8

The solution of a regular PMD and the set of impulsive free initial conditions

Abstract

In this chapter, we discuss the complete solution of the linear nonhomogeneous matrix differential equations. What is meant by the complete solution is the full solution taking into account the initial conditions of the state as well as the initial conditions of the input. The essence of the new results presented here with respect to the existing results is that the obtained solution displays the full solution components including the impulse response and the slow response created, not only by the initial conditions of the state, but also by the initial condition of the input. Special attention is drawn to the initial conditions of the system input. Compared to the known results, in which the initial conditions of the system input are usually assumed to be zero, our approach firstly considers this issue explicitly.

Keywords

Linear nonhomogeneous matrix differential equations (LNHMDEs); Complete solution; Initial conditions; Impulse response; Slow response; Generalized state space systems; Singular perturbation model; Algebraic matrix Riccati equation; Slow state (smooth state); Fast state (impulsive state)

8.1 Introduction

In this chapter, we discuss the complete solution of the linear nonhomogeneous matrix differential equations (LNHMDEs). What is meant by the complete solution is the full solution taking into account the initial conditions of the state as well as the initial conditions of the input. The essence of the new results presented here with respect to the existing results [13, 17, 102] is that the obtained solution displays the full solution components including the impulse response and the slow response created, not only by the initial conditions of the state, but also by the initial condition of the input. Special attention is drawn to the initial conditions of the system input. Compared to the known results [13, 17, 102], in which the initial conditions of the system input are usually assumed to be zero, our approach firstly considers this issue explicitly.

The LNHMDEs or linear nonhomogeneous regular polynomial matrix descriptions (PMDs) are described by

A(ρ)βNH(t)=B(ρ)μ(t),t0,

si1_e  (8.1)

where ρ := d/dt is the differential operator, A(ρ)=Aq1ρq1+Aq11ρq11++A1ρ+A0R[ρ]r×rsi2_e, rankR(ρ)A(ρ) = r, AiRr×r, i = 0, 1, 2, …, q1, q1 ≥ 1, B(ρ) = Blρl + Bl−1ρl−1 + ⋯ + B1ρ + B0R[ρ]r×m, BjRr×m, j = 0, 1, 2, …, l, l ≥ 0, βNH(t):[0,+)Rrsi3_e is the pseudo-state of the LNHMDE, u(t):[0,+)Rmsi4_e is an i times piecewise continuously differentiable function called the input of the LNHMDE. Their homogeneous cases

A(ρ)βH(t)=0,t0

si5_e

are called the linear homogeneous matrix differential equations (LHMDEs) or homogeneous PMDs. Both regular generalized state space systems (GSSSs), which are described by

Ex.=Ax(t)+Bu(t),

si6_e

where E is a singular matrix, rank(ρEA) = r, and the (regular) state space systems, which are described by

x.=Ax(t)+Bu(t)

si7_e

are special cases of the above LNHMDEs (4.1). There have been many discussions about GSSSs (see, e.g., [711, 103, 104]). In [12], the impulsive solution to the LHMDEs was presented in a closed form. For both the LNHMDEs and LHMDEs, Vardulakis [13] developed their solutions under the assumption that both the initial conditions of the state and the input are zero. However, as we will see later, in some real cases, the initial conditions of the state might result from a random disturbance entering the system, and a feedback controller is called for. Since the precise value of the initial conditions of the state is unpredictable and the control is likely to depend on those initial conditions of the state, so this assumption is somewhat stronger than necessary.

Example 8.1.1

This example is to display the fact that the initial conditions of u(t) are not necessarily equal to zero in some situations.

To the singular perturbation model [105]

x.(t)εŻ(t)=A11A12A21A22x(t)z(t)+B1B2u(t),x(0)z(0)=x0z0,t0

si8_e

y=M1,M2x(t)z(t),

si9_e

where x(t) ∈ Rn, z(t) ∈ Rm, u(t) ∈ Rr, and y(t) ∈ Rp. Kokotovic et al. [105] considered the so-called near-optimal regulator problem, i.e., to find a control u(t) ∈ Rr, t ≥ 0 so as to regulate the state x(t)z(t)si10_e to the original by way of minimizing the quadratic performance index

J=120(yT(t)y(t)+uT(t)Ru(t))dt,R>0,

si11_e

where the r × r weighting matrix R penalizes excessive values of control u(t). The solution of the above problem is the optimal linear feedback control law

uopt(t)=R1BTK(ε)x(t)z(t)=G(ε)x(t)z(t),t0,

si12_e

where K(ε) satisfies the algebraic matrix Riccati equation. When the original system satisfies some conditions, K(ε) exist as a positive-definite matrix (see [105, page 111, Theorem 4.1]).

Let us investigate a special case with B1 = In, B2 = Im, and note that the matrix K(ε) is positive-definite, and thus is nonsingular. In this case, the matrix G(ε) is of full column rank. Therefore if

x(0)z(0)0,

si13_e

then

μopt(0)=G(ε)x(0)z(0)0.

si14_e

In this chapter, we will present a solution to Eq. (8.1) that displays the impulse response and the slow response created not only by the initial conditions of βNH(t), but also by the initial condition of u(t). Also reformulations to the solution of the LNHMDEs in terms of the regular derivatives of u(t) are given. By defining the slow state (smooth state) and the fast state (impulsive state) of them, it is shown that the system behaviors of the LNHMDEs can be decomposed into the slow response (smooth response) and the fast response (impulsive response) completely. This approach is applied conveniently to discuss the impulse free initial conditions of Eq. (8.1).

So far there have been many discussions about the impulse free condition either of the GSSSs (see, e.g., [14, 15]) or of the LNHMDEs and the LNHMDEs (see, e.g., [13, 16]). However, the common concern in the known results is the impulse created by the appropriate initial conditions of the state alone. For LNHMDEs, a different analysis concerning this issue is carried out that considers both the impulse created by the initial conditions of u(t) and that created by the initial conditions of βNH(t).

8.2 Preliminary results

Any rational matrix A(s) is equivalent [87] at s=si15_e to its Smith-McMillan form, having the form:

SA(s)(s)=block diagsq1,sq2,,sqk,1sq^k+1,,1sq^r,0pr,mr,

si16_e  (8.2)

where 1 ≤ kr and q1q2qk0,q^rq^r1q^k+10.si17_e Any polynomial matrix A(s)=A0+A1s++Aq1sq1Rr×r[s]si18_e with rankR[s]A(s)=rsi19_e can be transformed by unimodular transformation to its Smith form

SA(s)C(s)=diag[1,1,,1,fk(s),fk+1(s),,fr(s)],

si20_e

where 1 ≤ kr, fj(s)/fj+1(s), j = k, k + 1, …, r − 1. We denote xj,0i,xj,1i,si21_e, xj,σij1iRr(xj,0i0)si22_e, iI, j = k, k + 1, …, r as the Jordan Chain of lengths σij corresponding to the eigenvalue λi of A(s) and consider matrices

Ci=[xk,0i,,xk,σi,k1i][xr,0i,,xr,σi,r1i]Rr×mi,

si23_e  (8.3)

where mi=j=krσij,i=1,2,si24_e and

Ji=block diag[Ji,k,Ji,k+1,,Ji,r]Rmi×mi,i=1,2,,

si25_e  (8.4)

where Ji,jRσij×σijsi26_e, iI, j = k, k + 1, …, r, is the Jordan block matrix.

Definition 8.2.1

Finite Jordan pair of A(s) is defined as (C, J), C = [C1, C2, …, Cl] ∈ Rr×n, J = block diag[J1, J2, …, Jl] ∈ Rn×n, with n := m1 + m2 + ⋯ + ml = deg det(A(s)).

Definition 8.2.2

([13])

The pair: CRr×vsi27_e, J=block diag[J1,J2,,Jξ]Rv×vsi28_e, where

Ji=0100001000010000Rvi×vi,i=1,2,,ξ

si29_e

v=i=1ξvi,vi,ξNsi30_e, is called an infinite Jordan pair of A(s) if it is a (finite) Jordan pair of the “dual” polynomial matrix: Ã(w)=wq1A(1/w)=A0wq1+A1wq11++Aq1R[w]r×rsi31_e corresponding to its zero at w = 0.

Theorem 8.2.1

([13])

For a regular matrix polynomial A(s), its inverse matrix A−1(s) can be written

A1(s)=C,CsInJ00sJIμ1BB,

si32_e  (8.5)

where n=deg detA(s),μ=j=k+1r(q^j+1)=j=k+1rq^j+(rk)si33_e where q^j,j=k+1,,rsi34_e are the orders of the zeros at s=si15_e of A(s).

Proposition 8.2.1

([106])

If u(t)(i) denotes the distributional derivative of u(t), u(t)[i] denotes the regular derivative of u(t), δ(t) denotes the impulsive function, then we have the identity

u(t)(i)=u(t)[i]+δ(t)u(0)[i1]+δ(t)(1)u(0)[i2]++δ(t)(i1)u(0),i=1,2,

si36_e  (8.6)

8.3 A solution for the LNHMDEs

To the LNHMDEs

A(ρ)βNH(t)=B(ρ)u(t),t0.

si37_e  (8.7)

Assuming that the initial values of u(t) and its (l − 1)-derivatives at t = 0 are u(0), u(1)(0)⋯u(l−1)(0) and that the initial values of βNH(t) and its (q1 − 1)-derivatives at t = 0 are βNH(0),βNH(1)(0),,βNH(q11)(0).si38_e Taking the Laplace transformation of Eq. (8.7), we obtain

A(s)β^NH(s)α^β(s)=B(s)û(s)α^u(s),

si39_e  (8.8)

where β^NH(s):=0+βNH(t)estdt,û(s):=0+u(t)estdtsi40_e. Because of the Laplace-transformation rule

LdidtiβNH(t)=siβ^NH(s)si1βNH(0)sβNHi2(0)βNHi1(0);i=0,1,

si41_e

Ldjdtju(t)=siû(s)sj1u(0)suj2(0)uj1(0);j=0,1,

si42_e

α^β(s),α^u(s)si43_e can be written [107] as follows

α^β(s)=sq11Ir,sq12Ir,,sIr,IrAq100Aq11Aq10A1A2Aq1βNH(0)βNH(1)(0)βNH(q11)(0)

si44_e

α^u(s)=[sl1Ir,sl2Ir,,sIr,Ir]Bl00Bl1Bl0B1B2Blu(0)u(1)(0)u(l1)(0).

si45_e

We denote A−1(s) = Hpol(s) + Hsp(s), where Hpol(s) is the polynomial part of A−1(s) and Hsp(s) is the strictly proper part of A−1(s). To find a minimal realization of Hsp(s)(C, J, B) and a minimal realization of Hpol(s)(C,J,B)si46_e such that (C, J) and (C,J)si47_e are a finite Jordan pair and an infinite Jordan pair of A(s), respectively, and

A1(s)=C(sJIμ)1B+C(sInJ)1B.

si48_e

We obtain from [13]

eq08-01-9780081019467

where

eq08-05-9780081019467

Similarly,

eq08-02-9780081019467

where

eq08-06-9780081019467

From [13] we also obtain

A1(s)B(s)û(s)=[C,C]ΨΦImsImsq^r+1Imû(s)+C[sInJ]1Ωû(s),

si53_e

where

eq08-03-9780081019467

Ω:=JlBBl+Jl1BBl1++JBBl+BB0Rn×m.

si55_e  (8.9)

Now Eq. (8.8) can be written as

β^NH(s)=A1(s)α^β(s)+A1(s)B(s)u(s)A1(s)α^u(s).

si56_e  (8.10)

By taking the inverse Laplace transformation of the above, we finally obtain the following theorem that represents the required complete solution of the LNHMDE (8.7) created by the nonzero initial conditions on both the control u(t) and βNH(t).

Theorem 8.3.1

The solution of the LNHMDE (8.7) corresponding to nonzero initial conditions both on the pseudo-state βNH(t) and the input u(t) is

βNH(t)=CeJtxsβ(0)CeJtxsu(0)Ci=1q^rδ(t)(i1)Ji1(Jxfβ(0))+Ci=1q^rδ(t)(i1)Ji1(Jxfu(0))+0tCeJ(tτ)Ωu(τ)dτ+[C,C]ΨΦu(t)u(t)1u(t)(q^r+l),t0

si57_e  (8.11)

Remark 8.3.1

The solution (8.11) is an extension of that given by Vardulakis [13] to the case where the initial conditions of the pseudo-state and the input are not zero. Also the solution and impulsive behavior of PMDs of free linear multivariable systems given in [102] can be obtained as special cases from our result here simply by letting B(ρ) = 0.

Remark 8.3.2

From the above result, it is clearly seen that the nonzero initial conditions of β(t) and u(t) both contribute to the corresponding slow (smooth) zero input response by means of the terms

CeJtxsβ(0),CeJtxsu(0)

si58_e

and to the fast (impulse) response through the terms

Ci=1q^rδ(t)(i1)Ji1(Jxfβ(0)),Ci=1q^rδ(t)(i1)Ji1(Jxfu(0)).

si59_e

8.4 The smooth and impulsive solution components and impulsive free initial conditions: Csi60_e is of full row rank

The main aims of this section are to analyze the fast and slow components in the solution of the LNHMDEs and then to characterize the impulsive behavior of the system. To this end, one is suggested to reformulate the solution that is given by Theorem 8.3.1 in terms of the regular derivative of u(t). This is the subject of the following result.

Consider the following notations:

xs(0):=xsβ(0)xsu(0),Jxf(0):=Jxfβ(0)Jβxfu(0),

si61_e

U(t)^:=u(t)u[1](t)u[2](t)u[q^r+l](t)R(q^r+l+1)m,δ(t)^:=δ(t)δ(1)(t)δq^r+l+1(t)R(q^r+l),

si62_e

U(0):=0000u(0)000u[1](0)u(0)00u[q^r+l1](0)u[q^r+l2](0)u[1](0)u(0)R(q^r+l+1)m×(q^r+l),

si63_e

J^xf(0):=[Jxf(0),J2xf(0),,Jq^rxf(0)]Rμ×q^r,

si64_e

Ĵxf(0)^:=[J^xf(0),0μ×l]Rμ×(q^r+l),

si65_e  (8.12)

Ψ1:=[Jl1B,Jl2B,,B]Rn×Ir,Ψ2:=[B,JB,,Jq^rB]Rμ×(q^r+1)r,

si66_e

Φ1(B):=Bl00000Bl1Bl0000B1B2Bl000RIr×(q^r+l+1)m,

si67_e

Φ2(B):=B0B1Bl1Bl000B0Bl2Bl1Bl000B0B1Bl1BlR(q^r+1)r×(q^r+l+1)m.

si68_e

Theorem 8.4.1

With the above notations and assume that Csi60_e has full row rank and that its {1}-inverse is C(1).si70_e Denote

βs(NH)(t):=eJtxs(0)+0teJ(tτ)Ωu(τ)dτβf(NH)(t):=(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(t)^+[(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0)Ĵxf(0)^]δ(t)^,

si71_e

then

βNH(t)=[C,C]βs(NH)(t)βf(NH)(t).

si72_e  (8.13)

Proof

From Eqs. (10.9), (8.12), we know

eq08-04-9780081019467

from Eq. (8.6), we have

u(t)u(1)(t)u(q^r+l)(t)=U(t)^+U(0)δ(t)^,

si73_e  (8.15)

if Csi60_e has full row rank, we have CC(1)=Ir×rsi75_e. Substituting the above into Eq. (10.11), we obtain

βNH(t)=CeJtxs(0)+C0teJ(tτ)Ωu(τ)dτCJ^xf(0)δ(t)^+(CΨ1Φ1(B)+CΨ2Φ2(B))(U(t)^+U(0)δ(t)^)=CeJtxs(0)+C0teJ(tτ)Ωu(τ)dτ+C(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(t)^+C[(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0)J^xf(0)^]δ(t)^=[C,C]βs(NH)(t)βf(NH)(t).

si76_e

Remark 8.4.1

The assumption that Csi60_e has full row rank will be relaxed later.

Remark 8.4.2

The above theorem is interesting not least for its clear designation of the fast and slow components of the system solution structure. It provides further interest from the point of view of characterizing those initial conditions that give rise to completely smooth solutions (the so-called impulse free initial conditions) of regular PMDs. By treating it thus, the impulsive behavior of the system can be interpreted in a natural and clear way as the following theorem reveals.

Now we shall generalize the concept of the state to the LNHMDEs as [13] has done for the LHMDEs and the GSSS.

Definition 8.4.1

We define the vector

xNH(t):=βs(NH)(t)βf(NH)(t)R(n+μ)×1,

si78_e  (8.16)

where

βs(NH)(t):=eJtxs(0)+0teJ(tτ)Ωu(τ)dτ,

si79_e

βf(NH)(t):=(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(t)^+[(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0)J^xf(0)^]δ(t)^,

si80_e

as the state of the LNHMDE. βs(NH)(t) is called the slow state or smooth state, βf(NH)(t) is called the fast state or impulsive state.

For the LHMDEs

A(ρ)βH(t)=0,

si81_e

its solution is

βH(t)=[C,C]xs(t)xf(t),

si82_e

where

xs(t)=eJtxs(0),xf(t)=i=1q^rδ(t)(i1)Jixf(0).

si83_e

It is clear that the impulsive behavior of βH(t) at t = 0 only depends on xf(0), which is only related to the initial conditions of βH(t) and its derivatives at t = 0. Thus the set of impulse free initial conditions for LHMDE A(ρ)βH(t) = 0, t ≥ 0 is [1316]

HI(H)=x(0)=xs(0)xf(0):xs(0)Rn,xf(0)KerJ=RnKerJ.

si84_e

However, for the LNHMDEs, this issue becomes much more complicated, for in this case not only the initial conditions of βNH(t), but also the initial conditions of u(t) influence the solution structure. The following result provides an answer to this difficulty.

Theorem 8.4.2

Assume that Csi60_e has full row rank. The set of the impulsive free initial conditions for the LNHMDE (8.7) is

HI(NH)=xNH(0)=βs(NH)(0)βf(NH)(0):βs(NH)(0)=xs(0)Rn,βf(NH)(0)=(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0)^

si86_e  (8.17)

Proof

For the LNHMDE (8.7), under the notations in Theorems 8.3.1 and 8.4.1, we partition

(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0):=[Π1(U(0)),Π2(U(0))],

si87_e

where

Π1(U(0))Rμ×q^r,Π2(U(0))Rμ×l.

si88_e

Observing Eqs. (8.12), (8.13), we can see that βNH(t) is impulse free at t = 0 iff

(Ψ2Φ2(B)+C(1)CΨ1Φ1(B))U(0)J^xf(0)^=0,

si89_e  (8.18)

which hold true iff

Π1(U(0))J^xf(0)=0,

si90_e

i.e.,

xf(0)KerJ+Im(Π1(U(0))),

si91_e

and

Π2(U(0))=0.

si92_e

The set of the impulsive free initial conditions is thus derived from Theorem 8.4.1.

Theorem 8.4.3

If initial conditions βH(i)(0),i=0,1,,q11si93_e of the LHMDE are compatible with A(ρ)βH(t) = 0, t ≥ 0, u(0) = u(i)(0), i = 1, 2, …, l − 1 and U(0)Ker(Ψ1Φ1(B))si94_eKer2Φ2(B)), then the state of the LNHMDE A(ρ)βNH(t) = B(ρ)u(t), t ≥ 0 is “impulse free”.

Proof

We have

U(0)Ker(Ψ2Φ2(B))Ker(Ψ1Φ1(B))Ker(Ψ2Φ2(B))+Ker(C(1)CΨ1Φ1(B))=Ker(Ψ2Φ2(B))+C(1)CΨ1Φ1(B).

si95_e

The initial conditions of the LHMDEs are compatible, from [13] it is known x(0) = 0. From u(0) = u(1)(0), i = 1, 2, …, l − 1, we know xfu(0) = 0. Subsequently from Eq. (8.12)), J^xf(0)^=0si96_e. So

βf(NH)(t)=(Ψ2Φ2(B))+(C(1)CΨ1Φ1(B))U(t)^,

si97_e

the state of A(ρ)βNH(t) = B(ρ)u(t), t ≥ 0 is impulse free.

8.5 The smooth and impulsive solution components and impulsive free initial conditions: Csi60_e is not of full row rank

This section is devoted to analyze the solution components and impulsive free initial conditions of the LNHMDEs without assuming that Csi60_e is of full row rank.

If Csi60_e is not of full row rank, say its row rank is r1 < r, then there exists a transformation called “row compression,” which reduces Csi60_e to the form

PC=C*0,

si102_e  (8.19)

where C*si103_eis of full row rank r1, it thus satisfies

C*(C*)(1)=Ir1.

si104_e  (8.20)

If one denotes

PβNH(t):=βNH1(t)βNH2(t),PC:=C1C2,

si105_e  (8.21)

where

βNH1(t)Rr1×l,βNH2(t)R(rr1)×1

si106_e

C1Rr1×n,C2R(rr1)×n

si107_e

then one has the following result, which designates the fast and the slow components of the system solution structure.

Theorem 8.5.1

With the above notations, further denoting

βs(NH)1(t)=βs(NH)2(t):=eJtχs(0)+0teJ(tτ)Ωu(τ)dτ

si108_e  (8.22)

and

βf(NH)1(t):=(Ψ2Φ2(B)+(C*)(1)C1Ψ1Φ1(B)U(t)^+(Ψ2Φ2(B)+(C*)(1)C1Ψ1Φ1(B))u(0)J^xf(0)^δ(t)^,

si109_e  (8.23)

βf(NH)2(t):=Ψ1Φ1(B)U(t)^+Ψ1Φ1(B)U(0)δ(t)^,

si110_e  (8.24)

the solution for the LNHMDE (8.7) is

βNH(t)=P1C100C2C*00C2βs(NH)1(t)βs(NH)2(t)βf(NH)1(t)βf(NH)2(t).

si111_e  (8.25)

Proof

From Theorem 8.3.1, one knows that the solution of the LNHMDE (8.7) corresponding to nonzero initial conditions both on the pseudo-state βNH(t) and the input u(t) is

βNH(t)=CeJtxsβ(0)CeJtxsu(0)Ci=1qr^δ(t)(i1)Ji1(Jxfβ(0))+Ci=1qr^δ(t)(i1)Ji1(Jxfu(0))+0tCeJ(tτ)Ωu(τ)dτ+C,CΨΦu(t)u(t)(1)u(t)(qr^+l),t0.

si112_e  (8.26)

From the Proof of Theorem 8.4.1, one further obtains

βNH(t)=CeJtxs(0)+C0teJ(tτ)Ωu(τ)dτCJ^xf(0)δ(t)^+(CΨ1Φ1(B)+CΨ2Φ2(B))(U(t)^+U(0)δ(t)^).

si113_e

Under the transformation P, the above βNH(t) is seen to be transformed into

PβNH(t):=βNH1(t)βNH2(t),

si114_e  (8.27)

where

βNH1(t)=C1eJtxs(0)+C10teJ(tτ)Ωu(τ)dτC*J^xf(0)δ(t)^+(C1Ψ1Φ1(B)+C*Ψ2Φ2(B))(U(t)^+U(0)δ(t)^),

si115_e

by the virtue of that C*si103_e is of full row rank and by using Theorem 8.4.1, the above formulation can subsequently be written into

βNH1(t)=C1,C*βs(NH)1(t)βf(NH)1(t),

si117_e  (8.28)

where the components βs(NH)1(t) and βf(NH)1(t) are given by Eqs. (8.22), (8.23), respectively

βNH2(t)=C2eJtxs(0)+C20teJ(tτ)Ωu(τ)dτ+C2Ψ1Φ1(B)U(t)^+C2Ψ1Φ1(B)U(0)δ(t)^=C2,C2βs(NH)2(t)βf(NH)2(t),

si118_e  (8.29)

where the components βs(NH)2(t) and βf(NH)2(t) are given by Eqs. (8.22), (8.24), respectively. By combining Eqs. (8.28), (8.29) and taking the inverse transformation P−1 of Eq. (8.27) one finally establishes the required results.

Remark 8.5.1

The above theorem serves to designate the fast and slow components in the solutions of LNHMDEs in a general setting; it also enables us to analyze the impulse free initial conditions of the systems in the following manner without assuming that Csi60_e is of full row rank.

Theorem 8.5.2

The set of impulsive free initial conditions for the LNHMDE (8.7) is

HI(NH)=βs(NH)1(0)βs(NH)2(0)βf(NH)10βf(NH)2(0):βs(NH)1(0)=βs(NH)2(0)=χs(0)Rn,βf(NH)1(0)=(Ψ2Φ2(B)+(C*)(1)C1Ψ1Φ1(B))U(0)^,βf(NH)2(0)=Ψ1Φ1(B)U(0)^

si120_e  (8.30)

Proof

From Theorem 8.5.1, it is clearly seen that βNH is impulsive free at t = 0 if and only if βf(NH)1(t) and βf(NH)2(t) are both impulse free at t = 0.

If one partitions

(Ψ2Φ2(B)+(C*)(1)C1Ψ1Φ1(B))U(0):=Π1*(U(0)),Π2*(U(0))

si121_e

where

Π1*(U(0))R×qr^,Π2*(U(0))Rμ×l.

si122_e

Observing Eqs. (8.12), (8.23), one can see that βf(NH)1(t) is impulse free at t = 0 iff

(Ψ2Φ2(B)+(C*)(1)C1Ψ1Φ1(B))U(0)J^xf(0)^=0

si123_e  (8.31)

which hold true iff

Π1*(U(0))J^xf(0)=0,

si124_e

i.e.,

xf(0)KerJ+Im(Π1*(U(0))),

si125_e

and

Π2*(U(0))=0.

si126_e

βf(NH)2(t) is impulse free at t = 0, if and only if

U(0)KerΨ1Φ1(B).

si127_e

The set of the impulsive free initial conditions is thus derived from Theorem 8.5.1.

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