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Adiabatic Approximation as a Method

The adiabatic approximation is a method for evolving states under a Hamiltonian whose eigenspaces change slowly. One first diagonalizes the instantaneous Hamiltonian, then estimates couplings generated by the moving basis, chooses a runtime or schedule that suppresses leakage, and finally tracks the phases accumulated by the followed eigenspaces.

This page owns that calculational workflow and its leading corrections. The concise theorem statement belongs in the Adiabatic Theorem reference card. The phase split needed for geometric phases is reviewed in Adiabatic Theorem Reminder. Berry connection, curvature, holonomy, and topology remain canonical in Berry Phase and its neighboring geometry pages.

Write a protocol of total duration TT using dimensionless time

s≡tT,0≤s≤1.s \equiv \frac{t}{T}, \qquad 0\le s\le1.

The Hamiltonian is

HT(t)=H(s).H_T(t) = H(s).

Increasing TT traverses the same path H(s)H(s) more slowly. This separation is essential: it distinguishes the geometric path through Hamiltonian space from the rate at which that path is followed.

At each ss, solve

H(s)∣n(s)⟩=En(s)∣n(s)⟩.H(s)\lvert n(s)\rangle = E_n(s)\lvert n(s)\rangle.

For a nondegenerate target level nn, define the instantaneous gaps

Δmn(s)≡Em(s)−En(s)\Delta_{mn}(s) \equiv E_m(s)-E_n(s)

and the minimum target gap

g(s)≡min⁡m≠n∣Δmn(s)∣,gmin⁡≡min⁡s∈[0,1]g(s).\begin{aligned} g(s) &\equiv \min_{m\ne n} \left\lvert \Delta_{mn}(s) \right\rvert, \\ g_{\min} &\equiv \min_{s\in[0,1]}g(s). \end{aligned}

The elementary gapped method assumes

gmin⁡>0.g_{\min}\gt0.

The label nn should follow a continuous eigenbranch or isolated spectral subspace, not merely “the third-lowest eigenvalue” if level ordering changes.

If the system starts in ∣n(0)⟩\lvert n(0)\rangle and the protocol is adiabatic, then

∣ψad(t)⟩=eiγn(t)exp⁡[−iℏ∫0tEn(t′) dt′]×∣n(t)⟩.\begin{aligned} \lvert\psi_{\mathrm{ad}}(t)\rangle &= e^{i\gamma_n(t)} \exp\left[ -\frac{i}{\hbar} \int_0^tE_n(t')\,dt' \right] \\ &\quad\times \lvert n(t)\rangle. \end{aligned}

The dynamical phase is

δn(t)=−1ℏ∫0tEn(t′) dt′,\delta_n(t) = -\frac{1}{\hbar} \int_0^tE_n(t')\,dt',

while, in a chosen smooth gauge, the geometric contribution is

γn(t)=i∫0t⟨n(t′)∣n˙(t′)⟩ dt′.\gamma_n(t) = i \int_0^t \langle n(t')\vert\dot n(t')\rangle\,dt'.

Adiabatic following means that population remains near the corresponding instantaneous eigenspace. It does not mean that the ket is constant. The eigenspace moves, the dynamical phase grows with runtime, and geometric transport can contribute an additional phase.

For final energy populations, an overall phase is irrelevant. For interferometry, coherent superpositions, cyclic evolution, or later recombination, relative dynamical and geometric phases are observable and must be retained. Their gauge structure and closed-loop interpretation belong in the geometry volume.

Exact Equations in the Instantaneous Basis

Section titled “Exact Equations in the Instantaneous Basis”

Choose a smooth local phase convention satisfying

⟨n(s)∣∂sn(s)⟩=0.\langle n(s)\vert \partial_s n(s)\rangle = 0.

This is the parallel-transport gauge along the open interval. Expand the exact state as

∣ψ(s)⟩=∑kak(s)×exp⁡[−iTℏ∫0sEk(u) du]×∣k(s)⟩.\begin{aligned} \lvert\psi(s)\rangle &= \sum_k a_k(s) \\ &\qquad\times \exp\left[ -\frac{iT}{\hbar} \int_0^sE_k(u)\,du \right] \\ &\qquad\times \lvert k(s)\rangle. \end{aligned}

Substituting into the Schrödinger equation gives

∂sam(s)=−∑k≠mak(s)⟨m(s)∣∂sk(s)⟩×exp⁡[iTℏ∫0sΔmk(u) du].\begin{aligned} \partial_s a_m(s) &= - \sum_{k\ne m} a_k(s) \langle m(s)\vert \partial_s k(s)\rangle \\ &\qquad\times \exp\left[ \frac{iT}{\hbar} \int_0^s \Delta_{mk}(u)\,du \right]. \end{aligned}

This equation contains the whole mechanism:

  • the moving eigenbasis generates off-diagonal couplings ⟨m∣∂sk⟩\langle m\vert\partial_s k\rangle;
  • the accumulated gap generates a rapidly oscillating phase;
  • slow evolution means that destructive interference suppresses net transfer between separated eigenspaces.

The approximation is therefore not based only on a small instantaneous coupling. Oscillatory cancellation, endpoints, smoothness, and the full path all matter.

Replace Eigenvector Derivatives by Hamiltonian Derivatives

Section titled “Replace Eigenvector Derivatives by Hamiltonian Derivatives”

Differentiate

H(s)∣n(s)⟩=En(s)∣n(s)⟩H(s)\lvert n(s)\rangle = E_n(s)\lvert n(s)\rangle

and project onto ⟨m(s)∣\langle m(s)\rvert with m≠nm\ne n. One obtains

⟨m∣∂sn⟩=⟨m∣∂sH∣n⟩En−Em.\langle m\vert \partial_s n\rangle = \frac{ \langle m\vert \partial_sH \lvert n\rangle }{ E_n-E_m }.

In physical time,

H˙(t)=1T∂sH(s).\dot H(t) = \frac{1}{T} \partial_sH(s).

The familiar pairwise diagnostic is therefore

ηmn(s)≡ℏ∣⟨m(s)∣H˙(t)∣n(s)⟩∣∣Δmn(s)∣2≪1.\eta_{mn}(s) \equiv \frac{ \hbar \left\lvert \langle m(s)\vert \dot H(t) \lvert n(s)\rangle \right\rvert }{ \left\lvert \Delta_{mn}(s) \right\rvert^2 } \ll1.

Equivalently,

ηmn(s)=ℏT∣⟨m(s)∣∂sH(s)∣n(s)⟩∣∣Δmn(s)∣2.\eta_{mn}(s) = \frac{\hbar}{T} \frac{ \left\lvert \langle m(s)\vert \partial_sH(s) \lvert n(s)\rangle \right\rvert }{ \left\lvert \Delta_{mn}(s) \right\rvert^2 }.

A conservative runtime estimate is

T≫ℏmax⁡s∈[0,1]m≠n∣⟨m(s)∣∂sH(s)∣n(s)⟩∣∣Δmn(s)∣2.T \gg \hbar \max_{\substack{s\in[0,1]\\m\ne n}} \frac{ \left\lvert \langle m(s)\vert \partial_sH(s) \lvert n(s)\rangle \right\rvert }{ \left\lvert \Delta_{mn}(s) \right\rvert^2 }.

This estimate has the right dimensions and exposes the squared gap. It is a diagnostic, not a theorem by itself. It can be overly pessimistic, and a small pointwise ratio does not automatically control endpoint effects, rapidly changing derivatives, long sums over states, unbounded domains, or many-body limits.

Suppose

an(0)=1,am(0)=0(m≠n).a_n(0)=1, \qquad a_m(0)=0 \quad (m\ne n).

Keeping the target amplitude fixed at leading order gives

am(1)(1)=−∫01ds ⟨m(s)∣∂sn(s)⟩×exp⁡[iT∫0sωmn(u) du],\begin{aligned} a_m^{(1)}(1) &= - \int_0^1ds\, \langle m(s)\vert \partial_s n(s)\rangle \\ &\qquad\times \exp\left[ iT \int_0^s \omega_{mn}(u)\,du \right], \end{aligned}

where

ωmn(s)≡Δmn(s)ℏ.\omega_{mn}(s) \equiv \frac{\Delta_{mn}(s)}{\hbar}.

This formula is adiabatic perturbation theory at first order. It keeps the entire path and phase history, unlike a local maximum criterion.

Define

fmn(s)≡⟨m(s)∣∂sn(s)⟩f_{mn}(s) \equiv \langle m(s)\vert \partial_s n(s)\rangle

and

Θmn(s)≡∫0sωmn(u) du.\Theta_{mn}(s) \equiv \int_0^s\omega_{mn}(u)\,du.

When ωmn\omega_{mn} never vanishes, integration by parts gives

am(1)(1)=−[fmn(s)eiTΘmn(s)iTωmn(s)]01+1iT∫01ds eiTΘmn(s)×∂s(fmn(s)ωmn(s)).\begin{aligned} a_m^{(1)}(1) &= - \left[ \frac{ f_{mn}(s) e^{iT\Theta_{mn}(s)} }{ iT\omega_{mn}(s) } \right]_{0}^{1} \\ &\quad+ \frac{1}{iT} \int_0^1ds\, e^{iT\Theta_{mn}(s)} \\ &\qquad\times \partial_s \left( \frac{f_{mn}(s)}{\omega_{mn}(s)} \right). \end{aligned}

The explicit factor 1/T1/T explains the generic scaling

am(1)=O(T−1),Pm←n=O(T−2).a_m^{(1)} = O(T^{-1}), \qquad P_{m\leftarrow n} = O(T^{-2}).

It also reveals two facts hidden by the pointwise diagnostic:

  1. boundary terms can dominate;
  2. derivatives of couplings and gaps enter the remainder.

For a smooth finite-dimensional Hamiltonian with a nondegenerate target level and gap g(s)≥gmin⁡>0g(s)\ge g_{\min}\gt0, a representative bound has the structure

ϵleak≲ℏT[∥∂sH(0)∥g2(0)+∥∂sH(1)∥g2(1)+∫01ds ∥∂s2H∥g2+∫01ds ∥∂sH∥2g3].\begin{aligned} \epsilon_{\mathrm{leak}} \lesssim \frac{\hbar}{T} \Bigg[ & \frac{ \lVert\partial_sH(0)\rVert }{ g^2(0) } \\ &\quad+ \frac{ \lVert\partial_sH(1)\rVert }{ g^2(1) } \\ &+ \int_0^1ds\, \frac{ \lVert\partial_s^2H\rVert }{ g^2 } \\ &\quad+ \int_0^1ds\, \frac{ \lVert\partial_sH\rVert^2 }{ g^3 } \Bigg]. \end{aligned}

Here ϵleak\epsilon_{\mathrm{leak}} denotes a norm of the component outside the followed eigenspace, and omitted numerical constants depend on the precise theorem and norm. This is a scaling template, not a universal bound for all Hamiltonians. Its purpose is to show why the minimum gap alone is insufficient: endpoint derivatives and path smoothness also enter.

For unbounded operators, changing domains, continuous spectra, or many-body thermodynamic limits, one must use a theorem suited to the problem rather than substituting formal operator norms.

Boundary Cancellation and Smooth Schedules

Section titled “Boundary Cancellation and Smooth Schedules”

If the protocol begins and ends smoothly,

∂sH(0)=∂sH(1)=0,\partial_sH(0) = \partial_sH(1) = 0,

then the leading boundary term often vanishes. With a nonclosing gap and sufficient differentiability, a second integration by parts can improve the leading transition amplitude to

am=O(T−2).a_m = O(T^{-2}).

Higher-order endpoint cancellation can produce further algebraic improvement when the required derivatives vanish and the Hamiltonian remains smooth. This does not mean that every smooth-looking schedule is exponentially accurate. The result depends on differentiability, analytic structure, gap behavior, and how the protocol is switched.

The practical lesson is simple: avoid abruptly turning a supposedly adiabatic protocol on or off.

Suppose the Hamiltonian depends on one control λ\lambda:

H=H(λ).H=H(\lambda).

Then

H˙=λ˙ ∂λH.\dot H = \dot\lambda\, \partial_\lambda H.

A local speed budget for the target level is

∣λ˙∣≪min⁡m≠n∣Δmn(λ)∣2ℏ∣⟨m(λ)∣∂λH∣n(λ)⟩∣.\left\lvert\dot\lambda\right\rvert \ll \min_{m\ne n} \frac{ \left\lvert\Delta_{mn}(\lambda)\right\rvert^2 }{ \hbar \left\lvert \langle m(\lambda)\vert \partial_\lambda H \lvert n(\lambda)\rangle \right\rvert }.

One may choose a schedule that moves rapidly where gaps are large and slows near a small avoided crossing. Holding a chosen local diagnostic near a small constant η0\eta_0 gives

∣λ˙∣=η0min⁡m≠n∣Δmn(λ)∣2ℏ∣⟨m(λ)∣∂λH∣n(λ)⟩∣.\left\lvert\dot\lambda\right\rvert = \eta_0 \min_{m\ne n} \frac{ \left\lvert\Delta_{mn}(\lambda)\right\rvert^2 }{ \hbar \left\lvert \langle m(\lambda)\vert \partial_\lambda H \lvert n(\lambda)\rangle \right\rvert }.

The resulting runtime is

T=∫λiλfdλ∣λ˙∣.T = \int_{\lambda_i}^{\lambda_f} \frac{d\lambda}{ \left\lvert\dot\lambda\right\rvert }.

This local schedule is a design heuristic. The integrated transition amplitude and endpoint smoothness still need to be checked.

Avoided-crossing gap and local adiabatic speed budget

The energy gap is smallest near an avoided crossing. A local adiabatic schedule lowers the control speed in that region and uses a larger speed where the gap and transition budget permit it. The matrix element of ∂λH\partial_\lambda H, not the gap alone, determines the allowed speed.

Worked Example: A Rotating Two-Level Hamiltonian

Section titled “Worked Example: A Rotating Two-Level Hamiltonian”

Consider

H(t)=−ℏω02cos⁡θ(t) σz−ℏω02sin⁡θ(t) σx,ω0>0.\begin{aligned} H(t) &= -\frac{\hbar\omega_0}{2} \cos\theta(t)\,\sigma_z \\ &\quad- \frac{\hbar\omega_0}{2} \sin\theta(t)\,\sigma_x, \\ \omega_0 &\gt 0. \end{aligned}

The instantaneous gap is constant:

Δeg=ℏω0.\Delta_{eg} = \hbar\omega_0.

Choose real instantaneous eigenvectors. Their off-diagonal derivative coupling has magnitude

∣⟨e(t)∣g˙(t)⟩∣=∣θ˙(t)∣2.\left\lvert \langle e(t)\vert\dot g(t)\rangle \right\rvert = \frac{ \left\lvert\dot\theta(t)\right\rvert }{2}.

The local diagnostic is

∣θ˙(t)∣2ω0≪1.\frac{ \left\lvert\dot\theta(t)\right\rvert }{ 2\omega_0 } \ll1.

For a constant angular speed

θ˙=Ω\dot\theta = \Omega

over a duration TT, first-order adiabatic perturbation theory gives

ae(1)(T)=−Ω2∫0Teiω0t dt=−Ω2iω0(eiω0T−1).\begin{aligned} a_e^{(1)}(T) &= - \frac{\Omega}{2} \int_0^T e^{i\omega_0t}\,dt \\ &= - \frac{\Omega}{ 2i\omega_0 } \left( e^{i\omega_0T}-1 \right). \end{aligned}

Hence

Pe←g(1)=Ω2ω02sin⁡2(ω0T2).P_{e\leftarrow g}^{(1)} = \frac{\Omega^2}{\omega_0^2} \sin^2\left( \frac{\omega_0T}{2} \right).

The probability is bounded by

Pe←g(1)≤(Ωω0)2.P_{e\leftarrow g}^{(1)} \le \left( \frac{\Omega}{\omega_0} \right)^2.

This example shows both the expected small parameter and the oscillatory cancellation missed by a worst-case local estimate. If the rotation is switched on and off abruptly, its endpoint terms remain visible. A smooth θ˙(t)\dot\theta(t) can suppress them.

Example: A Locally Scheduled Avoided Crossing

Section titled “Example: A Locally Scheduled Avoided Crossing”

Use

H(λ)=12(λ σz+g σx),g>0.H(\lambda) = \frac12 \left( \lambda\,\sigma_z + g\,\sigma_x \right), \qquad g\gt0.

The gap is

Δ(λ)=λ2+g2,\Delta(\lambda) = \sqrt{\lambda^2+g^2},

and

∣⟨e∣∂λH∣g⟩∣=g2λ2+g2.\left\lvert \langle e\vert \partial_\lambda H \lvert g\rangle \right\rvert = \frac{ g }{ 2\sqrt{\lambda^2+g^2} }.

Holding the pairwise diagnostic at η0\eta_0 gives

∣λ˙∣=2η0(λ2+g2)3/2ℏg.\left\lvert\dot\lambda\right\rvert = \frac{ 2\eta_0 \left( \lambda^2+g^2 \right)^{3/2} }{ \hbar g }.

For a symmetric sweep from −Λ-\Lambda to +Λ+\Lambda,

T=ℏg2η0∫−ΛΛdλ(λ2+g2)3/2=ℏΛη0gΛ2+g2.\begin{aligned} T &= \frac{\hbar g}{2\eta_0} \int_{-\Lambda}^{\Lambda} \frac{d\lambda}{ (\lambda^2+g^2)^{3/2} } \\ &= \frac{ \hbar\Lambda }{ \eta_0g \sqrt{\Lambda^2+g^2} }. \end{aligned}

When Λ≫g\Lambda\gg g,

T≃ℏη0g.T \simeq \frac{\hbar}{ \eta_0g }.

This improves on applying the minimum-gap speed limit uniformly over the entire range. It does not replace the exact Landau–Zener Transition result for a specified linear sweep.

Degenerate Eigenspaces and Projector Transport

Section titled “Degenerate Eigenspaces and Projector Transport”

Internal degeneracy does not automatically destroy adiabatic following. Let P(s)P(s) project onto a possibly degenerate spectral cluster separated from the rest of the spectrum by a nonzero gap. The adiabatic statement is that the evolved state remains close to

Ran⁡P(s).\operatorname{Ran}P(s).

Kato’s adiabatic Hamiltonian is

HA(t)=H(t)+iℏ[P˙(t),P(t)].H_{\mathrm A}(t) = H(t) + i\hbar \left[ \dot P(t),P(t) \right].

Its evolution intertwines the projectors:

UA(t)P(0)UA†(t)=P(t).U_{\mathrm A}(t)P(0) U_{\mathrm A}^\dagger(t) = P(t).

Indeed,

[[P˙,P],P]=P˙,\left[ \left[ \dot P,P \right], P \right] = \dot P,

which follows from differentiating P2=PP^2=P. The commutator term transports the subspace while the block of HH supplies dynamical evolution inside it.

For a one-dimensional eigenspace this reduces to phase transport. For a degenerate cluster, evolution within the subspace can be matrix valued. The non-Abelian connection and its geometric interpretation belong in Non-Abelian Berry Phase Preview.

At a true gap closing,

gmin⁡=0,g_{\min}=0,

the elementary isolated-eigenspace argument fails. Several distinct situations must be separated:

  • an avoided crossing has a small but nonzero gap and may require a long runtime;
  • an exact crossing protected by symmetry can preserve a symmetry sector even though globally ordered energy labels cross;
  • an accidental or symmetry-breaking crossing can mix the target with another state;
  • a continuum threshold can destroy the finite-dimensional gap picture entirely.

Near an isolated avoided crossing, reduce to the relevant low-energy subspace when justified and use Landau–Zener or direct propagation. Do not hide a closing gap by relabeling eigenvalues.

If the initial state is a superposition,

∣ψ(0)⟩=∑ncn∣n(0)⟩,\lvert\psi(0)\rangle = \sum_n c_n\lvert n(0)\rangle,

and each occupied branch remains isolated, then

∣ψad(t)⟩=∑ncneiγn(t)×exp⁡[−iℏ∫0tEn(t′) dt′]×∣n(t)⟩.\begin{aligned} \lvert\psi_{\mathrm{ad}}(t)\rangle &= \sum_n c_n e^{i\gamma_n(t)} \\ &\qquad\times \exp\left[ -\frac{i}{\hbar} \int_0^tE_n(t')\,dt' \right] \\ &\qquad\times \lvert n(t)\rangle. \end{aligned}

Relative phases can change interference even when every branch has negligible leakage. Population fidelity alone is therefore not a complete error metric.

For an initial density operator diagonal in isolated projectors,

ρ(0)=∑npnPn(0),\rho(0) = \sum_n p_nP_n(0),

adiabatic evolution transports each population to the corresponding final projector, up to leakage and any internal unitary dynamics in degenerate blocks. Coherences require phase-sensitive tracking.

In Born–Oppenheimer reasoning, nuclear coordinates R(t)\mathbf R(t) vary slowly compared with electronic dynamics. Electronic derivative couplings have the form

dmn(R)≡⟨m(R)∣∇Rn(R)⟩,\mathbf d_{mn}(\mathbf R) \equiv \langle m(\mathbf R)\vert \nabla_{\mathbf R}n(\mathbf R)\rangle,

and nuclear motion drives transitions through

R˙⋅dmn(R).\dot{\mathbf R} \cdot \mathbf d_{mn}(\mathbf R).

Large electronic gaps and slow nuclear velocities suppress transitions between electronic surfaces. The exact channel equations, mass scaling, and wavepacket-level diagnostics are developed in Born–Oppenheimer Approximation as Scale Separation. Conical intersections and near-degeneracies invalidate a single-surface approximation and can generate geometric effects; the latter belong in Born–Oppenheimer Berry Phase.

Choose H(0)H(0) with an accessible eigenstate and a path to a target Hamiltonian H(1)H(1). If the followed spectral subspace stays gapped and the runtime is sufficient, the protocol prepares the corresponding final eigenstate. A useful design must report the path, gap, coupling matrix elements, schedule, endpoint smoothness, and target error.

Adiabatic quantum computation encodes a problem in a final Hamiltonian and begins from an easily prepared ground state. Its performance depends on the gap along the interpolation, matrix elements of the driving term, schedule choice, precision, noise, and how these quantities scale with problem size. The slogan “runtime is inverse gap squared” is only a rough worst-case guide, not a complete complexity statement. Adiabatic Quantum Computation owns the corresponding computation-model record: instance encoding, accepted ground subspace and decoder, uniform Hamiltonian path, declared schedule and error certificate, circuit equivalence, and normalized logical resources; this page retains the general instantaneous-eigenspace and leakage calculation.

Slow passage can transfer population robustly when the desired eigenbranch is isolated. Real protocols balance adiabatic leakage against decoherence, control noise, and finite experimental time. In an open system, a closed-system adiabatic theorem is not automatically the right approximation.

Relation to Sudden and Landau–Zener Limits

Section titled “Relation to Sudden and Landau–Zener Limits”

The Sudden Approximation holds the state vector nearly fixed while the Hamiltonian basis changes. The adiabatic approximation instead transports the state with an instantaneous eigenspace. These are opposite controlled limits of a protocol family.

Landau–Zener dynamics resolves a standard intermediate problem. It gives an exact transition probability for an ideal linear two-level sweep and quantifies how the slow and fast limits are approached. General protocols need their own dynamics; one should not interpolate linearly between sudden and adiabatic probabilities.

  1. Parameterize a fixed path. Write H(s)H(s) with s∈[0,1]s\in[0,1] and keep the runtime TT explicit.
  2. Identify the target projector. Follow a continuous eigenbranch or isolated spectral cluster.
  3. Compute all relevant gaps. Find the minimum separation from states outside the target subspace.
  4. Compute derivative couplings. Use ⟨m∣∂sH∣n⟩/(En−Em)\langle m\vert\partial_sH\lvert n\rangle/(E_n-E_m) rather than differentiating arbitrary eigenvector phases numerically.
  5. Choose a schedule. Slow down where the gap-coupling ratio demands it and smooth the endpoints.
  6. Estimate leakage. Evaluate the pointwise diagnostic, the first-order oscillatory integral, or a theorem-level bound appropriate to the model.
  7. Track phases when needed. Retain dynamical and geometric relative phases for coherent observables.
  8. Treat degeneracy with projectors. Do not choose a physically meaningless basis inside an unresolved degenerate subspace.
  9. Check the dangerous limits. Inspect crossings, continuum thresholds, domain changes, system-size scaling, and environmental time scales.
  10. Validate against propagation. For a tractable truncation, compare with direct numerical evolution over representative runtimes.
  • Calling a protocol slow without naming a gap and coupling. Slowness is dimensionless only after comparison with the relevant spectral scales.
  • Using the minimum gap alone. Matrix elements, endpoint derivatives, and path smoothness also control leakage.
  • Forgetting the runtime parameterization. A derivative with respect to ss is not a physical time derivative until divided by TT.
  • Treating the local ratio as a proof. It is a useful diagnostic, but rigorous control needs hypotheses and often integrated derivative bounds.
  • Ignoring endpoint switching. Abrupt start and stop can dominate the leading 1/T1/T transition amplitude.
  • Dropping all phases because populations follow. Relative phases matter for superpositions and interference.
  • Differentiating eigenvectors in a noisy gauge. Use Hamiltonian matrix elements or phase-aligned numerical eigenvectors.
  • Following an ordered eigenvalue through a crossing. Track a continuous eigenbranch, symmetry sector, or spectral projector.
  • Applying a nondegenerate formula inside a degenerate cluster. Use projector transport and an internal matrix-valued evolution.
  • Assuming a closed-system theorem survives decoherence unchanged. Open-system adiabatic approximations have different conditions.
  • Promoting finite-dimensional bounds to unbounded or thermodynamic systems. Domains, ultraviolet sectors, and volume scaling require separate control.

Derive

⟨m∣∂sn⟩=⟨m∣∂sH∣n⟩En−Em\langle m\vert \partial_s n\rangle = \frac{ \langle m\vert \partial_sH \lvert n\rangle }{ E_n-E_m }

for m≠nm\ne n.

Solution

Differentiate the eigenvalue equation:

(∂sH)∣n⟩+H∣∂sn⟩=(∂sEn)∣n⟩+En∣∂sn⟩.\begin{aligned} (\partial_sH)\lvert n\rangle + H\lvert\partial_sn\rangle &= (\partial_sE_n)\lvert n\rangle \\ &\quad+ E_n\lvert\partial_sn\rangle. \end{aligned}

Project with ⟨m∣\langle m\rvert. Orthogonality removes the ∂sEn\partial_sE_n term, while

⟨m∣H=Em⟨m∣.\langle m\rvert H = E_m\langle m\rvert.

Thus

⟨m∣∂sH∣n⟩+Em⟨m∣∂sn⟩=En⟨m∣∂sn⟩.\begin{aligned} \langle m\vert\partial_sH\lvert n\rangle &+ E_m\langle m\vert\partial_sn\rangle \\ &= E_n\langle m\vert\partial_sn\rangle. \end{aligned}

Solving for the derivative coupling gives the stated identity. It fails as written when Em=EnE_m=E_n; degenerate subspaces require projectors.

For the rotating two-level Hamiltonian with constant θ˙=Ω\dot\theta=\Omega, show that the first-order excitation probability is bounded by (Ω/ω0)2(\Omega/\omega_0)^2.

Solution

The derivative coupling is Ω/2\Omega/2, so

ae(1)(T)=−Ω2∫0Teiω0t dt.a_e^{(1)}(T) = - \frac{\Omega}{2} \int_0^T e^{i\omega_0t}\,dt.

Integrating,

ae(1)(T)=−Ω2iω0(eiω0T−1).a_e^{(1)}(T) = - \frac{\Omega}{ 2i\omega_0 } \left( e^{i\omega_0T}-1 \right).

Since

∣eix−1∣=2∣sin⁡x2∣,\left\lvert e^{ix}-1 \right\rvert = 2 \left\lvert \sin\frac{x}{2} \right\rvert,

one obtains

Pe(1)=Ω2ω02sin⁡2(ω0T2)≤Ω2ω02.P_e^{(1)} = \frac{\Omega^2}{\omega_0^2} \sin^2\left( \frac{\omega_0T}{2} \right) \le \frac{\Omega^2}{\omega_0^2}.

For

H(λ)=12(λσz+gσx),H(\lambda) = \frac12 \left( \lambda\sigma_z+g\sigma_x \right),

verify the local schedule and runtime quoted in the worked example.

Solution

The gap is

Δ=λ2+g2,\Delta = \sqrt{\lambda^2+g^2},

and the off-diagonal control matrix element is

∣⟨e∣∂λH∣g⟩∣=g2Δ.\left\lvert \langle e\vert \partial_\lambda H \lvert g\rangle \right\rvert = \frac{g}{2\Delta}.

Setting

η0=ℏ∣λ˙∣Δ2g2Δ\eta_0 = \frac{ \hbar\lvert\dot\lambda\rvert }{ \Delta^2 } \frac{g}{2\Delta}

gives

∣λ˙∣=2η0Δ3ℏg.\lvert\dot\lambda\rvert = \frac{ 2\eta_0\Delta^3 }{ \hbar g }.

Therefore

T=ℏg2η0∫−ΛΛdλ(λ2+g2)3/2=ℏΛη0gΛ2+g2.\begin{aligned} T &= \frac{\hbar g}{2\eta_0} \int_{-\Lambda}^{\Lambda} \frac{d\lambda}{ (\lambda^2+g^2)^{3/2} } \\ &= \frac{ \hbar\Lambda }{ \eta_0g \sqrt{\Lambda^2+g^2} }. \end{aligned}

For Λ≫g\Lambda\gg g, the last factor approaches ℏ/(η0g)\hbar/(\eta_0g).

Use the integration-by-parts expression for am(1)a_m^{(1)} to explain why imposing ∂sH(0)=∂sH(1)=0\partial_sH(0)=\partial_sH(1)=0 can improve the asymptotic error.

Solution

For m≠nm\ne n,

fmn=⟨m∣∂sH∣n⟩En−Em.f_{mn} = \frac{ \langle m\vert \partial_sH \lvert n\rangle }{ E_n-E_m }.

If ∂sH\partial_sH vanishes at both endpoints, then fmn(0)=fmn(1)=0f_{mn}(0)=f_{mn}(1)=0 as long as the gap remains nonzero. The boundary term

−[fmniTωmneiTΘmn]01- \left[ \frac{ f_{mn} }{ iT\omega_{mn} } e^{iT\Theta_{mn}} \right]_0^1

vanishes. The remaining integral already carries one factor 1/T1/T. If its differentiated integrand is smooth and the gap stays open, integrating by parts again supplies another factor 1/T1/T, giving an O(T−2)O(T^{-2}) amplitude.

Let P(t)P(t) be a differentiable projector. Show that

[[P˙,P],P]=P˙.\left[ \left[ \dot P,P \right], P \right] = \dot P.
Solution

Differentiate P2=PP^2=P:

P˙P+PP˙=P˙.\dot PP+P\dot P = \dot P.

Multiplying on both sides by PP gives

PP˙P=0.P\dot PP=0.

Now expand the double commutator:

[[P˙,P],P]=P˙P2−2PP˙P+P2P˙=P˙P+PP˙=P˙.\begin{aligned} \left[ \left[ \dot P,P \right], P \right] &= \dot PP^2 - 2P\dot PP + P^2\dot P \\ &= \dot PP+P\dot P \\ &= \dot P. \end{aligned}

This identity makes the commutator term in HAH_{\mathrm A} transport the range of PP.

An initial state is

∣ψ(0)⟩=12(∣0(0)⟩+∣1(0)⟩).\lvert\psi(0)\rangle = \frac{1}{\sqrt2} \left( \lvert0(0)\rangle + \lvert1(0)\rangle \right).

Assume both levels follow adiabatically. What information is needed to predict interference in the final basis?

Solution

The final state is

∣ψad(T)⟩=12[eiγ0+iδ0∣0(1)⟩+eiγ1+iδ1∣1(1)⟩],\begin{aligned} \lvert\psi_{\mathrm{ad}}(T)\rangle = \frac{1}{\sqrt2} \Bigg[ & e^{i\gamma_0+i\delta_0} \lvert0(1)\rangle \\ &+ e^{i\gamma_1+i\delta_1} \lvert1(1)\rangle \Bigg], \end{aligned}

where

δn=−1ℏ∫0TEn(t) dt.\delta_n = -\frac{1}{\hbar} \int_0^TE_n(t)\,dt.

The populations of the two followed levels remain 1/21/2, but interference depends on

(δ1−δ0)+(γ1−γ0).(\delta_1-\delta_0) + (\gamma_1-\gamma_0).

Thus population following alone is insufficient; both relative dynamical and geometric phases are required.

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