1. Introduction
Control stochastic systems (CStS) described by nonstationary linear stochastic differential equations (SDE) in the Ito sense with parametric noises are the most adequate models at single shock disturbance (ShD) and Gaussian and non-Gaussian multi-ShD. The exact accuracy theory of stochastic processes for such SDE is developed in [
1,
2]. For StS with impulse, ShD asymptotic theory is given in [
3,
4]. Nowadays wavelet methods are intensively applied to the problem of deterministic and stochastic numerical analysis and modeling. In the past few decades, a broad range of numerical methods based on Haar wavelet methods achieved great success [
5]. These methods are simple in sense versatility and flexibility and possess less computational cost for accuracy problems. A wavelet is a numerical mathematical function used to divide a given function into different scale components. The usage and study of wavelets has attained its modern growth due to mathematical analysis of the wavelet in [
6,
7,
8]. The concept of multiresolution analysis (MRA) was developed in [
9]. In [
10], z method to construct wavelets with compact support and scale function was presented. A review of basic properties of wavelets and MRA is given in [
11]. Among the wavelet families, which are described by an analytical expression, special attention deserves the Haar wavelets. Haar wavelets are very effective and popular for solving ordinary differential equations [
11,
12,
13,
14,
15]. The wavelet solution of integral and evolutionary equation is discussed in [
16,
17,
18,
19,
20,
21].
The application of a wavelet for canonical expansions of random functions and SDE has been suggested in [
22] and developed [
23,
24]. In [
25,
26], a combination of Haar wavelets and the Galerkin method [
22] numerical solution of linear equations were presented. Development of the Haar–Galerkin method and experimental software tools for accuracy analysis of CStS at single ShD is given in [
19,
20].
Let us consider modeling the wavelet Haar–Galerkin methodology and experimental software tools for covariance accuracy analysis of CStS at complex multi-ShD.
2. Stochastic Systems at Complex Shock Disturbances
Let us consider the differential stochastic system described by the following Ito vector equation:
Here, is the Markovian state vector, is the shock white noise (non-Gaussian in the general case), and and are known functions defined by ShD.
For single ShD in cases when Equation (1) satisfies the “filter hypotheses”, nonlinear effects are not able and it is enough to use linear or linear with parametric noises models:
In case of independent multi-echelon ShD at time moments, it is necessary to input additional items:
Here,
and
are small functions depending on
and
. At practice functions
,
,
,
are approximated by formulae:
The shock white noise in Equation (2) may be non-Gaussian in general cases, whereas in Equation (3) is strictly Gaussian.
The analytical off-line modeling Equations (2)–(5) at given ShD and system parameters
are based on known methods [
1,
2].
3. Wavelet Covariance Modeling at Additive Complex ShD
Let us consider linear nonstationary differential StS:
Here,
is the state vector;
,
is the vector of the forming filter
;
is the additive complex ShD;
,
,
,
are coefficients of corresponding dimensions;
and
,
are random variables;
is the impulse forming functions;
is non-Gaussian in the general-case white noise,
, with the matrix intensity
v. Using:
we come to the following linear vector stochastic equation:
Using Equation (9),
,
,
, we have the following set of equations for the mathematical expectation
, covariance matrix
, and matrix of covariance functions
[
1,
2]:
Let us consider Equation (9) on the time interval
. After a change of variables at
we transform Equation (14) to the following:
at
and white noise
with intensity
), where:
Here, prime is differential by . Furthermore, briefly, we use .
For solving equation:
defining
, we apply [
15,
16] at condition for functions
,
,
,
(
h,
k = 1,2,…,
p) belonging to
; as shown in [
13], these functions can be expanded into convergent wavelet series. Following [
15], we define the orthonormal basis of the Haar wavelet:
Here,
is the scaling function,
is the maternal wavelet
K = 0, 1, …, l − 1; l = ; j = 1, 2, …, J; L =; i = l + k + 1; I = 3, 4, …, L; J is the maximal resolution level.
Then, we introduce integrals:
where:
For every component,
; Equation (16) gives expressions:
Expanding
in the form of Haar wavelet expansion (WLE),
we obtain from (22):
After substituting Equations (23) and (24) into (22), we have expression:
Projecting (25) on
, we receive
linear algebraic Equations
Due to orthonormality
, we obtain from (26) the following Equations:
Then, we expand functions
,
,
in the form of WLE:
where:
Equation (27) may be presented in resultant form:
So we obtain the following algorithm.
Theorem 1. Let the following conditions be satisfied:
Equations (6)–(8) are reducible to Equation (9) and Equation (15) for composed vector Y;
Scalar functions, , , (h, k = 1,2, …, p) belong to space ;
In spacethe wavelet basic Haar is defined by Formulaes (17)–(20).
Then, the solution of Equation (22) for componentof composed vectoris as follows:where functionsare defined by (21), coefficientsare the solutions of linear algebraic Equation (34).
From Equation (11), for every element covariance matrix , we have the following ordinary differential equation:
Due to the
symmetry, it is sufficient to compose Equations for
,
. In this case, elements
at
are replaced by
and
at
by
. As a result, we have only
equations. Let us introduce notation:
As a result of applying the Haar–Galerkin method to the solution of the Equation (36), we obtain the following formulae:
After substituting (38) and (40) into (37), we have:
Protecting (41) on basis
, we receive
equations for
:
where:
So, we come to the following algorithm:
Theorem 2. Let the conditions of Theorem 1 and additional conditions be considered:
Equations for elements of covariance matrix Equation (11) are reduced to Equation (36);
The scalar functions, belonging to spaceare fulfilled.
Then, the solution of Equation (36) for elementsof the covariance matrix of the composed vectoris expressed by Equation (40), whereis defined by (21), coefficientsbeing the solution of linear algebraic Equation (42).
From Equation (12) for every element of matrix at we have the following ordinary equations with corresponding initial condition:
As a result of applying the Haar–Galerkin method to the solution of the Equation (43) with initial conditions (44), we obtain the following expressions:
After projecting (47) on basis
and tauing into consideration on Expressions (31), (32), we have a system of
linear equations for coefficients
Theorem 3. Let the conditions of Theorems 1, 2, and additional conditions be considered:
Equation (12) may be reduced to Equations (43) and (44);
functions, atbelong to spaceat fixedall valid.
Then, the solution of Equations (43) and (44) for elementsof the covariance matrix of the composed vectorforis as follows: (47). Here,is defined by (21), coefficientsare defined by (49), and the values ofare taken from Theorem 2.
4. Wavelet Covariance Modeling at Parametric Complex Shd
Let us consider the Ito linear with parametric noises nonstationary differential StS:
Here,
is Gaussian while noise with intensity matrix
. Equations (50) and (51) may be transformed into the following form:
where:
For Equations (52) and (53), the following covariance equations are valid [
1,
2]:
Here, , , .
Equation (52) for
(Formula (14)) may be transformed to the following one:
The equation for mathematical expectation is separated from equations for covariance characteristics and is defined by Equation (16) (see Theorem 1).
The equations for elements
,
, due to their symmetry (
, have the form:
Using notations:
we transform Equation (58) into:
After, the Haar expanding left hand of Equation (58) is equal to:
We obtain the solution (59):
Substituting Equations (60) and (61) into (58), we have the following results:
At last taking into account the notations:
and projecting (62) on wavelet basis
, we obtain the
linear algebraic Equation relatively on coefficients
:
Theorem 4. Let the conditions of Theorem 1 and:
Equations (55) are reduced to Equations (58);
scalar functions, , , , , , , belong to space.
Then, the solutions of Equation (58) is expressed by Equations (61) and (63).
For solution of Equation (56), we use Theorem 3.
5. Examples
Let us consider the information-control system (ICS) of the third order at ShD described by the following equations:
Here,
represents the components of the state vector
,
are the system parameters;
is the rectangular impulse function at time moment
;
is the angle between acceleration
and longitudinal ICS axis;
is the white noise with intensity
. The equation may be presented in the vector form:
where:
Equations for mathematical expectations
and elements of covariance matrix
are as follows:
Typical
Figure 1 and
Figure 2 for ICS with parameters
show the accumulation effect of systematic and random errors for output variable
.
Typical
Figure 1a,b for ICS with parameter
. Typical
Figure 2a,b—with parameter
.
So, for single ShD and , the following conclusions are valid:
Systematic restricted error takes place for variables , , whereas for variable , we have an accumulation growing effect (linear systematic drift);
A random restricted effect takes place for variables , whereas for , we have only the accumulation effect.
Let us consider the information-control system (ICS) of the third order at ShD described by the following equations:
Here,
represents the components of the state vector
,
is the system parameters;
is rectangular impulse function at time moment
;
is the angle between accelation
and longitudinal ICS axis;
is the white noise with intensity
. The equation may be presented in the vector form:
where:
Equations for mathematical expectations
and elements of covariance matrix
are as follows:
Typical
Figure 3,
Figure 4,
Figure 5,
Figure 6,
Figure 7,
Figure 8,
Figure 9 and
Figure 10 for ICS with parameters
.
show the accumulation effect of systematic and random errors for output variable
.
Typical
Figure 3a,b for ICS with parameters
. Typical
Figure 4a,b—with parameters
.
Typical
Figure 5a,b for ICS with parameters
. Typical
Figure 6a,b—with parameters
.
Typical
Figure 7a,b for ICS with parameters
. Typical
Figure 8a,b—with parameters
.
Typical
Figure 9a,b for ICS with parameter
. Typical
Figure 10a,b—with parameters
.
So, for multi-echelon ShD and , we have the nonlinear systematic and random accumulation and drift effects for the corresponding variables.
At fixed N and various , we have different quality graphs. So, at mathematical expectations, , are restricted, whereas is not restricted. Variances , are restricted and is not restricted.
6. Conclusions
For control stochastic systems at nonstationary shock disturbances described by linear stochastic differential equations with stochastic parametric noises, corresponding modeling methodological support and experimental software tools are developed. The methodology is based on the deterministic Haar–Galerkin algorithms for the solution of equations for the mathematical expectation, covariance matrix, and matrix of covariance functions.
Original new results include methods and algorithms of stochastic covariance analysis and modeling on the basis of the Galerkin method and wavelet expansion for linear, linear with parametric noises, and quasilinear control stochastic systems with complex shock disturbances. A new methodology may be called quick “analytical numerical modeling”. This methodology does not use Monte Carlo methods.
For the accuracy confirmation wavelet methodology, two special examples in the form of an information-control system at single and multi-echelon shock disturbances was presented. New nondeterministic error accumulations and drift effects are detected. Future works include nonlinear covariance analysis and probabilistic distributions problems in the field of nonlinear stochastic systems and dependent multi-shock disturbances.
The research was carried out using the infrastructure of shared research facilities CKP «Informatics» of FRC CSC RAS [
27].