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Dynamical Correlation Functions Numerically

A numerical spectrum is trustworthy only when the exact target, the algorithmic approximation, and the displayed line shape are kept distinct. Direct Lehmann sums, Lanczos continued fractions, and real-time Fourier transforms can represent the same finite-system correlation function, but they distribute cost and error very differently.

For a finite isolated system, the exact answer is usually a weighted set of delta functions. Smooth curves arise only after a declared resolution operation, a physical broadening mechanism, or a controlled thermodynamic limit. The same finite spectral measure can be computed in several ways, making small-system comparisons especially useful.

Required background. Time-dependent correlations defines operator ordering; spectral functions explains spectral measures and line shapes.

Let

H∣n⟩=En∣n⟩,En≥E0,H|n\rangle = E_n|n\rangle, \qquad E_n\ge E_0,

and select a normalized global ground state ∣0⟩|0\rangle, with specified symmetry labels. Alternatively, restrict HH and AA to a fixed invariant sector containing its sector ground state. If AA changes particle number from a merely fixed-number ground state, addition/removal energies can be negative relative to E0E_0; specify a chemical-potential reference and allow that support instead of assuming the inequality above. For an operator AA, define the connected insertion

A~=A−⟨0∣A∣0⟩.\widetilde A = A-\langle0|A|0\rangle.

The response seed is

∣f0⟩=A~∣0⟩,W0=⟨f0∣f0⟩.|f_0\rangle = \widetilde A|0\rangle, \qquad W_0 = \langle f_0|f_0\rangle.

Subtracting the expectation value removes the elastic ground-state contribution for this autocorrelation channel. It does not remove other exactly zero-energy transitions caused by degeneracy or conserved components.

This page uses energy transfer EE, not angular frequency, as the spectral variable:

E=ℏω.E = \hbar\omega.

The positive spectral measure and its time-domain partner are

SA(E)=∑n∣⟨n∣A~∣0⟩∣2δ ⁣(E−En+E0),CA(t)=⟨f0∣e−i(H−E0)t/ℏ∣f0⟩.\begin{aligned} S_A(E) &= \sum_n |\langle n|\widetilde A|0\rangle|^2 \delta\!\left( E-E_n+E_0 \right), \\ C_A(t) &= \langle f_0| e^{-i(H-E_0)t/\hbar} |f_0\rangle. \end{aligned}

With these conventions,

CA(t)=∫−∞∞dE SA(E)e−iEt/ℏ,SA(E)=12πℏ∫−∞∞dt eiEt/ℏCA(t).\begin{aligned} C_A(t) &= \int_{-\infty}^{\infty} dE\, S_A(E)e^{-iEt/\hbar}, \\ S_A(E) &= \frac{1}{2\pi\hbar} \int_{-\infty}^{\infty} dt\, e^{iEt/\hbar}C_A(t). \end{aligned}

Specify the operator, its normalization, the initial state, the destination sectors, and the energy interval of interest. For a global ground state the measure has support on E≥0E\ge0, including possible weight at exactly zero. Integrating over the full real line avoids an ambiguous half-weight convention for a delta function at the endpoint.

This ordered autocorrelation is not the full retarded commutator response. For a perturbation H′=−fAH'=-fA, the physical susceptibility uses +iθ(t)⟨[A(t),A(0)]⟩/ℏ+i\theta(t)\langle[A(t),A(0)]\rangle/\hbar for Hermitian AA and includes both transition orderings.

One calculation can produce three mathematically different objects.

For finite dimension,

SA,L(E)=∑jwj,Lδ(E−εj,L),S_{A,L}(E) = \sum_j w_{j,L} \delta(E-\varepsilon_{j,L}),

where LL labels the finite geometry. The pole positions and weights are exact only for the represented finite Hamiltonian and state.

An iterative method returns approximations such as

{ε~j, w~j},C~(tk),orG~(E+iη).\begin{gathered} \left\{ \widetilde\varepsilon_j,\, \widetilde w_j \right\}, \qquad \widetilde C(t_k), \\ \text{or} \qquad \widetilde G(E+i\eta). \end{gathered}

These carry solver, propagation, truncation, and floating-point errors before any physical limit is considered.

A plotted function is commonly

S~A,L,K(E)=∫dE′ K(E−E′)S~A,L(E′),\widetilde S_{A,L,K}(E) = \int dE'\, K(E-E') \widetilde S_{A,L}(E'),

for a declared kernel KK. Its peak widths include the chosen kernel even when the exact finite-system lines have zero intrinsic width.

These objects answer different questions. Convergence of the algorithmic approximation does not establish convergence in LL, and visual smoothness does not establish an intrinsic continuum.

Route Primary computed object Natural strength Dominant limitation
direct Lehmann sum eigenvalues and matrix elements exact finite benchmark and all operators after diagonalization exponential state count and eigenvector storage
Lanczos response projected resolvent or tridiagonal poles many frequencies from one operator seed Krylov convergence, loss of orthogonality, finite-size poles
real-time evolution sampled overlap CA(tk)C_A(t_k) broad spectral window and space-time data reachable time, time step, recurrence, entanglement growth
correction vector response state at selected E+iηE+i\eta controlled narrow frequency windows one difficult linear solve per frequency or block
polynomial expansion spectral moments uniform broad windows with explicit kernels rescaling, recursion order, moment stability

The first three routes are developed in detail below. The final two are included to prevent a false three-method taxonomy: they can be preferable when the desired frequency window or representation makes them a better match.

Complete diagonalization gives the finite-system spectrum most literally:

εn=En−E0,wn=∣⟨n∣A~∣0⟩∣2.\varepsilon_n = E_n-E_0, \qquad w_n = |\langle n|\widetilde A|0\rangle|^2.

The workflow is:

  1. construct and verify the finite Hamiltonian;
  2. diagonalize the ground-state sector;
  3. apply A~\widetilde A to determine the destination sector;
  4. diagonalize every destination-sector state needed in the requested window;
  5. evaluate matrix elements and preserve the unbroadened line list;
  6. verify exact identities before choosing a display kernel.

The zeroth and first moments are

μ0=∑nwn=⟨0∣A~†A~∣0⟩,μ1=∑nwnεn=⟨0∣A~†(H−E0)A~∣0⟩.\begin{aligned} \mu_0 &= \sum_n w_n = \langle0| \widetilde A^\dagger\widetilde A |0\rangle, \\ \mu_1 &= \sum_n w_n\varepsilon_n \\ &= \langle0| \widetilde A^\dagger (H-E_0) \widetilde A |0\rangle. \end{aligned}

For Hermitian A~\widetilde A, the first moment can also be related to a double commutator under the conventions developed on Sum Rules.

If AA carries conserved quantum numbers ΔλA\Delta\lambda_A, then

A~:Hλ0⟶Hλ0+ΔλA.\widetilde A: \mathcal H_{\lambda_0} \longrightarrow \mathcal H_{\lambda_0+\Delta\lambda_A}.

A spin-raising operator changes total magnetization, a creation operator changes particle number, and a momentum-resolved operator changes crystal momentum. The destination basis may therefore differ from the ground-state basis.

A vanishing matrix element can be a physical selection rule, but it can also signal that the operator was represented in the wrong sector. The numerical record should distinguish those possibilities.

Individual weights inside an exactly degenerate eigenspace depend on the basis chosen within that space. The total weight does not. For the projector PDP_{\mathcal D} onto a degenerate block,

WD=⟨0∣A~†PDA~∣0⟩W_{\mathcal D} = \langle0| \widetilde A^\dagger P_{\mathcal D} \widetilde A |0\rangle

is basis invariant. Compare block weights rather than individual eigenvector labels when eigensolvers rotate a degenerate subspace.

Use direct sums when:

  • the full relevant sector is small enough to diagonalize and retain;
  • many different operators will be evaluated on the same eigenbasis;
  • exact thermal traces are required in a small system;
  • a benchmark is needed for iterative or compressed-state methods;
  • individual finite-size poles and selection rules are themselves the target.

Do not call a partial eigensystem a complete Lehmann sum. Missing high-energy states can violate normalization and moment identities even when the low-energy plot looks plausible.

Consider an operator-generated state supported on two exact excitations:

∣f0⟩=32∣1⟩+12∣2⟩,|f_0\rangle = \frac{\sqrt3}{2}|1\rangle + \frac12|2\rangle,

with

(H−E0)∣1⟩=Δ∣1⟩,(H−E0)∣2⟩=3Δ∣2⟩.\begin{aligned} (H-E_0)|1\rangle &= \Delta|1\rangle, \\ (H-E_0)|2\rangle &= 3\Delta|2\rangle. \end{aligned}

The exact line measure is

S(E)=34δ(E−Δ)+14δ(E−3Δ),S(E) = \frac34\delta(E-\Delta) + \frac14\delta(E-3\Delta),

and the exact correlator is

C(t)=34e−iΔt/ℏ+14e−i3Δt/ℏ.C(t) = \frac34e^{-i\Delta t/\hbar} + \frac14e^{-i3\Delta t/\hbar}.

The first moments are

μ0=1,μ1=32Δ,μ2=3Δ2.\mu_0=1, \qquad \mu_1=\frac32\Delta, \qquad \mu_2=3\Delta^2.

This tiny problem is useful because every numerical route must reproduce the same weights, phases, and moments while exposing its own approximation.

A response Lanczos run starts from

∣q1⟩=∣f0⟩W0|q_1\rangle = \frac{|f_0\rangle}{\sqrt{W_0}}

and projects H−E0H-E_0 onto the Krylov space generated by repeated Hamiltonian action. If TmT_m is the resulting m×mm\times m tridiagonal matrix, then

GA(m)(z)=W0e1T(zIm−Tm)−1e1,Im⁡z>0.\begin{gathered} G_A^{(m)}(z) = W_0 e_1^{\mathsf T} (zI_m-T_m)^{-1} e_1, \\ \operatorname{Im}z>0. \end{gathered}

Expanding this matrix element gives the familiar continued fraction. Its derivation, indexing, residual logic, and finite-precision safeguards belong to Lanczos Method Preview.

Diagonalizing the small TmT_m gives

GA(m)(z)=∑ℓ=1mwℓ(m)z−ϑℓ(m),G_A^{(m)}(z) = \sum_{\ell=1}^{m} \frac{w_\ell^{(m)}} {z-\vartheta_\ell^{(m)}},

where

wℓ(m)=W0∣(yℓ)1∣2≥0.w_\ell^{(m)} = W_0 |(y_\ell)_1|^2 \ge0.

One response run therefore supplies a compact pole representation that can be evaluated on many frequency grids and for many choices of η\eta without repeating Hamiltonian-vector products.

Lanczos is a moment method as well as a pole method. In exact arithmetic,

μp=W0e1TTmpe1\mu_p = W_0 e_1^{\mathsf T} T_m^p e_1

is exact for 0≤p≤2m−10\le p\le2m-1 for standard unrestarted Hermitian Lanczos before early termination; after exact invariant-subspace termination all moments of the seed measure are reproduced. Integrated spectral information can therefore converge before every visible pole.

This creates two opposite mistakes:

  • rejecting a useful response because individual high-energy poles still move even though the target moments and broadened window are stable;
  • accepting a detailed line assignment merely because low moments are correct.

Convergence must be tested at the level of the claimed observable.

For the three-level benchmark, the first diagonal coefficient and off-diagonal coefficient are

α1=32Δ,β2=32Δ.\alpha_1 = \frac32\Delta, \qquad \beta_2 = \frac{\sqrt3}{2}\Delta.

The second diagonal coefficient is

α2=52Δ.\alpha_2 = \frac52\Delta.

Thus

T2=Δ(3/23/23/25/2),T_2 = \Delta \begin{pmatrix} 3/2 & \sqrt3/2 \\ \sqrt3/2 & 5/2 \end{pmatrix},

whose eigenvalues are Δ\Delta and 3Δ3\Delta with the exact spectral weights 3/43/4 and 1/41/4. The Krylov space has exhausted the support of ∣f0⟩|f_0\rangle, so the response terminates exactly after two basis vectors even if the full Hilbert space is larger.

Keep at least four errors separate:

  1. Reference-state error: E0E_0 and ∣0⟩|0\rangle may be approximate.
  2. Response-Krylov error: finite mm limits the represented moments and pole detail.
  3. Finite-precision error: loss of orthogonality can create duplicate or unstable poles.
  4. Resolution choice: evaluating z=E+iηz=E+i\eta convolves the discrete measure with a Lorentzian.

Increasing mm does not remove ground-state bias, finite-size effects, or the chosen η\eta. Decreasing η\eta can reveal unconverged Krylov poles rather than more physics.

The time-domain route propagates the same response seed:

∣f(t)⟩=e−i(H−E0)t/ℏ∣f0⟩,|f(t)\rangle = e^{-i(H-E_0)t/\hbar} |f_0\rangle,

then evaluates

CA(t)=⟨f0∣f(t)⟩.C_A(t) = \langle f_0|f(t)\rangle.

The propagation may use exact exponentiation in a tiny space, a Krylov exponential, product formulas, matrix-product-state evolution, or another controlled representation. Those algorithms have different internal errors, but the spectral reconstruction sees only the accuracy and duration of the resulting time record.

Let

tj=jΔt,j=0,…,N,tmax⁡=NΔt.\begin{gathered} t_j = j\Delta t, \qquad j=0,\ldots,N, \\ t_{\max} = N\Delta t. \end{gathered}

For the ordered autocorrelation defined above, even if AA itself is not Hermitian,

CA(−t)=CA(t)∗,C_A(-t) = C_A(t)^*,

so a verified positive-time record can be extended to a total interval of length approximately 2tmax⁡2t_{\max}. The associated scales are

ENy=πℏΔt,δEgrid≃πℏtmax⁡.\begin{aligned} E_{\mathrm{Ny}} &= \frac{\pi\hbar}{\Delta t}, \\ \delta E_{\mathrm{grid}} &\simeq \frac{\pi\hbar}{t_{\max}}. \end{aligned}

The second quantity is a frequency-grid scale for the symmetrically extended record, not a universal resolving power. The main-lobe width of the chosen window is the relevant resolution measure.

For an even time window w(t)w(t) supported on [−tmax⁡,tmax⁡][-t_{\max},t_{\max}], define

S~w(E)=12πℏ∫−tmax⁡tmax⁡dt w(t)eiEt/ℏC~A(t).\widetilde S_w(E) = \frac{1}{2\pi\hbar} \int_{-t_{\max}}^{t_{\max}} dt\, w(t)e^{iEt/\hbar} \widetilde C_A(t).

For exact propagation, multiplication by the window, extended as zero outside its stated support, gives exactly the convolution

S~w(E)=∫dE′ Kw(E−E′)SA(E′),\widetilde S_w(E) = \int dE'\, K_w(E-E') S_A(E'),

with

Kw(E)=12πℏ∫dt w(t)eiEt/ℏ.K_w(E) = \frac{1}{2\pi\hbar} \int dt\, w(t)e^{iEt/\hbar}.

The window is therefore part of the spectral estimator, not cosmetic post-processing.

Exponential damping,

wη(t)=e−η∣t∣/ℏ,w_\eta(t) = e^{-\eta|t|/\hbar},

produces the normalized Lorentzian

Kη(E)=1πηE2+η2.K_\eta(E) = \frac1\pi \frac{\eta}{E^2+\eta^2}.

Gaussian damping,

wσ(t)=exp⁡ ⁣[−12(σtℏ)2],w_\sigma(t) = \exp\!\left[ -\frac12 \left( \frac{\sigma t}{\hbar} \right)^2 \right],

produces

Kσ(E)=12πσexp⁡ ⁣(−E22σ2).K_\sigma(E) = \frac{1}{\sqrt{2\pi}\sigma} \exp\!\left( -\frac{E^2}{2\sigma^2} \right).

A finite cutoff multiplies either window by an additional rectangle, so the realized kernel differs from the infinite-time formula unless the damped tail is already negligible at tmax⁡t_{\max}.

Using w(t)=1w(t)=1 inside the record gives a sinc-like kernel. It has a narrow main lobe and substantial oscillatory sidelobes; its width should be compared with other windows using a stated convention. Those sidelobes can create negative undershoots near a positive sharp spectrum.

A smoother window suppresses leakage at the price of a wider main lobe. There is no window that simultaneously preserves arbitrary sharp features, eliminates sidelobes, and uses only a short record.

Zero padding samples the same finite-record transform on a denser plotting grid. It does not increase tmax⁡t_{\max}, narrow the window kernel, or create new spectral information.

For time evolution, monitor errors before Fourier transformation:

  • norm drift;
  • conserved-energy drift;
  • time-reversal or forward-backward error when applicable;
  • time-step convergence;
  • Krylov-exponential residual or product-formula order;
  • bond-dimension and discarded-weight convergence for matrix-product states;
  • boundary reflections and finite-size recurrences;
  • loss of exact symmetry labels.

Fourier transformation can hide local oscillatory errors under a smooth curve. A stable-looking spectrum is not a substitute for a converged time record.

The exact resolvent and exact time record are related by

GA(z)=⟨f0∣[z−(H−E0)]−1∣f0⟩=1iℏ∫0∞dt eizt/ℏCA(t),\begin{aligned} G_A(z) &= \langle f_0| \bigl[z-(H-E_0)\bigr]^{-1} |f_0\rangle \\ &= \frac{1}{i\hbar} \int_0^\infty dt\, e^{izt/\hbar} C_A(t), \end{aligned}

Here Im⁡z>0\operatorname{Im}z>0. Setting z=E+iηz=E+i\eta inserts the exponential damping e−ηt/ℏe^{-\eta t/\hbar}. Consequently, an infinite-time exponentially damped transform and a resolvent evaluated at E+iηE+i\eta produce the same Lorentzian-broadened target under matched conventions.

The moments are also encoded in the short-time derivatives:

μp=(iℏ)pdpCA(t)dtp∣t=0.\mu_p = (i\hbar)^p \left. \frac{d^p C_A(t)} {dt^p} \right|_{t=0}.

These identities provide strong cross-checks:

  • direct Lehmann weights should reconstruct the propagated CA(t)C_A(t);
  • Lanczos moments should match derivatives or operator expectation values;
  • an exponentially damped time transform should match the continued fraction at the same η\eta;
  • all methods should agree on μ0\mu_0, low moments, and symmetry-forbidden weight.

Use the same kernel in a comparison: otherwise its shape can dominate the difference between algorithms.

For a normalized kernel,

∫−∞∞dE Kγ(E)=1,\int_{-\infty}^{\infty} dE\, K_\gamma(E) = 1,

the broadened finite spectrum is

SL,γ(E)=∑jwj,LKγ(E−εj,L).S_{L,\gamma}(E) = \sum_j w_{j,L} K_\gamma(E-\varepsilon_{j,L}).

The integrated weight is preserved only if the numerical integration covers the full broadened support. A finite plotting window can lose Lorentzian tails or clipped Gaussian weight.

Kernel Width parameter Useful feature Main caution
Lorentzian HWHM η\eta direct resolvent interpretation long tails and peak overlap
Gaussian standard deviation σ\sigma rapid tail suppression no simple retarded resolvent with constant imaginary part
finite rectangular time window record length no extra damping sinc ringing and negative sidelobes
smooth finite-time window stated main-lobe width reduced leakage broader peaks and window-dependent amplitude
Jackson-damped polynomial kernel expansion order positive controlled polynomial smoothing nonuniform physical resolution after rescaling choices

Always state whether a quoted width is HWHM, FWHM, standard deviation, first-zero spacing, or another main-lobe convention.

Let δL(E)\delta_L(E) denote a representative local level spacing among states that carry appreciable operator weight. Three qualitative regimes are:

γ≪δL:resolved finite-size lines,γ∼δL:kernel-dependent overlap,δL≪γ:smooth finite-size envelope.\begin{aligned} \gamma\ll\delta_L &: \quad \text{resolved finite-size lines}, \\ \gamma\sim\delta_L &: \quad \text{kernel-dependent overlap}, \\ \delta_L\ll\gamma &: \quad \text{smooth finite-size envelope}. \end{aligned}

The last regime does not by itself prove convergence to the thermodynamic spectrum. The broadening must also remain smaller than the physical energy scale being claimed.

A useful but model-dependent scaling design seeks a window

δL(E)≪γL≪ΔEphys,\delta_L(E) \ll \gamma_L \ll \Delta E_{\mathrm{phys}},

while increasing LL and decreasing γL\gamma_L. In many one-dimensional applications one tests γL∝1/L\gamma_L\propto 1/L, but this is not a universal law. Thresholds, gaps, exponentially small splittings, disorder, and momentum resolution can demand different scaling.

For a continuum thermodynamic claim, the intended distributional logic is commonly

S∞(E)=lim⁡γ→0+lim⁡L→∞SL,γ(E),S_\infty(E) = \lim_{\gamma\to0^+} \lim_{L\to\infty} S_{L,\gamma}(E),

or a documented joint sequence (L,γL)(L,\gamma_L). Taking γ→0\gamma\to0 at one fixed LL merely recovers the finite delta comb.

The order must be stated when E→0E\to0, momentum q→0q\to0, temperature T→0T\to0, or other singular limits are also present.

If the represented finite Hamiltonian is closed and Hermitian, its exact eigenstates have real energies and delta-function lines. A selected η\eta, σ\sigma, window width, or prediction damping is a numerical resolution unless the model includes a physical decay mechanism and the inferred intrinsic width is stable under removal of numerical resolution.

The practical test is to vary the numerical kernel independently. A claimed linewidth must survive deconvolution or forward fitting across a controlled range in which finite size and solver errors are smaller.

Finite size appears differently in the three routes:

  • direct Lehmann sums expose discrete levels immediately;
  • Lanczos represents those levels through projected poles;
  • real-time evolution reveals them through recurrences and boundary returns.

For a local disturbance with characteristic propagation speed vv, a boundary-return scale is roughly

treturn∼2dboundaryv,t_{\mathrm{return}} \sim \frac{2d_{\mathrm{boundary}}}{v},

for a disturbance returning to its source after reflection, up to dispersion and geometry. A one-way arrival at an edge takes about dboundary/vd_{\mathrm{boundary}}/v, while a periodic wraparound takes about L/vL/v. These are estimates of the relevant propagation mechanism, not exact universal recurrence times. Data beyond the first return do not represent the infinite system without an additional finite-size analysis.

If a desired energy resolution requires

tmax⁡≫treturn,t_{\max} \gg t_{\mathrm{return}},

then simply propagating longer on the same system is not a controlled route to the thermodynamic spectrum. One must increase the system size, exploit an infinite-system method, model the return, or accept coarser resolution.

Spatial and Momentum-Resolved Correlations

Section titled “Spatial and Momentum-Resolved Correlations”

For translation-invariant periodic systems, a normalized momentum operator may be

Aq=1L∑j=1LeiqrjAj.A_q = \frac{1}{\sqrt L} \sum_{j=1}^{L} e^{iqr_j} A_j.

With TAjT−1=Aj+1T A_jT^{-1}=A_{j+1} and T∣k⟩=e−ik∣k⟩T|k\rangle=e^{-ik}|k\rangle, this convention gives TAqT−1=e−iqAqT A_qT^{-1}=e^{-iq}A_q, so the response seed has momentum k0+qk_0+q when translation is an exact symmetry. This can greatly reduce a direct or Lanczos calculation.

Open boundaries do not have exact lattice momentum. A discrete Fourier transform of real-space data remains useful, but its peaks inherit boundary envelopes and momentum leakage. Sine transforms or spatial filter functions may better match the standing-wave geometry; their normalization must be declared.

In a real-time calculation, one can evaluate

C(r,t)=⟨0∣Ar(t)A0(0)∣0⟩C(r,t) = \langle0| A_r(t)A_0(0) |0\rangle

and transform in both space and time. Translation invariance can reduce the number of source positions, while open boundaries often require central sources, averaging over equivalent windows, or explicit boundary checks.

Approximate Ground States and Compressed Evolution

Section titled “Approximate Ground States and Compressed Evolution”

Suppose the reference state is an approximation ∣0~⟩|\widetilde0\rangle. Then the computed response contains both ground-state error and dynamical-method error:

C~(t)=⟨0~∣A~†U~(t)A~∣0~⟩.\widetilde C(t) = \langle\widetilde0| \widetilde A^\dagger \widetilde U(t) \widetilde A |\widetilde0\rangle.

Here U~(t)\widetilde U(t) approximates e−i(H−E~0)t/ℏe^{-i(H-\widetilde E_0)t/\hbar}. This is the stationary-seed approximation. If ∣0~⟩|\widetilde0\rangle is not an eigenstate, its actual two-time correlator is

⟨0~∣eiHt/ℏA~†e−iHt/ℏA~∣0~⟩,\langle\widetilde0|e^{iHt/\hbar}\widetilde A^\dagger e^{-iHt/\hbar}\widetilde A|\widetilde0\rangle,

which requires evolving the reference branch as well. Replacing that evolution by a scalar phase introduces a reference-state error that can grow with time. A small ground-state energy error does not guarantee accurate spectral weights. The operator may amplify a small missing component or probe a symmetry sector that was poorly represented during optimization.

Useful reference-state checks include:

  • the energy variance;
  • symmetry quantum numbers;
  • convergence of W0=⟨A~†A~⟩W_0=\langle\widetilde A^\dagger\widetilde A\rangle;
  • convergence of the first few moments;
  • comparison of equal-time correlators entering the sum rules;
  • stability under bond dimension, sweep tolerance, and initialization.

For matrix-product-state time evolution, report the evolution algorithm, time step, maximum bond dimension, truncation criterion, accumulated discarded-weight diagnostics, conservation drift, and reachable time. Entanglement growth usually sets a physical representation horizon that cannot be repaired by Fourier post-processing.

For

S(E)=34δ(E−Δ)+14δ(E−3Δ),S(E) = \frac34\delta(E-\Delta) + \frac14\delta(E-3\Delta),

derive C(t)C(t) and compute μ0\mu_0, μ1\mu_1, and μ2\mu_2. Explain which quantities remain unchanged after convolution with a normalized even kernel.

Solution

Using

C(t)=∫dE S(E)e−iEt/ℏ,C(t) = \int dE\, S(E)e^{-iEt/\hbar},

gives

C(t)=34e−iΔt/ℏ+14e−i3Δt/ℏ.C(t) = \frac34e^{-i\Delta t/\hbar} + \frac14e^{-i3\Delta t/\hbar}.

The moments are

μ0=34+14=1,μ1=34Δ+14(3Δ)=32Δ,μ2=34Δ2+14(3Δ)2=3Δ2.\begin{aligned} \mu_0 &= \frac34+\frac14 =1, \\ \mu_1 &= \frac34\Delta + \frac14(3\Delta) = \frac32\Delta, \\ \mu_2 &= \frac34\Delta^2 + \frac14(3\Delta)^2 = 3\Delta^2. \end{aligned}

A normalized convolution preserves the total weight μ0\mu_0 on the full energy axis. If a centered kernel has a finite first moment, it also preserves μ1\mu_1 when all tails are included. Higher moments generally acquire contributions from the kernel’s own width moments. A Lorentzian has no finite ordinary first or higher absolute moments, so moment checks should use the raw line measure or an explicitly finite integration convention. A finite plotting interval can spoil even the apparent conservation of total weight.

Show that wη(t)=e−η∣t∣/ℏw_\eta(t)=e^{-\eta|t|/\hbar} produces a Lorentzian kernel. What practical condition makes a finite cutoff at tmax⁡t_{\max} close to the infinite-time result?

Solution

The kernel is

Kη(E)=12πℏ∫−∞∞dt e−η∣t∣/ℏeiEt/ℏ=1πℏ∫0∞dt e−ηt/ℏcos⁡(Et/ℏ)=1πηE2+η2.\begin{aligned} K_\eta(E) &= \frac{1}{2\pi\hbar} \int_{-\infty}^{\infty} dt\, e^{-\eta|t|/\hbar} e^{iEt/\hbar} \\ &= \frac{1}{\pi\hbar} \int_0^\infty dt\, e^{-\eta t/\hbar} \cos(Et/\hbar) \\ &= \frac1\pi \frac{\eta}{E^2+\eta^2}. \end{aligned}

The omitted tail is small when

e−ηtmax⁡/ℏ≪εtarget,e^{-\eta t_{\max}/\hbar} \ll \varepsilon_{\mathrm{target}},

This dimensionless tail condition should be translated into the desired spectral error. Since ∣CA(t)∣≤W0|C_A(t)|\le W_0, the omitted exponentially damped tail contributes at most W0e−ηtmax⁡/ℏ/(πη)W_0 e^{-\eta t_{\max}/\hbar}/(\pi\eta) to the absolute error in SA,η(E)S_{A,\eta}(E). This bound has the correct spectral-density units and becomes more demanding as η\eta decreases. If this condition fails, the sharp cutoff adds sinc-like structure on top of the intended Lorentzian broadening.

Exercise 4: Time sampling and energy resolution

Section titled “Exercise 4: Time sampling and energy resolution”

A time-domain calculation uses

Δt=0.05ℏJ,tmax⁡=40ℏJ.\Delta t = 0.05\frac{\hbar}{J}, \qquad t_{\max} = 40\frac{\hbar}{J}.

Assuming a verified Hermitian extension to negative time, estimate the Nyquist energy and the Fourier-grid spacing. Does padding the record by a factor of eight improve either physical scale?

Solution

The Nyquist energy is

ENy=πℏΔt=20πJ≈62.8J.E_{\mathrm{Ny}} = \frac{\pi\hbar}{\Delta t} = 20\pi J \approx 62.8J.

The extended interval has length approximately 2tmax⁡2t_{\max}, so the Fourier-grid spacing is

δEgrid≃2πℏ2tmax⁡=π40J≈0.0785J.\delta E_{\mathrm{grid}} \simeq \frac{2\pi\hbar}{2t_{\max}} = \frac{\pi}{40}J \approx 0.0785J.

The actual resolving width is the main-lobe width of the chosen window and is generally a constant multiple of ℏ/tmax⁡\hbar/t_{\max}. Eightfold zero padding reduces only the plotted grid spacing between interpolated samples. It changes neither ENyE_{\mathrm{Ny}} nor the information-limited resolution.

Exercise 5: Design a finite-size broadening test

Section titled “Exercise 5: Design a finite-size broadening test”

Let vv be a velocity and LL a physical length. Near a regular continuum, suppose the operator-weighted finite-size spacing scales as

δL∼ℏvL.\delta_L \sim \frac{\hbar v}{L}.

Design a joint sequence of sizes and Lorentzian widths that could test a feature of physical width Γ\Gamma. State what must be seen before interpreting Γ\Gamma as intrinsic.

Solution

One possible design uses

L1<L2<L3<⋯ ,ηL=cℏvL,L_1<L_2<L_3<\cdots, \qquad \eta_L = c\frac{\hbar v}{L},

with cc large enough to average over several operator-bright finite-size lines but small enough that ηL≪Γ\eta_L\ll\Gamma on the largest sizes. The proportionality should be varied, for example by repeating with several values of cc.

To identify an intrinsic width, check:

  • convergence of the forward-broadened line shape across increasing LL;
  • stability under changing cc and the kernel family;
  • a fitted intrinsic Γ\Gamma larger than the controlled numerical resolution;
  • stable integrated weight and low moments;
  • no unresolved boundary, solver, or propagation error on the same scale;
  • a physical mechanism or pole model under which linewidth has the claimed interpretation.

If the apparent width tracks ηL\eta_L or disappears as the kernel narrows, only a resolution-limited upper bound has been established.

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