For real variables p , s , a , b , c p,s,a,b,c p , s , a , b , c , set
K = a 2 + b 2 + c 2 − 2 ( a b + b c + c a ) , S = p 2 + s 2 , 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 = a 2 + b 2 + c 2 − 2 ( ab + b c + c a ) , S = p 2 + s 2 , C = S + K .
The shear components and wall rates are
P = K p − 2 a 2 + b 2 + c 2 + a b − 2 b c + a c , P=Kp-2a^2+b^2+c^2+ab-2bc+ac, P = K p − 2 a 2 + b 2 + c 2 + ab − 2 b c + a c ,
Q = K s + 3 ( − b 2 + c 2 + a b − a c ) , Q=Ks+\sqrt{3}(-b^2+c^2+ab-ac), Q = K s + 3 ( − b 2 + c 2 + ab − a c ) ,
r 1 = − S + 2 p , r 2 = − S − p + 3 s , r 3 = − S − p − 3 s . r_1=-S+2p,\qquad r_2=-S-p+\sqrt{3}s,\qquad r_3=-S-p-\sqrt{3}s. r 1 = − S + 2 p , r 2 = − S − p + 3 s , r 3 = − S − p − 3 s .
These functions define the normalized vacuum Bianchi IX vector field
( P , Q , r 1 a , r 2 b , r 3 c ) (P,Q,r_1a,r_2b,r_3c) ( P , Q , r 1 a , r 2 b , r 3 c ) .
For y = ( m , u , v , w ) ∈ R 4 y=(m,u,v,w)\in\mathbb R^4 y = ( m , u , v , w ) ∈ R 4 , define
K ( u , v , w ) = u 2 + v 2 + w 2 − 2 ( u v + v w + w u ) , 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 ) = u 2 + v 2 + w 2 − 2 ( uv + v w + w u ) , κ = u ( v + w − u ) ,
F m = − v 2 + w 2 + u ( v − w ) − m κ , F u = 1 2 ( 1 − m 2 − ( v − w ) 2 + u 2 ) 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, F m = − v 2 + w 2 + u ( v − w ) − mκ , F u = 2 1 ( 1 − m 2 − ( v − w ) 2 + u 2 ) u ,
F v = ( m − 1 − κ ) v , F w = ( − m − 1 − κ ) w , F = ( F m , F u , F v , F w ) , F_v=(m-1-\kappa)v,\qquad F_w=(-m-1-\kappa)w,\qquad
F=(F_m,F_u,F_v,F_w), F v = ( m − 1 − κ ) v , F w = ( − m − 1 − κ ) w , F = ( F m , F u , F v , F w ) ,
and E ( m , v ) = ( m − 1 ) 2 + v 2 E(m,v)=(m-1)^2+v^2 E ( m , v ) = ( m − 1 ) 2 + v 2 .
For x = ( p , s , a , b , c ) x=(p,s,a,b,c) x = ( p , s , a , b , c ) , put
ψ ( p , z ) = 3 z 1 + 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 + p 3 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 + m 2 + K ( u , v , w ) D(y)=3+m^2+K(u,v,w) D ( y ) = 3 + m 2 + K ( u , v , w ) and
Ξ A ( y ) = ( A − 1 , A m 3 , A u 3 , A v 3 , A w 3 ) , Ξ ( y ) = Ξ 6 / 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). Ξ A ( y ) = ( A − 1 , 3 A m , 3 A u , 3 A v , 3 A w ) , Ξ ( y ) = Ξ 6/ D ( y ) ( y ) .
Write N ( x ) = ( P , Q , r 1 a , r 2 b , r 3 c ) N(x)=(P,Q,r_1a,r_2b,r_3c) N ( x ) = ( P , Q , r 1 a , r 2 b , r 3 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 R 5 \mathbb R^5 R 5 and R 4 \mathbb R^4 R 4
with their finite-product norms. The maps Π , Ξ , D , F \Pi,\Xi,D,F Π , Ξ , D , F act on these state spaces.
The projective vector field in normalized time is
G ( y ) = 6 D ( y ) F ( y ) . G(y)=\frac6{D(y)}F(y). G ( y ) = D ( y ) 6 F ( y ) .
Write X = R 5 X=\mathbb R^5 X = R 5 , Y = R 4 Y=\mathbb R^4 Y = R 4 , and let α x , t 0 \alpha_{x,t_0} α x , t 0 be the
maximal solution of α ′ = N ( α ) \alpha'=N(\alpha) α ′ = N ( α ) with initial value x x x at t 0 t_0 t 0
and domain I max ( x , t 0 ) I_{\max}(x,t_0) I m a x ( x , t 0 ) . Put
J x , t 0 ( t ) = d x α x , t 0 ( t ) , Ψ t 0 ( y , t ) = Π ( α Ξ ( y ) , t 0 ( 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)), J x , t 0 ( t ) = d x α x , t 0 ( t ) , Ψ t 0 ( y , t ) = Π ( α Ξ ( y ) , t 0 ( t )) ,
J y , t 0 ( t ) = d Π α Ξ ( y ) , t 0 ( t ) ∘ J Ξ ( y ) , t 0 ( t ) ∘ d Ξ y . \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. J y , t 0 ( t ) = d Π α Ξ ( y ) , t 0 ( t ) ∘ J Ξ ( y ) , t 0 ( t ) ∘ d Ξ y .
Put c = u ( v + w − u ) c=u(v+w-u) c = u ( v + w − u ) , s ( m , u , v , w ) = m − 1 − c s(m,u,v,w)=m-1-c s ( m , u , v , w ) = m − 1 − c ,
b ( m , u , v , w ) = ( 1 − m 2 − ( v − w ) 2 + u 2 ) / 2 b(m,u,v,w)=(1-m^2-(v-w)^2+u^2)/2 b ( m , u , v , w ) = ( 1 − m 2 − ( v − w ) 2 + u 2 ) /2 ,
D ( m , u , v , w ) = 3 + m 2 + K ( u , v , w ) D(m,u,v,w)=3+m^2+K(u,v,w) D ( m , u , v , w ) = 3 + m 2 + K ( u , v , w ) , and r ( m , v ) = ( m − 1 ) 2 + v 2 r(m,v)=\sqrt{(m-1)^2+v^2} r ( m , v ) = ( m − 1 ) 2 + v 2 .
Define
E k = { ( m , u , v , w ) : m ≥ 1 , ∣ r ( m , v ) − k ∣ ≤ k / 100 , 0 ≤ u , w ≤ 1 / 10000 , 0 ≤ v ≤ 1 } , \mathcal E_k=\{(m,u,v,w):m\geq1,\ |r(m,v)-k|\leq k/100,
\ 0\leq u,w\leq1/10000,\ 0\leq v\leq1\}, E k = {( m , u , v , w ) : m ≥ 1 , ∣ r ( m , v ) − k ∣ ≤ k /100 , 0 ≤ u , w ≤ 1/10000 , 0 ≤ v ≤ 1 } ,
and ω + ( m , u , v , w ) = s ( m , u , v , w ) \omega_+(m,u,v,w)=s(m,u,v,w) ω + ( m , u , v , w ) = s ( m , u , v , w ) .
For a normalized trajectory write
β ( t ) = Π ( α x , t 0 ( t ) ) , A ( t ) = 1 + ( α x , t 0 ( t ) ) 0 , I = I max ( x , t 0 ) . \beta(t)=\Pi(\alpha_{x,t_0}(t)),\quad A(t)=1+(\alpha_{x,t_0}(t))_0,
\quad I=I_{\max}(x,t_0). β ( t ) = Π ( α x , t 0 ( t )) , A ( t ) = 1 + ( α x , t 0 ( t ) ) 0 , I = I m a x ( x , t 0 ) .
For y ∈ R 4 y\in\mathbb R^4 y ∈ R 4 , put x y = Ξ ( y ) x_y=\Xi(y) x y = Ξ ( y ) ,
T + ( y ) = inf { t > 0 : t ∈ I max ( x y , 0 ) , ( Ψ 0 ( y , t ) ) v = 1 } , P + ( y ) = Ψ 0 ( y , T + ( y ) ) . T_+(y)=\inf\{t>0:t\in I_{\max}(x_y,0),\ (\Psi_0(y,t))_v=1\},
\qquad P_+(y)=\Psi_0(y,T_+(y)). T + ( y ) = inf { t > 0 : t ∈ I m a x ( x y , 0 ) , ( Ψ 0 ( y , t ) ) v = 1 } , P + ( y ) = Ψ 0 ( y , T + ( y )) .
Let V + ( y ) V_+(y) V + ( y ) mean that this infimum is a least element, the full interval
[ 0 , T + ( y ) ] [0,T_+(y)] [ 0 , T + ( y )] lies in the maximal domain with
1 + ( α x y , 0 ( t ) ) 0 > 0 1+(\alpha_{x_y,0}(t))_0>0 1 + ( α x y , 0 ( t ) ) 0 > 0 , the active wall
is below one before the endpoint, and its normalized-time derivative is
strictly positive throughout the interval. The infimum has its total
real-order meaning.
On the invariant plane with zero active wall, use y = ( m , u , w ) ∈ R 3 y=(m,u,w)\in\mathbb R^3 y = ( m , u , w ) ∈ R 3 ,
the inclusion ι ( m , u , w ) = ( m , u , 0 , w ) \iota(m,u,w)=(m,u,0,w) ι ( m , u , w ) = ( m , u , 0 , w ) and the restriction
π s ( m , u , v , w ) = ( m , u , w ) \pi_s(m,u,v,w)=(m,u,w) π s ( m , u , v , w ) = ( m , u , w ) . Define
f ( y ) = ( m u 2 − ( m + 1 ) u w + w 2 , 1 − m 2 − w 2 + u 2 2 u , − ( m + 1 + u w − u 2 ) w ) , f(y)=\left(mu^2-(m+1)uw+w^2,
\frac{1-m^2-w^2+u^2}{2}u,-(m+1+uw-u^2)w\right), f ( y ) = ( m u 2 − ( m + 1 ) u w + w 2 , 2 1 − m 2 − w 2 + u 2 u , − ( m + 1 + u w − u 2 ) w ) ,
Δ ( y ) = 3 + m 2 + ( u − w ) 2 , f o ( y ) = 6 f ( y ) / Δ ( y ) . \Delta(y)=3+m^2+(u-w)^2,\qquad f_o(y)=6f(y)/\Delta(y). Δ ( y ) = 3 + m 2 + ( u − w ) 2 , f o ( y ) = 6 f ( y ) /Δ ( y ) .
Write J = d f J=df J = df , H = d 2 f H=d^2f H = d 2 f , J o = d f o J_o=df_o J o = d f o , H o = d 2 f o H_o=d^2f_o H o = d 2 f o for their explicit
Jacobian and Hessian expressions. The denominator derivatives are
d Δ = ( 2 m , 2 ( u − w ) , 2 ( w − u ) ) d\Delta=(2m,2(u-w),2(w-u)) d Δ = ( 2 m , 2 ( u − w ) , 2 ( w − u )) and
d 2 Δ ( v , z ) = 2 v 0 z 0 + 2 ( v 1 − v 2 ) ( z 1 − z 2 ) d^2\Delta(v,z)=2v_0z_0+2(v_1-v_2)(z_1-z_2) d 2 Δ ( v , z ) = 2 v 0 z 0 + 2 ( v 1 − v 2 ) ( z 1 − z 2 ) .
The exact original-time boundary flow and its projected variation are
Φ ( y , t ) = π s Ψ 0 ( ι y , t ) , L ( y , t ) = π s J ι y , 0 ( t ) ι . \Phi(y,t)=\pi_s\Psi_0(\iota y,t),\qquad
L(y,t)=\pi_s\mathcal J_{\iota y,0}(t)\iota. Φ ( y , t ) = π s Ψ 0 ( ιy , t ) , L ( y , t ) = π s J ιy , 0 ( t ) ι .
For a fixed scale K K K , set Φ K ( y , s ) = Φ ( y , K s ) \Phi_K(y,s)=\Phi(y,Ks) Φ K ( y , s ) = Φ ( y , K s ) ,
L K ( y , s ) = L ( y , K s ) L_K(y,s)=L(y,Ks) L K ( y , s ) = L ( y , K s ) and Q K ( y , s ) = d y L K ( y , s ) Q_K(y,s)=d_yL_K(y,s) Q K ( y , s ) = d y L K ( y , s ) .
For directions v , z v,z v , z , define
S K ( y , s ; v , z ) = K [ H o ( Φ K ) ( L K v , L K z ) + J o ( Φ K ) Q K ( v , z ) ] . S_K(y,s;v,z)=K\left[H_o(\Phi_K)(L_Kv,L_Kz)+J_o(\Phi_K)Q_K(v,z)\right]. S K ( y , s ; v , z ) = K [ H o ( Φ K ) ( L K v , L K z ) + J o ( Φ K ) Q K ( v , z ) ] .
All vector norms are sup norms, and operator norms are induced by them.
Write b ( y ) = ∣ u ∣ + ∣ w ∣ b(y)=|u|+|w| b ( y ) = ∣ u ∣ + ∣ w ∣ , E ( y ) = e 512 b ( y ) E(y)=e^{512b(y)} E ( y ) = e 512 b ( y ) , v s = ( v 1 , v 2 ) v_s=(v_1,v_2) v s = ( v 1 , v 2 ) , and
H ( y ; v , z ) = b ( y ) ∥ v ∥ ∥ z ∥ + ∥ v s ∥ ∥ z ∥ + ∥ v ∥ ∥ z s ∥ , \mathcal H(y;v,z)=b(y)\|v\|\|z\|+\|v_s\|\|z\|+\|v\|\|z_s\|, H ( y ; v , z ) = b ( y ) ∥ v ∥∥ z ∥ + ∥ v s ∥∥ z ∥ + ∥ v ∥∥ z s ∥ ,
B 2 ( y ) = 192 b ( y ) ( 40000 E ( y ) 3 ) + 10000 E ( y ) 2 . B_2(y)=192b(y)(40000E(y)^3)+10000E(y)^2. B 2 ( y ) = 192 b ( y ) ( 40000 E ( y ) 3 ) + 10000 E ( y ) 2 .
The closed boundary region is
S c = { ( m , u , 0 , w ) : ∣ m − c ∣ ≤ 1 / 10 , ∣ u ∣ , ∣ w ∣ ≤ 1 / 100 } \mathcal S_c=\{(m,u,0,w):|m-c|\leq1/10,\ |u|,|w|\leq1/100\} S c = {( m , u , 0 , w ) : ∣ m − c ∣ ≤ 1/10 , ∣ u ∣ , ∣ w ∣ ≤ 1/100 } .
The boundary projection P ( m , u , w ) P(m,u,w) P ( m , u , w ) is the limit of Φ ( m , u , w ; t ) 0 \Phi(m,u,w;t)_0 Φ ( m , u , w ; t ) 0
as t → ∞ t\to\infty t → ∞ , using the total limit convention of the formal definitions.
For y = ( m , u , v , w ) y=(m,u,v,w) y = ( m , u , v , w ) , define p ( y ) = P ( m , u , w ) p(y)=P(m,u,w) p ( y ) = P ( m , u , w ) ,
ρ ( y ) = ( p ( y ) − 1 ) 2 + v 2 \rho(y)=\sqrt{(p(y)-1)^2+v^2} ρ ( y ) = ( p ( y ) − 1 ) 2 + v 2 , ω ( y ) = m − 1 − u ( v + w − u ) \omega(y)=m-1-u(v+w-u) ω ( y ) = m − 1 − u ( v + w − u ) ,
and χ ( y ) = ( ρ ( y ) , u , v , w ) \chi(y)=(\rho(y),u,v,w) χ ( y ) = ( ρ ( y ) , u , v , w ) . Write p i = ∂ i p p_i=\partial_i p p i = ∂ i p .
The inverse differential J χ ( y ) J_\chi(y) J χ ( y ) preserves the last three coordinates
and has first row
( ρ ( p − 1 ) p 0 , − p 1 p 0 , − v ( p − 1 ) p 0 , − p 3 p 0 ) . \left(\frac{\rho}{(p-1)p_0},-\frac{p_1}{p_0},
-\frac{v}{(p-1)p_0},-\frac{p_3}{p_0}\right). ( ( p − 1 ) p 0 ρ , − p 0 p 1 , − ( p − 1 ) p 0 v , − p 0 p 3 ) .
An admissible local inverse ψ \psi ψ at y y y is C 2 C^2 C 2 at χ ( y ) \chi(y) χ ( y ) ,
maps χ ( y ) \chi(y) χ ( y ) to y y y , has derivative J χ ( y ) J_\chi(y) J χ ( y ) there, and is a
two-sided inverse to χ \chi χ on neighborhoods of these points.
For a scalar function f f f , write ∂ ˉ i f = d ( f ∘ ψ ) χ ( y ) e i \bar\partial_i f=d(f\circ\psi)_{\chi(y)}e_i ∂ ˉ i f = d ( f ∘ ψ ) χ ( y ) e i .
The radial coefficients and drift are
N ( y ) = m − 1 − u ( w − u ) − ( p − 1 ) p 0 , B ( y ) = N ( y ) ρ ω , N(y)=m-1-u(w-u)-(p-1)p_0,\qquad B(y)=\frac{N(y)}{\rho\omega}, N ( y ) = m − 1 − u ( w − u ) − ( p − 1 ) p 0 , B ( y ) = ρ ω N ( y ) ,
A ( y ) = ( p − 1 ) ( ( 1 − m ) p 0 + w ( p 1 − p 3 ) ) − v 2 − 1 2 ( p − 1 ) v p 1 ρ ω , G ( y ) = u v A ( y ) + v 2 B ( y ) . A(y)=\frac{(p-1)((1-m)p_0+w(p_1-p_3))-v^2
-\tfrac12(p-1)vp_1}{\rho\omega},\qquad G(y)=uvA(y)+v^2B(y). A ( y ) = ρ ω ( p − 1 ) (( 1 − m ) p 0 + w ( p 1 − p 3 )) − v 2 − 2 1 ( p − 1 ) v p 1 , G ( y ) = uv A ( y ) + v 2 B ( y ) .
Set
S ( y ) = ( p − 1 ) ( ( p − m ) − ( m − 1 ) ( p 0 − 1 ) ) + ( p − 1 ) w ( p 1 − p 3 ) − 1 2 ( p − 1 ) v p 1 , H ( y ) = p − 1 − ( m − 1 ) p 0 , S(y)=(p-1)((p-m)-(m-1)(p_0-1))+(p-1)w(p_1-p_3)
-\tfrac12(p-1)vp_1,\quad H(y)=p-1-(m-1)p_0, S ( y ) = ( p − 1 ) (( p − m ) − ( m − 1 ) ( p 0 − 1 )) + ( p − 1 ) w ( p 1 − p 3 ) − 2 1 ( p − 1 ) v p 1 , H ( y ) = p − 1 − ( m − 1 ) p 0 ,
N 2 ( y ) = ( 1 − L − 2 ) u 2 + ( − 1 + 4 L − 2 ) u w − w 2 / L 2 , L = m + 1 , N_2(y)=(1-L^{-2})u^2+(-1+4L^{-2})uw-w^2/L^2,\qquad L=m+1, N 2 ( y ) = ( 1 − L − 2 ) u 2 + ( − 1 + 4 L − 2 ) u w − w 2 / L 2 , L = m + 1 ,
R e ( y ) = R q ( m , u , w ) , N 4 ( y ) = − R e − ( m − 1 ) ∂ 0 R e − ( p − m ) ( p 0 − 1 ) , E ( y ) = ρ ( y ) − r ( m , v ) . R_e(y)=R_q(m,u,w),\quad
N_4(y)=-R_e-(m-1)\partial_0R_e-(p-m)(p_0-1),\quad
E(y)=\rho(y)-r(m,v). R e ( y ) = R q ( m , u , w ) , N 4 ( y ) = − R e − ( m − 1 ) ∂ 0 R e − ( p − m ) ( p 0 − 1 ) , E ( y ) = ρ ( y ) − r ( m , v ) .
Here
R q ( m , u , w ) = P ( m , u , w ) − [ m + m u 2 m 2 − 1 − 2 u w m + 1 + w 2 2 ( m + 1 ) ] . R_q(m,u,w)=P(m,u,w)-
\left[m+\frac{mu^2}{m^2-1}-\frac{2uw}{m+1}+\frac{w^2}{2(m+1)}\right]. R q ( m , u , w ) = P ( m , u , w ) − [ m + m 2 − 1 m u 2 − m + 1 2 u w + 2 ( m + 1 ) w 2 ] .
The logarithmic wall rates are
a s = 1 − m 2 − ( v − w ) 2 + u 2 2 ω , a w = − 1 − 2 ( 1 + u ( v + w − u ) ) ω . a_s=\frac{1-m^2-(v-w)^2+u^2}{2\omega},\qquad
a_w=-1-\frac{2(1+u(v+w-u))}{\omega}. a s = 2 ω 1 − m 2 − ( v − w ) 2 + u 2 , a w = − 1 − ω 2 ( 1 + u ( v + w − u )) .
Let D χ f = d f J χ D_\chi f=df\,J_\chi D χ f = df J χ , define
c ( y ) = ( D χ G e 0 , u D χ G e 1 , w D χ G e 3 ) , c(y)=(D_\chi G\,e_0,uD_\chi G\,e_1,wD_\chi G\,e_3), c ( y ) = ( D χ G e 0 , u D χ G e 1 , w D χ G e 3 ) ,
A k ( y ) = ( u D χ a s e 1 ( w / k 2 ) D χ a s e 3 k 2 u D χ a w e 1 w D χ a w e 3 ) , \mathcal A_k(y)=
\begin{pmatrix}uD_\chi a_s\,e_1&(w/k^2)D_\chi a_s\,e_3\\
k^2uD_\chi a_w\,e_1&wD_\chi a_w\,e_3\end{pmatrix}, A k ( y ) = ( u D χ a s e 1 k 2 u D χ a w e 1 ( w / k 2 ) D χ a s e 3 w D χ a w e 3 ) ,
and ℓ k ( y ) = ( log u , k 2 log w ) \ell_k(y)=(\log u,k^2\log w) ℓ k ( y ) = ( log u , k 2 log w ) .
All vector and operator norms use the sup norm.
Let k ≥ 7 / 4 k\geq7/4 k ≥ 7/4 , s ≤ t s\leq t s ≤ t and Y ′ = a F ( Y ) Y'=aF(Y) Y ′ = a F ( Y ) on [ s , t ] [s,t] [ s , t ] ,
where a a a is continuous and nonnegative. Assume Y ( r ) ∈ E k Y(r)\in\mathcal E_k Y ( r ) ∈ E k
and Y ( r ) 2 > 0 Y(r)_2>0 Y ( r ) 2 > 0 throughout. Put
q ( r ) = a ( r ) ω ( Y ( r ) ) , l ( r ) = log Y ( r ) 2 − log Y ( s ) 2 , ( u 0 , v 0 , w 0 ) = ( Y ( s ) 1 , Y ( s ) 2 , Y ( s ) 3 ) . q(r)=a(r)\omega(Y(r)),\quad l(r)=\log Y(r)_2-\log Y(s)_2,\quad
(u_0,v_0,w_0)=(Y(s)_1,Y(s)_2,Y(s)_3). q ( r ) = a ( r ) ω ( Y ( r )) , l ( r ) = log Y ( r ) 2 − log Y ( s ) 2 , ( u 0 , v 0 , w 0 ) = ( Y ( s ) 1 , Y ( s ) 2 , Y ( s ) 3 ) .
Writing ( m , u , v , w ) = Y ( r ) (m,u,v,w)=Y(r) ( m , u , v , w ) = Y ( r ) in the integrands,
∫ s t [ u + k u ( v + u + w ) ] q d r ≤ 12 u 0 , \int_s^t[u+ku(v+u+w)]q\,dr\leq12u_0, ∫ s t [ u + k u ( v + u + w )] q d r ≤ 12 u 0 ,
∫ s t [ w / k 2 + u w / k + w ( u + w ) / k 3 ] q d r ≤ 6 w 0 / k 2 . \int_s^t[w/k^2+uw/k+w(u+w)/k^3]q\,dr\leq6w_0/k^2. ∫ s t [ w / k 2 + u w / k + w ( u + w ) / k 3 ] q d r ≤ 6 w 0 / k 2 .