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The strong variational row has damping and amplitude-dependent forcing

Proved
BianchiIX.coreRegion_strong_forcing

by trppppp · Nov 5, 2026 · Mathlib 0df444a (Lean v4.33.1)

bianchi-ix-era-statisticsdynamical-systems

For real variables p,s,a,b,cp,s,a,b,cp,s,a,b,c, set

K=a2+b2+c2−2(ab+bc+ca),S=p2+s2,C=S+K.K=a^2+b^2+c^2-2(ab+bc+ca),\qquad S=p^2+s^2,\qquad C=S+K.K=a2+b2+c2−2(ab+bc+ca),S=p2+s2,C=S+K.

The shear components and wall rates are

P=Kp−2a2+b2+c2+ab−2bc+ac,P=Kp-2a^2+b^2+c^2+ab-2bc+ac,P=Kp−2a2+b2+c2+ab−2bc+ac, Q=Ks+3(−b2+c2+ab−ac),Q=Ks+\sqrt{3}(-b^2+c^2+ab-ac),Q=Ks+3​(−b2+c2+ab−ac), r1=−S+2p,r2=−S−p+3s,r3=−S−p−3s.r_1=-S+2p,\qquad r_2=-S-p+\sqrt{3}s,\qquad r_3=-S-p-\sqrt{3}s.r1​=−S+2p,r2​=−S−p+3​s,r3​=−S−p−3​s.

These functions define the normalized vacuum Bianchi IX vector field (P,Q,r1a,r2b,r3c)(P,Q,r_1a,r_2b,r_3c)(P,Q,r1​a,r2​b,r3​c). For y=(m,u,v,w)∈R4y=(m,u,v,w)\in\mathbb R^4y=(m,u,v,w)∈R4, define

K(u,v,w)=u2+v2+w2−2(uv+vw+wu),κ=u(v+w−u),K(u,v,w)=u^2+v^2+w^2-2(uv+vw+wu),\qquad \kappa=u(v+w-u),K(u,v,w)=u2+v2+w2−2(uv+vw+wu),κ=u(v+w−u), Fm=−v2+w2+u(v−w)−mκ,Fu=12(1−m2−(v−w)2+u2)u,F_m=-v^2+w^2+u(v-w)-m\kappa,\qquad F_u=\tfrac12(1-m^2-(v-w)^2+u^2)u,Fm​=−v2+w2+u(v−w)−mκ,Fu​=21​(1−m2−(v−w)2+u2)u, Fv=(m−1−κ)v,Fw=(−m−1−κ)w,F=(Fm,Fu,Fv,Fw),F_v=(m-1-\kappa)v,\qquad F_w=(-m-1-\kappa)w,\qquad F=(F_m,F_u,F_v,F_w),Fv​=(m−1−κ)v,Fw​=(−m−1−κ)w,F=(Fm​,Fu​,Fv​,Fw​),

and E(m,v)=(m−1)2+v2E(m,v)=(m-1)^2+v^2E(m,v)=(m−1)2+v2.

For x=(p,s,a,b,c)x=(p,s,a,b,c)x=(p,s,a,b,c), put

ψ(p,z)=3 z1+p,Π(x)=(ψ(p,s),ψ(p,a),ψ(p,b),ψ(p,c)).\psi(p,z)=\frac{\sqrt3\,z}{1+p},\qquad \Pi(x)=(\psi(p,s),\psi(p,a),\psi(p,b),\psi(p,c)).ψ(p,z)=1+p3​z​,Π(x)=(ψ(p,s),ψ(p,a),ψ(p,b),ψ(p,c)).

For y=(m,u,v,w)y=(m,u,v,w)y=(m,u,v,w), set D(y)=3+m2+K(u,v,w)D(y)=3+m^2+K(u,v,w)D(y)=3+m2+K(u,v,w) and

ΞA(y)=(A−1,Am3,Au3,Av3,Aw3),Ξ(y)=Ξ6/D(y)(y).\Xi_A(y)=\left(A-1,\frac{Am}{\sqrt3},\frac{Au}{\sqrt3}, \frac{Av}{\sqrt3},\frac{Aw}{\sqrt3}\right),\qquad \Xi(y)=\Xi_{6/D(y)}(y).ΞA​(y)=(A−1,3​Am​,3​Au​,3​Av​,3​Aw​),Ξ(y)=Ξ6/D(y)​(y).

Write N(x)=(P,Q,r1a,r2b,r3c)N(x)=(P,Q,r_1a,r_2b,r_3c)N(x)=(P,Q,r1​a,r2​b,r3​c) for the normalized vector field and C(x)=C(p,s,a,b,c)\mathcal C(x)=C(p,s,a,b,c)C(x)=C(p,s,a,b,c) for its constraint.

The normalized and projective state spaces are R5\mathbb R^5R5 and R4\mathbb R^4R4 with their finite-product norms. The maps Π,Ξ,D,F\Pi,\Xi,D,FΠ,Ξ,D,F act on these state spaces.

Define the core radius, angle, and clock factor by

r(m,v)=(m−1)2+v2,θ(m,v)=arsinh⁡1−mv,d(r,u,w)=1−(u−w)2r2.r(m,v)=\sqrt{(m-1)^2+v^2},\qquad \theta(m,v)=\operatorname{arsinh}\frac{1-m}{v},\qquad d(r,u,w)=1-\frac{(u-w)^2}{r^2}.r(m,v)=(m−1)2+v2​,θ(m,v)=arsinhv1−m​,d(r,u,w)=1−r2(u−w)2​.

For y=(m,u,v,w)y=(m,u,v,w)y=(m,u,v,w), write ry=r(m,v)r_y=r(m,v)ry​=r(m,v), θy=θ(m,v)\theta_y=\theta(m,v)θy​=θ(m,v), and dy=d(ry,u,w)d_y=d(r_y,u,w)dy​=d(ry​,u,w). All quotients use the total convention x/0=0x/0=0x/0=0.

The core state space is R3\mathbb R^3R3 with coordinates Y=(r,u,p)Y=(r,u,p)Y=(r,u,p). Define

η(m,u,v,w)=(r(m,v),u,vw),ιz(r,u,p)=(1−rtanh⁡z,u,rcosh⁡z,pr/cosh⁡z).\eta(m,u,v,w)=(r(m,v),u,vw),\qquad \iota_z(r,u,p)=\left(1-r\tanh z,u,\frac r{\cosh z}, \frac p{r/\cosh z}\right).η(m,u,v,w)=(r(m,v),u,vw),ιz​(r,u,p)=(1−rtanhz,u,coshzr​,r/coshzp​).

For fixed (z,Y)(z,Y)(z,Y) put v=r/cosh⁡zv=r/\cosh zv=r/coshz, w=p/vw=p/vw=p/v, d=d(r,u,w)d=d(r,u,w)d=d(r,u,w), and define

V(z,Y)=(−κ(u,v,w)−tanh⁡z (u−w)2/rd,u[−r/2+tanh⁡z+w/cosh⁡z+(u2−w2)/(2r)]d,−2p(1+κ(u,v,w))rd).\mathcal V(z,Y)=\left( \frac{-\kappa(u,v,w)-\tanh z\,(u-w)^2/r}{d},\quad \frac{u[-r/2+\tanh z+w/\cosh z+(u^2-w^2)/(2r)]}{d},\quad \frac{-2p(1+\kappa(u,v,w))}{rd}\right).V(z,Y)=(d−κ(u,v,w)−tanhz(u−w)2/r​,du[−r/2+tanhz+w/coshz+(u2−w2)/(2r)]​,rd−2p(1+κ(u,v,w))​).

For real kkk, put εk=1/(10000k)\varepsilon_k=1/(10000k)εk​=1/(10000k) and define

Kk={(m,u,v,w):∣E(m,v)−k2∣≤1/8,v≥1,0≤u≤εk,0≤vw≤εk}.\mathcal K_k=\{(m,u,v,w): |E(m,v)-k^2|\leq1/8,\quad v\geq1, \quad0\leq u\leq\varepsilon_k,\quad0\leq vw\leq\varepsilon_k\}.Kk​={(m,u,v,w):∣E(m,v)−k2∣≤1/8,v≥1,0≤u≤εk​,0≤vw≤εk​}.

For real variables p,s,a,b,cp,s,a,b,cp,s,a,b,c, set

K=a2+b2+c2−2(ab+bc+ca),S=p2+s2,C=S+K.K=a^2+b^2+c^2-2(ab+bc+ca),\qquad S=p^2+s^2,\qquad C=S+K.K=a2+b2+c2−2(ab+bc+ca),S=p2+s2,C=S+K.

The shear components and wall rates are

P=Kp−2a2+b2+c2+ab−2bc+ac,P=Kp-2a^2+b^2+c^2+ab-2bc+ac,P=Kp−2a2+b2+c2+ab−2bc+ac, Q=Ks+3(−b2+c2+ab−ac),Q=Ks+\sqrt{3}(-b^2+c^2+ab-ac),Q=Ks+3​(−b2+c2+ab−ac), r1=−S+2p,r2=−S−p+3s,r3=−S−p−3s.r_1=-S+2p,\qquad r_2=-S-p+\sqrt{3}s,\qquad r_3=-S-p-\sqrt{3}s.r1​=−S+2p,r2​=−S−p+3​s,r3​=−S−p−3​s.

These functions define the normalized vacuum Bianchi IX vector field (P,Q,r1a,r2b,r3c)(P,Q,r_1a,r_2b,r_3c)(P,Q,r1​a,r2​b,r3​c). For y=(m,u,v,w)∈R4y=(m,u,v,w)\in\mathbb R^4y=(m,u,v,w)∈R4, define

K(u,v,w)=u2+v2+w2−2(uv+vw+wu),κ=u(v+w−u),K(u,v,w)=u^2+v^2+w^2-2(uv+vw+wu),\qquad \kappa=u(v+w-u),K(u,v,w)=u2+v2+w2−2(uv+vw+wu),κ=u(v+w−u), Fm=−v2+w2+u(v−w)−mκ,Fu=12(1−m2−(v−w)2+u2)u,F_m=-v^2+w^2+u(v-w)-m\kappa,\qquad F_u=\tfrac12(1-m^2-(v-w)^2+u^2)u,Fm​=−v2+w2+u(v−w)−mκ,Fu​=21​(1−m2−(v−w)2+u2)u, Fv=(m−1−κ)v,Fw=(−m−1−κ)w,F=(Fm,Fu,Fv,Fw),F_v=(m-1-\kappa)v,\qquad F_w=(-m-1-\kappa)w,\qquad F=(F_m,F_u,F_v,F_w),Fv​=(m−1−κ)v,Fw​=(−m−1−κ)w,F=(Fm​,Fu​,Fv​,Fw​),

and E(m,v)=(m−1)2+v2E(m,v)=(m-1)^2+v^2E(m,v)=(m−1)2+v2.

For x=(p,s,a,b,c)x=(p,s,a,b,c)x=(p,s,a,b,c), put

ψ(p,z)=3 z1+p,Π(x)=(ψ(p,s),ψ(p,a),ψ(p,b),ψ(p,c)).\psi(p,z)=\frac{\sqrt3\,z}{1+p},\qquad \Pi(x)=(\psi(p,s),\psi(p,a),\psi(p,b),\psi(p,c)).ψ(p,z)=1+p3​z​,Π(x)=(ψ(p,s),ψ(p,a),ψ(p,b),ψ(p,c)).

For y=(m,u,v,w)y=(m,u,v,w)y=(m,u,v,w), set D(y)=3+m2+K(u,v,w)D(y)=3+m^2+K(u,v,w)D(y)=3+m2+K(u,v,w) and

ΞA(y)=(A−1,Am3,Au3,Av3,Aw3),Ξ(y)=Ξ6/D(y)(y).\Xi_A(y)=\left(A-1,\frac{Am}{\sqrt3},\frac{Au}{\sqrt3}, \frac{Av}{\sqrt3},\frac{Aw}{\sqrt3}\right),\qquad \Xi(y)=\Xi_{6/D(y)}(y).ΞA​(y)=(A−1,3​Am​,3​Au​,3​Av​,3​Aw​),Ξ(y)=Ξ6/D(y)​(y).

Write N(x)=(P,Q,r1a,r2b,r3c)N(x)=(P,Q,r_1a,r_2b,r_3c)N(x)=(P,Q,r1​a,r2​b,r3​c) for the normalized vector field and C(x)=C(p,s,a,b,c)\mathcal C(x)=C(p,s,a,b,c)C(x)=C(p,s,a,b,c) for its constraint.

The normalized and projective state spaces are R5\mathbb R^5R5 and R4\mathbb R^4R4 with their finite-product norms. The maps Π,Ξ,D,F\Pi,\Xi,D,FΠ,Ξ,D,F act on these state spaces.

Define the core radius, angle, and clock factor by

r(m,v)=(m−1)2+v2,θ(m,v)=arsinh⁡1−mv,d(r,u,w)=1−(u−w)2r2.r(m,v)=\sqrt{(m-1)^2+v^2},\qquad \theta(m,v)=\operatorname{arsinh}\frac{1-m}{v},\qquad d(r,u,w)=1-\frac{(u-w)^2}{r^2}.r(m,v)=(m−1)2+v2​,θ(m,v)=arsinhv1−m​,d(r,u,w)=1−r2(u−w)2​.

For y=(m,u,v,w)y=(m,u,v,w)y=(m,u,v,w), write ry=r(m,v)r_y=r(m,v)ry​=r(m,v), θy=θ(m,v)\theta_y=\theta(m,v)θy​=θ(m,v), and dy=d(ry,u,w)d_y=d(r_y,u,w)dy​=d(ry​,u,w). All quotients use the total convention x/0=0x/0=0x/0=0.

The core state space is R3\mathbb R^3R3 with coordinates Y=(r,u,p)Y=(r,u,p)Y=(r,u,p). Define

η(m,u,v,w)=(r(m,v),u,vw),ιz(r,u,p)=(1−rtanh⁡z,u,rcosh⁡z,pr/cosh⁡z).\eta(m,u,v,w)=(r(m,v),u,vw),\qquad \iota_z(r,u,p)=\left(1-r\tanh z,u,\frac r{\cosh z}, \frac p{r/\cosh z}\right).η(m,u,v,w)=(r(m,v),u,vw),ιz​(r,u,p)=(1−rtanhz,u,coshzr​,r/coshzp​).

For fixed (z,Y)(z,Y)(z,Y) put v=r/cosh⁡zv=r/\cosh zv=r/coshz, w=p/vw=p/vw=p/v, d=d(r,u,w)d=d(r,u,w)d=d(r,u,w), and define

V(z,Y)=(−κ(u,v,w)−tanh⁡z (u−w)2/rd,u[−r/2+tanh⁡z+w/cosh⁡z+(u2−w2)/(2r)]d,−2p(1+κ(u,v,w))rd).\mathcal V(z,Y)=\left( \frac{-\kappa(u,v,w)-\tanh z\,(u-w)^2/r}{d},\quad \frac{u[-r/2+\tanh z+w/\cosh z+(u^2-w^2)/(2r)]}{d},\quad \frac{-2p(1+\kappa(u,v,w))}{rd}\right).V(z,Y)=(d−κ(u,v,w)−tanhz(u−w)2/r​,du[−r/2+tanhz+w/coshz+(u2−w2)/(2r)]​,rd−2p(1+κ(u,v,w))​).

At (z,Y)(z,Y)(z,Y) use the abbreviations

s=1/cosh⁡z,c=−tanh⁡z,δ=u−w,s=1/\cosh z,\quad c=-\tanh z,\quad \delta=u-w,s=1/coshz,c=−tanhz,δ=u−w, C=u(v+w−u),a=−r/2+tanh⁡z+w/cosh⁡z+(u2−w2)/(2r),g=−C+cδ2/r.C=u(v+w-u),\quad a=-r/2+\tanh z+w/\cosh z+(u^2-w^2)/(2r), \quad g=-C+c\delta^2/r.C=u(v+w−u),a=−r/2+tanhz+w/coshz+(u2−w2)/(2r),g=−C+cδ2/r.

Let Q(z,Y)=(C,d,a,g)\mathcal Q(z,Y)=(C,d,a,g)Q(z,Y)=(C,d,a,g). Define the 4×34\times34×3 matrix H(z,Y)H(z,Y)H(z,Y) by its rows, in the order (C,d,a,g)(C,d,a,g)(C,d,a,g) and columns (r,u,p)(r,u,p)(r,u,p):

HC=(u(s−w/r), v−2u+w, u/v),H_C=(u(s-w/r),\ v-2u+w,\ u/v),HC​=(u(s−w/r), v−2u+w, u/v), Hd=(2δ(u−2w)/r3, −2δ/r2, 2δ/(vr2)),H_d=(2\delta(u-2w)/r^3,\ -2\delta/r^2,\ 2\delta/(vr^2)),Hd​=(2δ(u−2w)/r3, −2δ/r2, 2δ/(vr2)), Ha=(−1/2−sw/r+(3w2−u2)/(2r2), u/r, (1−w/v)/r),H_a=(-1/2-sw/r+(3w^2-u^2)/(2r^2),\ u/r,\ (1-w/v)/r),Ha​=(−1/2−sw/r+(3w2−u2)/(2r2), u/r, (1−w/v)/r), Hg=(−u(s−w/r)+cδ(3w−u)/r2, −(v−2u+w)+2cδ/r, −u/v−2cδ/(rv)).H_g=(-u(s-w/r)+c\delta(3w-u)/r^2,\ -(v-2u+w)+2c\delta/r,\ -u/v-2c\delta/(rv)).Hg​=(−u(s−w/r)+cδ(3w−u)/r2, −(v−2u+w)+2cδ/r, −u/v−2cδ/(rv)).

For j=0,1,2j=0,1,2j=0,1,2, define the 3×33\times33×3 matrix A(z,Y)A(z,Y)A(z,Y) by

A0j=Hgj/d−gHdj/d2,A_{0j}=H_{gj}/d-gH_{dj}/d^2,A0j​=Hgj​/d−gHdj​/d2, A1j=δj1a/d+uHaj/d−uaHdj/d2,A_{1j}=\delta_{j1}a/d+uH_{aj}/d-uaH_{dj}/d^2,A1j​=δj1​a/d+uHaj​/d−uaHdj​/d2, A2j=δj02p(1+C)r2d−δj22(1+C)rd−2pHCjrd+2p(1+C)Hdjrd2,A_{2j}=\delta_{j0}\frac{2p(1+C)}{r^2d} -\delta_{j2}\frac{2(1+C)}{rd}-\frac{2pH_{Cj}}{rd} +\frac{2p(1+C)H_{dj}}{rd^2},A2j​=δj0​r2d2p(1+C)​−δj2​rd2(1+C)​−rd2pHCj​​+rd22p(1+C)Hdj​​,

where δij\delta_{ij}δij​ is the Kronecker symbol.

For real kkk, define Sk(ξ0,ξ1,ξ2)=(ξ0,kξ1,ξ2)S_k(\xi_0,\xi_1,\xi_2)=(\xi_0,k\xi_1,\xi_2)Sk​(ξ0​,ξ1​,ξ2​)=(ξ0​,kξ1​,ξ2​) and

Bk(z,Y)=(A00A01/kA02kA10A11kA12A20A21/kA22).B_k(z,Y)=\begin{pmatrix} A_{00}&A_{01}/k&A_{02}\\ kA_{10}&A_{11}&kA_{12}\\ A_{20}&A_{21}/k&A_{22} \end{pmatrix}.Bk​(z,Y)=​A00​kA10​A20​​A01​/kA11​A21​/k​A02​kA12​A22​​​.

Let k≥6k\geq6k≥6, y∈Kky\in\mathcal K_ky∈Kk​, and ξ∈R3\xi\in\mathbb R^3ξ∈R3 satisfy ∥ξ∥∞≤Q\|\xi\|_\infty\leq Q∥ξ∥∞​≤Q. For B=Bk(θy,η(y))B=B_k(\theta_y,\eta(y))B=Bk​(θy​,η(y)),

B11≤−k/4,∣B10ξ0+B12ξ2∣≤3kyuQ.B_{11}\leq-k/4,\qquad |B_{10}\xi_0+B_{12}\xi_2|\leq3k y_u Q.B11​≤−k/4,∣B10​ξ0​+B12​ξ2​∣≤3kyu​Q.
Preamble
import Definitions.Def_BianchiIX_Algebra_Projective
import Definitions.Def_BianchiIX_Algebra_CoreAngle
import Definitions.Def_BianchiIX_Dynamics_ProjectiveState
import Definitions.Def_BianchiIX_Dynamics_CoreAngle
import Definitions.Def_BianchiIX_Dynamics_CoreCoordinateDifferential
import Definitions.Def_BianchiIX_Dynamics_CoreWeightedVariation
import Definitions.Def_BianchiIX_Dynamics_CoreEntry
import Mathlib.Analysis.ODE.Gronwall
import Mathlib.Data.Matrix.Mul
import Mathlib.Tactic.FieldSimp
import Mathlib.Tactic.FunProp
import Mathlib.Analysis.Calculus.FDeriv.Symmetric
import Mathlib.Analysis.Calculus.Deriv.Mul
import Mathlib.Tactic.NormNum
import Mathlib.Analysis.Calculus.Deriv.Prod
import Mathlib.Tactic.Module
import Mathlib.Analysis.Calculus.Deriv.Pow
import Mathlib.Analysis.Calculus.Deriv.Add
import Mathlib.Analysis.Real.Sqrt
import Mathlib.Tactic.Linarith
import Mathlib.Tactic.Ring
import Mathlib.Analysis.SpecialFunctions.Arsinh
import Mathlib.Analysis.SpecialFunctions.Sqrt
import Mathlib.Analysis.Calculus.ContDiff.Operations
import Mathlib.Analysis.Calculus.MeanValue
import Mathlib.Data.Fin.VecNotation
import Mathlib.Tactic.FinCases
import Mathlib.Analysis.Calculus.Deriv.Inv
import Mathlib.Tactic.LinearCombination
import Mathlib.Analysis.SpecialFunctions.Arcosh
import Mathlib.MeasureTheory.Integral.IntervalIntegral.FundThmCalculus
import Mathlib.Analysis.Calculus.InverseFunctionTheorem.Deriv
import Mathlib.Analysis.Calculus.Deriv.MeanValue
import Mathlib.Analysis.SpecialFunctions.Pow.Deriv
import Mathlib.Analysis.SpecialFunctions.Integrals.Basic
import Mathlib.Analysis.ODE.ExistUnique
import Mathlib.Algebra.BigOperators.Fin
import Mathlib.Analysis.Calculus.FDeriv.Partial
import Mathlib.Analysis.Calculus.ImplicitContDiff
import Mathlib.Data.Real.Basic
import Mathlib.Analysis.SpecialFunctions.Trigonometric.ArctanDeriv
import Mathlib.Analysis.SpecialFunctions.Trigonometric.DerivHyp
import Mathlib.Analysis.SpecialFunctions.Log.Basic
import Mathlib.Topology.Instances.Real.Lemmas
import Mathlib.MeasureTheory.Integral.IntervalIntegral.DistLEIntegral
import Mathlib.Tactic.GCongr
import Mathlib.Analysis.Calculus.Deriv.Slope
import Mathlib.Topology.Order.OrderClosed
import Mathlib.Topology.Order.IntermediateValue

noncomputable section
open BianchiIX
open Set

Formal statement
theorem BianchiIX.coreRegion_strong_forcing {k Q : ℝ} {y : ProjectiveState} {v : CoreAngleState}
    (hk : 6 ≤ k) (hy : coreRegion k y) (hQ : ‖v‖ ≤ Q) :
    let B := coreWeightedJacobian k (projectiveCoreAngle y) (toCoreAngleState y)
    B 1 1 ≤ -k / 4 ∧ |B 1 0 * v 0 + B 1 2 * v 2| ≤ 3 * k * y 1 * Q := by sorry
Source
https://github.com/l46430640-del/ERA-STATISTICS-FORMAL/blob/d74c241819f896ab8d050b21ace80c8e90eabd9e/BianchiIX/Dynamics/CoreStrongVariation.lean#L10-L37

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