Universidad Nacional de Chimborazo
NOVASINERGIA, 2020, Vol. 3, No. 1, diciembre-mayo, (37-44)
ISSN: 2631-2654
https://doi.org/10.37135/ns.01.05.04
Research Article
Controllability of semilinear evolution equations with impulses and
delays
Controlabilidad de ecuaciones de evolución semilineales con impulsos y retardos
Jesús Aponte
1
, Hugo Leiva
2
*
1
Departamento de Matemáticas, Escuela Superior Politécnica del Litoral. Guayaquil, Ecuador, 090604;
japonte@espol.edu.ec
2
Escuela de Ciencias Matemáticas y Computacionales, Universidad de Tecnología Experimental Yachay. San Miguel de
Urcuquí, Ecuador. 100115
* Correspondence: hleiva@yachaytech.edu.ec
Recibido 20 abril 2020; Aceptado 30 abril 2020; Publicado 01 junio 2020
Abstract:
For many control systems in real life, impulses and delays are intrinsic phenomena that
do not modify their controllability. So we conjecture that, under certain conditions,
perturbations of the system caused by abrupt changes and delays do not affect certain
properties such as controllability. In this regard, we show that under certain conditions,
the impulses and delays as perturbations do not destroy the controllability of systems
governed by evolution equations. As application, we consider a semi-linear wave
equation with impulses and delays.
Keywords:
Controllability, impulsive semilinear evolution equations, semilinear wave equation,
strongly continuous semigroup
Resumen:
Para muchos sistemas de control en la vida real, impulsos y retardos son fenómenos
intrínsecos que no modifican su controlabilidad. Así conjeturamos que, bajo ciertas
condiciones, perturbaciones del sistema causadas por cambios abruptos y retardos no
afectan ciertas propiedades como la controlabilidad. A este respecto, mostramos que
bajo ciertas condiciones, los impulsos y retardos como perturbaciones no destruyen la
controlabilidad de sistemas gobernados por ecuaciones de evolución. Como aplicación
consideramos una ecuación de ondas semilineal con impulsos y retardos.
Palabras clave:
Controlabilidad, ecuaciones de evolución semilineales, ecuación de onda semilineal,
semigrupos fuertemente continuos
1 Introduction
There are several practical examples of control
systems with impulses and delays: a chemical
reactor system with the quantities of different
chemicals serving as the state, a financial system
with two state variables being the amount of money
in a market and the saving rates of a central bank,
and the growth of a population diffusing throughout
its habitat, often modeled by reaction-diffusion
equation. However, one may easily visualize
situations in nature where abrupt changes such as
http://novasinergia.unach.edu.ec
harvesting, disasters, or instantaneous stoking may
occur.
This paper has been motivated by the works done
by Hugo Leiva in Leiva (2015a,c,b) where the
approximate controllability of Semilinear Evolution
Equation with impulses was proved in the case of
non necessarily compact semigroup and bounded
non linear perturbation.
In this paper, we study a more general problem since
we consider the following semilinear evolution
equation with impulses and delays simultaneously
z
0
= Az + Bu(t) + F(t,z
t
,u), z Z, t (0,τ],
z(s) = φ(s), s [r,0],
z(t
+
k
) = z(t
k
) + I
k
(t
k
,z(t
k
),u(t
k
)), k = 1, ..., p.
(1)
where 0 < t
1
< t
2
< t
3
< ·· · < t
p
< τ, Z and U
are Hilbert Spaces, u L
2
(0,τ;U), B : U Z
is a bounded linear operator, standard notation z
t
defines a function from [r,0] to Z by z
t
(s) = z(t +
s),r s 0, I
k
: [0, τ] × Z ×U Z, F : [0,τ] ×
C(r,0;Z) ×U Z are smooth functions, and A :
D(A) Z Z is an unbounded linear operator in
Z which generates a strongly continuous semigroup
{T (t)}
t0
Z non necessarily compact.
We assume the following hypotheses:
(H1) The linear system without impulses (6) is
approximately controllable on [τ δ,τ] for all
0 < δ < τ.
(H2) The functions F, I
k
smooth enough and
kF(t,φ,u)k
Z
akφ(r)k + b,
u U, φ C(r,0;Z). (2)
DEFINITION 1.1 (Approximate Controllability).
The system (1) is said to be approximately
controllable on [0,τ] if for every φ C(r,0; Z),
z
1
Z, ε > 0 there exists u L
2
(0,τ;U) such that
the solution z(t) of (1) corresponding to u satisfies:
kz(τ) z
1
k
Z
< ε.
To address this problem we use a characterization
dense range linear operator from Leiva et al.
(2013), the approximate controllability of the
linear equation on [τ δ,τ] for all τ > 0 and
the ideas presented in Bashirov et al. (2007),
Bashirov & Ghahramanlou (2013) and Bashirov
& Ghahramanlou (2014). The controllability of
impulsive evolution equations has been studied
recently by several authors, but most them study
the exact controllability only, e.g. in Chalishajar
(2011), studied the exact controllability of
impulsive partial neutral functional differential
equations with infinite delay, Radhakrishnan &
Blachandran (2012) studied the exact controllability
of semilinear impulsive integro–differential
evolution systems with nonlocal conditions,
and Selvi & Arjunan (2012) studied the exact
controllability for impulsive differential systems
with finite delay. To the best of our knowledge,
there are a few works on approximate controllability
of impulsive semilinear evolution equations,
worth mentioning: Chen & Li (2010) studied
the approximate controllability of impulsive
differential equations with nonlocal conditions,
using measure of noncompactness and Monch’s
Fixed Point Theorem, and assuming that the
nonlinear term f (t,z) does not depend on the
control variable; Leiva & Merentes (2015) studied
the approximate controllability of the semilinear
impulsive heat equation using the fact that the
semigroup generated by is compact.
When it comes to the wave equation, the situation
is totally different: the semigroup generated by
the linear part is not compact; it is in fact a
group, which can never be compact. Furthermore,
if the control acts on a portion ω of the domain
for the spatial variable, then the system is
approximately controllable only on [0, τ] for τ 2,
which was proved by Leiva & Merentes (2010).
More precisely, the following system governed by
the wave equations was studied.
y
tt
= y + 1
ω
u(t,x), on (0,τ) × ;
y = 0, on (0,τ) × ∂Ω;
y(0,x) = y
0
(x), y
t
(0,x) = y
1
(x), in .
(3)
where is a bounded domain in R
n
, ω is an open
nonempty subset of , 1
ω
denotes the characteristic
function of the set ω, the distributed control u
L
2
([0,τ]; L
2
()) and y
0
H
2
() H
1
0
,y
1
L
2
().
However, if the control acts on the whole domain ,
it was proved in Larez et al. (2011) that the system
is controllable [0, τ], for all τ > 0. More specifically,
the authors studied the following system
y
tt
= y + u(t,x), on (0,τ) × ;
y = 0, on (0,τ) × ∂Ω;
y(0,x) = y
0
(x), y
t
(0,x) = y
1
(x), in ,
(4)
where is a bounded domain in R
n
, the distributed
control u L
2
([0,τ]; L
2
()) and y
0
H
2
()
H
1
0
,y
1
L
2
().
To justify the use of this new technique (Bashirov
& Ghahramanlou, 2014), we consider as an
http://novasinergia.unach.edu.ec 38
application the following semilinear wave equation
with impulses, delays and controls acting on the
whole domain , so that the hypotheses (H1) and
(H2) hold:
2
y
2
t
=
y + u(t,x)
+ f (t,y(t r),
y
t
(t r), u(t)),
on (0,τ) × ;
y = 0, on (0,τ) × ∂Ω;
y(s,x) = φ
0
(s,x),
y
t
(s,x) = φ
1
(s,x),
s [r,0], x ;
y
t
(t
+
k
,x) =
y
t
(t
k
,x)
+ I
k
(t,y(t
k
,x),y
t
(t
k
,x),u(t
k
,x)),
x ,
where 0 < t
1
< t
2
< t
3
< ·· · < t
p
< τ, is a
bounded domain in R
n
, the distributed control u
L
2
([0,τ]; L
2
()), φ
0
C(r,0;H
2
() H
1
0
),φ
1
C(r,0;L
2
()) and the nonlinear functions f ,I
k
:
[0,τ] × R × R × R R are smooth enough and
| f (t, y,v,u)| a
0
p
y
2
+ v
2
+ b
0
, y, v, u R. (5)
2 Controllability of the Linear
Equation
In this section we present some characterization of
the approximate controllability of the corresponding
linear equations without impulses and delays. To
this end, we note that for all z
0
Z and u
L
2
(0,τ;U) the initial value problem
(
z
0
= Az + Bu(t), z Z;
z(t
0
) = z
0
,
(6)
admits only one mild solution given by
z(t) = z(t,t
0
,z
0
,u) =
T (t)z
0
+
Z
t
t
0
T (t s)Bu(s)ds, t [t
0
,τ], 0 t
0
τ.
(7)
(See for example (Curtain & Zwart, 1995; Leiva,
2003)).
DEFINITION 2.1. For system (6) we define the
following concept: The controllability map G
τδ
:
L
2
(τ δ,τ;U)) Z defined by
G
τδ
u =
Z
τ
τδ
T (τ s)Bu(s)ds, u L
2
(τ δ,τ;U),
(8)
The adjoint of this operator G
τδ
: Z L
2
(τδ,τ;U)
is given by
(G
τδ
z)(t) = B
T
(τ t)z, t [τ δ,τ].
The Gramian controllability operators are given by:
Q
τδ
= G
τδ
G
τδ
=
Z
τ
τδ
T (τt)BB
T
(τ t)dt. (9)
The following lemma holds in general for a linear
bounded operator G : W Z between Hilbert
spaces W and Z (Bashirov et al., 2007; Leiva et al.,
2013; Curtain & Pritchard, 2010; Curtain & Zwart,
1995).
LEMMA 2.1. The following statements are
equivalent to the approximate controllability of the
linear system (6) on [τ δ,τ].
a) Range(G
τδ
) = Z.
b) Ker(G
τδ
) = {0}.
c) hQ
τδ
z,zi > 0, z 6= 0 in Z.
d) lim
α0
+
α(αI + Q
τδ
)
1
z = 0.
e) For all z Z, we have G
τδ
u
α
= z α(αI +
Q
T δ
)
1
z, where
u
α
= G
τδ
(αI + Q
τδ
)
1
z, α (0,1].
So, lim
α0
G
τδ
u
α
= z and the error E
τδ
z of this
approximation is given by the formula
E
τδ
z = α(αI + Q
τδ
)
1
z, α (0, 1].
f) Moreover, if we consider for each v L
2
(τ
δ,τ;U)) the sequence of controls given by
u
α
= G
τδ
(αI + Q
τδ
)
1
z+
(v G
τδ
(αI + Q
τδ
)
1
G
τδ
v), α (0,1],
we get that:
G
τδ
u
α
= z α(αI + Q
T δ
)
1
(z + G
τδ
v)
and
lim
α0
G
τδ
u
α
= z,
with the error E
τδ
z of this approximation given
by the formula
E
τδ
z = α(αI + Q
τδ
)
1
(z + G
τδ
v), α (0, 1].
REMARK 2.1. The foregoing lemma implies that the
family of linear operators
Γ
ατδ
: Z W , defined for 0 < α 1 by
Γ
ατδ
z = G
τδ
(αI + Q
τδ
)
1
z, (10)
is an approximate right inverse of the operator W ,
in the sense that
lim
α0
G
τδ
Γ
ατδ
= I. (11)
in the strong topology.
http://novasinergia.unach.edu.ec 39
LEMMA 2.2. Leiva et al. (2013) Q
τδ
> 0 if and only
if the linear system (6) is controllable on [τ δ,τ].
Moreover, given an initial state y
0
and a final state
z
1
we can find a sequence of controls {u
δ
α
}
0<α1
L
2
(τ δ,τ;U)
u
α
= G
τδ
(αI +G
τδ
G
τδ
)
1
(z
1
T (τ)y
0
), α (0,1],
such that the solutions y(t) = y(t, τδ,y
0
,u
δ
α
) of the
initial value problem
(
y
0
= Ay + Bu
α
(t), y Z, t > 0;
y(τ δ) = y
0
,
(12)
satisfy
lim
α0
+
y(τ,τ δ,y
0
,u
α
) = z
1
,
i.e.,
lim
α0
+
y(τ) =
lim
α0
+
T (δ)y
0
+
Z
τ
τδ
T (τ s)Bu
α
(s)ds
= z
1
.
3 Controllability of the Semilinear
Equation
In this section we prove the main result of this
paper, that is, the approximate controllability of the
semilinear impulsive evolution equation given by
(1). To this end, for all φ C and u C(0,τ;U)
the initial value problem
z
0
= Az + Bu + F(t,z
t
,u(t)), z Z, t 0;
z(s) = φ(s), s [r,0];
z(t
+
k
) = z(t
k
) + I
k
(t
k
,z(t
k
),u(t
k
)), k = 1, ..., p,
(13)
admits only one mild solution z PC(r,τ; Z) given
by
z(t) =
T (t)φ(0)+
Z
t
0
T (t s)Bu(s) ds
+
Z
t
0
T (t s)F(s,z
s
,u(s)) ds
+
0<t
k
<t
T (t t
k
)I
k
(t
k
,z(t
k
),u(t
k
))
t [0, τ];
φ(t), t [r,0].
(14)
Now, we are ready to present and prove the
main result of this paper, which is the interior
approximate controllability of heat equation with
delays (1).
THEOREM 3.1. Under conditions (H1) and (H2),
the semilinear system (1) with impulses and delays
is approximately controllable on [0, τ].
Proof. Given an initial state φ, a final state z
1
and
ε > 0, we want to find a control u
δ
α
L
2
(0,τ;U)
steering the system from φ(0) to an ε-neighborhood
of z
1
at time τ. In other word, there exists
control u
δ
α
L
2
(0,τ; U) such that corresponding of
solutions z
δ,α
of (1) satisfies:
kz
δ,α
(τ) z
1
k ε.
In fact, consider any u L
2
(0,τ;U) and the
corresponding solution z(t) = z(t,0,z
0
,u) of the
initial value problem (13). For α (0,1] we define
the control u
δ
α
L
2
(0,τ;U) as
u
δ
α
(t) =
(
u(t), if 0 t τ δ;
u
α
(t), if τ δ < t τ,
where
u
α
(t) =
B
T
(τ t)(αI + G
τδ
G
τδ
)
1
(z
1
T (δ)z(τ δ)),
τ δ < t τ.
Now, assume that 0 < δ < τ t
p
. Then the
corresponding solution z
δ
α
(t) = z(t,0, z
0
,u
δ
α
) of the
initial value problem (13) at time τ can be written as
follows:
z
δ,α
(τ) =
T (τ)φ(0) +
Z
τ
0
T (τ s)Bu
δ
α
(s)ds
+
Z
τ
0
T (τ s)F(s,z
δ,α
s
,u
δ
α
(s))ds
+
0<t
k
<τ
T (τ t
k
)I
k
(z
δ,α
(t
k
),u
δ
α
(t
k
))
= T (δ)
T (τ δ)φ(0) +
Z
τδ
0
T (τ δ s)Bu
δ
α
(s)ds
+
Z
τδ
0
T (τ δ s)F(s,z
δ,α
s
,u
δ
α
(s))ds
+
0<t
k
<τδ
T (τ δ t
k
)I
k
(z
δ,α
(t
k
),u
δ
α
(t
k
))
)
+
Z
τ
τδ
T (τ s)Bu
δ
α
(s)ds
+
Z
τ
τδ
T (τ s)F(s,z
δ,α
s
),u
δ
α
(s))ds
= T (δ)z(τ δ) +
Z
τ
τδ
T (τ s)Bu
α
(s)ds
+
Z
τ
τδ
T (τ s)F(s,z
δ,α
s
,u
α
(s))ds.
http://novasinergia.unach.edu.ec 40
Thus,
z
δ,α
(τ) = T (δ)z(τ δ) +
Z
τ
τδ
T (τ s)Bu
α
(s)ds
+
Z
τ
τδ
T (τ s)F(s,z
δ,α
s
,u
α
(s))ds.
The corresponding solution y
δ
α
(t) = y(t,τ δ,z(τ
δ),u
α
) of the initial value problem (12) at time τ is
given by:
y
δ
α
(τ) = T (δ)z(τ δ) +
Z
τ
τδ
T (τ s)Bu
α
(s)ds.
Therefore,
kz
δ,α
(τ) y
δ
α
(τ)k
Z
τ
τδ
kT (τ s)k{akz
δ,α
(s r)k+b}ds.
If we take 0 < δ < r and τ δ s τ, then s r
τ r < τ δ and
z
δ,α
(s r) = z(s r).
Thus, there exists δ small enough such that 0 < δ <
min{r,τ t
p
} and
kz
δ,α
(τ) y
δ,α
(τ)k
Z
τ
τδ
kT (τ s)k{akz(s r)k + b} ds <
ε
2
.
Hence,
kz
δ,α
(τ) z
1
k
Z
τ
τδ
kT (τ s)k{akz
δ,α
(s r)k+b}ds
+ ky
δ,α
(τ) z
1
k
=
Z
τ
τδ
kT (τ s)k{akz(s r)k + b} ds
+ ky
δ,α
(τ) z
1
k
<
ε
2
+
ε
2
< ε.
Geometrically, the proof goes as follows:
CONTROLLABILITY OF EVOLUTION EQUATIONS WITH IMPULSES AND DELAY. 7
if we take 0 < δ < r and τ δ s τ, then s r τ r < τ δ and
z
δ,α
(s r) = z(s r).
Therefore, there exists δ small enough such that 0 < δ < min{r, τ t
p
} and
kz
δ,α
(τ) y
δ,α
(τ)k
Z
τ
τ δ
kT (τ s)k{akz(s r)k + b}ds <
ǫ
2
.
Hence,
kz
δ,α
(τ) z
1
k
Z
τ
τ δ
kT (τ s)k{akz
δ,α
(s r)k + b}ds + ky
δ,α
(τ) z
1
k
=
Z
τ
τ δ
kT (τ s)k{akz(s r)k + b}ds + ky
δ,α
(τ) z
1
k
<
ǫ
2
+
ǫ
2
< ǫ.
Geometrically, the proof goes as follows:
z
0
z(τ δ)
z
δ,α
(
s
r) = z
(s
r)
z(τ )
z
δ
α
(τ )
y
δ
α
(τ )
z
1
ε
This completes the proof of the theor em.
This completes the proof of the theorem.
4 Applications
As an application, we prove the approximate
controllability of the following control system
governed by the semilinear wave equation with
impulses and delays
2
y
2
t
=
y + u(t,x)
+ f (t,y(t r),
y
t
(t r), u(t)),
on (0,τ) × ;
y = 0, on (0,τ) × ∂Ω;
y(s,x) = φ
0
(s,x),
y
t
(s,x) = φ
1
(s,x),
s [r,0], x ;
y
t
(t
+
k
,x) =
y
t
(t
k
,x)
+ I
k
(t,y(t
k
,x),y
t
(t
k
,x),u(t
k
,x)),
x ,
(15)
where 0 < t
1
< t
2
< t
3
< ·· · < t
p
< τ, is a
bounded domain in R
n
, the distributed control u
L
2
([0,τ]; L
2
()), φ
0
C(r,0;H
2
() H
1
0
),φ
1
C(r,0;L
2
()) and the nonlinear functions f ,I
k
:
[0,τ] × R × R × R R are smooth enough and f
satisfies (5).
4.1 Abstract Formulation of the
Problem
First we choose the space where this problem will
be set up as an abstract control system in a Hilbert
space. Let X = L
2
() = L
2
(,R) and consider
the linear unbounded operator A : D(A) X X
defined by Aφ = ∆φ, where
D(A) = H
2
(,R) H
1
0
(,R). (16)
Then the eigenvalues λ
j
of A have finite multiplicity
γ
j
equal to the dimension of the corresponding
eigenspace and 0 < λ
1
< λ
2
< ·· · < λ
n
.
Moreover,
a) there exists a complete orthonormal set {φ
j,k
} of
eigenvectors of A;
b) for all x D(A) we have
Ax =
j=1
λ
j
γ
j
k=1
< x,φ
j,k
> φ
j,k
=
j=1
λ
j
E
j
x,
(17)
where < ·,· > is the usual inner product in L
2
and
E
j
x =
γ
j
k=1
< x,φ
j,k
> φ
j,k
, (18)
http://novasinergia.unach.edu.ec 41
which means the set {E
j
}
j=1
is a complete
family of orthogonal projections in X and x =
j=1
E
j
x, x X;
c) A generates an analytic semigroup {e
At
}
given by
e
At
x =
j=1
e
λ
j
t
E
j
x; (19)
d) the fractional powered spaces X
r
are given by:
X
r
= D(A
r
) = {x X :
n=1
λ
2r
n
kE
n
xk
2
< }, r 0,
with the norm
kxk
r
= kA
r
xk =
(
n=1
λ
2r
n
kE
n
xk
2
)
1/2
,x X
r
, and
A
r
x =
n=1
λ
r
n
E
n
x. (20)
Also, for r 0 we define Z
r
= X
r
× X, which is
a Hilbert space endowed with the norm:
y
v
Z
r
=
q
kyk
2
r
+ kvk
2
.
Then, the equations (1) can be written as an abstract
second order ordinary differential equations in Z
1/2
as follows
y
00
=
Ay + u
+ f
e
(t,y(t r),y
0
(t r), u),
t (0, τ], t 6= t
k
,
y(s) = φ
0
(s), y
0
(s) = φ
1
(s), s [r,0],
y
0
(t
+
k
) =
y
0
(t
k
) + I
e
k
(t
k
,y(t
k
),y
0
(t
k
),u(t
k
)),
k = 1, ..., p,
(21)
where
I
e
k
: [0,τ] × Z
1/2
×U Z
1/2
and
f
e
: [0,τ] ×C
0
×C
1
×U Z
1/2
with C
0
= C(r,0;Z
1/2
) and C
1
= C(r,0;Z) are
defined by
I
e
k
(t,y,v,u)(x) =
I
k
(t,y(x), v(x),u(x)), x , k = 1,2,..., p,
f
e
(t,φ
0
,φ
1
,u)(x) =
f (t,φ
0
(r,x),φ
1
(r,x),u(x)),
x ,
φ
0
φ
1
C
0
×C
1
.
With the change of variables y
0
= v, we can write the
second order equation (21) as a first order system of
ordinary differential equations in the Hilbert space
Z
1/2
= X
1/2
× X as follows:
z
0
=
Az + Bu
+ F(t,z(t r),u(t)),
z Z
1/2
, t (0,τ], t 6= t
k
;
z(s) = φ(s), s [r,0];
z(t
+
k
) =
z(t
k
) + J
k
(t
k
,z(t
k
),u(t
k
)),
k = 1, ..., p,
(22)
where u L
2
([0,τ];U) and C = C
0
× C
1
=
C(r,0;Z
1/2
),
φ =
φ
0
φ
1
C, z =
y
v
, B =
0
I
z and A =
0 I
X
A 0
(23)
is an unbounded linear operator with domain
D(A) = D(A) × D(A
1/2
) and
J
k
: [0,τ] × Z
1/2
× U Z
1/2
, F : [0,τ] × C ×U
Z
1/2
are defined by:
F(t,φ,u) =
0
f
e
(t,φ
0
,φ
1
,u)
and J
k
(t,z, u) =
0
I
e
k
(t,y,v,u)
. (24)
The following result follows from condition (5)
PROPOSITION 4.1. Under the conditions (5) the
functions F satisfy:
kF(t,φ,u)k
Z
1/2
˜a
0
kφ(r)k
Z
1/2
+ b
0
. (25)
It is well known that the operator A generates a
strongly continuous group
{
T (t)
}
t0
in the space
Z = Z
1/2
= X
1/2
× X (Chen & Triggiani, 1989).
Now, using Lemma 2.1 from Leiva (2003) or
Lemma 3.1 from Carrasco & Leiva (2007), one can
get the following representation for this group.
PROPOSITION 4.2. The group
{
T (t)
}
t0
generated
by the operator A has the following representation
T (t)z =
n j=1
e
A
j
t
P
j
z, z Z
1/2
, t 0, (26)
where
P
j
j0
is a complete family of orthogonal
projections in the Hilbert space Z
1/2
given by
P
j
=
E
j
0
0 E
j
, j 1, (27)
and
A
j
= R
j
P
j
, R
j
=
0 1
λ
j
0
, j 1. (28)
http://novasinergia.unach.edu.ec 42
4.2 Approximate Controllability
Now, we are ready to formulate and prove the main
result of the this section, which is the approximate
of the semilinear impulsive wave equation with
bounded nonlinear perturbation.
THEOREM 4.1. The semilinear wave equation
(15) with impulses and delays is approximately
controllable on [0,τ].
Proof. From Larez et al. (2011), we know that the
corresponding linear system without impulses
(
z
0
= Az + Bu, z Z
1/2
, t (0,τ];
z(0) = z
0
,
(29)
is controllable on [τ δ,τ] for all 0 < δ < τ. On
the other hand, the hypothesis (H1) and (H2) in
Theorem 3.1 are satisfied, and we get the result.
5 Final Remark
This technique can be applied to those systems
where the linear part does not generate a compact
semigroup, are controllable on any [0,δ] for δ >
0, and the nonlinear perturbation is bounded. An
example of such systems is the following controlled
thermoelastic plate equation whose linear part was
studied in Larez et al. (2011).
y
tt
+
2
y + α∆θ
=u
1
(t,x) + f
1
(t,y,y
t
,θ, u(t)),
on (0,τ) × ,
θ
t
β∆θ α∆y
t
= u
2
(t,x) + f
2
(t,y,y
t
,θ, u(t)),
on (0,τ) × ,
θ = y = y = 0, on (0,τ) × ∂Ω,
y
t
(t
+
k
,x) =
y
t
(t
k
,x)
+ I
1
k
(t,y(t
k
,x),y
t
(t
k
,x),u(t
k
,x)),
x ,
θ(t
+
k
,x) =
θ(t
k
,x)+I
2
k
(t
k
,θ(t
k
,x),u(t
k
,x)),
x ,
(30)
in the space Z = X
1
× X × X, where is a
bounded domain in R
n
, the distributed controls
u
1
,u
2
L
2
([0,τ]; L
2
()) and I
i
k
, f
i
are smooth
functions with f
i
,i = 1, 2 bounded. Of course,
for finite-dimensional control systems, all these
results are valid for exact controllability; so from
the point of view of applications, we can study
real life control systems governed by ordinary
differential equations in finite-dimensional spaces,
with impulses and delays.
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