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Discrete Dynamics in Nature and Society Volume 2011, Article ID 760878,20pages doi:10.1155/2011/760878

Research Article

Delay-Dependent H

Filtering for Singular Time-Delay Systems

Zhenbo Li

1, 2

and Shuqian Zhu

3

1School of Statistics and Mathematics, Shandong Economic University, Jinan 250014, China

2Shandong Provincial Key Laboratory of Digital Media Technology, Shandong Economic University, Jinan 250014, China

3School of Mathematics, Shandong University, Jinan 250100, China

Correspondence should be addressed to Shuqian Zhu,sqzhu@sdu.edu.cn Received 14 February 2011; Accepted 29 April 2011

Academic Editor: Xue He

Copyrightq2011 Z. Li and S. Zhu. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

This paper deals with the problem of delay-dependent H filtering for singular time-delay systems. First, a new delay-dependent condition which guarantees that the filter error system has a prescribedHperformanceγis given in terms of linear matrix inequalitiesLMIs. Then, the sufficient condition is obtained for the existence of theHfilter, and the explicit expression for the desiredHfilter is presented by using LMIs and the cone complementarity linearization iterative algorithm. A numerical example is provided to illustrate the effectiveness of the proposed method.

1. Introduction

Over the past decades, the filtering problem has been widely studied and has found many applications 1, 2. Current efforts on this topic can be mainly divided into two classes:

the Kalman filtering approach and the H filtering approach. The objective of the latter one is to find a filter such that the resulting error system is asymptotically stable and the L2-induced normfor continuous systemsorl2-induced normfor discrete systemsfrom the disturbance input to the filtering error output satisfies a prescribed H performance level. In contrast to the Kalman filtering, the H filtering approach does not require the exact knowledge of the statistics of the external noise signals, and it is insensitive to the uncertainties. These features render the H filtering attracting much attention, and many efforts have been made on this issue3–6. The filtering problem for singular systems has also been investigated by many researchers. For example, a necessary and sufficient condition is obtained in 7for the solvability of the H filtering problem and the designed filter is proper with a McMillan degree no more than the exponential modes of the plant, while,

(2)

in8, a linear normalH filter is obtained for singular systems. Reduced-orderHfilters are designed in 9 for both continuous and discrete singular systems. In10, a reduced- orderH filter design approach is developed for a class of discrete singular systems with lossy measurements.

On the other hand, for many practical control systems, time delays are frequently encountered and they are often the sources of instability and degradation in control performance. So, recently, there has been increasing interest inHfiltering for time-delay systems. Existing results can be classified into two types: delay-independent ones11–14and delay-dependent ones15–23; the former do not include any information on the size of delay while the latter employ such information. Generally speaking, delay-dependent results are less conservative than the delay-independent ones, especially when the size of delay is small.

Singular time-delay systems, which are also referred to as implicit time-delay systems, descriptor time-delay systems, or generalized differential-difference equations, often appear in various engineering systems, including aircraft attitude control, flexible arm control of robots, large-scale electric network control, chemical engineering systems, and lossless transmission linessee, e.g.,24. Since singular time-delay systems are more general, it is of significance to consider theHfiltering problem for them. Recently, some delay-dependent 25–27 and delay-dependent28–31results aboutH filters for such systems have been obtained. In 28, the delay-independent filter is of the Luenberger observer type and the decomposition and transformation of the system matrices are involved, which would result in some numerical problems. A full-order filter is designed in29for singular systems with communication delays, and H filtering problems are concerned in 30, 31 for singular systems with time-varying delay in a range.

In this paper, the problem of delay-dependentHfiltering is investigated for singular time-delay systems. We consider the case of discrete delay which is assumed to be constant and known. First, based on the result in32, we derive a new delay-dependent condition which guarantees that the filter error system has a prescribedHperformanceγ; and it can be seen that this new condition is more “efficient” than that in32since no redundant variables are involved. Then, the sufficient condition for the existence of the full-orderHfilter, which is an admissible singular time-delay system, is obtained and the explicit expression for the desiredHfilter is given by using LMIs and the cone complementarity linearization iterative algorithm.

Notations

Rn denotes the n-dimensional Euclidean space and Rn×m denotes the set of alln×mreal matrices,In is then-dimensional identity matrix, and diag{· · · }is a block-diagonal matrix.

For real symmetric matrixX, the notationX≥0 X >0means that the matrixXis positive- semidefinitepositive-definite. The superscriptTrepresents the transpose; the symbol∗will be used in some matrix expressions to induce a symmetric structure.L20,∞refers to the space of square-integrable vector functions over0,∞with normf2:

0 ft2dt1/2.

2. Problem Statement

Consider the following singular time-delay system:

Ext ˙ Axt Aτxtτ Bwt, yt Cxt Cτxtτ B1wt,

(3)

zt Gxt Gτxtτ B2wt, xt φt, t∈−τ,0,

2.1 where xtRn is the state,wtRr is the external disturbance signal that belongs to L20,∞, yt∈ Rmis the measurement output, andztRs is the signal to be estimated.

E, A, Aτ, B, C, Cτ, B1, G, Gτ, andB2 are known real constant matrices with appropriate dimensions and 0 <rankE p < n.τ > 0 is the known delay constant andφtCn,τ is a compatible vector-valued initial function.

Without loss of generality, we assume that Cτ 0, B1 0, Gτ 0, andB2 0.

Otherwise, system2.1can be equivalently changed into E 0

0 0 xt˙

ζt˙

A 0 0 −Im s

xt ζt

⎢⎢

⎢⎢

⎢⎢

⎢⎣

Aτ | 0

−− − −−

Cτ | 0m s Gτ |

⎥⎥

⎥⎥

⎥⎥

⎥⎦

xtτ ζtτ

⎢⎢

⎢⎢

⎢⎣ B

−−

B1

B2

⎥⎥

⎥⎥

⎥⎦wt,

yt zt

⎢⎢

C |

Im s G |

⎥⎥

xt

ζt

.

2.2

Then in the sequel, we discuss the system model as follows:

Ext ˙ Axt Aτxtτ Bwt, yt Cxt,

zt Gxt, xt φt, t∈−τ,0.

2.3

Throughout this paper, we need the following assumption for system2.3.

Assumption 2.1. System2.3is admissible, that is, whenwt0, system2.3is regular, impulse free, and asymptotically stable.

Remark 2.2. About the definitions of regularity, absence of impulses and asymptotical stability for singular time-delay systems, we refer the readers to33.

For the estimates ofzt, we consider the following linear filter with delay:

Ext ˙ Afxt Aτfxtτ Bfyt,

zt Cfxt,

xt ψt, t∈−τ,0,

2.4

(4)

wherextRn and ztRs are the state and the output of the filter, respectively. The constant matricesAf, Aτf, Bf, andCf are filter parameters to be determined.

Letting

et:

xTt xTtT

, zt :ztzt, 2.5

one obtains the filter error system

Eet ˙ Aet Aτetτ Bwt, zt Get,

et

φTt ψTtT

, t∈−τ,0,

2.6

where

E E 0

0 E

, A

A 0 BfC Af

,

Aτ

Aτ 0 0 Aτf

, B B

0

, G G −Cf

.

2.7

Thus, the filtering problem to be addressed is stated as follows.

H Filtering Problem

For a givenγ >0, design a full-order filter with delay of the form of2.4such that the filter error system2.6has prescribedHperformanceγ, that is,

1system2.6is admissible;

2under zero initial condition, for any nonzerowtL20,∞, theHperformance zt2γwt2is guaranteed.

Remark 2.3. Similar to17, it is easy to see that system2.3is admissible if the error system 2.6is admissible. That is why we made Assumption2.1on system2.3.

3. Main Results

At first, we will concentrate our attention onHperformance analysis for the error system 2.6. The following lemma is useful in the proof of Theorem3.2.

Lemma 3.1 see32. Given a scalar γ > 0, the filter error system2.6 has a prescribed H performanceγif there exist matricesQ > 0, Z > 0, P , Y, andWsatisfying

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ETPT PE≥0, 3.1

Φ

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

Φ1 Φ2 τYT PB τ ATZ GT

∗ Φ3 τWT 0 τATτZ 0

∗ ∗ −τZ 0 0 0

∗ ∗ ∗ −γ2I τBTZ 0

∗ ∗ ∗ ∗ −τZ 0

∗ ∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

<0, 3.2

where

Φ1 PA ATPT QYTEETY , Φ2PAτ YTEETW, Φ3Q WTE ETW.

3.3

Based on Lemma3.1, we will present a new delay-dependent bounded real lemma BRLfor the performance analysis of system2.6, which can be shown to be more “efficient”

than Lemma3.1.

Theorem 3.2. Given a scalarγ >0, the filter error system2.6has a prescribedHperformanceγ if there exist matricesQ > 0, Z > 0 andPsatisfying3.1and

Ω

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎣

Ω1 Ω2 PB τ ATZ GT

∗ Ω3 0 τATτZ 0

∗ ∗ −γ2I τBTZ 0

∗ ∗ ∗ −τZ 0

∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎦

<0, 3.4

where

Ω1PA ATPT Q−1

τETZE, Ω2PAτ

1

τETZE, Ω3Q −1

τETZE. 3.5

Proof. From Lemma3.1, if we can prove that the feasibility ofΩ<0 for solutionQ > 0,Z >

0,P is equivalent to that ofΦ< 0 for solutionQ > 0,Z > 0,P , Y , W, then Theorem 3.2is proved.

(6)

Similar to Lemma 4 of34, take

Ψ ΠΦΠT

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

Ω1 Ω2 τYTETZ PB τ ATZ GT

∗ Ω3 τWT ETZ 0 τATτZ 0

∗ ∗ −τZ 0 0 0

∗ ∗ ∗ −γ2I τBTZ 0

∗ ∗ ∗ ∗ −τZ 0

∗ ∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

, 3.6

with

Π

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎣ I 0 1

τET 0 0 0 0 I −1

τET 0 0 0

0 0 I 0 0 0

0 0 0 I 0 0

0 0 0 0 I 0

0 0 0 0 0 I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎦

. 3.7

It follows from Schur complement that

Φ<0⇐⇒Ψ<0⇐⇒Z > 0, Ω

⎢⎢

⎢⎢

⎢⎢

⎢⎢

τYTETZ τWT ETZ

0 0 0

⎥⎥

⎥⎥

⎥⎥

⎥⎥

τZ−1

⎢⎢

⎢⎢

⎢⎢

⎢⎢

τYTETZ τWT ETZ

0 0 0

⎥⎥

⎥⎥

⎥⎥

⎥⎥

T

<0. 3.8

If there existQ > 0, Z > 0,P , Y, andWsatisfyingΦ< 0, from3.8it is easy to see that the aboveQ, Z, P is a feasible solution ofΩ<0. Conversely, if there existQ > 0, Z > 0 andP such thatΩ < 0 holds, via takingY 1/τZE andW −1/τZE, Φ < 0 is also feasible for the aboveQ, Z, P , Y , W. This completes the proof.

The following corollary is easy to be obtained from Theorem3.2.

Corollary 3.3. The filter error system2.6is admissible if there exist matricesQ > 0, Z > 0 andP satisfying3.1and

(7)

⎢⎢

⎢⎢

PA ATPT Q− 1

τETZE PAτ

1

τETZE τ ATZ

∗ −Q −1

τETZE τ ATτZ

∗ ∗ −τZ

⎥⎥

⎥⎥

<0. 3.9

Remark 3.4. Theorem3.2can also be proved by employing the relationship of two integral inequalities concluded in 35. In fact, we can see that Lemma 3.1 is obtained by using the integral inequality 7 in 35, while using the integral inequality 9 in 35 yields Theorem 3.2. As shown by 35, the upper bound provided by 9 in 35 is the least upper bound provided by 7 in 35; therefore introducing more free matrices cannot reduce the conservativeness. Then, Theorem3.2can be obtained from Lemma3.1, and the introduced slack variablesY andWin Lemma3.1are redundant variables. Hence, from the computational point of view, Theorem3.2is more “efficient” than Lemma3.1.

In the sequel, based on Theorem3.2, we are devoted to the design of the filter param- eters Af, Aτf, Bf, and Cf. Noticing that 3.4 is nonlinear about the unknown variables A, Aτ, P, and Z, to reduce the number of the unknown variables, we can do as follows.

From3.4we know that

⎢⎣

PA ATPT Q− 1

τETZE PAτ 1 τETZE

∗ −Q−1

τETZE

⎥⎦<0. 3.10

Multiplying3.10byI Ifrom the left and byI ITfrom the right results in

P A Aτ

A Aτ

T

PT<0, 3.11

which implies thatPis nonsingular. Let

P P P2

P3 P4

, PRn×n, PiRn×n, i2,3,4. 3.12

Without loss of generality, we can assume thatP, Pi, i2,3,4, are all nonsingular36. Then, from3.1, we have that

ETPTP E, ETP3T P2E, ETP4TP4E. 3.13

Taking

T1 I 0

0 P P3−1

, T2 I 0

0 P2−1P

, T3diag

T1, T1, I, T2T, I

3.14

(8)

and combining with2.7and3.12, we obtain

ET2−1ET 1T

E 0 0 P−1P2EP3−TPT

E 0 0 P−1ETP3TP3−TPT

E 0 0 E

,

P T1P T 2

P P P P P3−1P4P2−1P

,

AT2−1AT 1T

A 0

P−1P2BfC P−1P2AfP3−TPT

A 0 BfC Af

,

Aτ T2−1AτT1T

Aτ 0 0 P−1P2AτfP3−TPT

Aτ 0 0 Aτf

,

BT2−1B B

0

,

GGT 1T

G −CfP3−TPT

G −Cf

,

3.15

where

Af P−1P2AfP3−TPT, Aτf P−1P2AτfP3−TPT, Bf P−1P2Bf, Cf CfP3−TPT, 3.16

and denote

QT1QT 1T, ZT2TZT 2. 3.17

Premultiplying byT1and postmultiplying byT1T on both sides of3.1, we have that

T1ETT2−TT2TPTT1T T1P T 2T2−1ET 1T≥0, 3.18

that is,

ETPTP E≥0. 3.19

(9)

Multiplying3.4byT3from the left and byT3T from the right yields

Ω

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎣

P A ATPT Q−1

τETZ E P Aτ

1

τETZ E P B τATZ GT

∗ −Q− 1

τETZ E 0 τATτZ 0

∗ ∗ −γ2I τBTZ 0

∗ ∗ ∗ −τZ 0

∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎦

<0. 3.20

It can be seen that the systemsE, A, Aτ,B, G and E, A, Aτ, B, G are algebraically equivalent under the r.s.e. restricted system equivalence transformation, where T2−1 and T1T are taken as the row full rank transformation matrix and the coordinate full rank transformation matrix, respectively, and comparing the coefficient matrices of the two systems, we can see that the difference between them is just the filter parameters Af, Aτf, Bf, Cf, andAf, Aτf, Bf, Cf. Moreover, in the r.s.e. transformation, the state and the equation of the filter change while the state and the equation of system 2.3 do not change. So, in the design of the filter, we can directly substitute Af, Aτf, Bf, Cf for Af, Aτf, Bf, Cf. Noticing that

I 0

−P3P−1 I

P P2

P3 P4

I −P−1P2

0 I

P 0 0 P4P3P−1P2

, 3.21

thenP4P3P−1P2is nonsingular. Let

P P3−1P4P2−1PPP P3−1

P4P3P−1P2

P2−1PS−1; 3.22

thenPcan be written as

P

P P P P S−1

. 3.23

Denote

JT S P−1, T4

JT −S I 0

, T5 T4P Z−1. 3.24

SincePS P−1 P S−1SP P3−1P4P2−1P Sis nonsingular,Jis also a nonsingular matrix.

From3.19, we have that,

T4ETPTT4TT4P ET4T ≥0. 3.25

(10)

Noticing3.23and3.24, we derive

T4P I 0

P P

,

T4P ET4T

EJ E P EJP EST P E

EJ E P EP−T P E

EJ E ET P E

,

T4ETPTT4T

JTET E ET ETPT

;

3.26

then3.25is just

EJJTET, P EETPT,

EJ E ET P E

≥0. 3.27

Premultiplying by diag{T4, T4, I, T5, I}and postmultiplying by diag{T4T, T4T, I, T5T, I}on both sides of3.20, we have

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

T4ATPTT4T T4P AT4T T4QT4T− 1

τT4ETZ ET4T T4P AτT4T 1

τT4ETZ ET4T T4P B τT4ATZT5T T4GT

∗ −T4QT4T−1

τT4ETZ ET4T 0 τT4ATτZT5T 0

∗ ∗ −γ2I τBTZT5T 0

∗ ∗ ∗ −τT5ZT5T 0

∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

<0. 3.28

Noticing that

T4P AT4T

AJ A

P AJ P BfCJP AfST P A P BfC

,

T4P AτT4T

AτJ Aτ

P AτJP AτfST P Aτ

,

T4P B B

P B

, T4GT

JTGT SCTf GT

,

(11)

T4ATZT5T T4ATZ Z−1PTT4T T4ATPTT4T, T4ATτZT5T T4ATτZ Z−1PTT4T T4ATτPTT4T, BTZT5TBTZ Z−1PTT4T BTPTT4T, T5ZT5T T4P Z−1Z Z−1PTT4T T4P Z−1PTT4T,

3.29 denote

QT4QT4T

Q1 Q2

QT2 Q3

, 3.30

ZT4P Z−1PTT4T

Z1 Z2

ZT2 Z3

, 3.31

LP AJ P BfCJP AfST, Lτ P AτJP AτfST, 3.32

WBP Bf, WC CfST. 3.33

Since3.31implies thatZPTT4TZ−1T4P, then

T4ETZ ET4T T4ETPTT4TZ−1T4P ET4T

EJ E ET P E

Z−1

EJ E ET P E

. 3.34

Introduce matrixW W

1 W2

W2T W3

≥0 satisfying

τW

EJ E ET P E

Z−1

EJ E ET P E

, 3.35

then

⎢⎣−1

τT4ETZ ET4T 1

τT4ETZ ET4T

∗ −1

τT4ETZ ET4T

⎥⎦≤

−W W

∗ −W

; 3.36

Obviously, if there exist matrices Q1 > 0, Q3 > 0, W1 ≥ 0, W3 ≥ 0, Z1 > 0, Z3 >

0, P, J, WB, WC, L, Lτ, Q2, W2, andZ2withP, Jbeing nonsingular, satisfying3.35and

(12)

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎢

⎢⎣

Ξ11 Ξ12 AτJ W1 Aτ W2 B τJTAT τLT JTGT WcT

∗ Ξ22 Lτ W2T P Aτ W3 P B τAT τATPT τCTWBT GT

∗ ∗ −Q1W1 −Q2W2 0 τJTATτ τLTτ 0

∗ ∗ ∗ −Q3W3 0 τATτ τATτPT 0

∗ ∗ ∗ ∗ −γ2I τBT τBTPT 0

∗ ∗ ∗ ∗ ∗ −τZ1 −τZ2 0

∗ ∗ ∗ ∗ ∗ ∗ −τZ3 0

∗ ∗ ∗ ∗ ∗ ∗ ∗ −I

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎥

⎥⎦

<0 3.37

with

Ξ11 AJ JTAT Q1W1, Ξ12 A LT Q2W2,

Ξ22 P A ATPT WBC CTWBT Q3W3, 3.38

then taking

SJTP−1, Bf P−1WB, Cf WCS−T, Af P−1P AJ WBCJLS−T, Aτf P−1P AτJLτS−T,

3.39

one obtains that there are solutionsQ >0, Z >0, andPto3.20.

Hence we get the following theorem for the design of the filter2.4.

Theorem 3.5. Given a scalarγ >0, if there are matricesQ1 >0, Q3>0, W1 ≥0, W3 ≥0, Z1 >

0, Z3 > 0, P, J, WB, WC, L, Lτ, Q2, W2, Z2 with P, J being nonsingular, satisfying 3.27, 3.35, and3.37, then theH filter of the form of 2.4exists and the parameters are given by 3.39.

Remark 3.6. It is worth noting that3.35is not an LMI. In order to use the LMI Toolbox in MATLAB to get the solutions, we can do as follows.

Assume thatE

Ip 0 0 0

; otherwise, we can find nonsingular matricesMandNsuch

thatMEN

Ip0 0 0

. It is worth noting that the feasibility of3.27,3.35, and3.37is not affected by the selection ofMandN. Then, the matricesP, Jsatisfying3.27are of the forms

P

P11 P12

0 P22

, J

J11 0 J21 J22

, P11Rp×p, J11Rp×p 3.40

with

J11 I I P11

≥0. 3.41

(13)

Introduce another variableU >0; then3.35can be replaced by

τW

EJ E ET P E

U

EJ E ET P E

, 3.42

UZI. 3.43

WriteUas

U

⎢⎢

⎢⎢

⎢⎣

U11 U12 U13 U14

UT12 U22 U23 U24

UT13 UT23 U33 U34

UT14 UT24 UT34 U44

⎥⎥

⎥⎥

⎥⎦>0, 3.44

where

U11Rp×p, U22Rn−p×n−p, U33Rp×p, U44Rn−p×n−p. 3.45

Noticing that

EJ E ET P E

U

EJ E ET P E

⎢⎢

⎢⎢

⎢⎣

Π11 0 Π13 0

∗ 0 0 0

∗ ∗ Π33 0

∗ ∗ ∗ 0

⎥⎥

⎥⎥

⎥⎦, 3.46

where

Π11J11U11J11 UT13J11 J11U13 U33, Π13J11U11 UT13 J11U13P11 U33P11, Π33U11 P11UT13 U13P11 P11U33P11,

3.47

we can assume that

W

⎢⎢

⎢⎢

⎢⎣

W11 0 W21 0

0 0 0 0

W21T 0 W31 0

0 0 0 0

⎥⎥

⎥⎥

⎥⎦≥0,

W11 W21

W21T W31

>0. 3.48

(14)

Then3.42is just

τ

W11 W21

W21T W31

J11 I I P11

U11 U13

U13T U33

J11 I I P11

. 3.49

Invoking Schur complement again, we have that3.49is equivalent to

⎢⎢

⎢⎢

⎢⎣

U11 U13

UT13 U33

J11 I I P11

−1

J11 I I P11

−1 τ

W11 W21

W21T W31

−1

⎥⎥

⎥⎥

⎥⎦≥0. 3.50

Introducing

α

α1 α2

αT2 α3

>0, θ

θ1 θ2

θ2T θ3

>0, 3.51

then3.50can be replaced by

⎢⎢

⎢⎢

⎢⎣

U11 U13 τα1 τα2

U33 ταT2 τα3

∗ ∗ τθ1 τθ2

∗ ∗ ∗ τθ3

⎥⎥

⎥⎥

⎥⎦≥0, 3.52

J11 I I P11

α1 α2

αT2 α3

I,

W11 W21

W21T W31

θ1 θ2

θT2 θ3

I. 3.53

Therefore, one can consider theHfilter design problem as the following cone complemen- tary problems:

Minimize

trUZ tr

J11 I I P11

α1 α2

αT2 α3

W11 W21

W21T W31

θ1 θ2

θT2 θ3

3.54 subject to LMIs3.30,3.31,3.37,3.40,3.41,3.44,3.48,3.51,3.52, and

Q >0, Z >0,

U I I Z

≥0,

⎢⎢

⎢⎢

⎢⎣

α1 α2 I 0 αT2 α3 0 I I 0 J11 I 0 I I P11

⎥⎥

⎥⎥

⎥⎦≥0,

⎢⎢

⎢⎢

⎢⎣

θ1 θ2 I 0 θT2 θ3 0 I I 0 W11 W21

0 I W21T W31

⎥⎥

⎥⎥

⎥⎦≥0.

3.55

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Then the filer2.4can be solved by using the iterative algorithm as37, in the interests of economy, which is omitted here.

Remark 3.7. Since the filter2.4is designed with parameters3.39such that inequality3.20 holds, we have

⎢⎢

⎢⎢

P A ATPT Q− 1

τETZ E P Aτ

1

τETZ E τATZ

∗ −Q− 1

τETZ E τATτZ

∗ ∗ −τZ

⎥⎥

⎥⎥

<0. 3.56

By3.15,3.16,3.17,3.23and lettingPf :P S−1,Q Q

1Q2

Q3

, and Z

Z1Z2

Z3

with

Q1Rn×nandZ1Rn×n, we can conclude from3.56that

⎢⎢

⎢⎢

PfAf ATfPfT Q3−1

τETZ3E PfAτf

1

τETZ3E τATfZ3

∗ −Q3− 1

τETZ3E τATτfZ3

∗ ∗ −τZ3

⎥⎥

⎥⎥

<0. 3.57

In addition,3.19implies that

ETPfT PfE≥0. 3.58

Invoking Corollary3.3, it is obtained that the designed filter2.4is admissible, and then it is proper and can be realized in practice.

4. Numerical Examples

Example 4.1. Consider the singular time-delay system given in25without uncertainties and distributed delay and with

E

⎢⎢

⎣ 1 0 0 0 1 0 0 0 0

⎥⎥

, A

⎢⎢

−2 0 0.5 0.1 −0.9 0.2 0 0.5 0.3

⎥⎥

, Aτ

⎢⎢

0.2 0.1 0 0.2 0 0.15 0.1 −0.23 0.1

⎥⎥

,

B

⎢⎢

0.2 0 0 0 0.2 0 0 0 0.2

⎥⎥

, C 1 0 0

, G

1 0.7 0.8 .

4.1

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−3

−2.5

−2

−1.5

−1

−0.5 0 0.5 1 1.5

0 5 10 15

Times(s) x1

x2

x3

Figure 1: State responsesxtof the original system.

x1

x2

x3

−3

−2.5

−2

−1.5

−1

−0.5 0 0.5 1 1.5

0 5 10 15

Times(s)

Figure 2: State responsesxt of the filter system.

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−1.5

−1

−0.5 0 0.5 1 1.5 2

z

0 5 10 15

Times(s)

Figure 3: Error estimation signalzt with the designed filter.

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1

−10 −8 −6 −4 −2 0 2 4 6 8 10

Frequency

Singularvalues

Figure 4: Singular value curve of the filtering error system.

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By Theorem3.2, forτ 2 andγ 1, after 10 iterations, the corresponding filter is obtained with the following parameters:

Af

⎢⎢

−0.9429 −0.0102 0.3206

−0.1042 −0.8493 0.1904 0.3750 0.4870 0.3369

⎥⎥

, Aτf

⎢⎢

0.0983 0.0960 0.0046 0.1248 −0.0071 0.1461 0.0749 −0.2438 0.0966

⎥⎥

,

Bf

⎢⎢

⎣ 0.6224

−0.2077 0.4488

⎥⎥

, Cf

−0.8379 −0.7382 −0.9940 .

4.2

With this filter, Figures1,2, and3show the state responsesxtof the original system, the state responsesxt of the filter system, and the error estimation signalzt ztzt with the initial conditionφt 1 1 −1.425T,ψt 1 1 −2.6341T for t ∈ −2,0and the exogenous disturbance inputwtdiag{e−0.5t, e−0.5t, e−0.5t}. By connecting the filter to the original system, the singular value curve of the resulting filtering error system is also plotted in Figure4. We can see that all the maximum singular values are less than 1, which illustrate the effectiveness of the proposed method in this paper.

5. Conclusions and Future Works

In this paper, we have studied theHfiltering problem for singular system with a constant discrete delay. Based on an improved BRL, a delay-dependent sufficient condition for the existence of the H filter with delay is obtained. Then, by using LMIs and the cone complementarity linearization iterative algorithm, the H filter is designed, which guarantees that the resulting error system is regular, impulse-free, internally stable, and the L2-induced norm from the disturbance input to the filtering error output satisfies a prescribed Hperformance level. It can be seen that the designed filter in this paper is a full-order filter, that is, the finite mode of the filter is equal to rankE. To study the delay-dependent reduced- orderHfiltering problem for singular time-delay systems is the key research in the future.

Acknowledgments

The authors would like to thank the Editor, the Associate Editor, and the anonymous reviewers very much for the valuable comments and good suggestions. This work was supported by National Natural Science Foundation of P. R. China61004011.

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