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In connection with the fact that

γ

= (

k

M

1

k

εL

+

k

P

k

)

e

λt

1

λ

0

.

947

<

1

, the condition of theorem 3 has been satisfied and the

terminal problem under consideration has got a solution.

Now we select the function

b

1

(

t

) =

t

3

+

t

2

as the function

b

1

(

t

)

,

which satisfies the conditions

b

1

(0) = 0

, b

0

1

(0) = 0

, b

1

(2) =

4

, b

0

1

(2) =

8

,

and the function

b

2

(

t

) =

t

3

2

t

2

as the function

b

2

(

t

)

, which satisfies the

conditions

b

2

(0) = 0

, b

0

2

(0) = 0

, b

2

(2) = 0

, b

0

2

(2) = 4

.

Let us specify the initial approximation for the vector of parameters

c

(0)

= (0; 0)

T

and the accuracy

σ

= 0

.

001

. Let us build the sequence

of approximations

{

c

(

j

)

}

using formula (25), assuming that

η

= (

5; 4)

T

,

Ψ(

c

(

j

)

) =

η

(

t

, c

(

j

)

)

, where

η

(

t, c

(

j

)

) = (

η

1

(

t, c

(

j

)

)

, η

2

(

t, c

(

j

)

))

T

, which is

the solution to the Cauchy problem:

˙

η

1

=

0

.

1

η

2

+

b

1

(

t

) +

c

(

j

)

1

d

(

t

) +

b

0

2

(

t

)+

+

c

(

j

)

2

d

0

(

t

) + 0

.

08 cos(

b

0

1

(

t

) +

c

(

j

)

1

d

0

(

t

);

˙

η

2

= 0

.

1

η

1

+

b

2

(

t

) +

c

(

j

)

2

d

(

t

) +

b

1

0

(

t

)+

+

c

(

j

)

1

d

0

(

t

)

0

.

08 sin(

b

0

2

(

t

) +

c

(

j

)

2

d

0

(

t

);

η

1

(0) = 0

, η

2

(0) = 0

,

being determined on each iteration using the Runge – Kutta method of the

fourth order. The calculations showed that inequality (27) can be fulfilled

with

J

= 6

, hence the point

c

(6)

= (

3

.

287; 8

.

933)

T

is the fixed point of

the mapping v with the accuracy

σ

. The functions

z

1

1

=

b

1

(

t

) +

c

(6)

1

d

(

t

)

, z

1

2

=

b

0

1

(

t

) +

c

(6)

1

d

0

(

t

)

, z

2

1

=

b

2

(

t

) +

c

(6)

2

d

(

t

)

,

z

2

2

=

b

0

2

(

t

) +

c

(6)

2

d

0

(

t

);

η

1

=

η

1

(

t, c

(6)

)

, η

2

=

η

2

(

t, c

(6)

)

specify the

t

-parameter curve in the range of system (28) conditions,

connecting the initial and final system statuses. The controls

u

1

=

b

00

1

(

t

) +

+

c

(6)

1

d

00

(

t

)

,

u

2

=

b

00

2

(

t

) +

c

(6)

2

d

00

(

t

)

realize this curve as the trajectory of

system (28) and are a solution of the terminal problem under consideration.

Functional relations

z

1

1

(

t

)

,

z

2

1

(

t

)

,

z

1

2

(

t

)

,

z

2

2

(

t

)

,

η

1

(

t

)

,

η

2

(

t

)

,

u

1

(

t

)

,

u

2

(

t

)

are

shown in the picture.

Conclusion.

The terminal problem for the affine systems, which are

not linearizable by a feedback, is considered. It is supposed that using

a smooth nondegenerate change of variables within the range of states,

28

ISSN 1812-3368. Herald of the BMSTU. Series “Natural Sciences”. 2014. No. 5