The Cohn–Elkies exponent and sign uncertainty

5.3. Saddle geometry🔗

Stationary radii, the centered phase, damping and moment quantities, and the damping estimates (Section 4.3: (43)–(49) and Lemmas 4.4–4.7).

Definition5.3.1
Group: Saddle geometry (21)
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Definition 5.3.2
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Recall u_0, U from Definition 5.2.1 and set (equation (43)) u_* = -1 + \dfrac{\log\lambda}{4\lambda}. For u > -1 put \eta = 1 + u > 0, m = \dfrac{\lambda\eta}{2}, and use \psi = (\log\Gamma)' from Definition 3.1.4, with the branch of \log\Gamma real on the positive axis. Note m \ge \lambda(1+u_*)/2 = \tfrac18\log\lambda for u \ge u_*.

Lean code for Definition5.3.1●1 definition
  • def CohnElkies.u_star (_ε : ℝ) (d : ℕ) : ℝ
    def CohnElkies.u_star (_ε : ℝ) (d : ℕ) : ℝ
    Report Lemma 4.10: the near-optimal contour height `u_* = -1 + (log λ)/(4λ)`, `λ = d/2`. 
Definition5.3.2
Group: Saddle geometry (21)
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Definition 5.3.3
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On the contour t = \lambda(T + iu), the logarithm of E_\lambda(t)r^{it} (Definition 5.2.11) is \tfrac{i\lambda(T+iu)}{2}\log\pi + \log\Gamma\bigl(m - \tfrac{i\lambda T}{2}\bigr) + \lambda h_\epsilon(T+iu) + i\lambda(T+iu)\log r, whose T-derivative at T = 0 is i\lambda(\tfrac12\log\pi - \tfrac12\psi(m) - \int_0^\infty w(a)a\sinh(ua)\,da + \log r) (Lemma 5.2.5). Thus T = 0 is stationary precisely when r = e^{v(u)}, where (equation (44)) v(u) = -\tfrac12\log\pi + \tfrac12\psi(m) + \int_0^\infty w(a)\,a\sinh(ua)\,da. Uses Definition 5.3.1, Definition 5.2.4.

Lean code for Definition5.3.2●3 declarations
  • complete
    def CohnElkies.vℓ (ε ℓ u : ℝ) : ℝ
    def CohnElkies.vℓ (ε ℓ u : ℝ) : ℝ
    Report (44): the stationary log radius `v_ℓ(u)`. 
  • def CohnElkies.logRadius (ε : ℝ) (d : ℕ) (u : ℝ) : ℝ
    def CohnElkies.logRadius (ε : ℝ) (d : ℕ)
      (u : ℝ) : ℝ
    Report (83): the logarithm of the saddle radius `r(u)` in dimension `d`. 
  • complete
    theorem CohnElkies.saddleLogRadius_eq_digamma_add_shellDerivative (ε : ℝ)
      (d : ℕ) (u : ℝ) :
      CohnElkies.logRadius ε d u =
        -Real.log Real.pi / 2 + (↑d / 2 * (1 + u) / 2).digamma / 2 +
          CohnElkies.saddleSourceShellDerivative ε u
    theorem CohnElkies.saddleLogRadius_eq_digamma_add_shellDerivative
      (ε : ℝ) (d : ℕ) (u : ℝ) :
      CohnElkies.logRadius ε d u =
        -Real.log Real.pi / 2 +
            (↑d / 2 * (1 + u) / 2).digamma /
              2 +
          CohnElkies.saddleSourceShellDerivative
            ε u
Definition5.3.3
Group: Saddle geometry (21)
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Definition 5.3.11
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The saddle variance is V(u) = V_\gamma - V_s + V_B with the moments of Definition 5.3.10 (formally V = v' for v of Definition 5.3.2).

Lean code for Definition5.3.3●4 definitions
  • def CohnElkies.upperSaddleVariance (ε ℓ δ : ℝ) : ℝ
    def CohnElkies.upperSaddleVariance
      (ε ℓ δ : ℝ) : ℝ
    The saddle variance `V_γ + (V_B - V_s)` of report (48). 
  • def CohnElkies.V_γ (ℓ η : ℝ) : ℝ
    def CohnElkies.V_γ (ℓ η : ℝ) : ℝ
    The variance `V_γ` of the gamma density, report (48). 
  • def CohnElkies.V_s (ε δ : ℝ) : ℝ
    def CohnElkies.V_s (ε δ : ℝ) : ℝ
    Variance `V_s` carried by the short shell on the contour of height `1 + δ`. 
  • def CohnElkies.V_B (ε δ : ℝ) : ℝ
    def CohnElkies.V_B (ε δ : ℝ) : ℝ
    Variance `V_B` carried by the positive shell on the contour of height `1 + δ`. 
Definition5.3.4
Group: Saddle geometry (21)
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Lemma 5.3.5
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For \lambda, \eta > 0 and T \in \mathbb{R}, with \mu_{\lambda,\eta} from Definition 5.2.6, the centered log-gamma phase is (equation (45)) G_{\lambda,\eta}(T) := \int_0^\infty(e^{iaT} - 1 - iaT)\,\mu_{\lambda,\eta}(a)\,da.

Lean code for Definition5.3.4●1 definition
  • complete
    def CohnElkies.G_ℓη (ℓ η T : ℝ) : ℂ
    def CohnElkies.G_ℓη (ℓ η T : ℝ) : ℂ
    Report (45): the centred log-gamma phase `G_{ℓ,η}(T) = ∫₀^∞ (e^{iaT} - 1 - iaT) dμ_ℓ(a)`. 
Lemma5.3.5
Group: Saddle geometry (21)
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For \lambda, \eta > 0, m = \lambda\eta/2, and T \in \mathbb{R}, the phase of Definition 5.3.4 satisfies e^{G_{\lambda,\eta}(T)} = \dfrac{\Gamma\bigl(m - \tfrac{i\lambda T}{2}\bigr)}{\Gamma(m)}\,e^{i\lambda T\psi(m)/2}, that is, G_{\lambda,\eta}(T) = \log\Gamma\bigl(m - \tfrac{i\lambda T}{2}\bigr) - \log\Gamma(m) + \tfrac{i\lambda T}{2}\psi(m) (Binet-type representation; Definition 3.1.4).

Lean code for Lemma5.3.5●1 theorem
  • complete
    theorem CohnElkies.exp_G_ℓη {ℓ η : ℝ} (hℓ : 0 < ℓ) (hη : 0 < η) (T : ℝ) :
      Complex.exp (CohnElkies.G_ℓη ℓ η T) =
        Complex.Gamma (↑ℓ * ↑η / 2 - Complex.I * (↑ℓ * ↑T / 2)) /
            ↑(Real.Gamma (ℓ * η / 2)) *
          Complex.exp (Complex.I * (↑ℓ * ↑T / 2 * ↑(ℓ * η / 2).digamma))
    theorem CohnElkies.exp_G_ℓη {ℓ η : ℝ} (hℓ : 0 < ℓ)
      (hη : 0 < η) (T : ℝ) :
      Complex.exp (CohnElkies.G_ℓη ℓ η T) =
        Complex.Gamma
              (↑ℓ * ↑η / 2 -
                Complex.I * (↑ℓ * ↑T / 2)) /
            ↑(Real.Gamma (ℓ * η / 2)) *
          Complex.exp
            (Complex.I *
              (↑ℓ * ↑T / 2 *
                ↑(ℓ * η / 2).digamma))
    Report (45): `exp G_{ℓ,η}(T) = Γ(m - i b)/Γ(m) · e^{i b ψ(m)}` with `m = ℓη/2`, `b = ℓT/2`. 
Proof for Lemma 5.3.5
uses 0

Apply the Malmstén–Binet integral representation of \log\Gamma, \log\Gamma(z+w) - \log\Gamma(z) - w\psi(z) = \int_0^\infty (e^{-ws} - 1 + ws)\,\dfrac{e^{-zs}}{s(1-e^{-s})}\,ds (\operatorname{Re} z > 0, \operatorname{Re}(z+w) > 0), with z = m, w = -i\lambda T/2, and substitute a = \lambda s/2. (The formalization proves the exponentiated identity through the Euler product of \Gamma: truncating the geometric series in 1/(1 - e^{-2a/\lambda}) gives the ratios \Gamma_N(m - ib)/\Gamma_N(m) of the partial products, which converge to the gamma ratio.)

Definition5.3.6
Group: Saddle geometry (21)
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Definition 5.3.1
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Lemma 5.3.7
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The gamma damping is D_\gamma(T) := -\operatorname{Re}G_{\lambda,\eta}(T) = \int_0^\infty(1 - \cos(aT))\,\mu_{\lambda,\eta}(a)\,da (Definition 5.3.4).

Lean code for Definition5.3.6●1 definition
  • def CohnElkies.D_γ (ℓ η T : ℝ) : ℝ
    def CohnElkies.D_γ (ℓ η T : ℝ) : ℝ
    `D_γ(T) = ∫₀^∞ (1 - cos (aT)) μ_{λ,η}(a) da`, the gamma damping of report (45). 
Lemma5.3.7
Group: Saddle geometry (21)
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D_\gamma(T) \ge 0 for every T (Definition 5.3.6): the gamma function in the Mellin envelope always damps the integrand away from T = 0.

Lean code for Lemma5.3.7●1 theorem
  • complete
    theorem CohnElkies.upperGammaDamping_nonneg {ℓ η : ℝ} (hℓ : 0 < ℓ) (T : ℝ) :
      0 ≤ CohnElkies.D_γ ℓ η T
    theorem CohnElkies.upperGammaDamping_nonneg
      {ℓ η : ℝ} (hℓ : 0 < ℓ) (T : ℝ) :
      0 ≤ CohnElkies.D_γ ℓ η T
Proof for Lemma 5.3.7
uses 0

1 - \cos(aT) \ge 0 and \mu_{\lambda,\eta} > 0.

Definition5.3.8
Group: Saddle geometry (21)
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Definition 5.3.9
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Normalize E_\lambda(\lambda(T+iu))r^{i\lambda T} by the positive number E_\lambda(i\lambda u) = \pi^{-\lambda u/2}\Gamma(m)e^{\lambda h_\epsilon(iu)} and set r = e^{v(u)}. The linear terms cancel by the saddle equation, and (36) gives (equations (46), (47)) \mathcal{L}_u(T) := \log\dfrac{E_\lambda(\lambda(T+iu))}{E_\lambda(i\lambda u)} + i\lambda Tv(u), which equals G_{\lambda,\eta}(T) + \lambda\int_0^\infty w(a)\cosh(ua)(\cos(aT)-1)\,da + i\lambda\int_0^\infty w(a)\sinh(ua)(aT - \sin(aT))\,da. Uses Definition 5.3.2, Definition 5.3.4 and Lemma 5.3.5.

Lean code for Definition5.3.8●1 definition
  • complete
    def CohnElkies.L_u (ε ℓ u T : ℝ) : ℂ
    def CohnElkies.L_u (ε ℓ u T : ℝ) : ℂ
    The centred saddle phase `L_u(T)` of report (46): gamma part plus shell part. 
Definition5.3.9
Group: Saddle geometry (21)
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Definition 5.3.11
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The total damping is (equation (47)) D_u(T) := -\operatorname{Re}\mathcal{L}_u(T) = D_\gamma(T) + \lambda\int_0^\infty w(a)\cosh(ua)(1 - \cos(aT))\,da (Definition 5.3.8, Definition 5.3.6). Equation (47) isolates the main difficulty: w_s reduces D_u, while w_B increases it. We must prove D_u(T) > 0 for every T \ne 0 and V(u) > 0 for every u \ge u_*.

Lean code for Definition5.3.9●2 definitions
  • def CohnElkies.D_u (ε ℓ δ T : ℝ) : ℝ
    def CohnElkies.D_u (ε ℓ δ T : ℝ) : ℝ
    The total damping `D_u = D_γ + D_B - D_s` of report (47). 
  • def CohnElkies.saddleSourceContourDamping (ε ℓ u T : ℝ) : ℝ
    def CohnElkies.saddleSourceContourDamping
      (ε ℓ u T : ℝ) : ℝ
    The damping exponent `D(u, T) = D_γ + D_B - D_s` of the contour `z = λ(1 + u) - iλT`,
    report (46) and (49). 
Definition5.3.10
Group: Saddle geometry (21)
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Lemma 5.3.12
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The quadratic and cubic sizes of the phase are measured by (equation (48)) V_\gamma = \dfrac1\lambda\int_0^\infty a^2\mu_{\lambda,\eta}(a)\,da, M_3 = \dfrac1\lambda\int_0^\infty a^3\mu_{\lambda,\eta}(a)\,da + \int_0^\infty\bigl(|w_s(a)| + w_B(a)\bigr)a^3\cosh(ua)\,da (Definition 5.2.6, Definition 5.2.3).

Lean code for Definition5.3.10●3 definitions
  • def CohnElkies.V_γ (ℓ η : ℝ) : ℝ
    def CohnElkies.V_γ (ℓ η : ℝ) : ℝ
    The variance `V_γ` of the gamma density, report (48). 
  • def CohnElkies.M₃_γ (ℓ η : ℝ) : ℝ
    def CohnElkies.M₃_γ (ℓ η : ℝ) : ℝ
    The third moment `M₃_γ` of the gamma density, report (48). 
  • def CohnElkies.M₃ (ε ℓ δ : ℝ) : ℝ
    def CohnElkies.M₃ (ε ℓ δ : ℝ) : ℝ
    The saddle third moment `M₃_γ + (M₃_B - M₃_s)` of report (48). 
Definition5.3.11
Group: Saddle geometry (21)
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Lemma 5.3.16
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The shell contributions are (equation (49)) D_s(T) = \lambda\int_{a_0}^A|w_s(a)|\cosh(ua)(1-\cos(aT))\,da, D_B(T) = \lambda\int_B^{B+1}w_B(a)\cosh(ua)(1-\cos(aT))\,da, V_s = \int_{a_0}^A|w_s(a)|a^2\cosh(ua)\,da, V_B = \int_B^{B+1}w_B(a)a^2\cosh(ua)\,da (Definition 5.2.2, Definition 5.2.3). In particular D_u = D_\gamma - D_s + D_B and V(u) = V_\gamma - V_s + V_B (Definition 5.3.9, Definition 5.3.3).

Lean code for Definition5.3.11●4 definitions
  • def CohnElkies.D_s (ε ℓ δ T : ℝ) : ℝ
    def CohnElkies.D_s (ε ℓ δ T : ℝ) : ℝ
    Damping `D_s(T)` produced by the short shell on the contour of height `1 + δ`. 
  • complete
    def CohnElkies.D_B (ε ℓ δ T : ℝ) : ℝ
    def CohnElkies.D_B (ε ℓ δ T : ℝ) : ℝ
    Damping `D_B(T)` produced by the positive shell on the contour of height `1 + δ`. 
  • def CohnElkies.V_s (ε δ : ℝ) : ℝ
    def CohnElkies.V_s (ε δ : ℝ) : ℝ
    Variance `V_s` carried by the short shell on the contour of height `1 + δ`. 
  • def CohnElkies.V_B (ε δ : ℝ) : ℝ
    def CohnElkies.V_B (ε δ : ℝ) : ℝ
    Variance `V_B` carried by the positive shell on the contour of height `1 + δ`. 
Lemma5.3.12
Group: Saddle geometry (21)
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For every \lambda > 0, u > -1 and T \in \mathbb{R}, the quantities of Definition 5.3.8, Definition 5.3.3 and Definition 5.3.10 satisfy (equation (50)) \Bigl|\mathcal{L}_u(T) + \dfrac{\lambda V(u)}{2}T^2\Bigr| \le \dfrac{\lambda M_3}{6}|T|^3.

Lean code for Lemma5.3.12●1 theorem
  • complete
    theorem CohnElkies.norm_L_u_add_le {ε ℓ u : ℝ} (hε : 0 < ε) (hℓ : 0 < ℓ)
      (hu : -1 < u) (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (T : ℝ) :
      ‖CohnElkies.L_u ε ℓ u T + ↑ℓ * ↑(CohnElkies.V_u ε ℓ u) / 2 * ↑T ^ 2‖ ≤
        ℓ * CohnElkies.M₃ ε ℓ (u - 1) / 6 * |T| ^ 3
    theorem CohnElkies.norm_L_u_add_le {ε ℓ u : ℝ}
      (hε : 0 < ε) (hℓ : 0 < ℓ) (hu : -1 < u)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (T : ℝ) :
      ‖CohnElkies.L_u ε ℓ u T +
            ↑ℓ * ↑(CohnElkies.V_u ε ℓ u) / 2 *
              ↑T ^ 2‖ ≤
        ℓ * CohnElkies.M₃ ε ℓ (u - 1) / 6 *
          |T| ^ 3
Proof for Lemma 5.3.12
uses 0

The globally valid Taylor estimates e^{ix} - 1 - ix = -x^2/2 + O(|x|^3) and x - \sin x = O(|x|^3), applied to (45) and (46) with |\sinh(ua)| \le \cosh(ua).

Lemma5.3.13
Group: Saddle geometry (21)
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Lemma 5.3.16
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For \lambda, \eta > 0 the gamma moments of Definition 5.3.10 satisfy (equations (51)–(52)) \dfrac{1}{2\eta} \le V_\gamma \le \dfrac{1}{2\eta} + \dfrac{1}{\lambda\eta^2}, \dfrac{1}{2\eta^2} \le \dfrac1\lambda\int_0^\infty a^3\mu_{\lambda,\eta}(a)\,da \le \dfrac{1}{2\eta^2} + \dfrac{2}{\lambda\eta^3}.

Lean code for Lemma5.3.13●2 theorems
  • complete
    theorem CohnElkies.upperGammaVariance_bounds {ℓ η : ℝ} (hℓ : 0 < ℓ)
      (hη : 0 < η) :
      1 / (2 * η) ≤ CohnElkies.V_γ ℓ η ∧
        CohnElkies.V_γ ℓ η ≤ 1 / (2 * η) + 1 / (ℓ * η ^ 2)
    theorem CohnElkies.upperGammaVariance_bounds
      {ℓ η : ℝ} (hℓ : 0 < ℓ) (hη : 0 < η) :
      1 / (2 * η) ≤ CohnElkies.V_γ ℓ η ∧
        CohnElkies.V_γ ℓ η ≤
          1 / (2 * η) + 1 / (ℓ * η ^ 2)
    Report (48): `1/(2η) ≤ V_γ ≤ 1/(2η) + 1/(λη²)`. 
  • complete
    theorem CohnElkies.upperGammaThirdMoment_bounds {ℓ η : ℝ} (hℓ : 0 < ℓ)
      (hη : 0 < η) :
      1 / (2 * η ^ 2) ≤ CohnElkies.M₃_γ ℓ η ∧
        CohnElkies.M₃_γ ℓ η ≤ 1 / (2 * η ^ 2) + 2 / (ℓ * η ^ 3)
    theorem CohnElkies.upperGammaThirdMoment_bounds
      {ℓ η : ℝ} (hℓ : 0 < ℓ) (hη : 0 < η) :
      1 / (2 * η ^ 2) ≤ CohnElkies.M₃_γ ℓ η ∧
        CohnElkies.M₃_γ ℓ η ≤
          1 / (2 * η ^ 2) + 2 / (ℓ * η ^ 3)
    Report (48): `1/(2η²) ≤ M₃_γ ≤ 1/(2η²) + 2/(λη³)`. 
Proof for Lemma 5.3.13

Both follow from x \le e^x - 1 \le xe^x applied to the density \mu_{\lambda,\eta} of Definition 5.2.6 (the report instead inserts uniform trigamma and polygamma estimates into the polygamma expressions of the moments).

Lemma5.3.14
Group: Saddle geometry (21)
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Lemma 5.3.22
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✓L∃∀N

For \lambda, \eta > 0 and all T (equation (53)), D_\gamma(T) \ge \dfrac{\lambda}{8e}\min\Bigl(\dfrac{T^2}{\eta}, |T|\Bigr) (Definition 5.3.6).

Lean code for Lemma5.3.14●1 theorem
  • complete
    theorem CohnElkies.upperGammaDamping_lower_bound {ℓ η : ℝ} (hℓ : 0 < ℓ)
      (hη : 0 < η) (T : ℝ) :
      ℓ / (8 * Real.exp 1) * min (T ^ 2 / η) |T| ≤ CohnElkies.D_γ ℓ η T
    theorem CohnElkies.upperGammaDamping_lower_bound
      {ℓ η : ℝ} (hℓ : 0 < ℓ) (hη : 0 < η)
      (T : ℝ) :
      ℓ / (8 * Real.exp 1) *
          min (T ^ 2 / η) |T| ≤
        CohnElkies.D_γ ℓ η T
    Report (45): `λ/(8e) · min (T²/η, |T|) ≤ D_γ(T)`. 
Proof for Lemma 5.3.14
uses 0

1 - e^{-x} \le x in (37) gives \mu_{\lambda,\eta}(a) \ge \lambda e^{-\eta a}/(2a^2). For T \ne 0 take L = \min(\eta^{-1}, |T|^{-1}); on 0 < a < L both e^{-\eta a} and (1-\cos(aT))/(a^2T^2) are bounded below by absolute positive constants, so D_\gamma(T) \ge c\lambda T^2L, which is (53).

Lemma 4.4 and (51)–(53) control the gamma contribution and cubic remainder. For u_* \le u \le U the negative shell removes at most a (1 - c\epsilon)-fraction of the gamma damping, while w_B contributes nonnegative damping.

Lemma5.3.15
Group: Saddle geometry (21)
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For every 0 < \epsilon \le 1/4, \lambda > 0 and -1 < u \le U, the total damping of Definition 5.3.9 satisfies (equation (55)) D_u(T) \ge 2\epsilon D_\gamma(T) for all T.

Lean code for Lemma5.3.15●1 theorem
  • complete
    theorem CohnElkies.upperFirstBranchSaddleDamping_lower_bound {ε ℓ u : ℝ}
      (hε : 0 < ε) (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ) (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (T : ℝ) :
      2 * ε * CohnElkies.D_γ ℓ (1 + u) T ≤
        CohnElkies.saddleSourceContourDamping ε ℓ u T
    theorem CohnElkies.upperFirstBranchSaddleDamping_lower_bound
      {ε ℓ u : ℝ} (hε : 0 < ε)
      (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (T : ℝ) :
      2 * ε * CohnElkies.D_γ ℓ (1 + u) T ≤
        CohnElkies.saddleSourceContourDamping
          ε ℓ u T
    Report (49): on the first branch the saddle damping dominates `2ε D_γ`. 
Proof for Lemma 5.3.15

Integrating (54) of Lemma 5.2.7 against 1 - \cos(aT) \ge 0 shows that the negative shell removes at most a (1-2\epsilon)-fraction of the gamma damping, and the contribution of w_B is nonnegative, so D_u(T) \ge D_\gamma(T) - (1-2\epsilon)\int_{a_0}^A(1-\cos(aT))\mu_{\lambda,\eta}(a)\,da \ge 2\epsilon D_\gamma(T).

Lemma5.3.16
Group: Saddle geometry (21)
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Lemma 5.3.17
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✓L∃∀N

For every 0 < \epsilon \le 1/4, \lambda > 0 and -1 < u \le U, with \eta = 1 + u, the variances of Definition 5.3.11 and Definition 5.3.3 satisfy (equation (56)) V_s \le (1 - 2\epsilon)V_\gamma, hence V(u) \ge 2\epsilon V_\gamma \ge \dfrac{\epsilon}{\eta} > 0.

Lean code for Lemma5.3.16●3 theorems
  • complete
    theorem CohnElkies.upperFirstBranch_shortVariance_le_gamma {ε ℓ u : ℝ}
      (hε : 0 < ε) (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ) (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      CohnElkies.V_s ε (u - 1) ≤ (1 - 2 * ε) * CohnElkies.V_γ ℓ (1 + u)
    theorem CohnElkies.upperFirstBranch_shortVariance_le_gamma
      {ε ℓ u : ℝ} (hε : 0 < ε)
      (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      CohnElkies.V_s ε (u - 1) ≤
        (1 - 2 * ε) * CohnElkies.V_γ ℓ (1 + u)
    Report §4.3: on the first branch the short shell carries at most `(1 - 2ε)` of the gamma
    variance. 
  • complete
    theorem CohnElkies.upperFirstBranch_saddleSourceGaussianVariance_lower_bound
      {ε ℓ u : ℝ} (hε : 0 < ε) (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u) (huupper : u ≤ 1 + ε / 2)
      (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      2 * ε * CohnElkies.V_γ ℓ (1 + u) ≤ CohnElkies.V_u ε ℓ u
    theorem CohnElkies.upperFirstBranch_saddleSourceGaussianVariance_lower_bound
      {ε ℓ u : ℝ} (hε : 0 < ε)
      (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      2 * ε * CohnElkies.V_γ ℓ (1 + u) ≤
        CohnElkies.V_u ε ℓ u
  • complete
    theorem CohnElkies.eventually_saddleSourceGaussianVariance_firstBranch_pos :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (u : ℝ), -1 < u → u ≤ 1 + ε / 2 → 0 < CohnElkies.V_u ε ℓ u
    theorem CohnElkies.eventually_saddleSourceGaussianVariance_firstBranch_pos :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (u : ℝ),
              -1 < u →
                u ≤ 1 + ε / 2 →
                  0 < CohnElkies.V_u ε ℓ u
Proof for Lemma 5.3.16
Proof uses 2
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Integrating (54) of Lemma 5.2.7 against a^2/\lambda gives V_s \le (1 - 2\epsilon)V_\gamma, hence V(u) \ge 2\epsilon V_\gamma + V_B \ge \epsilon/\eta by (51) of Lemma 5.3.13.

Lemma5.3.17
Group: Saddle geometry (21)
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used by 1✓L∃∀N

There is \epsilon_0 > 0 such that, for every 0 < \epsilon < \epsilon_0, there are constants C_\epsilon, \lambda_\epsilon > 0 with: for every \lambda \ge \lambda_\epsilon and u_* \le u \le U (equation (57)), M_3 \le C_\epsilon V(u) (Definition 5.3.10, Definition 5.3.3); moreover \lambda\eta \ge (\log\lambda)/4 on this range (Definition 5.3.1).

Lean code for Lemma5.3.17●1 theorem
  • complete
    theorem CohnElkies.upperFirstBranch_saddleSourceThirdMoment_scaled_le
      {ε ℓ u : ℝ} (hε : 0 < ε) (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u) (huupper : u ≤ 1 + ε / 2)
      (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (hscale : 1 ≤ ℓ * (1 + u)) :
      (1 + u) ^ 2 * CohnElkies.M₃ ε ℓ (u - 1) ≤
        CohnElkies.saddleSourceFirstBranchThirdMomentCoefficient ε
    theorem CohnElkies.upperFirstBranch_saddleSourceThirdMoment_scaled_le
      {ε ℓ u : ℝ} (hε : 0 < ε)
      (hεsmall : ε ≤ 1 / 4) (hℓ : 0 < ℓ)
      (hulower : -1 < u)
      (huupper : u ≤ 1 + ε / 2)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a)
      (hscale : 1 ≤ ℓ * (1 + u)) :
      (1 + u) ^ 2 *
          CohnElkies.M₃ ε ℓ (u - 1) ≤
        CohnElkies.saddleSourceFirstBranchThirdMomentCoefficient
          ε
Proof for Lemma 5.3.17
Proof uses 2
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For u_* \le u \le U the positive-shell variance satisfies V_B \le (B+1)^2Qe^{(U-1)(B+1)} = O_\epsilon(1), and since \lambda\eta \ge (\log\lambda)/4 and \eta \le 2 + \epsilon/2, (51) gives V(u) \le V_\gamma + V_B = O_\epsilon(\eta^{-1}), while V(u) \ge \epsilon/\eta by Lemma 5.3.16. Similarly (54) bounds the negative-shell third moment by the gamma third moment \frac1\lambda\int a^3\mu_{\lambda,\eta}, the positive-shell third moment is O_\epsilon(1), and (52) of Lemma 5.3.13 gives M_3 = O_\epsilon(\eta^{-2}) = O_\epsilon(V(u)).

When u > U, the factor \cosh(ua) in (47) can make w_s overwhelm the gamma contribution. Put \delta = u - 1. For T \ne 0 the ratios D_s(T)/(\lambda\min(T^2,1)) and D_B(T)/(\lambda\min(T^2,1)) have respective sizes at most C_0e^{\delta A} and at least Qe^{\delta B}, so the separation in Lemma 4.2 makes w_B dominate w_s throughout u \ge U. The interval support of w_B prevents frequency resonances: a shell concentrated at one a would have D_B(T) = 0 whenever aT \in 2\pi\mathbb{Z}, whereas (equation (58)) \int_B^{B+1}(1 - \cos(aT))\,da = 1 - \operatorname{sinc}(T/2)\cos\bigl((B+\tfrac12)T\bigr), \operatorname{sinc}(x) = \sin(x)/x, and 1 - |\operatorname{sinc}(T/2)| \asymp \min(T^2,1), so (58) is positive for every T \ne 0, uniformly at small and large frequencies. Define the separation error \rho_\epsilon = (A + a_0^{-1})Q^{-1}\exp\bigl(-\tfrac{\epsilon}{2}(B-A)\bigr) = C_0Q^{-1}e^{-(U-1)(B-A)}; Lemma 5.2.10 gives \rho_\epsilon = O(e^{-c/\epsilon^2}) = o(1) as \epsilon \downarrow 0.

Lemma5.3.18
Group: Saddle geometry (21)
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Lemma 5.3.19
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✓L∃∀N

For \lambda \ge 0, u = 1 + \delta \ge 1 and all T, the shell dampings of Definition 5.3.11 satisfy (equations (59)–(60)) D_s(T) \le \lambda C_0e^{\delta A}\min(T^2, 1) and D_B(T) \ge \dfrac{\lambda}{50}Qe^{\delta B}\min(T^2, 1), with C_0 = A + a_0^{-1} (Definition 5.2.1).

Lean code for Lemma5.3.18●2 theorems
  • complete
    theorem CohnElkies.upperShortShellDamping_global_bound {ε ℓ δ T : ℝ}
      (hε : 0 < ε) (hℓ : 0 ≤ ℓ) (hδ : 0 ≤ δ)
      (horder : CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀ a ∈ Set.Icc (CohnElkies.a₀ε ε) (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      CohnElkies.D_s ε ℓ δ T ≤
        ℓ * CohnElkies.upperShellShortCoefficient ε *
            Real.exp (δ * CohnElkies.Aε ε) *
          min (T ^ 2) 1
    theorem CohnElkies.upperShortShellDamping_global_bound
      {ε ℓ δ T : ℝ} (hε : 0 < ε) (hℓ : 0 ≤ ℓ)
      (hδ : 0 ≤ δ)
      (horder :
        CohnElkies.a₀ε ε ≤ CohnElkies.Aε ε)
      (hmargin :
        ∀
          a ∈
            Set.Icc (CohnElkies.a₀ε ε)
              (CohnElkies.Aε ε),
          0 ≤ CohnElkies.bε ε a) :
      CohnElkies.D_s ε ℓ δ T ≤
        ℓ *
              CohnElkies.upperShellShortCoefficient
                ε *
            Real.exp (δ * CohnElkies.Aε ε) *
          min (T ^ 2) 1
    Report (59): the short shell contributes at most `λ (A + a₀⁻¹) e^{δA} min(T², 1)`. 
  • complete
    theorem CohnElkies.positiveShellDamping_lower_bound {ε ℓ δ T : ℝ} (hε : 0 < ε)
      (hℓ : 0 ≤ ℓ) (hδ : 0 ≤ δ) :
      ℓ / 50 * CohnElkies.Qε ε * Real.exp (δ * CohnElkies.Bε ε) *
          min (T ^ 2) 1 ≤
        CohnElkies.D_B ε ℓ δ T
    theorem CohnElkies.positiveShellDamping_lower_bound
      {ε ℓ δ T : ℝ} (hε : 0 < ε) (hℓ : 0 ≤ ℓ)
      (hδ : 0 ≤ δ) :
      ℓ / 50 * CohnElkies.Qε ε *
            Real.exp (δ * CohnElkies.Bε ε) *
          min (T ^ 2) 1 ≤
        CohnElkies.D_B ε ℓ δ T
    Report (60): `D_B(T) ≥ c λ Q e^{δB} min(T², 1)`. 
Proof for Lemma 5.3.18
uses 0

For u = 1 + \delta the explicit densities satisfy |w_s(a)|\cosh(ua) \ll e^{\delta a}/a^2 and w_B(a)\cosh(ua) \asymp Qe^{\delta a} on their supports. If |T| \le 1, 1 - \cos(aT) = O(a^2T^2) gives D_s(T) \ll \lambda T^2\int_{a_0}^Ae^{\delta a}\,da \ll \lambda Ae^{\delta A}T^2; if |T| \ge 1, 1 - \cos(aT) = O(1) gives D_s(T) \ll \lambda e^{\delta A}\int_{a_0}^Aa^{-2}\,da \ll \lambda a_0^{-1}e^{\delta A}. These give (59). On the positive shell, (58) yields D_B(T) \gg \lambda Qe^{\delta B}\int_B^{B+1}(1-\cos(aT))\,da \gg \lambda Qe^{\delta B}\min(T^2,1), which is (60).

Lemma5.3.19
Group: Saddle geometry (21)
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used by 1✓L∃∀N

There is \epsilon_0 > 0 such that, for every 0 < \epsilon < \epsilon_0, every \lambda \ge 0, every u \ge U and every T \in \mathbb{R} (equations (61)–(62)), D_s(T) \le \dfrac{1}{100}D_B(T), hence D_u(T) \ge D_\gamma(T) + \dfrac{99}{100}D_B(T) (Definition 5.3.11, Definition 5.3.9).

Lean code for Lemma5.3.19●2 theorems
  • complete
    theorem CohnElkies.eventually_upper_shortShell_domination :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 ≤ ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.D_s ε ℓ δ T ≤ 1 / 100 * CohnElkies.D_B ε ℓ δ T
    theorem CohnElkies.eventually_upper_shortShell_domination :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 ≤ ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.D_s ε ℓ δ T ≤
                    1 / 100 *
                      CohnElkies.D_B ε ℓ δ T
    Report (61): the short-shell damping is at most `1/100` of the positive-shell damping. 
  • complete
    theorem CohnElkies.eventually_upperSaddleDamping_gamma_add_shell :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.D_γ ℓ (2 + δ) T +
                      99 / 100 * CohnElkies.D_B ε ℓ δ T ≤
                    CohnElkies.D_u ε ℓ δ T
    theorem CohnElkies.eventually_upperSaddleDamping_gamma_add_shell :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.D_γ ℓ (2 + δ) T +
                      99 / 100 *
                        CohnElkies.D_B ε ℓ δ
                          T ≤
                    CohnElkies.D_u ε ℓ δ T
Proof for Lemma 5.3.19
Proof uses 2
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For T \ne 0, division of (59) by (60) (Lemma 5.3.18) gives D_s(T)/D_B(T) \ll C_0Q^{-1}e^{-\delta(B-A)} \le \rho_\epsilon, and Lemma 5.2.10 makes the right side less than 1/100 for small \epsilon; at T = 0 both damping terms vanish. Then D_u = D_\gamma - D_s + D_B proves (62).

Lemma5.3.20
Group: Saddle geometry (21)
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Lemma 5.3.21
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✓L∃∀N

For u = 1 + \delta \ge 1 the positive-shell variance of Definition 5.3.11 satisfies (equation (64)) \tfrac12B^2Qe^{\delta B} \le V_B \le (B+1)^2Qe^{\delta(B+1)}.

Lean code for Lemma5.3.20●1 theorem
  • complete
    theorem CohnElkies.upperPositiveShellVariance_bounds {ε δ : ℝ} (hε : 0 < ε)
      (hδ : 0 ≤ δ) :
      1 / 2 * CohnElkies.Bε ε ^ 2 * CohnElkies.Qε ε *
            Real.exp (δ * CohnElkies.Bε ε) ≤
          CohnElkies.V_B ε δ ∧
        CohnElkies.V_B ε δ ≤
          (CohnElkies.Bε ε + 1) ^ 2 * CohnElkies.Qε ε *
            Real.exp (δ * (CohnElkies.Bε ε + 1))
    theorem CohnElkies.upperPositiveShellVariance_bounds
      {ε δ : ℝ} (hε : 0 < ε) (hδ : 0 ≤ δ) :
      1 / 2 * CohnElkies.Bε ε ^ 2 *
              CohnElkies.Qε ε *
            Real.exp (δ * CohnElkies.Bε ε) ≤
          CohnElkies.V_B ε δ ∧
        CohnElkies.V_B ε δ ≤
          (CohnElkies.Bε ε + 1) ^ 2 *
              CohnElkies.Qε ε *
            Real.exp
              (δ * (CohnElkies.Bε ε + 1))
    Report (45): two-sided bounds for the positive-shell variance `V_B`. 
Proof for Lemma 5.3.20
uses 0

Integrate w_B(a)\cosh(ua) \asymp Qe^{\delta a} against a^2 over [B, B+1].

Lemma5.3.21
Group: Saddle geometry (21)
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Lemma 5.3.22
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✓L∃∀N

There is \epsilon_0 > 0 such that, for every 0 < \epsilon < \epsilon_0, there is C_\epsilon > 0 with: for every \lambda \ge 1 and u \ge U (equations (63), (65)–(66)), V_s \le \dfrac{1}{100}V_B, hence V_\gamma + \dfrac{99}{100}V_B \le V(u) \le V_\gamma + V_B and V(u) > 0, and M_3 \le C_\epsilon V(u) (Definition 5.3.3, Definition 5.3.10, Definition 5.3.11).

Lean code for Lemma5.3.21●4 theorems
  • complete
    theorem CohnElkies.eventually_upper_shortShellVariance_domination :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (δ : ℝ),
          ε / 2 ≤ δ → CohnElkies.V_s ε δ ≤ 1 / 100 * CohnElkies.V_B ε δ
    theorem CohnElkies.eventually_upper_shortShellVariance_domination :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (δ : ℝ),
          ε / 2 ≤ δ →
            CohnElkies.V_s ε δ ≤
              1 / 100 * CohnElkies.V_B ε δ
    The short-shell variance is at most `1/100` of the positive-shell variance. 
  • complete
    theorem CohnElkies.eventually_upperSaddleVariance_bounds :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                1 / (2 * (2 + δ)) + 99 / 100 * CohnElkies.V_B ε δ ≤
                    CohnElkies.upperSaddleVariance ε ℓ δ ∧
                  CohnElkies.upperSaddleVariance ε ℓ δ ≤
                    1 / (2 * (2 + δ)) + 1 / (ℓ * (2 + δ) ^ 2) +
                      CohnElkies.V_B ε δ
    theorem CohnElkies.eventually_upperSaddleVariance_bounds :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                1 / (2 * (2 + δ)) +
                      99 / 100 *
                        CohnElkies.V_B ε δ ≤
                    CohnElkies.upperSaddleVariance
                      ε ℓ δ ∧
                  CohnElkies.upperSaddleVariance
                      ε ℓ δ ≤
                    1 / (2 * (2 + δ)) +
                        1 /
                          (ℓ * (2 + δ) ^ 2) +
                      CohnElkies.V_B ε δ
  • complete
    theorem CohnElkies.eventually_upperSaddleVariance_pos :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ), ε / 2 ≤ δ → 0 < CohnElkies.upperSaddleVariance ε ℓ δ
    theorem CohnElkies.eventually_upperSaddleVariance_pos :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                0 <
                  CohnElkies.upperSaddleVariance
                    ε ℓ δ
  • complete
    theorem CohnElkies.eventually_upperSaddleThirdMoment_le_variance :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          1 ≤ ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                CohnElkies.M₃ ε ℓ δ ≤
                  (2 +
                      100 / 99 *
                        CohnElkies.upperSaddleShellThirdCoefficient ε) *
                    CohnElkies.upperSaddleVariance ε ℓ δ
    theorem CohnElkies.eventually_upperSaddleThirdMoment_le_variance :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          1 ≤ ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                CohnElkies.M₃ ε ℓ δ ≤
                  (2 +
                      100 / 99 *
                        CohnElkies.upperSaddleShellThirdCoefficient
                          ε) *
                    CohnElkies.upperSaddleVariance
                      ε ℓ δ
    Report (48): the saddle third moment is dominated by the saddle variance. 
Proof for Lemma 5.3.21
Proof uses 3
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Lemma 5.2.10
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Comparing the quadratic coefficients of (59) and (60) gives V_s = O(\rho_\epsilon V_B), with \rho_\epsilon < 1/100 for small \epsilon by Lemma 5.2.10; then V(u) = V_\gamma - V_s + V_B gives (63). Since \delta \ge \epsilon/2, V_B \gg B^2Qe^{\epsilon B/2} = B^2e^{\epsilon B/8} \gg 1 by Lemma 5.3.20, while V_\gamma \ll \eta^{-1} \ll 1 by (51); thus V_\gamma = O(V_B). Since a \le A on the negative shell, \int_{a_0}^A|w_s|a^3\cosh(ua) \le AV_s \ll A\rho_\epsilon V_B, while a \le B+1 bounds the positive-shell third moment by (B+1)V_B; this proves (65). Finally, since \eta \ge 2 + \epsilon/2, (51)–(52) of Lemma 5.3.13 bound the gamma third moment by O(V_\gamma); the shell third moments are O_\epsilon(V_B), and V_\gamma = O(V_B), V_B \asymp V(u) give M_3 = O_\epsilon(V(u)), which is (66).

Set T_0 = (2(B+1))^{-1}. To bound the tails of the saddle integral for u \ge U, we sharpen the damping on three frequency ranges: |T| \le T_0, where D_u is quadratic; T_0 \le |T| \le \eta, where w_B supplies a uniform positive floor; and |T| \ge \eta, where the gamma contribution also grows linearly.

Lemma5.3.22
Group: Saddle geometry (21)
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Definition 5.3.1
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uses 1used by 1✓L∃∀N

There is \epsilon_0 > 0 such that, for every 0 < \epsilon < \epsilon_0, every \lambda > 0 and every u \ge U, with \delta = u - 1 and T_0 = (2(B+1))^{-1} (equations (67)–(69)), the damping D_u of Definition 5.3.9 admits the pointwise splitting (1+|T|^3)e^{-D_u(T)} \le (1+|T|^3)e^{-\frac{\lambda V(u)}{100e}T^2} + e^{-\Xi}\Bigl((1+|T|^3)e^{-\frac{\lambda}{8e(2+\delta)}T^2} + (1+|T|^3)e^{-\frac{\lambda}{8e}|T|}\Bigr) for all T \in \mathbb{R}, with the barrier \Xi = \dfrac{99}{5000}\lambda Qe^{\delta B}T_0^2: on |T| \le T_0 the damping is Gaussian with rate proportional to \lambda V(u), and for |T| \ge T_0 it exceeds the shell barrier \Xi plus the gamma damping D_\gamma (quadratic up to |T| \approx \eta, linear beyond).

Lean code for Lemma5.3.22●1 theorem
  • complete
    theorem CohnElkies.eventually_secondBranch_damping_pointwise :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.saddleGaussianTailWeight T *
                      Real.exp
                        (-CohnElkies.saddleSourceContourDamping ε ℓ (1 + δ)
                            T) ≤
                    CohnElkies.saddleGaussianTailWeight T *
                        Real.exp
                          (-CohnElkies.secondBranchRate ε ℓ δ * T ^ 2) +
                      Real.exp (-CohnElkies.secondBranchBarrier ε ℓ δ) *
                        (CohnElkies.saddleGaussianTailWeight T *
                            Real.exp
                              (-CohnElkies.secondBranchGammaRate ℓ δ *
                                T ^ 2) +
                          CohnElkies.saddleGaussianTailWeight T *
                            Real.exp
                              (-CohnElkies.secondBranchLinearRate ℓ * |T|))
    theorem CohnElkies.eventually_secondBranch_damping_pointwise :
      ∀ᶠ (ε : ℝ) in nhdsWithin 0 (Set.Ioi 0),
        ∀ (ℓ : ℝ),
          0 < ℓ →
            ∀ (δ : ℝ),
              ε / 2 ≤ δ →
                ∀ (T : ℝ),
                  CohnElkies.saddleGaussianTailWeight
                        T *
                      Real.exp
                        (-CohnElkies.saddleSourceContourDamping
                            ε ℓ (1 + δ) T) ≤
                    CohnElkies.saddleGaussianTailWeight
                          T *
                        Real.exp
                          (-CohnElkies.secondBranchRate
                                ε ℓ δ *
                            T ^ 2) +
                      Real.exp
                          (-CohnElkies.secondBranchBarrier
                              ε ℓ δ) *
                        (CohnElkies.saddleGaussianTailWeight
                              T *
                            Real.exp
                              (-CohnElkies.secondBranchGammaRate
                                    ℓ δ *
                                T ^ 2) +
                          CohnElkies.saddleGaussianTailWeight
                              T *
                            Real.exp
                              (-CohnElkies.secondBranchLinearRate
                                    ℓ *
                                |T|))
    Splitting `e^{-D_u}` into the local Gaussian and the barrier-suppressed outer part. 
Proof for Lemma 5.3.22
Proof uses 5
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Lemma 5.3.13
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If |T| \le T_0, then |aT| \le 1/2 on [B,B+1], so 1 - \cos(aT) \asymp a^2T^2 and D_B(T) \asymp \lambda V_BT^2. Since \eta \ge 2 + \epsilon/2 and |T| \le \eta, (53) and (51) of Lemma 5.3.14 and Lemma 5.3.13 give D_\gamma(T) \gg \lambda T^2/\eta \gg \lambda V_\gamma T^2. Combining these through (62) of Lemma 5.3.19 and (63) of Lemma 5.3.21 proves (67). If T_0 \le |T| \le \eta, then \min(T^2,1) \ge T_0^2, so (62) and (60) (Lemma 5.3.18) give D_u(T) \gg \lambda T_0^2Qe^{\delta B} \gg_\epsilon \lambda Qe^{\delta B}, which is (68). If |T| \ge \eta, then \min(T^2,1) = 1 and (53) gives D_\gamma(T) \gg \lambda|T|; adding the positive shell through (62) and (60) yields (69).