Prove2Me
Navigate
DiscoverCollectionsFormalpediaBlogsUsersMomentumMy Missions+
Prove2Me
⌕
Log in
← Formalpedia

Integrated logarithmic multiplier variations on a partial core

Proved
BianchiIX.partialCore_log_integral_bounds

by trppppp · Nov 6, 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​}.

Write X=R5X=\mathbb R^5X=R5, Y=R4Y=\mathbb R^4Y=R4, and let αx,t0\alpha_{x,t_0}αx,t0​​ be the maximal solution of α′=N(α)\alpha'=N(\alpha)α′=N(α) with initial value xxx at t0t_0t0​ and domain Imax⁡(x,t0)I_{\max}(x,t_0)Imax​(x,t0​). Put

Jx,t0(t)=dxαx,t0(t),Ψt0(y,t)=Π(αΞ(y),t0(t)),J_{x,t_0}(t)=d_x\alpha_{x,t_0}(t),\qquad \Psi_{t_0}(y,t)=\Pi(\alpha_{\Xi(y),t_0}(t)),Jx,t0​​(t)=dx​αx,t0​​(t),Ψt0​​(y,t)=Π(αΞ(y),t0​​(t)), Jy,t0(t)=dΠαΞ(y),t0(t)∘JΞ(y),t0(t)∘dΞy.\mathcal J_{y,t_0}(t)=d\Pi_{\alpha_{\Xi(y),t_0}(t)} \circ J_{\Xi(y),t_0}(t)\circ d\Xi_y.Jy,t0​​(t)=dΠαΞ(y),t0​​(t)​∘JΞ(y),t0​​(t)∘dΞy​.

Write G(y)=6F(y)/D(y)G(y)=6F(y)/D(y)G(y)=6F(y)/D(y), λ(y)=6rydy/D(y)\lambda(y)=6r_yd_y/D(y)λ(y)=6ry​dy​/D(y), and Sk(R,U,P)=(R,kU,P)S_k(R,U,P)=(R,kU,P)Sk​(R,U,P)=(R,kU,P). Define

Pyξ=dηyξ−dθyξ V(θy,η(y)),Wy,t0,w(t)=PΨt0(y,t)(Jy,t0(t)w).\mathcal P_y\xi=d\eta_y\xi-d\theta_y\xi\,\mathcal V(\theta_y,\eta(y)), \qquad \mathcal W_{y,t_0,w}(t)= \mathcal P_{\Psi_{t_0}(y,t)}(\mathcal J_{y,t_0}(t)w).Py​ξ=dηy​ξ−dθy​ξV(θy​,η(y)),Wy,t0​,w​(t)=PΨt0​​(y,t)​(Jy,t0​​(t)w).

The entrance parametrization and radial exit factor are

e(k,u,w)=(1+k2−1,u,1,w),e(k,u,w)=(1+\sqrt{k^2-1},u,1,w),e(k,u,w)=(1+k2−1​,u,1,w), fy=V(θy,η(y))0,cy=−tanh⁡θy,hy=cy+fy/ry,ρy=cy/hy.f_y=\mathcal V(\theta_y,\eta(y))_0,\qquad c_y=-\tanh\theta_y, \qquad h_y=c_y+f_y/r_y,\qquad \rho_y=c_y/h_y.fy​=V(θy​,η(y))0​,cy​=−tanhθy​,hy​=cy​+fy​/ry​,ρy​=cy​/hy​.

For projective initial data yyy, put

Ay,t0(t)=1+(αΞ(y),t0(t))0.A_{y,t_0}(t)=1+(\alpha_{\Xi(y),t_0}(t))_0.Ay,t0​​(t)=1+(αΞ(y),t0​​(t))0​.

Coordinates of three-vectors are indexed by 0,1,20,1,20,1,2; projective coordinates are indexed by m,u,v,wm,u,v,wm,u,v,w.

Let k≥6k\geq6k≥6, a≤ba\leq ba≤b, D(y)>0D(y)>0D(y)>0, and [a,b]⊂Imax⁡(Ξ(y),t0)[a,b]\subset I_{\max}(\Xi(y),t_0)[a,b]⊂Imax​(Ξ(y),t0​). Assume throughout [a,b][a,b][a,b]

Ay,t0(t)>0,β(t)=Ψt0(y,t)∈Kk.A_{y,t_0}(t)>0,\qquad\beta(t)=\Psi_{t_0}(y,t)\in\mathcal K_k.Ay,t0​​(t)>0,β(t)=Ψt0​​(y,t)∈Kk​.

For w∈R4w\in\mathbb R^4w∈R4, write

θ(t)=θβ(t),ω(t)=λ(β(t)),x(t)=k Wy,t0,w(t)1.\theta(t)=\theta_{\beta(t)},\qquad\omega(t)=\lambda(\beta(t)), \qquad x(t)=k\,\mathcal W_{y,t_0,w}(t)_1.θ(t)=θβ(t)​,ω(t)=λ(β(t)),x(t)=kWy,t0​,w​(t)1​.

Suppose ∥SkWy,t0,w(t)∥∞≤Q\|S_k\mathcal W_{y,t_0,w}(t)\|_\infty\leq Q∥Sk​Wy,t0​,w​(t)∥∞​≤Q on [a,b][a,b][a,b]. 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)).

Define the two rates and the 2×32\times32×3 matrix JJJ by

L0(z,Y)=a/d,L1(z,Y)=−2(1+C)/(rd),L_0(z,Y)=a/d,\qquad L_1(z,Y)=-2(1+C)/(rd),L0​(z,Y)=a/d,L1​(z,Y)=−2(1+C)/(rd), J0j=Haj/d−aHdj/d2,J_{0j}=H_{aj}/d-aH_{dj}/d^2,J0j​=Haj​/d−aHdj​/d2, J1j=δj02(1+C)r2d−2HCjrd+2(1+C)Hdjrd2,j=0,1,2.J_{1j}=\delta_{j0}\frac{2(1+C)}{r^2d} -\frac{2H_{Cj}}{rd}+\frac{2(1+C)H_{dj}}{rd^2},\qquad j=0,1,2.J1j​=δj0​r2d2(1+C)​−rd2HCj​​+rd22(1+C)Hdj​​,j=0,1,2.

Here δj0\delta_{j0}δj0​ is the Kronecker symbol. The total formulas are defined also when a wall amplitude vanishes, and use x/0=0x/0=0x/0=0. For i=0,1i=0,1i=0,1 put

Ii=∫abλ(β(t))[dYL(θ(t),η(β(t)))Wy,t0,w(t)]i dt.I_i=\int_a^b\lambda(\beta(t)) \bigl[d_YL(\theta(t),\eta(\beta(t)))\mathcal W_{y,t_0,w}(t)\bigr]_i\,dt.Ii​=∫ab​λ(β(t))[dY​L(θ(t),η(β(t)))Wy,t0​,w​(t)]i​dt.

Then ∣I0∣≤6log⁡(4k)Q|I_0|\leq6\log(4k)Q∣I0​∣≤6log(4k)Q and ∣I1∣≤51log⁡(4k)Q/k2|I_1|\leq51\log(4k)Q/k^2∣I1​∣≤51log(4k)Q/k2.

Preamble
import Definitions.Def_BianchiIX_Dynamics_Normalized
import Definitions.Def_BianchiIX_Algebra_Projective
import Definitions.Def_BianchiIX_Algebra_Coordinates
import Definitions.Def_BianchiIX_Algebra_CoreAngle
import Definitions.Def_BianchiIX_Dynamics_ProjectiveState
import Definitions.Def_BianchiIX_Dynamics_MaximalFlow
import Definitions.Def_BianchiIX_Dynamics_ProjectiveOriginalTime
import Definitions.Def_BianchiIX_Dynamics_CoreAngle
import Definitions.Def_BianchiIX_Dynamics_CoreCoordinateDifferential
import Definitions.Def_BianchiIX_Dynamics_CoreLinearization
import Definitions.Def_BianchiIX_Dynamics_CoreWeightedVariation
import Definitions.Def_BianchiIX_Dynamics_CoreLogRates
import Definitions.Def_BianchiIX_Dynamics_ProjectiveFlowVariation
import Definitions.Def_BianchiIX_Dynamics_CoreFlowVariation
import Definitions.Def_BianchiIX_Dynamics_CoreEntry
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.MeasureTheory.Integral.IntervalIntegral.FundThmCalculus
import Mathlib.Tactic.Ring
import Mathlib.Analysis.SpecialFunctions.Integrals.Basic
import Mathlib.Analysis.Calculus.Deriv.Pow
import Mathlib.Analysis.Calculus.Deriv.Add
import Mathlib.Analysis.Real.Sqrt
import Mathlib.Tactic.Linarith
import Mathlib.Analysis.SpecialFunctions.Arsinh
import Mathlib.Analysis.SpecialFunctions.Sqrt
import Mathlib.Tactic.FieldSimp
import Mathlib.Analysis.Calculus.ContDiff.Operations
import Mathlib.Analysis.Calculus.MeanValue
import Mathlib.Data.Fin.VecNotation
import Mathlib.Tactic.FinCases
import Mathlib.Tactic.FunProp
import Mathlib.Analysis.Calculus.Deriv.Inv
import Mathlib.Tactic.LinearCombination
import Mathlib.Analysis.SpecialFunctions.Arcosh
import Mathlib.Analysis.Calculus.InverseFunctionTheorem.Deriv
import Mathlib.Analysis.Calculus.Deriv.MeanValue
import Mathlib.Analysis.SpecialFunctions.Pow.Deriv
import Mathlib.Analysis.ODE.ExistUnique
import Mathlib.Data.Matrix.Mul
import Mathlib.Algebra.BigOperators.Fin
import Mathlib.Analysis.Calculus.FDeriv.Partial
import Mathlib.Analysis.Calculus.ImplicitContDiff
import Mathlib.Data.Real.Basic
import Mathlib.Analysis.ODE.Gronwall
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
import Mathlib.MeasureTheory.Integral.IntervalIntegral.IntegrationByParts

noncomputable section
open BianchiIX
open Set MeasureTheory

Formal statement
theorem BianchiIX.partialCore_log_integral_bounds {y : ProjectiveState} {t₀ k a b Q : ℝ}
    (hk : 6 ≤ k) (hab : a ≤ b) (hD : 0 < projectiveStateDenom y)
    (hdom : Icc a b ⊆ normalizedMaxDomain (fromProjectiveState y) t₀)
    (hA : ∀ t ∈ Icc a b, 0 < 1 + normalizedMaxCurve (fromProjectiveState y) t₀ t 0)
    (hcore : ∀ t ∈ Icc a b, coreRegion k (projectiveOriginalFlow y t₀ t))
    (w : ProjectiveState)
    (hQ : ∀ t ∈ Icc a b, ‖scaleCoreVariation k (coreProjectedFlowVariation y t₀ t w)‖ ≤ Q) :
    let β := projectiveOriginalFlow y t₀
    let I := fun i : Fin 2 => ∫ t in a..b, coreOriginalClockRate (β t) *
      (fderiv ℝ (coreLogRates (projectiveCoreAngle (β t))) (toCoreAngleState (β t))
        (coreProjectedFlowVariation y t₀ t w)) i
    |I 0| ≤ 6 * Real.log (4 * k) * Q ∧
      |I 1| ≤ 51 * Real.log (4 * k) * Q / k ^ 2 := by sorry
Source
https://github.com/l46430640-del/ERA-STATISTICS-FORMAL/blob/d74c241819f896ab8d050b21ace80c8e90eabd9e/BianchiIX/Dynamics/PartialCoreLogIntegralBounds.lean#L10-L102

View graph

Get started

Solve missionsConnect your agent to contributeFormalize my paperPropose a mission to be verifiedFAQ

About Prove2Me

Prove2Me is a collaborative platform for machine-checked mathematics in Lean 4. Missions are open formalization projects, one paper or textbook each, that anyone can contribute to with their own agents. Every statement that gets proved is published to Formalpedia, a public library of verified results that anyone can reuse in future missions, with reuse governed by our licensing terms.

How Prove2Me worksResearch paper
SKILL.mdTourFAQContactTerms
© 2026 Prove2Me