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Working Paper

On the Modified Maximum Principle in

Estimation Problenis for Uncertain Systems

T. F. Filippova

WP-92-032 April 1992

FflIIASA

International Institute for Applied Systems Analysis o A-2361 Laxenburg o Austria

kd:

Telephone: +43 2236 715210 o Telex: 079 137 iiasa a o Telefax: +43 2236 71313

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On the Modified Maximum Principle in

Estimation Problems for Uncertain Systems

T. F. Filippova

WP-92-032 April 1992

Working Papers are interim reports on work of the International Institute for Applied Systems Analysis and have received only limited review. Views or opinions expressed herein do not necessarily represent those of the Institute or of its National Member Organizations.

r!IIASA

International Institute for Applied Systems Analysis CI A-2361 Laxenburg Austria 8.8. Telephone: +43 2236 715210 o Telex: 079 137 iiasa a Telefax: +43 2236 71313

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Foreword

One of the principe features of modern modelling techniques for uncertain systems is to create a theory that would allow effective computation and graphic visualization. This requires a reconsideration of many previous schemes and the introduction of new insights. The present paper is written precisely in this context. It deals with estimation problems for uncertan dynamic models subjected t o on line measurements. The estimation scheme gives effective rules for solving the problem t o the end.

This paper was written under cooperation with IIASA, delivered a t an SDS workshop and finalized during the author's visit t o Laxenburg.

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Contents

1 Introduction

2 Problem Statement. Basic Definitions and Assumptions 3 Approximation of the Lagrangians

4 The Maximum Principle 5 Dynamic Relations

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On the Modified Maximum Principle in

Estimation Problems for Uncertain Systems

T. F. Filippova

Abstract

The present report is devoted to the problems of estimating the state of a linear dynamic system on the basis of on-line observation. It is assumed that the disturbances in the system inputs and in the current measurements are uncertain, a set-membership description of their values being only given in advance.

A considerable number of problems concerning systems of the above type are covered by the theory of control and observation under uncertainty conditions [I-31. The main problems of this paper deal with the description of certain informational domains that are consistent with the results of available measurements of the state space variables [3-51. Here we consider the case when the disturbances in the system dynamics and in the observation equation are subjected to instantaneous (or "geometric") constraints.

One approach to the problem based on a n imbedding procedure of the primary prob- lem into a n auxiliary one of linear-quadratic estimation theory is given in the paper. The proposed procedure involves certain quadratic forms to bound the uncertainties in the mod- ified problem. This method allows one to derive an appropriate maximum principle that is satisfied by system trajectories leading to boundary points of the informational domain.

1 Introduction

The topic of this paper is motivated by problems of estimation and control of uncertain dynamic processes described by ordinary differential equations or differential inclusions [I-81. Within the frame of linear models for system dynamics and observation mode

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we study some problems of estimating the phase vectors x(t) of a controlled process (1.1)- (1.2) that operates under imperfect information in the inputs or in the system parameters {xo, v(-), w(.)). The problems considered here are purely deterministic. It means that there is no statistical data for the unknown disturbances, the only information on these being the knowledge of some constraints on their admissible values.

One of the main steps t o solve the estimation problem for uncertain system is the construction in the phase space of the so-called informational domains [3,5,6]. These domains include the unknown actual states of the system and consist of all the phase vectors t h a t are compatible with the results of measurements. It is well known how t o describe the informational domains for systems with squarely bounded uncertain parameters and input functions (in this case, the informational domains are ellipsoids [3]). But, when the unknown values of system disturbances are restricted instantaneously the solution t o the problem under discussion is rather complicated.

The method proposed here to handle the latter problem is based on the approximation techniques for the Lagrange functionals. This approach outlines the possibility t o establish the "bridge"

between t h e two main estimation problems with set-membership uncertainties for quadratic and non-quadratic constraints on their values. Necessary optimality conditions corresponding to the nonlinear duality Theorem 3.3 are among the results of the paper. The theoretical background of the present investigation has been laid in [6,9].

2 Problem Statement. Basic Definitions and Assumptions

Let R k be the k-dimensional Euclidean space. For x, y E R k let x'y denote the usual inner product of x and y with the prime meaning transposition, llxll = (x'x)'/~. Also denote by convRk the set of convex compact subsets of R k by p(llX) the support function for X€convRk, l~ R k and by R k X m - the set of all kxm-matrixes.

Consider the following system

where x E R n , matrix functions A ( . ) , C ( - ) are continuous, A : [to, I91 ++ R n x n ; C : [to, 291 ++ R n X q . T h e input measurable function v(.) and the initial state x(to) = xo are assumed t o be unknown being restricted in advance by instantaneous "geometric" constraints

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where the set Xo E convRn and the continuous map Q(-) are given (Q : [to, 191 H convRq).

It is assumed further that direct observations of the current phase states x(t) are impossible, the available information of the system dynamics being generated by the equation

with continuous matrix functions G(-), F(-)(G : [to, 191 I+ R m x n ; F : [to, 291 I+ R m X r ; m

I

n).

The disturbances w(.) are also unknown and restricted by

with the continuous multivalued function W(.)(W : [to, 191 H conv R r ) given a priori.

The solution of system (2.1) that starts from a point xo a t the instant to and is generated by an admissible input v(.) will be denoted as x(. ; to, xo, .(a)).

According t o the known formula we have

x(t; to, "0, v(.)) = S(t0, t)xo+

where S(T, s ) is the matrix solution of the system

(here E is the identity matrix in R n X n ) .

Consider the problem of determining the current state x(t) of dynamic process (2.1) via on-line measurements y ( r ) (to

I

T

5

t). In order to indicate the interval [to, t] of observation time we shall use further the symbol yt(r) instead of y(r).

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Definition 2.1 [3]. The informational domain X ( t , yt(-)) of the system states compatible with measured signal yt(.) is the set of all the points (2,) in

Rn

through each of which at the instant t there passes at least one of the trajectories x(. ;to, xo, v(.)) of system (2.1)-(2.3) ( x. = x(t; to, xo, v(.)) ) that generates (together with certain w(.)) due t o equation (2.4) the same measurement yt (.).

Note that the set X ( t , yt(.)) is compact and convex in

Rn

with the support function p ( l ( X ( t , yt(.))) being determined by the following formula [3]:

where

Here LT[to, t] denotes the space of m-vector functions squarely integrable on the interval [to, t].

It should be pointed out that a direct computation due t o formulae (2.7)-(2.8) of the values of support function p(llX(t,yt(.))) is rather cumbersome procedure. Therefore, it would appear t o be of significant interest t o characterize X ( t , yt(.)) in a different manner. T h e main result of the present paper does this. The augmented Lagrangian method introduced in [6,9] for uncertain dynamic processes is developed here.

Another scheme t o prove the main approximation theorem than that in [6,9] is also suggested.

The well-known results of linear-quadratic estimation theory constitute the basis for the further consideration.

Concluding this paragraph we mention the close relations between the problem studied here and the viability one in the differential inclusions theory [10,13].

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3 Approximation of the Lagrangians

Let us set a few notations for standard function spaces. Denote by C;[to, 191 the space of all k times continuously differentiable functions f (.) ( f : [to, 191 H R n ) and CLxq [to, 191 t o be the set of all k times continuously differentiable matrix functions Z(.) ( Z : [to, 191 3 R n X Q ) . Let Cn[to, 191, C n x ' J [ t O , 191 be respectively the spaces C;[tO, 191,

to,

191 for k = 0. T h e symbol R:

stands for the cone in RQ that consists of symmetric positively definite q x q-matrices and the symbol C$k[to, 191 denotes the cone in C i X q [ t o , 191 formed by matrix functions Z ( . ) with values Z ( t ) in R t .

Let 1 be a n arbitrary vector in Rn. Consider the following set of functions displaced the { p ( . ;l,A)IA = { M , R ( - ) , H ( . ) ) E R; x C;[t0,19] x C+m[to,d])inLF[t0,19]:

where the linear operators DA : Rn H LF[to, 191 and LA : Ly[to, 61 H LF[to, 191 are defined by

( K l A(.))(t) =

jd

K ( t , r)X(r)dr, K ( t , r ) = ~ ( t ) ( ~ ( t o , t ) ~ - ' s ' ( t o , r )

+

t o

+

irr

S ( U , t ) ~ - ' ( u ) s ' ( u , r ) d u ) ~ ' ( r ) , t A 7 = min{t, r ) ,

Note that the functions { p ( . ; 1,A)) are well defined for all 1 E Rn and A = { M , R ( - ) , H ( . ) ) E

R; x C;[to, 191 x C+m[tO, 191 [14]. We shall use also the notation co@ for a convex hull. ([15]) of a function @ : Rn H R1 and the symbol r ( A ) will signify the rank of matrix A E R m X n .

Theorem 3.1 Suppose r ( G ( t ) ) = m for all t E [to,19]. Then for every 1 E Rn the following equality is true

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where @ ( I , A ) = Q s ( l , p(.; 1, A ) ) and functions Q J , p are define by (2.8), (3.1) (3.2).

To sketch the proof of this main theorem we first describe in a different ("geometric") fashion the set { p ( - ; 1, A ) ) introduced by relations (3.3). This new description will follow from a sequence of lemmas.

Lemma 3.1 For any vectors 1, b E Rn ( 1

#

0 , b

#

0 ) with positive scalar product l'b

>

0 one can present 1 = N b where N E R3, and vice versa.

Lemma 3.2 Suppose g ( - ) ,

4 ( - )

E Cn[to, 191 and for all t E [to, 191 g ( t )

#

O , 4 ( t )

#

0 . Then the following conditions are equivalent:

i. g ( t ) ' 4 ( t )

>

0 for every t E [to, 191,

ii. g ( t ) = N ( t ) 4 ( t ) for some matrix function N ( a ) E CT[to, 191.

Lemma 3.3 Assume g ( - ) E C y [ t o , 191 is such that for all t E [to, 191 ~ ( t )

#

O,g(t)

#

0 and vectors ( - g ( t ) and g ( t ) do not have the same directions. Then there exists a function

4 ( - )

E

C y [to, 191 with the properties

i. g(to)'4(to)

>

0 ,

ii. g(t)'+(t)

>

0 for every t E [to, 191, iii. g ( t ) ' $ ( t )

>

0 for every t E [to, 191.

Conversely if conditions (i)-(iii) are fulfilled for some functions g ( . ) , +(.) E C r [ t o , 191 then vectors g ( t ) , i ( t ) are not of opposite directions and g ( t )

#

O,g(t)

#

0 for every t E [to, 191 is.

Lemma 3.4 Assume g ( . ) E C?[to, 191 and g ( t )

#

O,g(t)

#

0 for every t E [to, 191. Then, the following two conditions are equivalent

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i. vectors g ( t ) , jl(t) are not directed oppositely i n Rn for every t E [ t o , d l ,

ii. there exists a triplet A = { M , R(.), H ( . ) } E R; x C;[to, d ] x C+m[to, 61 so that the following equation holds

Note that for

the latter equation coincides with the operator relation P ( - ) = (L:' o Da)l defining the function p(.) = p(.; 1 , A ) in the case A ( t ) = O , G ( t ) = E for all t E [to, dl in the system (2.1) and in the measurement equation (2.4).

From this remark and lemmas 3.1-3.4, one can conclude that for validity of the Theorem 3.1 it is sufficient t o prove the following property:

where

This last step of the proof is verified using the smoothing technique and approximation ideas as in [ l l ] .

The next result clarifies the meaning of the complicated constructions of the previous theorem.

Having fixed a triplet {x:, v*(.), w*(.)} of uncertain variables in (2.1)-(2.5) consider again the linear system (2.1), but with additional disturbances:

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y s ( t ) = G ( t ) z

+

F ( t ) w * ( t )

+

( ( t ) ,

where the unknown disturbances {C, q ( . ) , ( ( - ) ) are square-bounded jointly by

with { M , R ( . ) , H ( . ) ) E R y x CT[to, 191 x C+m[to, 19],p

>

0.

Denote Z(19, y s ( - ) ; w , A , p ) t o be the set of all the states ~ ( 1 9 ) of the system (3.5) compatible with measured signal y s ( - ) due t o (3.6); w = {z;,v*(.), w*(.)), A = { M , R ( . ) , H ( . ) ) . It is known that the setZ(19, ys(.); w , A, p ) is an ellipsoid and its center zo(19, ys(.); w , A ) does not depend on p [3]. Let us set one more notation

Theorem 3.2 [3,6]. The following equality is true

for all 1 E Rn and A = { M , R ( . ) , H ( - ) ) E Rn+ x C 3 [ t 0 , 61 x C+m[tO, 191 where @ ( l , A ) is defined in Theorem 3.1.

Combining Theorems 3.1, 3.2 we obtain

Theorem 3.3 Let r ( G ( t ) ) = m for every t E [to, 191. Then the following equality holds

~ ( 1 9 , Y*(.)) =

n{zo(19,

y8(.); A )

I

A = { M , R(.), H(.)I

Theorem 3.3 gives a precise description of informational domains X(19, ys(.)) by means of solu- tions Zo(19, ys(.); A ) t o t h e linear-quadratic problem (3.5)-(3.7) allowing t o vary matrix param- eters in joint integral constraint (3.7) on uncertain disturbances.

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4 The Maximum Principle

Introduce some more notations. Let ~ ( ' ) ( t ; A ) be the i-th column of matrix R ( t , A ) E R m x n .

.

z ( z = 1,

....,

n ) ,

Denote X(')(t; A ) t o be a solution t o the integral equation

A ) = T ( ' ) ( - ; A ) , i = I ,

....,

n,

where the operator LA is defined by (3.2). Let P ( t ; A ) be the matrix { X ( ' ) ( t ; A ) ,

. . . ,

~ ( ~ ) ( t ; A ) ) E

~ m x n

.

T h e symbol I'(t, 19; A ) signifies a solution t o the following system in R n x n

with t h e end condition I'(19,19; A ) = E . For every 1 E Rn denote 4 ( t , I ; A ) = llI'(t, 19; A ) .

Having fixed a direction 1 E Rn consider t h e problem of computing the value of t h e support function p(llX(19, y s ( - ) ) ) t o t h e informational domain X(19, ys(.)). Let z* be a support point of X(19, ys(.)) corresponding t o the given I :

and x*(.) be a solution of t h e system (2.1)-(2.5) so t h a t z*(19) = x*.

Theorem 4.1 Let the assumption of Theorem 3.1 be fulfilled and E be an arbitrary positive number. Then, there ezists a t ~ i p l e t A = { M , R ( - ) , H ( - ) ) E RI; x Cy[to,19] x C+m[to, 191 such that the following relations are true:

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function v* ( t ) is the input defining x * ( . ) via (2.1) and the sets Z o ( t , yt (.); A ) are constructed due to formulae (3.5)-(3.8).

Let us comment these necessary optimality conditions. The first group of inequalities ( 4 . 2 ) - ( 4 . 4 ) corresponds with t h e classical maximum principle written here in an approximate form with modification ( 4 . 1 ) of the conjugate system. The latter assertion ( 4 . 5 ) reflects the duality property of the convex compact set X ( t , y t ( - ) ) given by the Theorem 3.3: a point x E Rn lies outside the set X ( t , y t ( . ) ) if there exists an aggregate Z o ( t , y t ( . ) ; A ) so that x does not belong t o Z o ( t , y t ( - ) ; A ) . It means that the sets Z o ( t , y t ( - ) ; A ) play the same role in the description of informational domains X ( t , y t ( - ) ) as the usual linear hyperplanes of separability theorem in convex analysis.

5 Dynamic Relations

T h e final section of the paper deals with the evolution problem arising in the control and esti- mation theory for uncertain systems with set-membership d a t a [4,6,10,11]. T h e next theorems present the equations that describe the dynamics of informational domains X ( t ,

x(-))

under

variation of the observation time t .

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Theorem 5.1 [3]. The set Z o ( t , y t ( . ) ; A ) is a t-cross-section of the integral funnel to the fol- lowing differential inclusion

where C : [to, 191

+

R n x n is the solution of the Riccati equation

k

= A ( s ) C

+

C A 1 ( s ) - CG1(s)H ( s ) G ( s ) C

+

R-' ( s ) ,

Theorem 5.2 Under the assumption of Theorem 3.1 the set X ( t , yt(.)) equals the intersection over all matrix triplets A = { M , R ( - ) , H ( . ) ) E R ;

x

C;4[to,19] x Cy[to,19] of the t-cross-sections of the trajectory assemblies of system (5.1)-(5.2).

REFERENCES

[:I]

Krasovskii N.N. The control of a dynamic system. "Nauka", Moscow, 1986 (Russian).

[2] Krasovskii N.N. O n the theory of controllability and observability of linear dynamic systems.

Prikl. Mat. Mech., 28, 1, 3-14, 1964, (Russian).

[3] Kurzhanskii A.B. Control and observation under uncertainty. "Nauka", Moscow, 1977 (Rus- sian).

[4] Kurzhanskii A.B. Evolution equations for problems of control and estimation of uncertain systems. Proc. Intern. Congress o f Mathematicians, 1381-1402, Warsaw, 1983.

[5] Witsenhausen H.S. Sets of possible states of linear systems given perturbed observation.

IEEE Trans. Automat. Control, AC-13, 5 , 556-558, 1968.

[6] Kurzhanskii A.B. Dynamic control system estimation under uncertainty conditions. I , Prob- lems o f Control and Information Theory, 9, 6 , 395-406, 1980.

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[7] Kurzhanskii A.B. Set-valued calculus in problems of adaptive control. IIASA Working Paper, WP-87-115, Laxenburg, 1987.

[8] Schweppe F . Uncertain dynamic systems. Prentice-Hall Lnc., Englewood Cliff, New Jersey, 1973.

[9] Koscheev A.S. and Kurzhanskii A.B. On adaptive estimation of multistage systems under uncertainty. Isvestia Akad. Nauk SSSR, Teh. Kibernetika, 2, 72-93, 1983 (Russian).

[lO] Kurzhanskii A.B. and Filippova T.F. On the set-valued calculus in problems of viability and control for dynamic processes: the evolution equation. IIASA Working Paper, WP-88-091, Laxenburg, 1988.

[ll] Kurzhanskii A.B. and Filippova T.F. On the description of the set of viable trajectories of a control system. Different. Uravn., 23, 8, 1303-1315, 1987 (Russian).

[12] Aubin J.-P. and Cellina A. Differential inclusions. Springer-Verlag, Heidelberg, 1984.

[13] Aubin J.-P. and Ekeland I. Applied nonlinear analysis. Academic Press, New York, 1984.

[14] Balakrishnan A.V. Applied functional analysis. Springer-Verlag, Heidelberg, 1976.

[15] Rockefellar R.T. Convex analysis. Princeton University Press, 1970.

T.F. Filippova

Institute of Mathematics and Mechanics of the Ural Scientific Center

Russian Academy of Sciences, Yekaterinburg

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