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Variational Perturbation Theory

Variational perturbation theory reorganizes a perturbative calculation around an adjustable solvable problem and fixes the auxiliary parameters only after truncation. The exact answer does not depend on those parameters. A finite-order approximation does, so its residual dependence can be reduced, inspected, and used as a diagnostic.

The method is valuable when ordinary perturbation theory is accurate only near a weak-coupling point, especially when its coefficients form a divergent asymptotic series. It can absorb part of the interaction into a better reference scale and can build known strong-coupling behavior into an order-dependent sequence. It is not a universal convergence machine, and the word variational does not mean that every optimized approximant is a rigorous upper bound.

This page is the canonical home for the interpolation, re-expansion, and order-by-order optimization procedure. The ordinary Rayleigh–Schrödinger recursion belongs to Higher-Order Structure, the quartic oscillator as a multi-method model belongs to Anharmonic Oscillator, and static Gaussian expectations and covariance formulas belong to Gaussian Variational Methods.

Suppose an observable has a formal weak-coupling expansion

Q(g)∼∑n=0∞angn.Q(g) \sim \sum_{n=0}^{\infty}a_n g^n.

Three different difficulties can arise.

  1. The series can converge, but only inside a disk that does not reach the desired coupling.
  2. The series can be asymptotic, so its terms eventually grow at every fixed g≠0g\ne0.
  3. The first few terms can be poorly adapted to the physical scale of the interacting problem even before large-order growth becomes visible.

An adjustable reference Hamiltonian addresses the third problem directly and can sometimes address the first two. The guiding idea is simple: add and subtract a solvable term, treat the subtraction perturbatively, and let the reference scale depend on truncation order.

This changes the sequence of finite-order approximations without changing the exact problem. If every order could be summed, the auxiliary scale would disappear. At finite order, the scale records how the calculation was reorganized.

Let HH be the physical Hamiltonian. Choose a solvable family H0(α)H_0(\alpha) depending on one or more auxiliary parameters α\alpha, and define

ΔH(α)=H−H0(α).\Delta H(\alpha) = H-H_0(\alpha).

Introduce a bookkeeping parameter δ\delta:

Hδ(α)=H0(α)+δΔH(α).H_\delta(\alpha) = H_0(\alpha) + \delta\Delta H(\alpha).

The endpoints are

Hδ=0(α)=H0(α),Hδ=1(α)=H.H_{\delta=0}(\alpha)=H_0(\alpha), \qquad H_{\delta=1}(\alpha)=H.

For fixed α\alpha, ordinary perturbation theory in δ\delta gives

Q(δ,α)∼∑n=0∞qn(α)δn.Q(\delta,\alpha) \sim \sum_{n=0}^{\infty} q_n(\alpha)\delta^n.

Truncate at order NN and only then set δ=1\delta=1:

Q[N](α)=∑n=0Nqn(α)δn∣δ=1.Q_{[N]}(\alpha) = \left. \sum_{n=0}^{N} q_n(\alpha)\delta^n \right|_{\delta=1}.

The formal parameter δ\delta is not normally a new physical coupling. It labels how far the interpolation has moved from the chosen reference problem to the physical one.

At δ=1\delta=1, the exact Hamiltonian is HH for every admissible α\alpha. An exact observable therefore satisfies

∂Q∂α=0.\frac{\partial Q}{\partial\alpha}=0.

The truncated expression generally does not:

∂Q[N]∂α≠0.\frac{\partial Q_{[N]}}{\partial\alpha} \ne0.

This residual dependence is a truncation artifact. Optimization attempts to choose a region where the artifact has the least local effect. It does not turn α\alpha into a measurable parameter.

First-, second-, and third-order reorganized quartic-oscillator energies as functions of the auxiliary frequency

Residual auxiliary-frequency dependence at g=1g=1 for the quartic-oscillator approximants derived below. Filled markers show the first- and third-order PMS points. The open marker is a second-order inflection point, used as a heuristic continuation because that curve has no real PMS point. The horizontal line is a converged numerical benchmark.

The exact auxiliary independence does not specify a unique finite-order rule. Several prescriptions are used, and their equivalence must not be assumed.

The principle of minimal sensitivity, or PMS, chooses a stationary point:

∂Q[N](α)∂α∣α=αN=0.\left. \frac{\partial Q_{[N]}(\alpha)} {\partial\alpha} \right|_{\alpha=\alpha_N} =0.

For several parameters α\boldsymbol\alpha, the condition becomes

∇αQ[N](αN)=0.\nabla_{\boldsymbol\alpha} Q_{[N]}(\boldsymbol\alpha_N) = \mathbf0.

PMS asks for local insensitivity, not necessarily a minimum. A stationary point can be a maximum, saddle, or degenerate plateau.

If the order-NN contribution is denoted qN(α)q_N(\alpha), fastest apparent convergence, or FAC, sets

qN(αN)=0.q_N(\alpha_N)=0.

This makes the newest explicit correction vanish. It can be useful when a PMS point is absent, but it is a different criterion. A zero of the last term need not coincide with a stationary point of the partial sum.

At some orders there is no real PMS or FAC root. A common heuristic is then to choose a broad region of weak dependence or a turning point satisfying

∂2Q[N]∂α2=0.\frac{\partial^2Q_{[N]}} {\partial\alpha^2}=0.

This is sometimes called a turning-point or inflection prescription. It is not implied by exact auxiliary independence. Whenever it is used, it should be labeled as an additional choice and tested against neighboring orders.

Higher-order equations often have several real or complex roots. A defensible branch is selected before comparison with the desired answer, using criteria such as:

  • continuity from weak coupling or from the previous order;
  • a positive reference frequency or other admissibility constraint;
  • the expected scaling at strong coupling;
  • a broad plateau rather than an isolated sharp extremum;
  • stability under N↦N±1N\mapsto N\pm1;
  • preservation of exact symmetries and reality properties.

Choosing the root that happens to match a benchmark best is circular unless that benchmark is used only after the rule has been fixed.

The first-order ground-state energy has a special status. Let ∣0;α⟩\lvert0;\alpha\rangle be the normalized ground state of H0(α)H_0(\alpha). First-order perturbation theory in δ\delta gives

E[1](α)=E0(0)(α)+⟨0;α∣ΔH(α)∣0;α⟩=⟨0;α∣H∣0;α⟩.\begin{aligned} E_{[1]}(\alpha) &= E_0^{(0)}(\alpha) + \langle0;\alpha\rvert \Delta H(\alpha) \lvert0;\alpha\rangle \\ &= \langle0;\alpha\rvert H \lvert0;\alpha\rangle. \end{aligned}

If the trial state lies in the energy form domain of a Hamiltonian bounded below, then

E0≤E[1](α).E_0 \leq E_{[1]}(\alpha).

Minimizing this first-order expression is therefore an ordinary Rayleigh–Ritz calculation over the reference ground-state family.

At second and higher order, E[N]E_{[N]} includes virtual-state corrections. It is generally not the expectation value of HH in a normalized trial state. Consequently,

E[N](αN)need not be an upper bound for N≥2.\begin{gathered} E_{[N]}(\alpha_N) \\ \text{need not be an upper bound for }N\geq2. \end{gathered}

This distinction is central. Stationary in an auxiliary parameter and variational upper bound are different mathematical statements. Variational Principle gives the hypotheses behind the bound.

Use dimensionless units ℏ=m=ω=1\hbar=m=\omega=1 and consider

H=p22+x22+gx4,g>0.H = \frac{p^2}{2} + \frac{x^2}{2} + g x^4, \qquad g\gt0.

Its ground-state weak-coupling series begins

E0(g)∼12+34g−218g2+33316g3+⋯ .E_0(g) \sim \frac12 + \frac34g - \frac{21}{8}g^2 + \frac{333}{16}g^3 + \cdots.

The coefficient derivations and selection rules belong to Perturbation Theory for the Harmonic Oscillator and Anharmonic Oscillator by Perturbation Theory. The important fact here is that the weak series is asymptotic: fixed-gg partial sums eventually diverge even though low orders are useful as g→0+g\to0^+.

Choose a reference oscillator with adjustable frequency Ω>0\Omega\gt0:

H0(Ω)=p22+Ω2x22.H_0(\Omega) = \frac{p^2}{2} + \frac{\Omega^2x^2}{2}.

The interpolating Hamiltonian is

Hδ(Ω)=p22+Ω2x22+δ[1−Ω22x2+gx4].\begin{aligned} H_\delta(\Omega) ={}& \frac{p^2}{2} + \frac{\Omega^2x^2}{2} \\ &+ \delta \left[ \frac{1-\Omega^2}{2}x^2 + g x^4 \right]. \end{aligned}

At δ=1\delta=1, the added and subtracted quadratic terms cancel exactly.

Define

r=1−Ω2Ω2.r = \frac{1-\Omega^2}{\Omega^2}.

The quadratic part of HδH_\delta has frequency

ωδ=Ω1+δr.\omega_\delta = \Omega\sqrt{1+\delta r}.

The known weak-coupling series for an oscillator of frequency ωδ\omega_\delta can therefore be written

E0(δ,g,Ω)∼ωδ2+3δg4ωδ2−21δ2g28ωδ5+333δ3g316ωδ8+⋯ .\begin{aligned} E_0(\delta,g,\Omega) \sim{}& \frac{\omega_\delta}{2} \\ &+ \frac{3\delta g}{4\omega_\delta^2} - \frac{21\delta^2g^2} {8\omega_\delta^5} \\ &+ \frac{333\delta^3g^3} {16\omega_\delta^8} + \cdots. \end{aligned}

The order of operations matters:

  1. substitute ωδ=Ω(1+δr)1/2\omega_\delta=\Omega(1+\delta r)^{1/2};
  2. expand every factor in powers of δ\delta;
  3. discard terms beyond δN\delta^N;
  4. set δ=1\delta=1;
  5. optimize the remaining Ω\Omega dependence.

Setting δ=1\delta=1 before re-expanding would simply restore the original divergent weak series and erase the order-dependent reorganization.

Through first order,

E[1](g,Ω)=Ω2(1+r2)+3g4Ω2.E_{[1]}(g,\Omega) = \frac{\Omega}{2} \left( 1+\frac{r}{2} \right) + \frac{3g}{4\Omega^2}.

Using the definition of rr gives

E[1](g,Ω)=Ω4+14Ω+3g4Ω2.E_{[1]}(g,\Omega) = \frac{\Omega}{4} + \frac{1}{4\Omega} + \frac{3g}{4\Omega^2}.

This is exactly the expectation value of HH in the ground state of the frequency-Ω\Omega oscillator. Anharmonic Oscillator by Variational Methods owns its Rayleigh–Ritz derivation, upper-bound interpretation, and numerical comparison; Variational Parameters explains the equivalent width coordinate and general optimization geometry.

PMS and energy minimization coincide at this order:

∂E[1]∂Ω=14−14Ω2−3g2Ω3=0.\frac{\partial E_{[1]}} {\partial\Omega} = \frac14 - \frac{1}{4\Omega^2} - \frac{3g}{2\Omega^3} =0.

Equivalently,

Ω3−Ω−6g=0.\Omega^3-\Omega-6g=0.

For every g>0g\gt0, this equation has one positive root greater than one. At g=1g=1, it happens to be

Ω1=2,E[1](1,Ω1)=1316=0.8125.\Omega_1=2, \qquad E_{[1]}(1,\Omega_1) = \frac{13}{16} =0.8125.

Because this is still a Rayleigh quotient, the number is a rigorous upper bound to the ground-state energy.

The positive PMS branch has the expansion

Ω1(g)=1+3g−272g2+108g3+O(g4).\Omega_1(g) = 1+3g - \frac{27}{2}g^2 + 108g^3 + O(g^4).

Substituting it into the optimized energy gives

E[1]opt(g)=12+34g−94g2+272g3+O(g4).\begin{aligned} E_{[1]}^{\mathrm{opt}}(g) ={}& \frac12 + \frac34g \\ &- \frac94g^2 + \frac{27}{2}g^3 + O(g^4). \end{aligned}

The exact coefficient 3/43/4 is reproduced because the calculation was carried through first order. The higher powers shown here are predictions generated by optimizing the first-order expression; they are not the exact higher-order perturbative coefficients.

Rescale

x=g−1/6y,p=g1/6py.x=g^{-1/6}y, \qquad p=g^{1/6}p_y.

Then

H=g1/3[py22+y4+g−2/32y2].H = g^{1/3} \left[ \frac{p_y^2}{2} + y^4 + \frac{g^{-2/3}}{2}y^2 \right].

The exact strong-coupling structure is therefore

E0(g)=g1/3[b0+b1g−2/3+⋯ ].E_0(g) = g^{1/3} \left[ b_0+b_1g^{-2/3}+\cdots \right].

The first-order PMS equation gives

Ω1(g)∼(6g)1/3.\Omega_1(g) \sim (6g)^{1/3}.

Thus even the lowest optimized order has the correct leading power E∝g1/3E\propto g^{1/3}. Ordinary fixed-frequency truncation instead remains a polynomial in gg and cannot have this asymptotic form at any finite order.

The re-expansion rule produces compact expressions when r=(1−Ω2)/Ω2r=(1-\Omega^2)/\Omega^2 is retained. Through second order,

E[2]=E[1]−Ωr216−3gr4Ω2−21g28Ω5.\begin{aligned} E_{[2]} ={}& E_{[1]} - \frac{\Omega r^2}{16} - \frac{3gr}{4\Omega^2} \\ &- \frac{21g^2}{8\Omega^5}. \end{aligned}

Through third order,

E[3]=E[2]+Ωr332+3gr24Ω2+105g2r16Ω5+333g316Ω8.\begin{aligned} E_{[3]} ={}& E_{[2]} + \frac{\Omega r^3}{32} + \frac{3gr^2}{4\Omega^2} \\ &+ \frac{105g^2r}{16\Omega^5} + \frac{333g^3}{16\Omega^8}. \end{aligned}

At Ω=1\Omega=1, one has r=0r=0, so these expressions reduce to the ordinary weak-coupling partial sums. That is a useful algebraic check.

Expanding E[2]E_{[2]} gives

E[2]=3Ω16+38Ω−116Ω3+3g2Ω2−3g4Ω4−21g28Ω5.\begin{aligned} E_{[2]} ={}& \frac{3\Omega}{16} + \frac{3}{8\Omega} - \frac{1}{16\Omega^3} \\ &+ \frac{3g}{2\Omega^2} - \frac{3g}{4\Omega^4} - \frac{21g^2}{8\Omega^5}. \end{aligned}

Its derivative obeys the identity

16Ω63∂E[2]∂Ω=(Ω3−Ω−8g)2+6g2.\frac{16\Omega^6}{3} \frac{\partial E_{[2]}} {\partial\Omega} = \left( \Omega^3-\Omega-8g \right)^2 + 6g^2.

For g>0g\gt0, the right-hand side is strictly positive. The second-order approximant is monotone in Ω\Omega and has no real PMS point.

This is not an algebraic failure. It is a genuine feature of this order and prescription. One may continue with complex roots, FAC, an inflection criterion, or a different interpolation, but each choice adds information beyond the PMS equation.

For the numerical comparison below, use the following stated rules:

  • at first and third order, choose the positive real PMS root continuous from weak coupling;
  • at second order, where no real PMS root exists, choose the positive inflection point;
  • use a converged harmonic-oscillator basis diagonalization as an external benchmark.

At g=1g=1:

ApproximationAuxiliary choiceEnergy
Ordinary series through ggΩ=1\Omega=11.2500001.250000
Ordinary series through g2g^2Ω=1\Omega=1−1.375000-1.375000
Ordinary series through g3g^3Ω=1\Omega=119.43750019.437500
Reorganized first orderPMS, Ω1=2\Omega_1=20.8125000.812500
Reorganized second orderinflection, Ω2≃2.213607\Omega_2\simeq2.2136070.8041900.804190
Reorganized third orderPMS, Ω3≃2.328958\Omega_3\simeq2.3289580.8039140.803914
Numerical diagonalizationbasis-converged0.8037706510.803770651

The table illustrates possibility, not a universal error theorem. The second-order value depends on the explicitly stated inflection prescription. The third-order error is small, but a single successful coupling and a few orders do not prove convergence.

The second-order value also lies above the benchmark for this particular prescription, but higher-order theory supplies no general upper-bound guarantee. For example, evaluating the same second-order expression at g=1g=1 and Ω=2\Omega=2 gives

E[2](1,2)=0.80078125,E_{[2]}(1,2) = 0.80078125,

which is below the exact ground-state energy. The variational bound was lost when the second-order virtual-state correction was added.

The auxiliary parameter must generally depend on perturbative order:

Ω⟶ΩN.\Omega \longrightarrow \Omega_N.

Keeping Ω\Omega fixed while N→∞N\to\infty simply recovers another presentation of the original perturbative problem. The useful sequence coordinates the large-NN limit with an order-dependent reference scale.

For the quartic oscillator, rigorous results exist for particular scaled delta expansions. In the convention with interaction gq4/4gq^4/4, Guida, Konishi, and Suzuki proved convergence of the energy eigenvalue sequence when the trial frequency scales as

ΩN=CNγ,13<γ<12,C>0,\Omega_N = C N^\gamma, \qquad \frac13\lt\gamma\lt\frac12, \qquad C\gt0,

and also under a qualified boundary scaling at γ=1/3\gamma=1/3. The numerical constants at that boundary depend on the Hamiltonian normalization.

This theorem is strong but specific. It does not say that:

  • every interpolation converges;
  • every PMS root belongs to the convergent sequence;
  • every observable converges under the same hypotheses;
  • an oscillator proof transfers automatically to a quantum field theory;
  • optimization supplies a rigorous finite-order error bar.

Order-dependent mappings make the same structural lesson explicit. A coupling is mapped using an order-dependent parameter chosen from analytic or strong-coupling information. The mapping changes with NN so that the expansion point, singularity structure, and physical evaluation point are approached together.

Terminology varies across subfields. The following descriptions are safer than treating all names as exact synonyms.

NameCharacteristic stepMain emphasis
Linear δ expansionHδ=H0+δ(H−H0)H_\delta=H_0+\delta(H-H_0)interpolation and formal re-expansion
Optimized perturbation theoryfix auxiliary dependence after truncationPMS, FAC, or related optimization
Variational perturbation theorycombine re-expansion with variational or strong-coupling informationorder-dependent convergence and strong-coupling structure
Order-dependent mappingmap the coupling with parameters that vary with orderanalytic continuation and summation of divergent series

In the quartic oscillator these constructions overlap closely and can be transformed into one another. In other applications they may use different interpolations, optimization equations, renormalization conventions, or assumed strong-coupling exponents. A calculation should define its transformation and root prescription rather than relying on the method name alone.

The adjustable oscillator is only the simplest example. One can introduce several parameters:

H0(α)=H0(α1,…,αk).H_0(\boldsymbol\alpha) = H_0( \alpha_1,\ldots,\alpha_k ).

Examples include:

  • several normal-mode frequencies in a coupled oscillator;
  • a displacement and width for an asymmetric potential;
  • a self-consistent one-body potential in a many-body problem;
  • a trial mass in a finite-temperature field theory;
  • anisotropic Gaussian width matrices;
  • a reference basis whose nonlinear scale is optimized together with a truncated diagonalization.

The interpolation should preserve exact symmetries unless symmetry breaking is intentional and physically controlled. Adding and subtracting a term that violates a symmetry can make intermediate expressions simpler while obscuring Ward identities, degeneracies, or selection rules.

For several auxiliary parameters, stationary equations can be ill-conditioned. The Hessian

Hij(N)=∂2Q[N]∂αi∂αj\mathcal H_{ij}^{(N)} = \frac{\partial^2Q_{[N]}} {\partial\alpha_i\partial\alpha_j}

distinguishes broad insensitive directions from sharp or unstable ones. The coordinate and metric issues are developed on Variational Parameters.

For an excited reference state, first-order perturbation theory still gives an expectation value of HH. It is not automatically an upper bound to the corresponding exact excited energy. Rigorous excited-state bounds require orthogonality constraints or the ordered subspace statement of the Min–Max Principle.

For wavefunctions and general observables, optimization introduces further choices. If an observable AA is evaluated with an approximate state, one can optimize the energy and then compute AA, or optimize the truncated expression for AA itself. These procedures need not agree at finite order. Observable-specific optimization can also destroy relations among quantities that share a common state.

Useful checks include:

  • normalization and symmetry of the approximate state;
  • eigenpair residuals when a state is available;
  • Hellmann–Feynman consistency for parameter derivatives;
  • agreement among observables linked by exact identities;
  • stability under neighboring orders and auxiliary branches.

Adding and subtracting an auxiliary mass is widely used in thermal and quantum field theory. Schematically,

Lδ=L0(m∗)+δ[L−L0(m∗)].\mathcal L_\delta = \mathcal L_0(m_*) + \delta \left[ \mathcal L- \mathcal L_0(m_*) \right].

The reorganized propagator contains m∗m_*, while counterterms and interaction insertions compensate the change when the expansion is complete. At finite order, one may optimize m∗m_* or determine it through a gap equation.

The oscillator analogy is useful but incomplete. Field theory adds ultraviolet regularization, renormalization, scale and scheme dependence, infinitely many modes, and symmetry identities. A trial-mass reorganization must be renormalized consistently at the chosen order. The quartic-oscillator convergence theorem cannot simply be quoted as a proof for a field-theory expansion.

  1. Nondimensionalize the Hamiltonian. Identify the physical weak- and strong-coupling scales before introducing auxiliary parameters.
  2. Choose a solvable reference family. Preserve domain conditions and important symmetries.
  3. Write the interpolation explicitly. Verify both endpoints δ=0\delta=0 and δ=1\delta=1.
  4. Fix an order convention. State whether order counts powers of δ\delta, the physical coupling, loops, or another hierarchy.
  5. Re-expand before setting δ=1\delta=1. Keep all induced terms through the stated order.
  6. List every admissible optimization root. Record real, positive, continuous branches before using a benchmark.
  7. State the prescription. Distinguish PMS, FAC, inflection, and complex-root rules.
  8. Check limiting behavior. Recover the weak-coupling coefficients and the known strong-coupling exponent when available.
  9. Compare neighboring orders. Track both values and auxiliary parameters.
  10. Benchmark independently. Use basis diagonalization, shooting, a rigorous bound, or trusted asymptotic information.

Optimization alone does not provide a rigorous uncertainty. A practical assessment can combine:

ΔNorder=∣Q[N]−Q[N−1]∣,\Delta_N^{\mathrm{order}} = \left| Q_{[N]}-Q_{[N-1]} \right|,

with a root spread

ΔNroot=max⁡a,b∣Q[N](αN(a))−Q[N](αN(b))∣,\Delta_N^{\mathrm{root}} = \max_{a,b} \left| Q_{[N]}(\alpha_N^{(a)}) - Q_{[N]}(\alpha_N^{(b)}) \right|,

and an auxiliary variation across a declared plateau. These are diagnostics, not confidence intervals. They become more credible when their trends agree and when independent numerical errors are smaller.

For a divergent source series, raw term size, large-order information, and Borel-plane structure remain relevant. Asymptotic Analysis gives the mathematical language, while Resurgence Preview separates perturbative summation from nonperturbative sectors.

  • Setting δ=1\delta=1 before the re-expansion.
  • Treating the bookkeeping parameter as a physical small parameter.
  • Calling every stationary optimized energy a variational upper bound.
  • Assuming that a PMS root must exist and be real at every order.
  • Hiding an inflection or complex-root prescription under the label PMS.
  • Choosing among roots after looking at the exact answer.
  • Keeping the auxiliary scale fixed as perturbative order grows.
  • Using a first-order variational coincidence as proof of higher-order bounds.
  • Reporting neighboring-order agreement as a rigorous error bar.
  • Ignoring the expected strong-coupling exponent when selecting a mapping.
  • Transferring an oscillator convergence theorem to field theory without checking its hypotheses.
  • Optimizing different observables independently and then assuming exact identities still hold.

Show that Hδ=1(α)H_{\delta=1}(\alpha) is independent of α\alpha. Explain why this does not imply that Q[N](α)Q_{[N]}(\alpha) is independent of α\alpha at finite order.

Solution

By construction,

Hδ=1(α)=H0(α)+H−H0(α)=H.\begin{aligned} H_{\delta=1}(\alpha) &= H_0(\alpha) + H-H_0(\alpha) \\ &=H. \end{aligned}

Thus every exact observable of the physical Hamiltonian is independent of α\alpha. A truncated series keeps only finitely many powers of δ\delta. Terms that would cancel its α\alpha dependence at higher orders have been omitted, so in general

∂αQ[N]≠0.\partial_\alpha Q_{[N]}\ne0.

PMS uses this residual dependence to choose a locally insensitive point; it does not establish exact independence at finite NN.

For the quartic oscillator, use the ground state of H0(Ω)H_0(\Omega) to derive E[1](g,Ω)E_{[1]}(g,\Omega) and its PMS equation. Explain why the result is an upper bound.

Solution

The reference ground state has moments

⟨p2⟩=Ω2,⟨x2⟩=12Ω,⟨x4⟩=34Ω2.\begin{aligned} \langle p^2\rangle &= \frac{\Omega}{2}, \\ \langle x^2\rangle &= \frac{1}{2\Omega}, \\ \langle x^4\rangle &= \frac{3}{4\Omega^2}. \end{aligned}

Therefore

E[1]=Ω4+14Ω+3g4Ω2.E_{[1]} = \frac{\Omega}{4} + \frac{1}{4\Omega} + \frac{3g}{4\Omega^2}.

Differentiation gives

0=14−14Ω2−3g2Ω3,0 = \frac14 - \frac{1}{4\Omega^2} - \frac{3g}{2\Omega^3},

or

Ω3−Ω−6g=0.\Omega^3-\Omega-6g=0.

The expression is the expectation value of the physical Hamiltonian in a normalized admissible Gaussian. The Rayleigh–Ritz principle therefore gives E0≤E[1]E_0\leq E_{[1]} for every Ω>0\Omega\gt0, including the minimizing value.

3. Check weak- and strong-coupling behavior

Section titled “3. Check weak- and strong-coupling behavior”

Expand the positive solution of Ω3−Ω−6g=0\Omega^3-\Omega-6g=0 through g2g^2. Then determine its leading behavior as g→∞g\to\infty.

Solution

Set

Ω=1+ag+bg2+O(g3).\Omega = 1+ag+bg^2+O(g^3).

Substitution into the cubic gives

2a=6,3a2+2b=0.2a=6, \qquad 3a^2+2b=0.

Hence

a=3,b=−272,a=3, \qquad b=-\frac{27}{2},

and

Ω=1+3g−272g2+O(g3).\Omega = 1+3g- \frac{27}{2}g^2 + O(g^3).

At large gg, the linear term in Ω\Omega is subleading, so

Ω3∼6g,\Omega^3\sim6g,

which gives

Ω∼(6g)1/3.\Omega\sim(6g)^{1/3}.

Substitution into E[1]E_{[1]} then gives E[1]∝g1/3E_{[1]}\propto g^{1/3}, matching the exact scaling exponent.

4. Show that second-order PMS has no real root

Section titled “4. Show that second-order PMS has no real root”

Differentiate the expanded second-order energy and prove that it is strictly increasing for g>0g\gt0 and Ω>0\Omega\gt0.

Solution

Differentiation gives

∂E[2]∂Ω=316−38Ω2+316Ω4−3gΩ3+3gΩ5+105g28Ω6.\begin{aligned} \frac{\partial E_{[2]}} {\partial\Omega} ={}& \frac{3}{16} - \frac{3}{8\Omega^2} + \frac{3}{16\Omega^4} \\ &- \frac{3g}{\Omega^3} + \frac{3g}{\Omega^5} + \frac{105g^2}{8\Omega^6}. \end{aligned}

Multiplying by the positive factor 16Ω6/316\Omega^6/3 and completing the square yields

16Ω63∂E[2]∂Ω=(Ω3−Ω−8g)2+6g2.\frac{16\Omega^6}{3} \frac{\partial E_{[2]}} {\partial\Omega} = \left( \Omega^3-\Omega-8g \right)^2 + 6g^2.

For g>0g\gt0, the right-hand side is strictly positive. Therefore E[2]E_{[2]} is strictly increasing and has no real stationary point. Any second-order value selected by an inflection, complex root, or another criterion must be labeled with that extra prescription.

5. Demonstrate the loss of the upper bound

Section titled “5. Demonstrate the loss of the upper bound”

Evaluate E[2]E_{[2]} at g=1g=1 and Ω=2\Omega=2. Compare it with the numerical benchmark E0≃0.803770651E_0\simeq0.803770651.

Solution

Using

E[2]=3Ω16+38Ω−116Ω3+3g2Ω2−3g4Ω4−21g28Ω5,\begin{aligned} E_{[2]} ={}& \frac{3\Omega}{16} + \frac{3}{8\Omega} - \frac{1}{16\Omega^3} \\ &+ \frac{3g}{2\Omega^2} - \frac{3g}{4\Omega^4} - \frac{21g^2}{8\Omega^5}, \end{aligned}

one obtains

E[2](1,2)=205256=0.80078125.E_{[2]}(1,2) = \frac{205}{256} = 0.80078125.

This is below the exact ground-state energy. The result is not a contradiction because E[2]E_{[2]} is not a Rayleigh quotient. The upper-bound theorem applied to E[1]E_{[1]}, not to the higher-order perturbative correction.

6. Derive the compact third-order expression

Section titled “6. Derive the compact third-order expression”

Use

(1+z)1/2=1+12z−18z2+116z3+O(z4)\begin{aligned} (1+z)^{1/2} ={}& 1+\frac12z - \frac18z^2 \\ &+ \frac1{16}z^3 + O(z^4) \end{aligned}

and the corresponding binomial expansions of (1+z)−1(1+z)^{-1} and (1+z)−5/2(1+z)^{-5/2} to derive E[3]E_{[3]}.

Solution

Insert ωδ=Ω(1+δr)1/2\omega_\delta=\Omega(1+\delta r)^{1/2} into

ωδ2+3δg4ωδ2−21δ2g28ωδ5+333δ3g316ωδ8.\frac{\omega_\delta}{2} + \frac{3\delta g}{4\omega_\delta^2} - \frac{21\delta^2g^2}{8\omega_\delta^5} + \frac{333\delta^3g^3}{16\omega_\delta^8}.

The terms newly retained at order δ3\delta^3 are

Ωr332,3gr24Ω2,105g2r16Ω5,333g316Ω8.\begin{aligned} & \frac{\Omega r^3}{32}, \qquad \frac{3gr^2}{4\Omega^2}, \\ & \frac{105g^2r}{16\Omega^5}, \qquad \frac{333g^3}{16\Omega^8}. \end{aligned}

After setting δ=1\delta=1,

E[3]=E[2]+Ωr332+3gr24Ω2+105g2r16Ω5+333g316Ω8.\begin{aligned} E_{[3]} ={}& E_{[2]} + \frac{\Omega r^3}{32} + \frac{3gr^2}{4\Omega^2} \\ &+ \frac{105g^2r}{16\Omega^5} + \frac{333g^3}{16\Omega^8}. \end{aligned}

At Ω=1\Omega=1, r=0r=0, and the ordinary third-order weak-coupling partial sum is recovered.

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