Adopt the setting, hypotheses \textbf{(H1)}--\textbf{(H4)}, and notation of the \reftext{lem:approximate-kalman-policy-2026a}{approximate Kalman filter and policy lemma}: the \reftext{def:fluctuation-lqg-data-2026a}{fluctuation LQG data} of the \reftext{def:stationary-mean-field-triple-2026a}{stationary mean-field triple} ( S , A , P ) (S,A,P) ( S , A , P ) with matrices E t \mathcal{E}_t E t β , B t \mathcal{B}_t B t β , E ~ t \tilde{\mathcal{E}}_t E ~ t β , Ξ t β \Theta^\star_t Ξ t β β , Ξ ~ t β \tilde{\Theta}^\star_t Ξ ~ t β β , the coefficient matrices Q t Q_t Q t β , V t V_t V t β , R t R_t R t β , W t = Z t B t + 1 2 V t W_t=Z_t\mathcal{B}_t+\tfrac12V_t W t β = Z t β B t β + 2 1 β V t β , the feedback gain G t = R t β 1 W t β€ \mathcal{G}_t=R_t^{-1}W_t^{\top} G t β = R t β 1 β W t β€ β , the filter covariance Ξ = ( Ξ t ) t β [ 0 , T ] \Pi=(\Pi_t)_{t\in[0,T]} Ξ = ( Ξ t β ) t β [ 0 , T ] β with initial value Ξ 0 \Pi_0 Ξ 0 β from (H4), the Kalman gain K ~ t = Ξ t E ~ t β€ ( Ξ ~ t β ) β 1 \tilde{\mathcal{K}}_t=\Pi_t\tilde{\mathcal{E}}_t^{\top}(\tilde{\Theta}^\star_t)^{-1} K ~ t β = Ξ t β E ~ t β€ β ( Ξ ~ t β β ) β 1 , and D ~ t = E ~ t β€ ( Ξ ~ t β ) β 1 E ~ t \tilde{D}_t=\tilde{\mathcal{E}}_t^{\top}(\tilde{\Theta}^\star_t)^{-1}\tilde{\mathcal{E}}_t D ~ t β = E ~ t β€ β ( Ξ ~ t β β ) β 1 E ~ t β . Fix a natural number N β₯ 1 N\ge1 N β₯ 1 , an \reftext{def:n-agent-driving-system-2026a}{N N N -agent driving system} ( Ξ© , F , P ) (\Omega,\mathcal{F},\mathbb{P}) ( Ξ© , F , P ) , and a projected \reftext{def:n-agent-controlled-dynamics-2026a}{solution} as in conclusion 4 of the policy lemma: state processes Ο i \sigma^i Ο i , observation processes Ξ₯ Ο
\Upsilon^\upsilon Ξ₯ Ο
, the approximate Kalman control Ξ± \alpha Ξ± , the approximate Kalman filter s ^ N \hat{\mathfrak{s}}^N s ^ N , the regular event Ξ© 0 \Omega_0 Ξ© 0 β , the system filtration ( F t s y s ) t β [ 0 , T ] (\mathcal{F}^{\mathrm{sys}}_t)_{t\in[0,T]} ( F t sys β ) t β [ 0 , T ] β (the system filtration of the \reftext{def:n-agent-controlled-dynamics-2026a}{solution definition}), the empirical state measure Ξ£ t \Sigma_t Ξ£ t β , and the observation total c ~ t \tilde{c}_t c ~ t β with jump times Ο j \tau_j Ο j β and channels Ο
j \upsilon_j Ο
j β ; this collection is a solution of the controlled N N N -agent dynamics for Ξ² \beta Ξ² , Ξ² ~ \tilde{\beta} Ξ² ~ β , and the approximate Kalman policy h N h^N h N , by conclusion 4(a). Since ( S , A ) (S,A) ( S , A ) is a \reftext{def:mean-field-trajectory-pair-2026a}{mean-field trajectory pair} (part of the \reftext{def:stationary-mean-field-triple-2026a}{stationary triple}), the \reftext{def:n-agent-fluctuation-processes-2026a}{fluctuation processes} s t = N ( Ξ£ t β S t ) \mathfrak{s}_t=\sqrt{N}(\Sigma_t-S_t) s t β = N β ( Ξ£ t β β S t β ) and a t = N ( Ξ± t β A t ) \mathfrak{a}_t=\sqrt{N}(\alpha_t-A_t) a t β = N β ( Ξ± t β β A t β ) are defined; by conclusion 4(a) of the policy lemma, a t = β G t β s ^ t N \mathfrak{a}_t=-\mathcal{G}_t\,\hat{\mathfrak{s}}^N_t a t β = β G t β s ^ t N β at every point of Ξ© 0 Γ [ 0 , T ] \Omega_0\times[0,T] Ξ© 0 β Γ [ 0 , T ] . Let e s e_s e s β be the \reftext{lem:fluctuation-linearization-residual-2026a}{state linearization residual} of this solution about ( S , A ) (S,A) ( S , A ) (whose linearization matrices E s E_s E s β and B s \mathsf{B}_s B s β coincide with E s \mathcal{E}_s E s β and B s \mathcal{B}_s B s β , by the identical defining formulas of clauses 1 and 2 of the \reftext{def:fluctuation-lqg-data-2026a}{fluctuation LQG data}), let e ~ s \tilde{e}_s e ~ s β be the \reftext{lem:observation-linearization-residual-2026a}{observation linearization residual} (whose observation linearization matrix coincides with E ~ s \tilde{\mathcal{E}}_s E ~ s β , as noted there), let M t M_t M t β be the state martingale vector of the \reftext{thm:n-agent-martingale-decomposition-2026a}{martingale decomposition} (not to be confused with the closed-loop matrix M t = E t β B t G t β K ~ t E ~ t \mathcal{M}_t=\mathcal{E}_t-\mathcal{B}_t\mathcal{G}_t-\tilde{\mathcal{K}}_t\tilde{\mathcal{E}}_t M t β = E t β β B t β G t β β K ~ t β E ~ t β used in the proof below, written M t M_t M t β in the \reftext{lem:approximate-kalman-policy-2026a}{policy lemma}), and let
J ~ t = J ~ t K ~ \tilde{J}_t=\tilde{J}^{\tilde{\mathcal{K}}}_t J ~ t β = J ~ t K ~ β
be the \reftext{lem:n-agent-weighted-observation-sums-2026a}{weighted compensated observation sum} with weight F = K ~ F=\tilde{\mathcal{K}} F = K ~ (admissible there: all entries of t β¦ K ~ t t\mapsto\tilde{\mathcal{K}}_t t β¦ K ~ t β are continuous by conclusion 2 of the policy lemma; fix a real C K ~ β₯ 0 C_{\tilde{K}}\ge0 C K ~ β β₯ 0 bounding them in absolute value, by \reftext{lem:continuous-compact-interval-bounded-2026a}{boundedness of continuous functions}). Write E \mathbb{E} E for the \reftext{def:expectation-variance-2026a}{expectation}, β£ β
β£ |\cdot| β£ β
β£ for the Euclidean norm (\reftext{def:euclidean-distance-rn-2026a}{Euclidean distance} to the origin), 1 Ξ© 0 \mathbf{1}_{\Omega_0} 1 Ξ© 0 β β for the indicator of Ξ© 0 \Omega_0 Ξ© 0 β , and adopt the matrix entry notation of the \reftext{thm:fluctuation-control-coercivity-2026b}{completion-of-squares theorem}: x β
M y = β p , q M p q x p y q x\cdot My=\sum_{p,q}M^{pq}x^py^q x β
M y = β p , q β M pq x p y q , ( M M β² ) p q = β r M p r M β² r q (MM')^{pq}=\sum_{r}M^{pr}M'^{rq} ( M M β² ) pq = β r β M p r M β² r q , ( M β€ ) q p = M p q (M^{\top})^{qp}=M^{pq} ( M β€ ) qp = M pq . Let Ξ \Theta Ξ be the \reftext{def:aggregate-fluctuation-covariance-2026a}{aggregate fluctuation covariance} of Ξ² \beta Ξ² and b ~ \tilde{b} b ~ the \reftext{def:aggregate-observation-drift-2026a}{aggregate observation drift} of Ξ² ~ \tilde{\beta} Ξ² ~ β . Define the \textbf{filter error}
Ξ΅ t = s t β s ^ t N β R l ( t β [ 0 , T ] ) , \varepsilon_t=\mathfrak{s}_t-\hat{\mathfrak{s}}^N_t\in\mathbb{R}^l\qquad(t\in[0,T]), Ξ΅ t β = s t β β s ^ t N β β R l ( t β [ 0 , T ]) ,
and set
ΞΊ 0 = 1 + E [ β£ s 0 β£ 4 ] , \kappa_0=1+\mathbb{E}\big[|\mathfrak{s}_0|^4\big], ΞΊ 0 β = 1 + E [ β£ s 0 β β£ 4 ] ,
which is finite because β£ s 0 β£ β€ 2 N |\mathfrak{s}_0|\le2\sqrt{N} β£ s 0 β β£ β€ 2 N β everywhere (any two points of the \reftext{def:probability-simplex-2026a}{probability simplex} being at Euclidean distance at most 2 2 2 ). Then:
\textbf{(a) (Finiteness and well-definedness.)} The control energies
A = β« [ 0 , T ] E [ β£ a t β£ 2 ] β d t and A 4 = β« [ 0 , T ] E [ β£ a t β£ 4 ] β d t \mathcal{A}=\int_{[0,T]}\mathbb{E}\big[|\mathfrak{a}_t|^2\big]\,dt\qquad\text{and}\qquad\mathcal{A}_4=\int_{[0,T]}\mathbb{E}\big[|\mathfrak{a}_t|^4\big]\,dt A = β« [ 0 , T ] β E [ β£ a t β β£ 2 ] d t and A 4 β = β« [ 0 , T ] β E [ β£ a t β β£ 4 ] d t
are finite (they are well defined in [ 0 , β ] [0,\infty] [ 0 , β ] by clause (a) of the \reftext{lem:fluctuation-state-moment-bound-2026a}{a priori second-moment bound} and of the \reftext{lem:fluctuation-fourth-moment-bound-2026a}{a priori fourth-moment bound}); in particular the \reftext{lem:fluctuation-linearization-residual-2026a}{state residual lemma} applies to this solution. For every t t t , each Ξ΅ t Ξ³ \varepsilon^\gamma_t Ξ΅ t Ξ³ β is a \reftext{def:probability-space-random-variable-2026a}{random variable}, measurable with respect to F t s y s \mathcal{F}^{\mathrm{sys}}_t F t sys β , with E [ β£ Ξ΅ t β£ p ] < β \mathbb{E}[|\varepsilon_t|^p]<\infty E [ β£ Ξ΅ t β β£ p ] < β for every natural number p β₯ 1 p\ge1 p β₯ 1 ; each map ( t , Ο ) β¦ 1 Ξ© 0 ( Ο ) Ξ΅ t Ξ³ ( Ο ) (t,\omega)\mapsto\mathbf{1}_{\Omega_0}(\omega)\varepsilon^\gamma_t(\omega) ( t , Ο ) β¦ 1 Ξ© 0 β β ( Ο ) Ξ΅ t Ξ³ β ( Ο ) is \reftext{def:measurable-function-2026a}{measurable} for the \reftext{def:product-sigma-algebra-2026a}{product Ο \sigma Ο -algebra} of the \reftext{lem:interval-lebesgue-toolkit-2026a}{trace Borel Ο \sigma Ο -algebra} on [ 0 , T ] [0,T] [ 0 , T ] and F \mathcal{F} F ; and the \textbf{filter error covariance}
Ξ t N , Ξ³ Ξ΄ = E [ Ξ΅ t Ξ³ β Ξ΅ t Ξ΄ ] ( Ξ³ , Ξ΄ β { 1 , β¦ , l } ) \Pi^{N,\gamma\delta}_t=\mathbb{E}\big[\varepsilon^\gamma_t\,\varepsilon^\delta_t\big]\qquad(\gamma,\delta\in\{1,\dots,l\}) Ξ t N , Ξ³ Ξ΄ β = E [ Ξ΅ t Ξ³ β Ξ΅ t Ξ΄ β ] ( Ξ³ , Ξ΄ β { 1 , β¦ , l })
is finite, symmetric in ( Ξ³ , Ξ΄ ) (\gamma,\delta) ( Ξ³ , Ξ΄ ) , measurable and bounded as a function of t t t , with Ξ 0 N , Ξ³ Ξ΄ = E [ s 0 Ξ³ s 0 Ξ΄ ] \Pi^{N,\gamma\delta}_0=\mathbb{E}[\mathfrak{s}^\gamma_0\mathfrak{s}^\delta_0] Ξ 0 N , Ξ³ Ξ΄ β = E [ s 0 Ξ³ β s 0 Ξ΄ β ] (the filter starting at s ^ 0 N = 0 \hat{\mathfrak{s}}^N_0=0 s ^ 0 N β = 0 ).
\textbf{(b) (Error equation.)} \reftext{def:almost-surely-2026a}{Almost surely}, for every t β [ 0 , T ] t\in[0,T] t β [ 0 , T ] , componentwise,
Ξ΅ t = s 0 + β« [ 0 , t ] ( ( E r β K ~ r E ~ r ) β Ξ΅ r + e r β K ~ r β e ~ r ) β d r + N β M t β J ~ t , \varepsilon_t=\mathfrak{s}_0+\int_{[0,t]}\Big(\big(\mathcal{E}_r-\tilde{\mathcal{K}}_r\tilde{\mathcal{E}}_r\big)\,\varepsilon_r+e_r-\tilde{\mathcal{K}}_r\,\tilde{e}_r\Big)\,dr+\sqrt{N}\,M_t-\tilde{J}_t, Ξ΅ t β = s 0 β + β« [ 0 , t ] β ( ( E r β β K ~ r β E ~ r β ) Ξ΅ r β + e r β β K ~ r β e ~ r β ) d r + N β M t β β J ~ t β ,
all integrals existing componentwise at the relevant outcomes (the integral being 0 0 0 for t = 0 t=0 t = 0 ).
\textbf{(c) (Covariance evolution.)} Define, for r β [ 0 , T ] r\in[0,T] r β [ 0 , T ] and Ξ³ , Ξ΄ β { 1 , β¦ , l } \gamma,\delta\in\{1,\dots,l\} Ξ³ , Ξ΄ β { 1 , β¦ , l } ,
X r Ξ³ Ξ΄ = E [ Ξ΅ r Ξ³ β ( e r β K ~ r e ~ r ) Ξ΄ ] + E [ ( e r β K ~ r e ~ r ) Ξ³ β Ξ΅ r Ξ΄ ] . X^{\gamma\delta}_r=\mathbb{E}\big[\varepsilon^\gamma_r\,(e_r-\tilde{\mathcal{K}}_r\tilde{e}_r)^\delta\big]+\mathbb{E}\big[(e_r-\tilde{\mathcal{K}}_r\tilde{e}_r)^\gamma\,\varepsilon^\delta_r\big]. X r Ξ³ Ξ΄ β = E [ Ξ΅ r Ξ³ β ( e r β β K ~ r β e ~ r β ) Ξ΄ ] + E [ ( e r β β K ~ r β e ~ r β ) Ξ³ Ξ΅ r Ξ΄ β ] .
All expectations below are finite, all integrands are bounded and measurable in r r r , and for every t β [ 0 , T ] t\in[0,T] t β [ 0 , T ] :
Ξ t N , Ξ³ Ξ΄ = Ξ 0 N , Ξ³ Ξ΄ + β« [ 0 , t ] ( ( ( E r β K ~ r E ~ r ) Ξ r N + Ξ r N ( E r β K ~ r E ~ r ) β€ ) Ξ³ Ξ΄ + X r Ξ³ Ξ΄ + E [ Ξ Ξ³ Ξ΄ ( Ξ£ r , Ξ± r ) ] + β Ο
= 1 l ~ K ~ r Ξ³ Ο
K ~ r Ξ΄ Ο
β E [ b ~ Ο
( Ξ£ r ) ] ) β d r . \Pi^{N,\gamma\delta}_t=\Pi^{N,\gamma\delta}_0+\int_{[0,t]}\Big(\big((\mathcal{E}_r-\tilde{\mathcal{K}}_r\tilde{\mathcal{E}}_r)\Pi^N_r+\Pi^N_r(\mathcal{E}_r-\tilde{\mathcal{K}}_r\tilde{\mathcal{E}}_r)^{\top}\big)^{\gamma\delta}+X^{\gamma\delta}_r+\mathbb{E}\big[\Theta^{\gamma\delta}(\Sigma_r,\alpha_r)\big]+\sum_{\upsilon=1}^{\tilde{l}}\tilde{\mathcal{K}}^{\gamma\upsilon}_r\tilde{\mathcal{K}}^{\delta\upsilon}_r\,\mathbb{E}\big[\tilde{b}^\upsilon(\Sigma_r)\big]\Big)\,dr . Ξ t N , Ξ³ Ξ΄ β = Ξ 0 N , Ξ³ Ξ΄ β + β« [ 0 , t ] β ( ( ( E r β β K ~ r β E ~ r β ) Ξ r N β + Ξ r N β ( E r β β K ~ r β E ~ r β ) β€ ) Ξ³ Ξ΄ + X r Ξ³ Ξ΄ β + E [ Ξ Ξ³ Ξ΄ ( Ξ£ r β , Ξ± r β ) ] + Ο
= 1 β l ~ β K ~ r Ξ³ Ο
β K ~ r Ξ΄ Ο
β E [ b ~ Ο
( Ξ£ r β ) ] ) d r .
In particular each t β¦ Ξ t N , Ξ³ Ξ΄ t\mapsto\Pi^{N,\gamma\delta}_t t β¦ Ξ t N , Ξ³ Ξ΄ β is \reftext{def:continuity-closed-interval-c54-2026b}{continuous}.
\textbf{(d) (Uniform moment bounds.)} There is a real C 1 β₯ 0 C_1\ge0 C 1 β β₯ 0 , determined by l l l , l ~ \tilde{l} l ~ , m m m , T T T , the rate bounds B B B and B ~ \tilde{B} B ~ , the derivative bounds K K K and K ~ \tilde{K} K ~ (of the \reftext{def:c2-transition-rate-extension-2026a}{transition-rate} and \reftext{def:c2-observation-rate-extension-2026a}{observation-rate} extensions respectively), and the entry bounds of the continuous matrix families E \mathcal{E} E , B \mathcal{B} B , E ~ \tilde{\mathcal{E}} E ~ , G \mathcal{G} G , K ~ \tilde{\mathcal{K}} K ~ on [ 0 , T ] [0,T] [ 0 , T ] --- in particular the same for every N N N , every driving system, and every projected solution --- such that
sup β‘ t β [ 0 , T ] ( E [ β£ s t β£ 4 ] + E [ β£ s ^ t N β£ 4 ] + E [ β£ Ξ΅ t β£ 4 ] + E [ β£ a t β£ 4 ] ) Β β€ Β C 1 β ΞΊ 0 , \sup_{t\in[0,T]}\Big(\mathbb{E}\big[|\mathfrak{s}_t|^4\big]+\mathbb{E}\big[|\hat{\mathfrak{s}}^N_t|^4\big]+\mathbb{E}\big[|\varepsilon_t|^4\big]+\mathbb{E}\big[|\mathfrak{a}_t|^4\big]\Big)\ \le\ C_1\,\kappa_0 , t β [ 0 , T ] sup β ( E [ β£ s t β β£ 4 ] + E [ β£ s ^ t N β β£ 4 ] + E [ β£ Ξ΅ t β β£ 4 ] + E [ β£ a t β β£ 4 ] ) Β β€ Β C 1 β ΞΊ 0 β ,
and consequently, using E [ β£ β
β£ 2 ] β€ 1 + E [ β£ β
β£ 4 ] \mathbb{E}[|\cdot|^2]\le1+\mathbb{E}[|\cdot|^4] E [ β£ β
β£ 2 ] β€ 1 + E [ β£ β
β£ 4 ] and ΞΊ 0 β₯ 1 \kappa_0\ge1 ΞΊ 0 β β₯ 1 , also sup β‘ t ( E [ β£ s t β£ 2 ] + E [ β£ s ^ t N β£ 2 ] + E [ β£ Ξ΅ t β£ 2 ] + E [ β£ a t β£ 2 ] ) β€ ( 4 + C 1 ) β ΞΊ 0 \sup_t(\mathbb{E}[|\mathfrak{s}_t|^2]+\mathbb{E}[|\hat{\mathfrak{s}}^N_t|^2]+\mathbb{E}[|\varepsilon_t|^2]+\mathbb{E}[|\mathfrak{a}_t|^2])\le(4+C_1)\,\kappa_0 sup t β ( E [ β£ s t β β£ 2 ] + E [ β£ s ^ t N β β£ 2 ] + E [ β£ Ξ΅ t β β£ 2 ] + E [ β£ a t β β£ 2 ]) β€ ( 4 + C 1 β ) ΞΊ 0 β and A + A 4 β€ 2 T ( 4 + C 1 ) β ΞΊ 0 \mathcal{A}+\mathcal{A}_4\le2T(4+C_1)\,\kappa_0 A + A 4 β β€ 2 T ( 4 + C 1 β ) ΞΊ 0 β .
\textbf{(e) (Covariance comparison.)} There is a real C β₯ 0 C\ge0 C β₯ 0 , determined by the same data as C 1 C_1 C 1 β together with the entry bounds of Ξ \Pi Ξ and of ( Ξ ~ β ) β 1 (\tilde{\Theta}^\star)^{-1} ( Ξ ~ β ) β 1 on [ 0 , T ] [0,T] [ 0 , T ] --- again not depending on N N N , on the driving system, or on the solution --- such that for every t β [ 0 , T ] t\in[0,T] t β [ 0 , T ] and all Ξ³ , Ξ΄ β { 1 , β¦ , l } \gamma,\delta\in\{1,\dots,l\} Ξ³ , Ξ΄ β { 1 , β¦ , l } :
β£ Ξ t N , Ξ³ Ξ΄ β Ξ t Ξ³ Ξ΄ β£ Β β€ Β C β ( max β‘ Ξ³ β² , Ξ΄ β² β { 1 , β¦ , l } β£ E [ s 0 Ξ³ β² s 0 Ξ΄ β² ] β Ξ 0 Ξ³ β² Ξ΄ β² β£ Β + Β N β 1 / 2 β ΞΊ 0 ) . \big|\Pi^{N,\gamma\delta}_t-\Pi^{\gamma\delta}_t\big|\ \le\ C\,\Big(\max_{\gamma',\delta'\in\{1,\dots,l\}}\big|\mathbb{E}\big[\mathfrak{s}^{\gamma'}_0\mathfrak{s}^{\delta'}_0\big]-\Pi^{\gamma'\delta'}_0\big|\ +\ N^{-1/2}\,\kappa_0\Big) . β Ξ t N , Ξ³ Ξ΄ β β Ξ t Ξ³ Ξ΄ β β Β β€ Β C ( Ξ³ β² , Ξ΄ β² β { 1 , β¦ , l } max β β E [ s 0 Ξ³ β² β s 0 Ξ΄ β² β ] β Ξ 0 Ξ³ β² Ξ΄ β² β β Β + Β N β 1/2 ΞΊ 0 β ) .