ℏΩR2,\varepsilon_{g,\mathrm{ad}} = - \operatorname{sgn}(\Delta) \frac{\hbar\Omega_R}{2},

and the excited-connected branch has the opposite sign.

Subtracting the corresponding bare quasienergies gives

δEg=−sgn⁡(Δ)ℏ2(ΩR−∣Δ∣),δEe=+sgn⁡(Δ)ℏ2(ΩR−∣Δ∣).\begin{aligned} \delta E_g &= - \operatorname{sgn}(\Delta) \frac{\hbar}{2} \left( \Omega_R-|\Delta| \right), \\ \delta E_e &= + \operatorname{sgn}(\Delta) \frac{\hbar}{2} \left( \Omega_R-|\Delta| \right). \end{aligned}

These expressions remain exact within the constant-drive two-level RWA for Δ≠0\Delta\ne0. They also make the sign reversal across resonance explicit.

At

Δ=0,\Delta=0,

the eigenstates are equal superpositions of ∣g⟩|g\rangle and ∣e⟩|e\rangle, with separation

ε+−ε−=ℏΩ.\varepsilon_+-\varepsilon_- = \hbar\Omega.

Neither branch is uniquely “the shifted ground state” or “the shifted excited state.” A perturbative formula proportional to 1/Δ1/\Delta diverges because its bare-state labeling has lost validity, not because an observable energy becomes infinite.

Near resonance, one should use the dressed-state description or solve the open-system response. A separate weak probe can resolve an Autler–Townes doublet; a single driven transition can show Rabi oscillations and power broadening.

Suppose

∣Ω∣≪∣Δ∣.|\Omega| \ll |\Delta|.

Then

ΩR=∣Δ∣1+Ω2Δ2=∣Δ∣+Ω22∣Δ∣−Ω48∣Δ∣3+O(Ω6∣Δ∣5).\begin{aligned} \Omega_R &= |\Delta| \sqrt{ 1+ \frac{\Omega^2}{\Delta^2} } \\ &= |\Delta| + \frac{\Omega^2}{2|\Delta|} - \frac{\Omega^4}{8|\Delta|^3} + O \left( \frac{\Omega^6}{|\Delta|^5} \right). \end{aligned}

Therefore,

δEg=−ℏΩ24Δ+ℏΩ416Δ3+O(ℏΩ6Δ5),\delta E_g = - \frac{ \hbar\Omega^2 }{ 4\Delta } + \frac{ \hbar\Omega^4 }{ 16\Delta^3 } + O \left( \frac{\hbar\Omega^6}{\Delta^5} \right),

and

δEe=+ℏΩ24Δ−ℏΩ416Δ3+O(ℏΩ6Δ5).\delta E_e = + \frac{ \hbar\Omega^2 }{ 4\Delta } - \frac{ \hbar\Omega^4 }{ 16\Delta^3 } + O \left( \frac{\hbar\Omega^6}{\Delta^5} \right).

The leading two-level differential shift is

δωeg=δEe−δEgℏ≃Ω22Δ.\delta\omega_{eg} = \frac{ \delta E_e-\delta E_g }{ \hbar } \simeq \frac{\Omega^2}{2\Delta}.

This is a shift of the transition frequency. A common shift of both levels would not appear in spectroscopy, although it could still affect center-of-mass motion if it varies in space.

Under the convention Δ=ω0−ωL\Delta=\omega_0-\omega_L:

  • red detuning has Δ>0\Delta>0 and gives δEg<0\delta E_g<0;
  • blue detuning has Δ<0\Delta<0 and gives δEg>0\delta E_g>0;
  • the excited-state shift has the opposite sign in the closed two-level model;
  • changing to the alternative convention ΔL=ωL−ω0\Delta_L=\omega_L-\omega_0 reverses every displayed denominator.

The reliable procedure is to derive the shift from the declared Hamiltonian, not to memorize “red is negative” without recording the detuning definition.

Define

η=∣Ω∣∣Δ∣.\eta = \frac{|\Omega|}{|\Delta|}.

The exact magnitude of the ground-branch shift is

∣δEg∣exact=ℏ∣Δ∣2(1+η2−1).|\delta E_g|_{\mathrm{exact}} = \frac{ \hbar|\Delta| }{ 2 } \left( \sqrt{1+\eta^2}-1 \right).

The leading approximation is

∣δEg∣(2)=ℏ∣Δ∣η24.|\delta E_g|_{(2)} = \frac{ \hbar|\Delta|\eta^2 }{ 4 }.

Their relative difference begins as

∣δEg∣(2)−∣δEg∣exact∣δEg∣exact=η24+O(η4).\frac{ |\delta E_g|_{(2)} - |\delta E_g|_{\mathrm{exact}} }{ |\delta E_g|_{\mathrm{exact}} } = \frac{\eta^2}{4} + O(\eta^4).

Thus a small excited-state population is not the only accuracy criterion. Long coherent evolution can resolve a fourth-order phase correction even when η2≪1\eta^2\ll1.

For ∣Ω/Δ∣≪1|\Omega/\Delta|\ll1, the ground-connected dressed state contains an excited-state amplitude of order

ce∼−Ω2Δ.c_e \sim - \frac{\Omega}{2\Delta}.

Its excited-state probability is therefore

Pe(adm)∼Ω24Δ2.P_e^{(\mathrm{adm})} \sim \frac{\Omega^2}{4\Delta^2}.

The word virtual means that the excited component is part of an off-resonant dressed eigenstate rather than an independently populated, energy-conserving final state. It does not mean that energy conservation may be violated for a time fixed by an uncertainty relation.

The energy shift is first order in the small admixture amplitude times the coupling, hence second order in Ω\Omega:

δE∼ℏΩ(ΩΔ).\delta E \sim \hbar\Omega \left( \frac{\Omega}{\Delta} \right).

Phase accumulation without population transfer

Section titled “Phase accumulation without population transfer”

If a pulse begins and ends with zero field and the system follows the same bare-connected dressed branch throughout, its final state is

∣ψn(T)⟩∼exp⁡[−iℏ∫0TδEn(t) dt]∣n⟩,|\psi_n(T)\rangle \sim \exp \left[ - \frac{i}{\hbar} \int_0^T \delta E_n(t)\,dt \right] |n\rangle,

apart from the bare dynamical phase and any geometric contribution. While the field is on, the state is the instantaneous dressed vector, not exactly the bare ∣n⟩|n\rangle.

For a far-detuned ground state,

ϕg(LS)=−1ℏ∫0TδEg(t) dt≃∫0T∣Ω(t)∣24Δ(t)dt.\begin{aligned} \phi_g^{(\mathrm{LS})} &= - \frac1\hbar \int_0^T \delta E_g(t)\,dt \\ &\simeq \int_0^T \frac{ |\Omega(t)|^2 }{ 4\Delta(t) } dt. \end{aligned}

A tiny instantaneous shift can therefore create a large coherent phase over a long interrogation.

Introduce a mixing angle through

tan⁡2θ=ΩΔ.\tan2\theta = \frac{\Omega}{\Delta}.

Then

θ˙=ΔΩ˙−ΩΔ˙2(Δ2+Ω2).\dot\theta = \frac{ \Delta\dot\Omega-\Omega\dot\Delta }{ 2 \left( \Delta^2+\Omega^2 \right) }.

For fixed drive phase and a nonclosing gap, the usual local adiabatic criterion is

∣θ˙∣≪ΩR.|\dot\theta| \ll \Omega_R.

If a pulse switches too abruptly, it can leave coherent population transfer or ringing in addition to the intended phase. “Far detuned” does not by itself guarantee adiabatic turn-on. A varying phase also rotates the coupling axis, and prolonged resonant modulation can accumulate transitions even if an instantaneous ratio is small. Check the complete pulse history.

Rotating and counter-rotating denominators

Section titled “Rotating and counter-rotating denominators”

When Ω\Omega is small compared with both ∣ω0−ωL∣|\omega_0-\omega_L| and ω0+ωL\omega_0+\omega_L, nondegenerate second-order Floquet perturbation theory for a real cosine field gives, for the two-level ground state,

δEg≃−ℏΩ24[1ω0−ωL+1ω0+ωL].\begin{aligned} \delta E_g \simeq - \frac{ \hbar\Omega^2 }{ 4 } \left[ \frac{1}{ \omega_0-\omega_L } + \frac{1}{ \omega_0+\omega_L } \right]. \end{aligned}

The excited-state shift has the opposite sign within this ideal model. The first denominator is the co-rotating contribution retained by the RWA. The second is the leading counter-rotating contribution.

Near resonance,

∣ω0−ωL∣≪ω0+ωL,|\omega_0-\omega_L| \ll \omega_0+\omega_L,

so the RWA term dominates the off-resonant shift. Precision spectroscopy can still resolve the smaller correction.

Near resonance the co-rotating pair must instead be treated as a coupled degenerate subspace. Eliminating only the counter-rotating terms shifts the center of that resonance by

δωBS≃Ω22(ω0+ωL).\delta\omega_{\mathrm{BS}} \simeq \frac{ \Omega^2 }{ 2 \left( \omega_0+\omega_L \right) }.

Near ωL≃ω0\omega_L\simeq\omega_0,

δωBS≃Ω24ω0.\delta\omega_{\mathrm{BS}} \simeq \frac{\Omega^2}{4\omega_0}.

This coefficient follows the present lab-frame convention, in which the RWA Hamiltonian has transverse term ℏΩσx/2\hbar\Omega\sigma_x/2. Other definitions of drive amplitude move factors of two. The Hamiltonian must accompany any quoted Bloch–Siegert formula.

For a real atom or molecule, every dipole-coupled intermediate state brings both rotating and counter-rotating denominators. Contributions can have different signs and can cancel. A two-level estimate is reliable only when one transition dominates both the shift and the relevant scattering error.

For a nondegenerate state ∣n⟩|n\rangle in a weak monochromatic field with peak amplitude E0E_0, define the real dispersive light shift by

δEn=−14Re⁡[αn(ωL)]E02.\delta E_n = - \frac14 \operatorname{Re} \left[ \alpha_n(\omega_L) \right] E_0^2.

Using

I=12ϵ0cE02,I = \frac12\epsilon_0cE_0^2,

the same relation is

δEn=−Re⁡αn(ωL)2ϵ0cI.\delta E_n = - \frac{ \operatorname{Re}\alpha_n(\omega_L) }{ 2\epsilon_0c } I.

The dynamic polarizability packages the complete sum over intermediate states, polarizations, and both frequency denominators. Its imaginary part describes dissipative response under a declared Fourier and linewidth convention.

For the ideal two-level ground state,

αg(ω)=2ω0∣deg∣2ℏ(ω02−ω2).\alpha_g(\omega) = \frac{ 2\omega_0|d_{eg}|^2 }{ \hbar \left( \omega_0^2-\omega^2 \right) }.

Substitution into −αE02/4-\alpha E_0^2/4 reproduces the rotating and counter-rotating shift above.

Because

Erms=E02,E_{\mathrm{rms}} = \frac{E_0}{\sqrt2},

one may also write

δEn=−12Re⁡αn(ω)Erms2.\delta E_n = - \frac12 \operatorname{Re}\alpha_n(\omega) E_{\mathrm{rms}}^2.

For a truly static field of magnitude EdcE_{\mathrm{dc}}, the quadratic shift is

δEndc=−12αn(0)Edc2.\delta E_n^{\mathrm{dc}} = - \frac12 \alpha_n(0) E_{\mathrm{dc}}^2.

The AC formula with a fixed peak amplitude contains the additional cycle-average factor 1/21/2. Taking ω→0\omega\to0 after averaging over an ever-longer cycle is not the same experimental operation as applying a constant field E0E_0.

For angular-momentum manifolds, the response is generally not one scalar number. It decomposes into irreducible contributions.

The scalar shift:

  • is independent of magnetic sublevel within the ideal manifold;
  • follows the local intensity;
  • produces a common trapping potential for states with the same scalar polarizability.

It can still be differential between two clock or qubit states.

The vector shift:

  • depends on optical helicity;
  • changes sign with magnetic quantum number or reversed circular polarization;
  • behaves like a light-induced effective magnetic field;
  • vanishes for ideal linear polarization in the simplest geometry.

Residual ellipticity can therefore convert polarization drift into a frequency shift.

The tensor shift:

  • depends on polarization alignment relative to the quantization axis;
  • produces an even-in-mm splitting pattern;
  • requires sufficient angular momentum at the relevant electronic or hyperfine level;
  • can survive even when vector shifts are canceled by averaging opposite magnetic substates.

Exact normalizations of scalar, vector, and tensor polarizabilities differ among references. A coefficient is incomplete unless the angular-momentum, polarization, and reduced-matrix-element conventions are supplied.

Useful diagnostics include:

  • reverse helicity to isolate vector contributions;
  • compare +m+m and −m-m states;
  • rotate the quantization axis relative to linear polarization;
  • vary intensity to separate leading II and hyperpolarizability I2I^2 terms;
  • vary optical frequency to map dispersive sign changes.

These reversals separate irreducible responses more reliably than a single-intensity measurement.

A far-detuned field does not make the excited-state admixture exactly zero. If the excited state decays at population rate Γ\Gamma, the admixture produces the approximate scattering rate

Γsc≃ΓΩ24Δ2\Gamma_{\mathrm{sc}} \simeq \Gamma \frac{ \Omega^2 }{ 4\Delta^2 }

for a weak, isolated, lifetime-limited two-level transition in the window Γ,Ω≪∣Δ∣≪ω0+ωL\Gamma,\Omega\ll|\Delta|\ll\omega_0+\omega_L. This assumes adiabatic preparation or the weak-drive steady response; sudden turn-on can add transient excited population. Large detuning compared with a linewidth alone does not justify dropping the counter-rotating denominator.

The ground-state light-shift magnitude is

∣Ug∣≃ℏΩ24∣Δ∣.|U_g| \simeq \frac{ \hbar\Omega^2 }{ 4|\Delta| }.

Their ratio is

ℏΓsc∣Ug∣≃Γ∣Δ∣.\frac{ \hbar\Gamma_{\mathrm{sc}} }{ |U_g| } \simeq \frac{\Gamma}{|\Delta|}.

At fixed trap depth or phase rate, larger detuning reduces scattering in this ideal model, but maintaining the same shift then requires intensity proportional to ∣Δ∣|\Delta|. Available power, nearby transitions, photoionization, technical noise, and multilevel interference eventually limit this simple scaling.

Coherent and incoherent errors scale differently

Section titled “Coherent and incoherent errors scale differently”

For one dominant line:

∣δE∣∝I∣Δ∣,Γsc∝IΔ2.|\delta E| \propto \frac{I}{|\Delta|}, \qquad \Gamma_{\mathrm{sc}} \propto \frac{I}{\Delta^2}.

Thus:

  • light-shift phase is first order in 1/Δ1/\Delta;
  • scattering probability is second order in 1/Δ1/\Delta;
  • increasing detuning at fixed intensity reduces both, but the scattering falls faster;
  • increasing intensity to hold the phase fixed leaves a residual scattering cost proportional to 1/∣Δ∣1/|\Delta|.

Real multilevel systems can violate the one-line ratio because amplitudes and decay branches combine differently. Nor is every scattered photon an equal qubit-decoherence event: elastic scattering that cannot distinguish the qubit states may preserve internal coherence while still causing recoil.

If the field intensity varies slowly across the internal wavefunction, the position-dependent light shift becomes a center-of-mass potential:

Un(r)=−Re⁡αn(ωL)2ϵ0cI(r).U_n(\mathbf r) = - \frac{ \operatorname{Re}\alpha_n(\omega_L) }{ 2\epsilon_0c } I(\mathbf r).

The conservative dipole force is

Fn(r)=−∇Un(r).\mathbf F_n(\mathbf r) = - \boldsymbol\nabla U_n(\mathbf r).

In the dominant two-level ground-state limit,

Ug(r)≃−ℏ∣Ω(r)∣24Δ.U_g(\mathbf r) \simeq - \frac{ \hbar|\Omega(\mathbf r)|^2 }{ 4\Delta }.

With this page’s detuning convention:

  • a red-detuned field has Δ>0\Delta>0 and attracts the ground state toward high intensity;
  • a blue-detuned field has Δ<0\Delta<0 and repels it toward low intensity.

For a multilevel atom, the sign of the full polarizability, not the nearest line alone, decides where the atom is trapped.

Treating Un(r)U_n(\mathbf r) as a scalar mechanical potential requires:

  1. internal dressed-state following is adiabatic during motion;
  2. photon scattering is slow on the mechanical time scale;
  3. polarization gradients and vector/tensor forces are controlled;
  4. the field varies slowly over the internal size of the particle;
  5. nonadiabatic transitions at avoided crossings are negligible.

If the local dressed eigenvectors vary in space, motion can also acquire geometric vector and scalar potentials. Those effects are not contained in the simple gradient of one scalar αI\alpha I.

For a transition between states ∣a⟩|a\rangle and ∣b⟩|b\rangle,

δωba=δEb−δEaℏ.\delta\omega_{ba} = \frac{ \delta E_b-\delta E_a }{ \hbar }.

In the scalar polarizability limit,

δνba=−Δαba(ωL)2hϵ0cI,\delta\nu_{ba} = - \frac{ \Delta\alpha_{ba}(\omega_L) }{ 2h\epsilon_0c } I,

where

Δαba=Re⁡(αb−αa).\Delta\alpha_{ba} = \operatorname{Re}(\alpha_b-\alpha_a).

A large common light shift can coexist with a small transition shift. Conversely, a weakly trapped state pair can have a large differential shift.

If particles sample different intensities,

δωba=δωba[I(r)],\delta\omega_{ba} = \delta\omega_{ba} \left[ I(\mathbf r) \right],

then one nominal transition becomes a distribution of local frequencies. The result can be:

  • an inhomogeneously broadened line;
  • an asymmetric line if density and intensity are correlated;
  • dephasing from motion through the gradient;
  • a temperature-dependent fitted center;
  • sidebands when motion is quantized and resolved.

Replacing I(r)I(\mathbf r) by one mean value can bias both line center and linewidth.

A trapping field may be present continuously, while a probe field exists only during interrogation pulses. Their shifts enter differently:

  • a continuous trap changes the energy splitting throughout free evolution;
  • a pulsed probe can add phase only during the pulses;
  • Ramsey and composite-pulse sequences convert that phase into a lock-point shift in a protocol-dependent way;
  • switching transients can produce chirps and nonadiabatic excitation.

A clock correction therefore needs the complete timing sequence, not only a static value of δν/I\delta\nu/I.

A leading electric-dipole magic frequency satisfies

Δαba(ωm)=0\Delta\alpha_{ba}(\omega_{\mathrm m}) = 0

for a specified pair of states, polarization, magnetic sublevel, and geometry. The common optical potential can remain nonzero, allowing confinement with a canceled leading differential shift.

“Magic” does not mean field free. Residual terms can include:

  • vector and tensor light shifts;
  • electric-quadrupole and magnetic-dipole response;
  • hyperpolarizability proportional to I2I^2;
  • multiphoton resonances;
  • motional sampling and lattice anharmonicity;
  • imperfect polarization and magnetic-field alignment.

The clock probe can couple each clock state to off-resonant spectator states. Its differential shift often scales as

δνprobe∝Iprobe\delta\nu_{\mathrm{probe}} \propto I_{\mathrm{probe}}

in the weak-field regime. Useful controls include:

  1. interleave measurements at several probe intensities;
  2. extrapolate to zero intensity only after testing linearity;
  3. apply a calibrated frequency step during pulses;
  4. reverse polarization or magnetic sublevel where symmetry permits;
  5. use hyper-Ramsey or autobalanced protocols when pulse-only shifts dominate;
  6. monitor pulse transients and optical phase chirps independently.

Composite interrogation can suppress sensitivity to a modeled shift, but it does not remove the need to validate the model and bound residual imperfections.

Light Shifts in Raman and Effective Couplings

Section titled “Light Shifts in Raman and Effective Couplings”

In a detuned three-level Raman system, eliminating the intermediate state generates both:

  • an off-diagonal two-photon coupling of order Ω1∗Ω2/Δ\Omega_1^*\Omega_2/\Delta;
  • diagonal light shifts of order ∣Ω1∣2/Δ|\Omega_1|^2/\Delta and ∣Ω2∣2/Δ|\Omega_2|^2/\Delta.

They occur at the same perturbative order. Keeping the effective Raman coupling while dropping both diagonal shifts is generally inconsistent.

For beam 1 coupling ∣1⟩|1\rangle to the intermediate level and beam 2 coupling ∣2⟩|2\rangle, define δ2ph=(E2−E1)/ℏ−(ω1−ω2)\delta_{\rm 2ph}=(E_2-E_1)/\hbar-(\omega_1-\omega_2). The effective detuning includes the differential light shift:

δ2ph,eff=δ2ph+δE2−δE1ℏ.\delta_{\mathrm{2ph,eff}} = \delta_{\mathrm{2ph}} + \frac{ \delta E_2-\delta E_1 }{ \hbar }.

Balancing intensities can cancel a differential shift in one idealized model, but unequal detunings, hyperfine pathways, polarization impurity, spontaneous scattering, and spatial mode mismatch can leave a residual.

In the perturbative scalar regime,

νobs(I)=ν0+κI,\nu_{\mathrm{obs}}(I) = \nu_0+\kappa I,

with

κ=−Δα2hϵ0c.\kappa = - \frac{ \Delta\alpha }{ 2h\epsilon_0c }.

A reliable extraction should test:

  • linearity over the fitted intensity range;
  • calibration of intensity at the particle rather than at a remote monitor;
  • spatial averaging and temperature dependence;
  • polarization and magnetic-field stability;
  • correlations between intensity and line-shape asymmetry.

Curvature can indicate hyperpolarizability, saturation, changing spatial sampling, or a drifting population distribution.

For one dominant spectator line,

δE∝1Δ,\delta E \propto \frac{1}{\Delta},

so the shift changes sign across resonance. Close enough to resonance, however, scattering and dressed-state splitting invalidate the purely dispersive fit. Excluding the central region is a physical model choice, not merely a plotting preference.

If the same field drives the intended transition and couples off-resonantly to spectators, changing pulse area by changing intensity also changes the light shift. A Rabi-frequency calibration and a frequency calibration are then coupled. Jointly fitting power-dependent chevrons or Ramsey phases is safer than fixing a zero-power resonance center.

1. Sudden turn-on versus adiabatic preparation

Section titled “1. Sudden turn-on versus adiabatic preparation”

A far-detuned field is switched on instantaneously from ∣g⟩|g\rangle. Compare the maximum and time-averaged excited populations with the excited admixture in the ground-connected dressed eigenstate.

Solution

The closed-system population is

Pe(t)=Ω2Δ2+Ω2sin⁡2Δ2+Ω2 t2.P_e(t)=\frac{\Omega^2}{\Delta^2+\Omega^2} \sin^2\frac{\sqrt{\Delta^2+\Omega^2}\,t}{2}.

Thus Pe,max⁡≃Ω2/Δ2P_{e,\max}\simeq\Omega^2/\Delta^2 and its many-cycle average is Ω2/(2Δ2)\Omega^2/(2\Delta^2). Adiabatically following the ground-connected branch instead gives Peadm≃Ω2/(4Δ2)P_e^{\rm adm}\simeq\Omega^2/(4\Delta^2). Sudden preparation occupies both dressed branches, whose interference produces the oscillation. A single “virtual population” estimate does not describe every preparation. These comparisons assume negligible decay during the averaging interval.

Let

η=∣Ω∣∣Δ∣.\eta = \frac{|\Omega|}{|\Delta|}.

Evaluate the exact and second-order ground-shift magnitudes in units of ℏ∣Δ∣\hbar|\Delta| for η=0.20\eta=0.20. Find their relative difference.

Solution

The exact dimensionless magnitude is

∣δEg∣exactℏ∣Δ∣=12(1+η2−1).\frac{ |\delta E_g|_{\mathrm{exact}} }{ \hbar|\Delta| } = \frac12 \left( \sqrt{1+\eta^2}-1 \right).

At η=0.20\eta=0.20,

1+η2=1.04≃1.0198039,\sqrt{1+\eta^2} = \sqrt{1.04} \simeq 1.0198039,

so

∣δEg∣exactℏ∣Δ∣≃0.00990195.\frac{ |\delta E_g|_{\mathrm{exact}} }{ \hbar|\Delta| } \simeq 0.00990195.

Second order gives

∣δEg∣(2)ℏ∣Δ∣=η24=0.0100000.\frac{ |\delta E_g|_{(2)} }{ \hbar|\Delta| } = \frac{\eta^2}{4} = 0.0100000.

The relative overestimate is

ϵrel=0.0100000−0.009901950.00990195≃9.90×10−3.\begin{aligned} \epsilon_{\mathrm{rel}} &= \frac{ 0.0100000-0.00990195 }{ 0.00990195 } \\ &\simeq 9.90\times10^{-3}. \end{aligned}

Thus the second-order result is high by about 0.99%0.99\%.

A two-level atom has

Δ=2π×1.00 GHz,Ω=2π×20.0 MHz.\begin{aligned} \Delta &= 2\pi\times1.00\ \mathrm{GHz}, \\ \Omega &= 2\pi\times20.0\ \mathrm{MHz}. \end{aligned}

Estimate:

  1. the ground-state light shift in ordinary frequency;
  2. the excited-state admixture probability;
  3. the scattering rate if Γ=2π×6.00 MHz\Gamma=2\pi\times6.00\ \mathrm{MHz}.
Solution

The angular-frequency light shift is

δEgℏ≃−Ω24Δ.\frac{\delta E_g}{\hbar} \simeq - \frac{\Omega^2}{4\Delta}.

Dividing by 2π2\pi and using ordinary-frequency values consistently,

δEgh≃−(20.0 MHz)24(1000 MHz)=−0.100 MHz.\frac{\delta E_g}{h} \simeq - \frac{ (20.0\ \mathrm{MHz})^2 }{ 4(1000\ \mathrm{MHz}) } = -0.100\ \mathrm{MHz}.

Thus

δEgh≃−100 kHz.\frac{\delta E_g}{h} \simeq -100\ \mathrm{kHz}.

The admixture probability is

Pe(adm)≃14(20.01000)2=1.00×10−4.P_e^{(\mathrm{adm})} \simeq \frac14 \left( \frac{20.0}{1000} \right)^2 = 1.00\times10^{-4}.

The scattering rate is

Γsc≃ΓPe(adm).\Gamma_{\mathrm{sc}} \simeq \Gamma P_e^{(\mathrm{adm})}.

Therefore,

Γsc≃2π×600 Hz,\Gamma_{\mathrm{sc}} \simeq 2\pi\times600\ \mathrm{Hz},

or about

3.77×103 s−1.3.77\times10^3\ \mathrm{s^{-1}}.

A far-detuned field has constant detuning Δ\Delta and Rabi envelope

Ω(t)=Ω0e−t2/(2τ2).\Omega(t) = \Omega_0 e^{-t^2/(2\tau^2)}.

Find the light-shift phase accumulated by the ground state from t=−∞t=-\infty to +∞+\infty.

Solution

The ground-state phase is

ϕg(LS)≃∫−∞∞∣Ω(t)∣24Δdt.\phi_g^{(\mathrm{LS})} \simeq \int_{-\infty}^{\infty} \frac{ |\Omega(t)|^2 }{ 4\Delta } dt.

Because

∣Ω(t)∣2=Ω02e−t2/τ2,|\Omega(t)|^2 = \Omega_0^2e^{-t^2/\tau^2},

and

∫−∞∞e−t2/τ2 dt=π τ,\int_{-\infty}^{\infty} e^{-t^2/\tau^2}\,dt = \sqrt\pi\,\tau,

the result is

ϕg(LS)=π Ω02τ4Δ.\phi_g^{(\mathrm{LS})} = \frac{ \sqrt\pi\, \Omega_0^2\tau }{ 4\Delta }.

Its sign follows the sign of Δ\Delta. The result assumes adiabatic following and negligible scattering.

Let

ωL≃ω0=2π×5.00 GHz,\omega_L \simeq \omega_0 = 2\pi\times5.00\ \mathrm{GHz},

and

Ω=2π×50.0 MHz.\Omega = 2\pi\times50.0\ \mathrm{MHz}.

Estimate the Bloch–Siegert shift in ordinary frequency using this page’s Hamiltonian convention.

Solution

Near resonance,

δωBS≃Ω24ω0.\delta\omega_{\mathrm{BS}} \simeq \frac{\Omega^2}{4\omega_0}.

Because every angular frequency contains one common factor 2π2\pi,

δωBS2π=(50.0 MHz)24(5000 MHz).\frac{ \delta\omega_{\mathrm{BS}} }{ 2\pi } = \frac{ (50.0\ \mathrm{MHz})^2 }{ 4(5000\ \mathrm{MHz}) }.

Hence

δωBS2π=0.125 MHz=125 kHz.\frac{ \delta\omega_{\mathrm{BS}} }{ 2\pi } = 0.125\ \mathrm{MHz} = 125\ \mathrm{kHz}.

The correction is small compared with the carrier frequency but can be large compared with a precision spectroscopic uncertainty.

6. Optical potential and scattering budget

Section titled “6. Optical potential and scattering budget”

A ground-state optical trap has depth

∣U∣h=1.00 MHz.\frac{|U|}{h} = 1.00\ \mathrm{MHz}.

The dominant optical line has

Γ=2π×6.00 MHz,∣Δ∣=2π×100 GHz.\begin{aligned} \Gamma &= 2\pi\times6.00\ \mathrm{MHz}, \\ |\Delta| &= 2\pi\times100\ \mathrm{GHz}. \end{aligned}

Use the two-level far-detuned ratio to estimate the scattering rate, assuming the carrier frequency is much larger than this detuning.

Solution

Use

Γsc≃Γ∣Δ∣∣U∣ℏ.\Gamma_{\mathrm{sc}} \simeq \frac{\Gamma}{|\Delta|} \frac{|U|}{\hbar}.

The frequency ratio is

Γ∣Δ∣=6.00×1061.00×1011=6.00×10−5.\frac{\Gamma}{|\Delta|} = \frac{ 6.00\times10^6 }{ 1.00\times10^{11} } = 6.00\times10^{-5}.

Also,

∣U∣ℏ=2π×1.00×106 s−1.\frac{|U|}{\hbar} = 2\pi\times1.00\times10^6\ \mathrm{s^{-1}}.

Therefore,

Γsc≃(6.00×10−5)(2π×106)≃377 s−1.\begin{aligned} \Gamma_{\mathrm{sc}} &\simeq (6.00\times10^{-5}) (2\pi\times10^6) \\ &\simeq 377\ \mathrm{s^{-1}}. \end{aligned}

The estimated mean scattering time is about 2.65 ms2.65\ \mathrm{ms}. A real atom requires a multilevel calculation before treating this number as predictive.

At one lattice frequency,

Δαh=2.00×10−4Hz m2V2.\frac{ \Delta\alpha }{ h } = 2.00\times10^{-4} \frac{ \mathrm{Hz\,m^2} }{ \mathrm{V^2} }.

The peak electric-field amplitude is

E0=1.00×104 V/m.E_0 = 1.00\times10^4\ \mathrm{V/m}.

Find the scalar differential clock shift. What happens to the leading result at a magic frequency?

Solution

With a peak field,

δν=−14ΔαhE02.\delta\nu = - \frac14 \frac{\Delta\alpha}{h} E_0^2.

The product is

ΔαhE02=2.00×104 Hz.\frac{\Delta\alpha}{h}E_0^2 = 2.00\times10^4\ \mathrm{Hz}.

Therefore,

δν=−14(2.00×104 Hz)=−5.00×103 Hz.\begin{aligned} \delta\nu &= - \frac14 \left( 2.00\times10^4\ \mathrm{Hz} \right) \\ &= -5.00\times10^3\ \mathrm{Hz}. \end{aligned}

At a leading-order electric-dipole magic frequency,

Δα(ωm)=0,\Delta\alpha(\omega_{\mathrm m}) = 0,

so this term vanishes. Vector, tensor, multipolar, hyperpolarizability, and motional corrections may remain.

An experiment measures a transition at magnetic substates +m+m and −m-m with right- and left-circular polarization. Propose combinations of the four frequencies that isolate an mm-odd vector light shift from an mm-even scalar-plus-tensor shift.

Solution

Write the frequency schematically as

ν(m,ξ)=νeven(m2)+mνZ+ξm νv,\nu(m,\xi) = \nu_{\mathrm{even}}(m^2) + m\nu_Z+\xi m\,\nu_{\mathrm v},

where ξ=+1\xi=+1 and −1-1 label opposite helicities and mνZm\nu_Z is a helicity-independent linear Zeeman shift.

At fixed helicity, the mm-odd combination is

ν(+m,ξ)−ν(−m,ξ)2=mνZ+ξm νv.\frac{ \nu(+m,\xi)-\nu(-m,\xi) }{ 2 } = m\nu_Z+\xi m\,\nu_{\mathrm v}.

Equivalently, at fixed mm,

ν(m,+)−ν(m,−)2=m νv.\frac{ \nu(m,+)-\nu(m,-) }{ 2 } = m\,\nu_{\mathrm v}.

A useful normalized mm-reversal difference at each helicity is

Dξ=ν(+m,ξ)−ν(−m,ξ)2m=νZ+ξνv.D_\xi = \frac{ \nu(+m,\xi)-\nu(-m,\xi) }{ 2m } = \nu_Z+\xi\nu_{\mathrm v}.

A robust vector estimator is therefore

νv(est)=D+−D−2.\nu_{\mathrm v}^{(\mathrm{est})} = \frac{ D_+-D_- }{ 2 }.

For the even response, define

ν‾ξ=ν(+m,ξ)+ν(−m,ξ)2.\overline\nu_\xi = \frac{ \nu(+m,\xi)+\nu(-m,\xi) }{ 2 }.

The fully even average is

ν‾++ν‾−2.\frac{ \overline\nu_+ + \overline\nu_- }{ 2 }.

This average removes the ideal vector and linear Zeeman terms, retaining the scalar contribution plus any mm-even tensor shift. Additional orientations or magnetic-sublevel values are needed to separate scalar from tensor response. The double reversal cancels a helicity-independent Zeeman term; a single mm reversal does not. It assumes equal intensities and reproducible polarization magnitudes.