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HAL Id: hal-00977630

https://hal.inria.fr/hal-00977630v2

Submitted on 11 Apr 2014

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tracking: Numerical experiments

Johann Fichou, François Le Gland, Laurent Mevel

To cite this version:

Johann Fichou, François Le Gland, Laurent Mevel. Particle-based methods for parameter estimation and tracking: Numerical experiments. [Research Report] PI 1604, 2004. �hal-00977630v2�

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I

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I S

A

INST ITUT D

E R ECHE

RC HEE

N IN

FORMAT IQU

EET SYS

TÈMES A

ATOIRE S

P U B L I C A T I O N I N T E R N E

No

I R I S A

CAMPUS UNIVERSITAIRE DE BEAULIEU - 35042 RENNES CEDEX - FRANCE

ISSN 1166-8687

1604

PARTICLE–BASED METHODS

FOR PARAMETER ESTIMATION AND TRACKING : NUMERICAL EXPERIMENTS

JOHANN FICHOU, FRANÇOIS LE GLAND, LAURENT MEVEL

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Particlebased Methods

for Parameter Estimation and Tracking : Numerical Experiments

Johann Fichou

*

, FrançoisLe Gland

*

, Laurent Mevel

*

Thème 4 Simulation et optimisation de systèmes complexes

Projet SIGMA2 (σ2)

Publication interne n1604 Février 2004 59 pages

Abstract: The purpose of this work is to obtain as much intuition as possible, through numerical experiments in a simple case where exact solutions are explicitly available, about the particle approximation of nite signed measures. A prototypical example of a nite signed measure is the derivative, w.r.t. a parameter of the model, of some probability distributions related with a hidden Markov chain. This includes prior, prediction, ltering probability distributions, etc. Two points of view are considered here, to feel the quality of the approximation, at least in a qualitative manner :

(i) how accurate is the particle approximation of the nite signed measure, in view of an histogram representation of the weighted particle system ?

(ii) considering the loglikelihood function and the score function, how close is the approximate expression provided by the particle approximation to the exact expression ?

These two questions seem closely related, however the numerical experiments presented in this work show that one of the two particle approximation schemes fails to satisfy the rst criteria (quality of the approximation of the nite signed measure), and that both schemes satisfy the second criteria (quality of the approximation of the statistics).

Key-words: monitoring, mechanical system, modal parameter, recursive maximum likelihood, estimation, tracking, particle lter, linear tangent particle lter.

(Résumé : tsvp) Ce travail correspond au rapport nal d'un stage eectué dans le cadre du DESSMathématiques Appliquésde l'université de Rennes 1, dans la lièreStatistique. Il a été soutenu en partie par le projet Eurêka 2419Flight Test Easy(FLITE).

*IRISA / INRIA, Campus de Beaulieu, 35042 RENNES Cédex, France. {legland,lmevel}@irisa.fr

Centre National de la Recherche Scientifique Institut National de Recherche en Informatique (UPRESSA6074) Université de Rennes 1 – Insa de Rennes et en Automatique – unité de recherche de Rennes

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pour l'estimation et la poursuite de paramètres : Expériences numériques

Résumé : L'objectif de ce travail est de mieux comprendre l'approximation particulaire de mesures signées nies, au travers de quelques expériences numériques menées dans un cas simple où les solutions exactes sont connues de manière explicite. Un exemple typique de mesure signée nie est la dérivée, par rapport à un paramètre du modèle, de distributions de probabilité associées à une chaîne de Markov cachée.

Cela inclut la distribution a priori, le prédicteur, le ltre, etc. Deux points de vue sont considérés ici pour évaluer la qualité de l'approximation, au moins dans un sens qualitatif :

quelle est la précision de l'approximation particulaire de la mesure signée nie, au vu d'une représen- tation sous forme d'histogramme du système de particules pondérées ?

si on s'intéresse seulement à la fonction de logvraisemblance ou à la fonction score, quel est l'écart entre l'expression fournie par l'approximation particulaire et l'expression exacte de ces quantités ? Ces deux questions sont évidemment liées, mais les expériences numériques présentées dans ce travail mon- trent que l'un des deux schémas d'approximation particulaire proposés ne répond pas de manière satisfaisante au premier critère (qualité de l'approximation de la mesure signée nie), et que les deux schémas proposés donnent une bonne approximation pour le second critère (précison de l'approximation des statistiques).

Mots clés : surveillance, système mécanique, paramètre modal, maximum de vraisemblance récursif, estimation, poursuite, ltre particulaire, ltre particulaire linéaire tangent.

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1 Introduction

The purpose of this work is to obtain as much intuition as possible, through numerical experiments in a simple case where exact solutions are explicitly available, about the particle approximation of nite signed measures. A prototypical example of a nite signed measure is the derivative, w.r.t. a parameter of the model, of some probability distributions related with a hidden Markov chain. This includes prior, prediction, ltering probability distributions, etc. Two points of view are considered here, to feel the quality of the approximation, at least in a qualitative manner :

(i) how accurate is the particle approximation of the nite signed measure, in view of an histogram representation of the weighted particle system ?

(ii) considering the loglikelihood function and the score function, how close is the approximate expression provided by the particle approximation to the exact expression ?

These two questions seem closely related, however the numerical experiments presented in this work show that one of the two particle approximation schemes fails to satisfy the rst criteria (quality of the approximation of the nite signed measure), and that both schemes satisfy the second criteria (quality of the approximation of the statistics).

The initial motivation for this work was provided by an application to monitoring the integrity of struc- tural and mechanical systems. Detecting and localizing damages for monitoring the integrity of structural and mechanical systems is a topic of growing interest, due to the aging of many engineering constructions and machines and to increased safety norms. Automatic global vibrationbased monitoring techniques turn out to be useful alternatives to visual inspections or local non destructive (e.g. ultrasonic) evaluations performed manually.

Health monitoring techniques based on processing vibration measurements basically handle two types of characteristics: the structural parameters (mass, stiness, exibility, damping) and the modal parameters (modal frequencies, and associated damping values and modeshapes), see [22, 9, 21]. A central question for monitoring is to compute changes in those characteristics and to assess their signicance. For the frequencies, crucial issues are then: how to compute the changes, to assess that the changes are signicant, to handle correlations among individual changes. A related issue is how to compare the changes in the frequencies obtained from experimental data with the sensitivity of modal parameters obtained from an analytical model.

Furthermore, it has been widely acknowledged that changes in frequencies bear useful information for damage detection.

Our contribution in this work is to design a particle ltering method to track the modal parameters.

Particle ltering techniques are a set of powerful and versatile simulationbased methods to perform optimal state estimation in nonlinear nonGaussian statespace models, and we consider here an approach combin- ing particle ltering and gradient algorithm to perform recursive maximum likelihood parameter estimation and tracking. In the next section, the modeling issues are introduced and some key parameterizations are discussed. Section 3 details the particle approximation mechanisms. Section 4 is devoted to particle approx- imation of nite signed measures, with numerical experiments. In Section 5, the particle implementation of the recursive maximum likelihood (RML) algorithm is described.

2 Mechanical model

2.1 Dynamical model and structural parameters

It is assumed that the behavior of the mechanical system can be described by a stationary linear dynamical system, and that, in the frequency range of interest, the input forces can be modeled as a non-stationary white noise. This results in :

MZ¨(t) +CZ˙(t) +KZ(t) = ν(t)

Y(t) = LZ(t) (1)

where t denotes continuous time, M, C and K are the mass, damping and stiness matrices respectively, the (high dimensional) vectorZ collects the displacements of the degrees of freedom of the structure, the PI n1604

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external (non measured) forceν is modeled as a nonstationary white noise with timevarying covariance matrixQν(t), measurements are collected in the (often, low dimensional) vectorY, and the matrixLindicates which components of the state vector are actually measured, i.e. where the sensors are located.

The modes or eigenfrequencies, denoted generically byµ, are solutions of :

det(µ2M +µ C+K) = 0. (2)

The frequencyf and the damping coecientdare recovered from a continuous eigenvalueµthrough :

f = (µ)

2π and d=−ℜ(µ). (3)

Some comments are in order on parameterizations of interest for damage detection and localization. Since a local damage in the structure reduces the stiness and increases the damping, many damage detection techniques have been proposed which monitor the stiness matrixK. Monitoring its inverse K−1, namely the exibility matrix, has proven more tractable and computationally feasible [22, 13, 5]. In some cases, other structural parameterizations such as volumic mass and Young elasticity modulus may be preferable [14, 22].

Also, several methods in the literature are based on a transmissibility matrix [21, 23], which involves the processing of inputoutput data. However, in the case of non measured input excitation, processing output only data is mandatory [17, 3]. On the other hand, a reduced stiness and an increased damping result in decreased natural frequencies. Thus, monitoring the modal parameters is relevant.

2.2 Statespace model and parameterization

Sampling model (1) at rate1/∆yields the discrete time model in state space form [12, 18] :

Xk+1 = F Xk+Wk

Yk = H Xk (4)

where the state and the output are :

Xk =

Z(k∆) Z˙(k∆)

and Yk=Y(k∆) , (5) the state transition and observation matrices are :

F = exp(A∆) where A=M0−1K MI−1C and

H= L 0

. (6)

The measurement equation in (4) withH as in (6) implicitly assumes that the available sensors measure the (relative) displacements of the degrees of freedom themselves. The nature of the sensors used only inuences the observation matrixH. In (4), the unmeasured state noise{Wk, k0} is assumed to be a zeromean Gaussian white noise, with covariance matrix :

Qk

=E[WkWk] =

Z (k+1) ∆ k

exp(A s)Q(s) exp(Ae s)ds

and

Q(s) =e

0 0 0 M−1Qν(s)M−∗

.

The stateX and the observed outputY have dimensions2mandrrespectively, withr(often much) smaller than2min practice.

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Letλbe the modes of the state transition matrixF, namely :

det (Fλ I) = 0. (7)

The continuous modesµin (2) can be deduced from the discrete modesλin (7) using :

exp(∆µ) =λ .

The frequencyf and the damping coecientdare recovered from a discrete eigenvalueλthrough :

f = arg(λ)

2π and d=1 log|λ| . (8)

Because of the structure of the state in (5), the discrete modesλare pairwise complex conjugate. IfF andH are unknown matrices but we are able to track the coecients of these two matrices, then it is easy to obtain the frequency and the damping coecient using (8).

Remark 2.1. If we suppose noisy measurements, the model becomes :

Xk+1 = F Xk+Wk

Yk = H Xk+Vk (9)

where{Vk, k0}is an unmeasured Gaussian white noise with zero mean. It is essential to note that, with this assumption, the measurement noise does not aect the eigenstructure of (9).

3 About particle approximation

In this section, we will rst detail particle approximation of the lter and the derivative of the lter w.r.t. the parameter of interest, following [6, 16]. Then, we will see dierent resampling schemes and their eciency.

3.1 Hidden Markov model

The state sequence{Xk, k0}is a Markov chain taking values in the spaceE=Rd, with transition kernel

Q(x, dx)(which is assumed time independent for simplicity), i.e.

P[Xk+1dx|Xk=x] =Q(x, dx).

The kernel Q(x, dx) could depend on a parameter, that should be either estimated, or monitored (i.e.

changes w.r.t. a nominal value should be detected), however the dependence w.r.t. the parameter is not written explicitly, so as to avoid intricated notations. The following assumption is made

It is easy to simulate a r.v. X with probability distribution Q(x, dx), even though the analytical expression of the kernel Q(x, dx) is not known, or is so complicated that it is pratically impossible to compute such integrals as

Q φ(x) = Z

E

Q(x, dx)φ(x) or Q µ(dx) =Z

E

µ(dx)Q(x, dx).

The state sequence {Xk, k 0} is not observed, but instead an observation sequence {Yk, k 0} is available, which has the following property : given the hidden states{Xk, k0}, the observations{Yk, k 0} are mutually independent, and the conditionnal probability distribution of Yk (which is assumed time independent for simplicity) depends only on the hidden stateXk at the same time instant, and by denition

P[Ykdy|Xk=x] =g(x, y)λ(dy) and Ψk(x) =g(x, Yk).

Notice that whenx varies, all the conditionnal probability distributionsP[Yk dy |Xk =x] are assumed absolutely continuous w.r.t. a nonnegative measureλ(dy)which does not depend onx(with densitiesg(x, y) which do depend onx).

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Example This memoryless channel assumption is satised for instance in the case where the hidden state is observed in an additive white noise sequence, not necessarily Gaussian, i.e. in our model where the observationYk is related to the hidden stateXk by the relation

Yk =H Xk+Vk ,

where{Vk, k0}is a white noise sequence (i.e. a sequence of mutually independent r.v.'s) with probability distribution q(v)dv (which is assumed time independent for simplicity), independent of {Xk, k 0}. In this case

P[Ykdy|Xk=x] =q(yH x)dy and Ψk(x) =q(YkH x).

3.2 Particle approximation of the lter

Given observations, the objective is to estimate the hidden states, and to this eect the probability distri- butions

µk(dx) =P[Xkdx|Y0,· · · , Yk] and µk|k−1(dx) =P[Xkdx|Y0,· · · , Yk−1],

are introduced. The evolution of the sequence {µk, k0}taking values in the space of probability distri- butions onE, is very easily described by the following steps

µk−1

prediction

−−−−−−−−−→µk|k−1=Q µk−1

correction

−−−−−−−−−→µk= Ψk·µk|k−1 ,

where

µk|k−1(dx) =Q µk−1(dx) = Z

E

µk−1(dx)Q(x, dx),

can happen to be dicult (if not just impossible) to compute, and where· denotes the projective product, i.e.

µk(dx) = Ψk·µk|k−1(dx) = Ψk(x)µk|k−1(dx) hµk|k−1,Ψki .

In view of the key assumption that it is on the other hand easy to simulate r.v.'s with probability distri- butionQ(x, dx), the idea is to approximate the predictorµk|k−1 with the empirical probability distribution associated with anNsample, i.e.

µk|k−1µNk|k−1= 1 N

XN i=1

δξk|k−1i .

This approximation is completely characterized by the set {ξk|k−1i , i = 1,· · ·, N} of particles, and the algorithm is completely described by the mechanism which builds{ξik+1|k, i= 1,· · · , N}from {ξik|k−1, i= 1,· · · , N}. This mechanism is as follows :

(i) the correction step is applied exactly toµNk|k−1, which results in

µNk = Ψk·µNk|k−1= XN i=1

Ψkk|k−1i )δξk|k−1i XN

j=1

Ψkk|k−1j )

= XN

i=1

ωikδξik|k−1 ,

i.e. particles {ξk|k−1i , i = 1,· · ·, N} are now weighted, with weights {ωki, i = 1,· · · , N} which are more heavy for those particles which are more consistent with the current observationYk,

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(ii) instead of trying to compute Q µNk, the following particle approximation

µNk+1|k=SN(Q µNk ) = 1 N

XN i=1

δξk+1|ki ,

is used, where theNsample{ξk+1|ki , i= 1,· · ·, N}has precisely the probability distributionQ µNk, i.e.

N independent r.v.'s are simulated with common probability distributionQ µNk, which can be achieved in the following manner : independently for anyi= 1,· · · , N

ξki µNk (dx) = easy, since the probability distributionµNk is discrete,

ξk+1|ki Q(ξki, dx) = easy, by assumption.

3.3 Linear tangent kernel / extended kernel, etc.

If the transition kernelQ(x, dx)depends on a parameter, then the lterµk depends also on the parameter, and one would like to compute the linear tangent lter wk, i.e. the derivative of the lter µk w.r.t. the parameter. To this end, one needs rst to study the linear tangent kernelΓ(x, dx), i.e. the derivative of the transition kernelQ(x, dx)w.r.t. the parameter, and the following assumption is made

Assumption AC : The following probabilistic representation holds for the linear tangent kernelΓ(x, dx)

Γφ(x) = Z

E

Γ(x, dx)φ(x) =E[φ(Xk+1) Ξk+1|Xk=x],

where {(Xk,Ξk), k0} is a Markov chain taking values in the product spaceE×F, such that

P[Xk+1dx,Ξk+1 ds |Xk=x,Ξk =s]

=P[Xk+1dx,Ξk+1ds|Xk =x] =K(x, dx, ds).

The following assumption, which extends the similar assumption introduced in Section 3.1, is made

It is easy to simulate a r.v. (X,Ξ) with probability distribution K(x, dx, ds), even though the analytical expression of the kernel K(x, dx, ds) is not known, or is so complicated that it is pratically impossible to compute such integrals as

Γφ(x) = Z

E×F

sφ(x)K(x, dx, ds) or Γµ(dx) =Z

E×F

µ(dx)sK(x, dx, ds).

Example In our model, the Markov chain{Xk, k0} taking values inE=Rd, is dened by

Xk+1=F Xk+Wk ,

where only the matrixF depends on the parameter, and where {Wk, k0} is a sequence of independent r.v.'s taking values in Rd with probability distributionp(w)dw (coecients are assumed time independent for simplicity). For anyxRd, the transition kernelQ(x, dx)is given by

Q(x, dx) =p(xF x)dx ,

and one can show directly that

Γ(x, dx) =p(xF x) ∂F

∂θ x dx = p

p (xF x) ∂F

∂θ x Q(x, dx).

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It follows that

Γφ(x) = Z

E

Γ(x, dx)φ(x) = Z

E

φ(x) p

p (xF x) ∂F

∂θ x Q(x, dx)

= E[φ(Xk+1) p

p (Xk+1F Xk) ∂F

∂θ Xk|Xk=x],

i.e. Assumption AC is satised, with

Ξk+1 =p

p (Wk)∂F

∂θ Xk .

Notice that in the above example, the r.v. Ξk+1 depends only on (Xk, Wk), in which case it does not seem necessary to simulate Ξk+1 in addition to Wk. This apparently very particular situation is actually very general, as the following result shows.

Lemma 3.1. Under Assumption AC

Γ(x, dx) =I(x, x)Q(x, dx),

with

I(x, x) =E[Ξk+1|Xk=x, Xk+1=x],

for any x, x E.

Proof. For any probability distributionµonE, and any pair B, B of Borel subsets ofE

Eµk+11(Xk+1B, Xk B)] = Z

B×B

E[Ξk+1|Xk=x, Xk+1=x]µ(dx)Q(x, dx),

and

Eµk+11(Xk+1 B)1(XkB)] = Z

B

E[Ξk+11(Xk+1B)|Xk =x]µ(dx)

= Z

B

Γ(x, B)µ(dx),

hence takingB =Eyields

Z

E

Γ(x, B)µ(dx) = Z

E{ Z

B

E[Ξk+1|Xk=x, Xk+1=x]Q(x, dx)}µ(dx),

and since the probability distributionµis arbitrary, it holds

Γ(x, B) = Z

B

E[Ξk+1|Xk =x, Xk+1 =x]Q(x, dx),

which proves the result.

By denition

Γφ(x) = Z

E×F

φ(x)sK(x, dx, ds) and Q φ(x) =Z

E×F

φ(x)K(x, dx, ds),

hence

Γ(x, dx) = Z

F

sK(x, dx, ds) and Q(x, dx) =Z

F

K(x, dx, ds).

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On the product spaceE×E×F, dene the projectionπ0 : (x, x, s)7−→xon the (rst) spaceE, the projection π : (x, x, s)7−→ x on the (second) space E and the projection πF : (x, x, s) 7−→s on the auxiliary spaceF. For any probability distributionµon the spaceE, the probability distributionµK is dened on the product spaceE×E×F by

K)(dx, dx, ds) =µ(dx)K(x, dx, ds).

It follows that

Q µ(dx) = Z

E×F

µ(dx)K(x, dx, ds) = (µK)π−1(dx),

and

Γµ(dx) = Z

E×F

µ(dx)sK(x, dx, ds)

= Z

E×F

πF(x, x, s) (µK)(dx, dx, ds) = (πFK))π−1(dx),

and if the nite signed measurewis absolutely continuous w.r.t.µ, then

Q w(dx) = Z

E×F

w(dx)K(x, dx, ds)

= Z

E×F

dw

(x)µ(dx)K(x, dx, ds)

= Z

E×F

(dw

π0)(x, x, s) (µK)(dx, dx, ds) = ((dw

π0) (µK))π−1(dx),

i.e.

Q µ= (µK)π−1 and Γµ= (πFK))π−1 ,

and

(wµ = Q w= ((dw

π0) (µK))π−1).

Lemma 3.2. Under Assumption AC, Γµ Q µ for any probability distribution µ on E, with Radon Nikodym derivative (which depends on µ)

d(Γµ)

d(Q µ)(x) =Eµn+1|Xn+1=x].

Proof. For any Borel subsetB ofE, it holds

Γµ(B) = Z

E

µ(dx) Γ(x, B)

= Z

E

µ(dx)E[Ξk+11(Xk+1B)|Xk =x]

= Eµk+11(Xk+1B)] = Z

B

Eµk+1|Xk+1=x]Q µ(dx),

henceΓµis a signed measure, absolutely continuous w.r.t. Q µ, with RadonNikodym derivative

d(Γµ)

d(Q µ)(x) =Eµk+1 |Xk+1=x]

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For completeness, the following elementary property is recalled

Lemma 3.3. If the nite signed measure w is absolutely continuous w.r.t. the probability distribution µ, thenQ wQ µ, with RadonNikodym derivative

d(Q w)

d(Q µ)(x) =Eµ[dw

(Xk)|Xk+1=x].

Proof. For any Borel subsetB ofE, it holds

Q w(B) = Z

E

w(dx)Q(x, B)

= Z

E

dw

(x)µ(dx)Q(x, B)

= Eµ[dw

(Xk)1(Xk+1B)] = Z

BEµ[dw

(Xk)|Xk+1=x]Q µ(dx),

henceQ wis a signed measure, absolutely continuous w.r.t.Q µ, with RadonNikodym derivative

d(Q w)

d(Q µ)(x) =Eµ[dw

(Xk)|Xk+1=x]

The explicit expression of the RadonNikodym derivatives will not be used in the sequel : only the qualitative properties

ΓµQ µ and (wµ = Q wQ µ),

will be used.

By denition

Fk(µ)w= Ψkw

hµ,Ψkihw,Ψki hµ,Ψki

Ψkµ hµ,Ψki ,

is the derivative at pointµand in the directionw, of the mappingµ7−→Ψk·µ. The following elementary property holds

Lemma 3.4. If the nite signed measure w is absolutely continuous w.r.t. the probability distribution µ, thenFk(µ)wΨk·µ, with RadonNikodym derivative

d(Fk(µ)w)

d(Ψk·µ) (x) = dw

(x)− hΨk·µ,dw i.

3.4 Particle approximation of some nite signed measures

With the notations of the previous section, it easily seen that the probability distributionQ µand the nite signed measuresΓµandQ w can be put in the general form(rK))π−1 for some appropriate choice of the weight function r, namely r 1, r = πF and r = dw π0 respectively. The weighted particle approximation of a nite signed measure of the general formrK)is dened by

rK)r SNK) = 1 N

XN i=1

r(ξ0i, ξi,Ξi)δ

0i, ξi,Ξi),

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where the Nsample {ξ0i, ξi,Ξi, i = 1,· · · , N} has precisely the probability distribution µK, i.e. one simulate N independent r.v.'s with common probability distribution µK, which can be achieved in the following manner : independently for anyi= 1,· · ·, N

ξ0i µ(dx) and i,Ξi)K(ξ0i, dx, ds),

and the corresponding particle approximation for the marginal measure(r(Kµ))π−1 is dened by

(rK))π−1(r SNK))π−1= 1 N

XN i=1

r(ξi0, ξi,Ξi)δξi .

In particular for the weight functionsr1,r=πF andr=dw π0, it holds

Q µ= (µK)π−1 1 N

XN i=1

δξi ,

Γµ= (πFK))π−1 1 N

XN i=1

Ξiδξi ,

and

Q w= ((dw

π0) (µK))π−1 1 N

XN i=1

dw

0i)δξi ,

respectively. For any test functionφdened onE, it holds

E| 1 N

XN i=1

r(ξi0, ξi,Ξi)φ(ξi)− h(rK))π−1, φi |

1

N { Z

E×E×F|φ(x)|2|r(x, x, s)|2µ(dx)K(x, dx, ds)}1/2

1

N { Z

E×E×F|r(x, x, s)|2µ(dx)K(x, dx, ds)}1/2kφk,

and in particular for the weight functionsr1,r=πF andr= dw π0, it holds

sup

kφk=1E| 1 N

XN i=1

φ(ξi)− hQ µ, φi | ≤ 1

N ,

sup

kφk=1E| 1 N

XN i=1

Ξi φ(ξi)− hΓµ, φi | ≤ 1

N {sup

x∈E

Z

E×F|s|2K(x, dx, ds)}1/2,

and

sup

kφk=1E| 1 N

XN i=1

dw

0i)φ(ξi)− hQ w, φi | ≤ 1

N { Z

E|dw

(x)|2µ(dx)}1/2 ,

respectively.

PI n1604

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