Abstract: - This work is devoted to the refinement of the approximate solution, obtained by the pro-
jection method. The proposed approach uses expanding the design space by adding new coordinate
functions. As a result, it is possible to clarify previously obtained solution using small computer re-
sources. Applying this approach to the finite element method allows produce a local refinement of the
mentioned solution. Suggested Approach illustrated in the finite element method for a boundary value
problem second order in one-dimensional and two-dimensional cases.
Key-Words: - a posteriori improvement, refinement calculations, variational-grid methods
1 Introduction
The research in the field of artificial intelligence
covers many areas of the development of science
and practice. These studies give opportunities to
optimize efforts aimed at the effective solution of
difficult problems. Here we give examples of some
studies in the mentioned area.
Paper, [1], predicts the future of excitation
energy transfer with artificial intelligence-based
quantum dynamics.
In the paper, [2], the authors propose algo-
rithm with fast convergence rate for federated
edge learning.
In paper, [3], the authors propose a new algo-
rithm of machine learning techniques. Based on
recent advancements in music structure analysis,
the authors of paper, [4], automate the evaluation
process by introducing a collection of metrics.
The development of a disagreement-based on-
line learning algorithm is given in [5].
In [6], the authors develop a deep learning-
based approach to model.
Let us mention some works in which itis possi-
ble to effectively use learning systems and means
of artificial intelligence.
The paper, [7], is devoted to the solution of the
nonstationary integro-differential equation with a
degenerate elliptic differential operator.
It seems that adaptive methods developed
with the help of artificial intelligence greatly sim-
plify the solution of problems of mathematical
physics.
The article, [8], investigate the approxi-
mate solution to a nonlinear Volterra integro-
differential equation.
In the article, [9], the authors have proposed a
highly efficient and accurate collocation method.
It can also be assumed that the mentioned
means would be useful in solving the problems
considered in the works, [10], [11].
This paper is devoted to the posteriori im-
provement of the approximation in the projec-
tion method for solving a linear equation with a
self-adjoint positive definite operator. Improve-
ment was obtained by expanding the projection
space. The mentioned extension is a linear span,
an original projection space and an added element
energy space. The consideration of a given priori
parameterized class of elements that allow you to
build an adaptive method with the mentioned im-
provement. The proposed approach is applied to
the methods finite elements for one-dimensional
boundary second order tasks.
The consistent application of this approach al-
lows us to optimize the process of refining the nu-
merical solution of the boundary value problem
without significantly increasing the requirements
for computing system resources. The proposed
approach leads to the construction of adaptive
sequences of ambient spaces. These spaces form
a telescopic system of nested spaces, on the basis
of which an adaptive wavelet packet is built for
the economical transmission of information.
2 Background
Consider a Hilbert space Hwith a scalar prod-
uct (u, v). Let Abe a positively self-adjoint de-
fined operator with domain D(A). Consider the
energy space HAof the operator A. We denote
the norm and the scalar product in the space YA
IuIand [u, v] respectively, so that IuI=p[u, u].
A Posteriori Improvement in Projection Method
YURI K. DEM'YANOVICH, IRINA G.BUROVA
Saint Petersburg State University Saint Petersburg, RUSSIA
Received: December 13, 2022. Revised: May 29, 2023. Accepted: June 21, 2023. Published: July 24, 2023.
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Here u, v HA. In the discussed conditions the
solution of the problem
Au =f, f H(1)
is equivalent to the solution of the next problem
min
uHA
F(u),(2)
F(u) = IuI22(u, f).(3)
Denote uthe solution to problem (2) (and
hence also the solution to problem (1)). Let S
be a subspace of HA. Consider the solution euto
the problem
min
e
uSF(eu).(4)
Thanks to the well-known representation
F(u) = IuuI2IuI2(5)
problem (4) is equivalent to problem
min
e
uS
IueuI,(6)
so
IueuIIueuIeuS. (7)
It is clear from (4) that eusatisfies the identity
[eu,ev] = (f, ev)evS. (8)
Consider the element ϕof the energy space
HA, assuming that ϕ /S. Let S1be the linear
span of the space Sand element ϕ,
S1
def
=L{S, ϕ},(9)
where L{. . .}means the linear span of the ob-
jects, which are in curly brackets.
Consider the function
F(t)def
=F(eu+).(10)
Let us pose the question of finding the point
tof the minimum of this function,
min
tR1F(t).(11)
Since F(t) is a quadratic function and
limt→±∞ F(t)=+, a desired point exists and
it is unique. We have
F(eu+) = Ieu+I22(eu+tϕ, f) =
=IeuI2+ 2t[eu, ϕ] + t2IϕI22(eu, f)2t(ϕ, f).
(12)
Lemma 1. Representation
F(t) = At2+ 2Bt +C, (13)
is right. Here
A=IϕI2, B = [eu, ϕ](eu, f ),
C=IeuI22(eu, f).(14)
Proof. Formulas (13) (14) follow from rela-
tions (3), (9), and (12).
Lemma 2. Relations
t=(f, ϕ)[eu, ϕ]
IϕI2,(15)
F(t) = {(f, ϕ)[eu, ϕ]}2
IϕI2+F(eu).(16)
are fulfilled.
Proof. Obviously, the minimum point tof
quadratic form (13) has the form t=B/A, and
the value of this quadratic form at the mentioned
point is equal to Φ(t) = B2/A+C. Taking into
account formulas (14), we obtain the equalities
(15) and (16).
Theorem 1. A formula
F(eu+tϕ) = F(eu){(f, ϕ)[eu, ϕ]}2
IϕI2(17)
is correct.
Proof. Formula (17) is obtained from relations
(9) and (16).
Formula (17) means that for ϕ /Sthe energy
initial approximation eucan be reduced by the
transition to a new approximation eu+tϕ. The
inequality
Ieu+tϕuI2=IeuuI2E, (18)
follows from (17). Here
Edef
={[eu, ϕ](f, ϕ)}2
IϕI2.(19)
The element ϕis called qualifying element,
and the number Eis local energetic clarification.
Remark 1. By selecting the element ϕHA,
the energy approximation will be greatly im-
proved. Thus, it is necessary to find
Mdef
= max
ϕHA
{(f, ϕ)[eu, ϕ]}2
IϕI2.
Due to the relation (f, ϕ)[u, ϕ] we have
M= max
ϕHA, ϕ6=0
{[ueu, ϕ]}2
IϕI2.
It is clear that
M= max
ψHA,IψI=1{[ueu, ψ]}2.(20)
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It can now be seen that the maximum occurs at
ψ=ψ
def
=ueu
IueuI,
so M=IueuI2. In this way, the energy ap-
proximation is maximally improved if, in formula
(17) takes ϕ=ϕ
def
=ueu. According to for-
mula (15) for ϕ=ϕwe have
t=(f, ϕ)[eu, ϕ]
IϕI2=[ueu, ϕ]
IϕI2= 1,
for ϕ=ϕ.
From formulas (5) and (17) we obtain the min-
imum value IuI2of the functional F(u) in
space HA,F(eu+tϕ) = IuI2and eu+tϕ=
u. The result obtained indicates the logical in-
tegrity. The approach is under consideration.
3 Refinement space
Consider in the energy space HAalso one finite-
dimensional subspace Φ with the properties Φ
S={0}. Let ϕ1, . . . , ϕNbe the basis of this
space. Denote S1is the linear span of the spaces
Sand Φ
S1=L{S, Φ}.(21)
In what follows, tmeans a N-dimensional vec-
tor, tRN,t= (t1, t2, . . . , tN). The symbol ·
is used to denote the linear combination of ele-
ments ϕ1, . . . , ϕN,t·ϕ=PN
i=1 tiϕi. Consider
the function
F(t) = F(˜u+t·ϕ),(22)
where F(u) is the energy functional (3). Since
F(t) is a quadratic function with a positive defi-
nite principal part, then there exists and uniquely
problem solution t
min
tRNF(t).(23)
We have
F(˜u+t·ϕ) =
=I˜u+t·ϕI22(˜u+t·ϕ, f) =
=I˜uI22(˜u, f)+2
N
X
i=1
{[˜u, ϕi](˜
f, ϕi)}ti+
+
N
X
i,j=1
[ϕi, ϕj]titj.
(24)
Consider matrix A0, vector B0and constant
C0defined by equalities
A0= ([ϕi, ϕj])N
i,j=1, B0= ([˜u, ϕi](f, ϕi))N
i=1,
(25)
C0=I˜uI22(˜u, f).(26)
Lemma 3.
F(t)=(A0t, t) + 2(B0, t) + C0,(27)
where parentheses mean scalar preproduction
to RN.
Proof. Formula (27) follows from relations
(22) and (24) (26).
Lemma 4.
t=A1
0B0,F(t) = C0(B0, A1
0B0).(28)
Proof. From the positive definiteness of the
quadratic form (27) follows the existence and
uniqueness points of minimum t. Equating to
zero the partial derivatives with respect to ti,
i= 1,2, . . . , N, we get tin the first relation (28).
Substituting tinto (27) gives the second of the
relation (28).
Theorem 2.
F(˜u+t·ϕ) = F(˜u)(B0, A1
0B0).(29)
Proof. Formula (29) is obtained from relations
(21) and (25) (28).
Formula (29) means that under the conditions
considered, the energy initial approximation ˜u
can be reduced by transition to a new approxi-
mation ˜u+t·ϕ. From (29) follows the relation
I˜u+t·ϕuI2=I˜uuI2E, (30)
where
E= (B0, A1
0B0),(31)
while the matrix A0and the vector B0are defined
by relations (25).
The element t·ϕis called qualifying element,
and the number Eis local energetic clarification.
4 Triangulation and its refinement
with stable boundary
We consider regular rectilinear triangulations of
polygonal domains on the plane R2(otherwise
called triangular sets). Triangulation is consid-
ered regular if each edge is a side of some trian-
gle, and the end of the edge cannot be an interior
point of another rib. Proper triangulation allows
for refinement, which are again regular triangula-
tions.
Let Mbe a closed polygonal domain of the
plane R2. We denote its boundary by M. Con-
sider some triangulation Tof M. Denote the
s-skeleton of the triangulation Tby Ts,s
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{0,1,2}(i.e. T0is the set of vertices, T1is the
set of edges, and T2is the set of triangles). We
will assume that T0={vi|i= 1,2, . . . , K},T1=
{ls|s= 1,2, . . . , L},T2={Tj|j= 1,2, . . . , N}.
Triangulation Tis also called a two-
dimensional (triangular) complex. A set-
theoretic closure union of points of triangles in the
triangular complex Tis called the body of the tri-
angular complex. The triangular body complex
is denoted by |T |. It matches with area M. The
triangular body border complex Tis the set M.
Sets T0def
={vi|vi T 0, viM},T1def
=
{ls|ls T 1, lsM} with induced incidence
relations generate a one-dimensional complex T
subdividing the boundary Mof the region un-
der consideration M. Complex Tis called the
induced boundary complex. Its body coincides
with the boundary Mof the domain M.
Refining Ttriangulation Tis a new simplicial
complex. If at the same time the induced bound-
ary complex is preserved,
T=T,(32)
then the triangulation of Tis called refinement
with a stable boundary for the triangulation T.
In what follows, we associate the vertex viwith
the vector ri, emanating from the origin and end-
ing at the mentioned vertex. In the case under
consideration, a topological triangulation struc-
ture is described by an incidence matrix MTof
the size 3 ×N, whose i-th line contains the ver-
tices of the i-th triangle.
Remark 3. Changing the order of matrix
rows MTmatches the renumbered triangles, and
changing the order of the elements in any row
of the matrix does not change the incidence cor-
respondences between the triangle and vertices.
Thus, a matrix derived from the original one by
the mentioned transformations describes the old
topological structure of the triangulation. We
also note, that the duplication of the rows in the
incidence matrix does not violate the topologi-
cal structure of triangulation (because the ”mul-
tiplicity” triangles are not considered).
The barycentric star of vertex r T 0is de-
noted by Z(r). The closure for the union of the
points of its triangles is called the body of the
barycentric star. The body of a barycentric star
is denoted by |Z(r)|.
Two triangles are considered adjacent if they
have a common edge. We will assume that each
triangle Tof the triangulation under consider-
ation has sneighboring triangles, where s
{1,2,3}. If s= 3 then triangle Tis called the
inner triangle of the triangulation T, and for
s {1,2}the triangle Tis called boundary tri-
angle.
The set of neighboring triangles for Twith the
addition of the given triangle T, we call the a
star triangle T. The star of the triangle Twill
be denoted by Z(T). The set-theoretic union tri-
angles from Z(T) is called the body of the star
Z(T), and is denoted by |Z(T)|. Note that both
the barycentric vertex star and the star triangles
are regular triangulations (triangular complexes).
Therefore, it is possible to refine these triangula-
tions.
Consider an interior triangle Twith vertices
r1,r2,r3and its star Z(T). Select the fragment
MZ(T)of the matrix MTrelated to to the star
Z(T). In view of Remark 2 above, without loss
of generality, we have
MZ(T)= r1r1r2r1
r2r2r3r3
r3r5r6r4!T
.(33)
Consider vector functions of the variable ξ[0,1]
r12(ξ)def
=ξr1+ (1 ξ)r2,r23(ξ)def
=ξr2+ (1 ξ)r3,
(34)
r32(ξ)def
=ξr3+ (1 ξ)r1.(35)
Theorem 3. If Tis an interior triangle
with vertices r1,r2,r3, then for a fixed parameter
ξ(0,1) triangulation T(ξ)defined by incidence
matrix
M(ξ)
def
= (V1, V2, V3, V4, V5, V6, V7, V8, V9, V10)T,
(36)
where
V1= r12(ξ)
r23(ξ)
r31 !, V2= r2
r23(ξ)
r12(ξ)!,
V3= r3
r31(ξ)
r23(ξ)!, V4= r1
r12(ξ)
r31(ξ)!,
V5= r1
r5
r12(ξ)!, V6= r12(ξ)
r5
r2!,
V7= r2
r6
r23(ξ)!, V8= r3
r23(ξ)
r6!,
V9= r3
r4
r31(ξ)!, V10 = r1
r31(ξ)
r4!.
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M(ξ)is a refinement with a stable boundary for
triangulation Z(T). In addition, the relations
lim
ξ+0 T(ξ)= lim
ξ10T(ξ)=Z(T).(37)
Proof. For fixed ξ(0,1) formulas (34) (35)
define points lying inside the edges (sides) of tri-
angle T. Taking into account the structure of the
matrix (36), we arrive at the conclusion that the
simplicial complex T(ξ)is the subdivision of the
star Z(T). Relation (32) is obvious, and therefore
the subdivision T(ξ)is the refinement with a sta-
ble boundary for Z(T). Using Remark 1 and the
formulas r12(0) = r2,r12(1) = r1,r23(0) = r3,
r23(1) = r2,r32(0) = r2,r32(1) = r3, we derive
at relations (37).
Remark 3. Similar assertions hold for bound-
ary triangles.
5 Energy refinement for the finite
elements in a two-dimensional
problem
Triangulation refinement while maintaining less
correctness can be obtained by the successive
application of elementary grinding. Elementary
grinding is the grinding in which one vertex with
corresponding edges is added. Two types of ele-
mentary grindings exist.
The first type of elementary grinding is as fol-
lows. A pair of adjacent triangles with vertices r1,
r2,r3,r4after adding rξto the edge (r1,r3) and
after adding edges (r2,rξ) and (r4,rξ) becomes
four triangles according to display
r1r1
r2r3
r3r4!T
r1rξrξr1
r2r2r3rξ
rξr3r4r4!T
.
Let us describe the second type of elementary
grinding. In this case the vertex rξis placed in-
side the triangle and is connected to the edges
with its vertices r1,r2,r3according to the map-
ping
(r1r2r2) r1r2rξ
rξr2r3
r1rξr3!.
Both types of elemental refinements retain tri-
angulation correctness.
Let r0(r) be the Courant function for the ver-
tex r0= (x0, y0),
r0(r) =
1T(r)/0
T
for r |T|,T Z(r0),r0 |T|,
0
for r/ |Z(r0)|.
Here r0= (x0, y0), r1= (x1, y1), r2= (x2, y2) are
vertices of triangle T,r= (x, y),
T(r) = xx0yy0
x2x1y2y1,
0
T=x1x0y1y0
x2x0y2y0.
We associate each vertex rifrom the zero-
dimensional spanning tree T0with the Courant
function ri(r). These functions are a linear inde-
pendent system of functions. Consider the space
Sof the linear combinations of these functions,
Sdef
={eu|eu=X
ri∈T 0
viri, viR1}.
{ri}ri∈T 0system we call the standard basis
of Courant spaces.
Elementary triangulation refinement adds ver-
tex rξin triangulation, which allows us to con-
sider a new function rξchime corresponding to
the added top. It is clear that the added function
is linearly independent with the previous ones.
Consider the linear span S1of the functions
{ri}ri∈T 0and rξ. It is clear that the result
will be the extension of the space S,S S1.
It is easy to see that the set of the features just
listed are not the standard Courant basis for the
space S1. To go to the standard basis, you need
to take into account the change structure of the
barycentric stars, which is local in nature.
Consider an elementary refinement of trian-
gulation. Let us add a new vertex rξ(together
with the corresponding edges). We introduce the
function $rξchime corresponding to the added
vertex. It is clear that this function is linearly
independent with respect to system {$ri}ri∈T 0.
Considering the linear span of the set of functions
{$ri}ri∈T 0 {$rξ}, we obtain a linear space S1
containing the space S,S S1.
It is easy to see that the set of functions
{$ri}ri∈T 0 {$rξ}are not the standard Courant
basis for the space S1. The transition to the stan-
dard basis is obtained by a linear transformation
that takes into account the change structures of
the barycentric stars. The said transition is lo-
cal in the sense that it affects only those Courant
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functions whose support has a non-empty inter-
section with the support of the added function.
Later on, the transition to a standard basis is not
required.
6 Energy refinement for the finite
elements in a two-dimensional
problem
Consider the quadratic functional
F(u)def
=Z2
X
i,j=1
pij (x)u
xi
u
xj
+
+q(x)u22u(x)f(x)dx,
(38)
where x= (x1, x2), q(x)>0, aij (x) = aji(x),
2
X
i,j=1
pij (x)ζiζjγX
i∈{1,2}
ζ2
i, γ =const > 0
ζsR1, s = 1,2.
(39)
The functions pij (x), q(x) are measurable and
bounded. Functional F(u) is defined on the space
W1
2(Ω). As is known, the solution of a number
of boundary value problems for differential equa-
tions
2
X
i,j=1
xipij (x)u
xj+q(x)u=f(x), x
(40)
is reduced to the minimization of the functional
on the corresponding linear manifold of the space
W1
2(Ω). Its subspace is often called the energy
space and is denoted by HA, and the bilinear form
[u, v]def
=Z2
X
i,j=1
pij (x)u
xi
v
xj
+q(x)uvdx.
(41)
turns out to be an inner product in HA. Denote
uthe solution of the problem
min
uHA
F(u).(42)
Let Sbe a subspace in HA,PSbe orthopro-
jector of the space HAonto the subspace S, and
eu
def
=PSu(43)
be the approximate solution of problem (39).
Let us assume that the next condition is ful-
filled (A). The closure of contains a polygonal
domain Mwith triangulation T. The approx-
imate solution (42) of problem (38) on polygon
Mis a linear combination Courant functions,
eu(x)x∈M=X
ri∈T 0
v
i$ri(r).(44)
Under condition (A) we have
F(eu) = Z\M
G(x;eu(x))dx+
+X
T∈T 2Z|T|
G(x;eu(x))dx,
(45)
where
G(x;u) =
2
X
i,j=1
pij (x)u
xi
u
xj
+q(x)u22f(x)u.
(46)
Let T1and T2be two neighboring triangles,
T1, T2 T 2defined by the matrix
r1r2r3
r1r3r4.(47)
Let us perform an elementary refinement (5.1).
Consider the linear span of the space Sand the
coordinate span of the Courant function $rξ(r).
According to formulas (25) we have N= 1
A0= [ϕrξ, ϕrξ], B0= [˜u, ϕrξ](f, ϕrξ),(48)
so that the decrease in energy in this case has the
form
E=|[˜u, ϕrξ](f, ϕrξ)|2
[ϕrξ, ϕrξ].
In this case we have
$rξ(r) =
e
Ti,rξ(r)/0
e
Ti,rξ
for r | e
Ti|, i = 1,2,3,4,
0
for r/ |Z(rξ)|,
(49)
where
rξ= (xξ, yξ),ri= (xi, yi),ri+1 = (xi+1, yi+1)
are vertices of the triangle e
Ti, and r= (x, y),
e
Ti,rξ(r) = xix yiy
xi+1 xiyi+1 yi,
0
e
Ti,rξ=xixξyiyξ
xi+1 xξyi+1 yξ.
(50)
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Hence, for (x, y) | e
Ti|,i= 1,2,3,4, we get
$rξ
x =yi+1 yi
0
e
Ti,rξ
,
$rξ
y =xi+1 xi
0
e
Ti,rξ
,
0
e
Ti,rξ=xixξyiyξ
xi+1 xiyi+1 yi.
(51)
According to formulas (25) we have N= 1
A0= [$rξ, $rξ], B0= [˜u, $rξ](f, $rξ),(52)
so that the decrease in energy in this case has the
form
E=|[˜u, $rξ](f, $rξ)|2
[$rξ, $rξ].
Our task is to evaluate the expressions
[$rξ, $rξ],[˜u, $rξ],(f, $rξ).
For brevity, we confine ourselves to the case
q(x, y)(x,y)∈|T1|∪|T2|= 0.
So we have
[$rξ, $rξ] =
=
4
X
i=1
1
4mes2|e
Ti|Z|
e
Ti|np11(yi+1 yi)2+
+p22(xi+1 xi)2odxdy.
(53)
For r |Tj|,j= 1,2, we have
$r1(r) = Tj,r1(r)/0
Tj,r1,(54)
where r1= (x1, y1), rj+1 = (xj+1, yj+1), rj+2 =
(xj+2, yj+2) are vertices of triangle Tj,j= 1,2,
r= (x, y),
Tj,r1(r) = xj+1 x yj+1 y
xj+2 xj+1 yj+2 yj+1,
0
Tj,r1=xj+1 x1yj+1 y1
xj+2 x1yj+2 y1.
(55)
Therefore, for r |Tj|,j= 1,2, we get
$r1
x (r) = (yj+2 yj+1)/0
Tj,r1,
$r1
y (r)=(xj+2 xj+1)/0
Tj,r1.
(56)
Similarly for r |T1|, we have
$r2(r) = T1,r2(r)/0
T1,r2.(57)
Let r1= (x1, y1), r2= (x2, y2), r3= (x3, y3)
be vertex of the triangle T1,r= (x, y), where
r1= (x1, y1), r2= (x2, y2), r3= (x3, y3) are
vertices of triangle T1,r= (x, y),
T1,r2(r) = xx1yy1
x3x1y3y1,
0
T1,r2=x2x1y2y1
x3x2y3y2.
(58)
Therefore, for r |T1|, we get
$r2
x (r)=(y3y1)/0
T1,r2,
$r2
y (r) = (x3x1)/0
T1,r2.
(59)
For r |Tj|,j= 1,2, we have
$r3(r)=∆Tj,r3(r)/0
Tj,r3,(60)
where r1= (x1, y1), r2= (x2, y2), r3= (x3, y3)
are vertices of T1,r1= (x1, y1), r3= (x3, y3),
r4= (x4, y4) are vertices of T2,r= (x, y),
T1,r3(r) = x1x y1y
x2x1y2y1,
0
T1,r3=x2x1y2y1
x3x2y3y2,
(61)
T2,r3(r) = xx1yy1
x4x1y4y1,
0
T2,r3=x3x1y3y1
x4x3y4y3.
(62)
Therefore, for r |T1|we get
$r3
x (r) = (y2y1)/0
T1,r3,
$r3
y (r) = (x2x1)/0
T1,r3,
(63)
and for r |T2|we find
$r3
x (r)=(y4y1)/0
T2,r3,
$r3
y (r) = (x4x1)/0
T2,r3.
(64)
Similarly for r |T2|, we have
$r4(r) = T2,r4(r)/0
T2,r4,(65)
WSEAS TRANSACTIONS on MATHEMATICS
DOI: 10.37394/23206.2023.22.60
Yuri K. Dem'yanovich, Irina G. Burova
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Volume 22, 2023
where r1= (x1, y1), r3= (x3, y3), r4= (x4, y4)
are vertices of triangle T2,r= (x, y),
T2,r4(r) = x1x y1y
x3x1y3y1,
0
T2,r4=x3x1y3y1
x4x3y4y3.
(66)
Therefore, for r |T2|, we get
$r4
x (r) = (y3y1)/0
T2,r4,
$r4
y (r)=(x3x1)/0
T2,r4.
(67)
Let as proceed to the calculation of the expres-
sion [˜u, $rξ]. We have
[˜u, $rξ] =
4
X
j=1
vj[$rj, $rξ],(68)
[$rj, $rξ] =
4
X
i=1
[$rj, $rξ]e
Ti.(69)
Let us introduce the notation
Aji(ξ)def
= [$rj, $rξ]e
Ti,
ep(i)
k
def
=Z|
e
Ti|
pkkdxdy,
xij
def
=xixj,
yij
def
=yiyj.
From relations (68) (69) we have
[˜u, $rξ] =
4
X
j=1
vj
4
X
i=1
Aji(ξ).(70)
Using formulas (51), (56), (59), (63) (64), (67),
we successively find
A11(ξ)=(mT1me
T1)1[y32y21 ep(1)
1+x32x21 ep(1)
2],
A12(ξ)=(mT1me
T2)1[y2
32 ep(2)
1+x2
32 ep(2)
2],
A13(ξ)=(mT2me
T3)1[y2
43 ep(3)
1+x2
43 ep(3)
2],
A14(ξ)=(mT2me
T4)1[y43y14 ep(4)
1+x43x14 ep(4)
2],
A21(ξ)=(mT1me
T1)1[y13y21 ep(1)
1+x13x21 ep(1)
2],
A22(ξ)=(mT1me
T2)1[y13y32 ep(2)
1+x13x32 ep(2)
2],
A23(ξ) = A24(ξ) = 0.
7 Conclusion
A refinement of the approximate solution in the
projection method is usually obtained by an or-
thogonal projection in HAonto a wider space.
This requires significant computer resources. The
approach proposed in this paper leads to signif-
icant resource savings due to the use of a re-
fined approximate solution. The peculiarity of
this work lies in a fairly simple clarification of
an obtained solution in a small subdomain of the
considered area.
This paper also gives an energy estimate clar-
ification. This paper is devoted to the posteriori
improvement of the approximation in the projec-
tion method for solving a linear equation with
self-adjoint positive definite operator. Improve-
ment was obtained by expanding of the projec-
tion space.
The mentioned expanding is a linear span for
original projection space and added element of
energy space. Consideration of a priori given
parameterized class of such elements allows the
construction of an adaptive method for the men-
tioned improvement. In this work, the proposed
approach is applied to the method finite elements
for a two-dimensional boundary value problem of
the second order. The use of this approach allows
you to optimize the process refinement of the nu-
merical solution of the boundary value problem
without significant increase in computation time
and resource requirements computing system.
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DOI: 10.37394/23206.2023.22.60
Yuri K. Dem'yanovich, Irina G. Burova
E-ISSN: 2224-2880
551
Volume 22, 2023
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The authors contributed in the present re-
search, at all stages from the formulation of
the problem to the final findings and solution.
Sources of Funding for Research Presented in a
Scientific Article or Scientific Article Itself
The authors are highly gratefully and indebted to
St. Petersburg University for financial supporting
the preparation of this paper (Pure ID 94029567).
Conflicts of Interest
The authors have no conflict of interest to declare
that is relevant to the content of this article.
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WSEAS TRANSACTIONS on MATHEMATICS
DOI: 10.37394/23206.2023.22.60
Yuri K. Dem'yanovich, Irina G. Burova
E-ISSN: 2224-2880
552
Volume 22, 2023