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Independent perturbed-observation reference members follow the Kalman filter

Statement

Assume AC and the finite-horizon linear-Gaussian model of Linear-Gaussian state-space models with independent noises, with Rk≻0 for 1≤k≤T. Fix the observation values y1:T. For each N, initialize UN,ia,0 iid with the model's N(m0,P0) prior. At each time use independent per-member noises qN,ik∼N(0,Qk) and ηN,ik∼N(0,Rk), independent across i,k and from the preceding ensemble, and form UN,if,k=FkUN,ia,k−1+qN,ik,UN,ia,k=UN,if,k+Kk(yk+ηN,ik−HkUN,if,k), where Kk=Pk∣k−1HkT(HkPk∣k−1HkT+Rk)−1 is the deterministic gain from Exact linear-Gaussian Kalman filter. Then, for every k≤T, the analysis members UN,1a,k,…,UN,Na,k are iid with law N(mk∣k,Pk∣k), the exact Kalman filtering law at the fixed data y1:k.

Facts & Assumptions

Given: AC, the finite-horizon linear-Gaussian model, Rk≻0, and the independent per-member initialization and perturbations in the Statement.

[A1]

AC is the axiom required by the multivariate-normal and Kalman suppliers. The Axiom of Choice

[F1]

The state and observation equations are affine with mutually independent Gaussian initial, process, and observation noises; their covariance matrices may be positive semidefinite. Linear-Gaussian state-space models with independent noises

[F2]

A finite independent stack of multivariate normal vectors is jointly multivariate normal, including for singular covariance blocks. A finite stack of independent Gaussian vectors is jointly Gaussian

[F3]

The Kalman algorithm predicts mf=Fkm, Pf=FkPFkT+Qk and updates by ma=mf+Kk(yk−Hkmf), Pa=Pf−KkSkKkT. Exact linear-Gaussian Kalman filter

[F4]

Under the stated model and positive-definite innovation matrices, these recursions are exact Gaussian conditional laws at every observation history. The finite-horizon linear-Gaussian Kalman filter is exact

[F5]

A multivariate normal law permits singular positive-semidefinite covariance and is closed under the defining affine projections. Multivariate normal law, including singular covariance

Proof

Given: The hypotheses in the Statement.

1.1A1F1F5givenbase

At k=0, the analysis members are iid with law N(m0,P0) by their initialization, so the claim holds at the base time.

2.1A1F1F2F5givenstep 1.1IH

Assume the induction hypothesis: the members at time k−1 are iid with law N(mk−1∣k−1,Pk−1∣k−1). Each forecast is an affine image of the independent Gaussian pair (UN,ia,k−1,qN,ik). By [F2] the pair is jointly Gaussian; every scalar projection of its affine image is a scalar Gaussian projection, so [F5] makes the forecasts iid Gaussian with mean mf=Fkmk−1∣k−1 and covariance Pf=FkPk−1∣k−1FkT+Qk.

3.1F1F2F3F5step 2.1algebra

Since Pf⪰0 and Rk≻0, S=HkPfHkT+Rk≻0, so K=PfHkTS−1 is defined. The independent Gaussian pair (UN,if,k,yk+ηN,ik) and [F2] show that UN,ia,k=AUN,if,k+K(yk+ηN,ik), with A=I−KHk, is Gaussian. Its mean is mf+K(yk−Hkmf) and its covariance is APfAT+KRkKT=Pf−KSKT, because KSKT=PfHkTKT=KHkPf. These are precisely the Kalman update parameters in [F3].

4.1A1F1F4step 1.1step 2.1step 3.1

For distinct member indices the pairs of forecast and perturbed observation are independent by the input independence and the induction hypothesis; applying the same deterministic affine update separately to each pair preserves independence. Therefore the updated members are iid with the Gaussian law from step 3.1. By [A1] and [F4] that law is the exact filtering law at the fixed data.

5.1step 1.1step 4.1discharge-induction: step 1.1step 4.1∎

The initialization in step 1.1 is the base case, and step 4.1 proves the claim at time k from the induction hypothesis at time k−1. Induction therefore gives the asserted iid exact filtering law for every k≤T.

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