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Mathematical Problems in Engineering
VolumeΒ 2012Β (2012), Article IDΒ 342705, 15 pages
doi:10.1155/2012/342705
Research Article

Asymptotic Parameter Estimation for a Class of Linear Stochastic Systems Using Kalman-Bucy Filtering

1School of Information Science and Technology, Donghua University, Shanghai 200051, China
2School of Science, Donghua University, Shanghai 200051, China

Received 21 June 2012; Accepted 21 July 2012

Academic Editor: JunΒ Hu

Copyright Β© 2012 Xiu Kan et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Abstract

The asymptotic parameter estimation is investigated for a class of linear stochastic systems with unknown parameter πœƒ ∢ 𝑑 𝑋 𝑑 = ( πœƒ 𝛼 ( 𝑑 ) + 𝛽 ( 𝑑 ) 𝑋 𝑑 ) 𝑑 𝑑 + 𝜎 ( 𝑑 ) 𝑑 π‘Š 𝑑 . Continuous-time Kalman-Bucy linear filtering theory is first used to estimate the unknown parameter θ based on Bayesian analysis. Then, some sufficient conditions on coefficients are given to analyze the asymptotic convergence of the estimator. Finally, the strong consistent property of the estimator is discussed by comparison theorem.

1. Introduction

Stochastic differential equations (SDEs) are a natural choice to model the time evolution of dynamic systems which are subject to random influences. Such models have been used with great success in a variety of application areas, including biology, mechanics, economics, geophysics, oceanography, and finance. For instance, refer to [18]. In reality, it is unavoidable that a stochastic system contains unknown parameters. Since 1962, Arato et al. [10] first applied parameter estimation to geophysical problem. Parameter estimation for SDEs has attracted the close attention of many researchers, and many parameter estimation methods for various advanced models have been studied, such as maximum likelihood estimation (MLE), Bayes estimation (BE), maximum probability estimation (MPE), minimum distance estimation (MDE), minimum contrast estimation (MCE), and M-estimation (ME). See [1015] for details.

In practice, most stochastic systems cannot be observed completely, but the development of filtering theory provides an effective method to solve this problem. Over the past few decades, a lot of effective approaches have been proposed to overcome the difficulties in parameter estimation for stochastic models by filtering methods. It turns out to be helpful both in computability and asymptotic studies. See [9, 1626]. In particular, the parameter estimation has been studied based on filtering observation, and the strong consistency property has also been shown in [27, 28]. In [29], a large deviation inequality has been obtained which implies the strong consistency, local asymptotic normality, and the convergence of moments. The asymptotic properties of estimators have been studied for a class of special Gaussian Itô processes with noisy observations in [30]. It should be pointed out that, so far, although the parameter estimation problem has been widely investigated for SDEs, the parameter estimation problem for stock price model has gained much less research attention due probably to the mathematical complexity.

Stock return volatility process is an important topic in options pricing theory. During the past decades, many SDEs have been modeled to solve the financial problems. For instance, refer to [2, 3135]. Particularly, the so-called Hull-White model has been established by Hull and White [34] to analyze European call options prices under stochastic volatility at 1987. Using Taylor series expansion, an accurate formula for call options has been derived where stock returns and stock volatilities are uncorrelated. In addition, the Hull-White model readily lends itself to the estimation of underlying stochastic process parameters. Since the Hull-White formula is an effective options pricing model, it has been widely used to model the practice stock price problem. Therefore, it is reasonable to study the parameter estimation problem for Hull-White model with unknown parameter. Unfortunately, to the best of the authors’ knowledge, the parameter estimation for Hull-White model with unknown parameter based on Kalman-Bucy linear filtering theory has not been fully studied despite its potential in practical application, and this situation motivates our present investigation.

Summarizing the above discussions, in this paper, we aim to investigate the parameter estimation problem for a general class of linear stochastic systems. The main contributions of this paper lie in the following aspects. (1) Kalman-Bucy linear filtering is used to solve the parameter estimation problem. (2) The asymptotic convergence of the estimator is investigated by analyzing Riccati equation. (3) The strong consistent property is studied by comparison theorem. The rest of this paper is organized as follows. In Section 2, we formulate the problem and state the well-known fact which would be used later. In Section 3, we study the asymptotic convergence of the estimator. In Section 4, the strong consistent of estimator is given. In Section 5, some conclusions are drawn.

Notation. The notation used here is fairly standard except where otherwise stated. ℝ = ( βˆ’ ∞ , + ∞ ) and ℝ + = [ 0 , + ∞ ) . For a vector π‘₯ = ∈ ℝ , | π‘₯ | is the Euclidean norm (or 𝐿 2 norm) with √ | π‘₯ | = π‘₯ β‹… π‘₯ . 𝑀 𝑇 and 𝑀 βˆ’ 1 represent the transpose and inverse of the matrix 𝑀 . d e t ( 𝑀 ) denotes the determinant of the matrix 𝑀 . 𝐼 denotes the identity matrix of compatible dimension. Moreover, let ( Ξ© , β„± , 𝐏 ) be a complete probability space with a natural filtration { β„± 𝑑 } 𝑑 β‰₯ 0 satisfying the usual conditions (i.e., it is right continuous, and β„± 0 contains all 𝐏 -null sets). 𝔼 [ π‘₯ ] stands for the expectation of the stochastic variable π‘₯ with respect to the given probability measure 𝐏 . 𝐢 ( ℝ + ) denotes the class of all continuous time on 𝑑 ∈ ℝ + .

2. Problem Statement

Hull-White model is a continuous-time, real stochastic process as follows: 𝑋 𝑑 = 𝑋 0 + ξ€œ 𝑑 0 ξ€· 𝛼 ( 𝑠 ) + 𝛽 ( 𝑠 ) 𝑋 𝑠 ξ€Έ ξ€œ 𝑑 𝑠 + 𝑑 0 𝜎 ( 𝑠 ) 𝑑 π‘Š 𝑠 ( 2 . 1 ) with initial value 𝑋 0 as a Gaussian random variable, where 𝛼 , 𝛽 , 𝜎 are deterministic continuous functions on time 𝑑 , π‘Š 𝑑 is a Brownian motion independent of the initial value 𝑋 0 . Obviously, Hull-White model (2.1) is a general continuous-time linear SDE for 𝑋 𝑑 , and we assume that the coefficient 𝛼 contains an unknown parameter πœƒ ∈ 𝑅 as follows: 𝑑 𝑋 𝑑 = ξ€· πœƒ 𝛼 ( 𝑑 ) + 𝛽 ( 𝑑 ) 𝑋 𝑑 ξ€Έ 𝑑 𝑑 + 𝜎 ( 𝑑 ) 𝑑 π‘Š 𝑑 𝑑 β‰₯ 0 , ( 2 . 2 ) and we observe the process 𝑋 𝑑 by the following filtering observations: 𝑑 π‘Œ 𝑑 = πœ‡ ( 𝑑 ) 𝑋 𝑑 𝑑 𝑑 + 𝛾 ( 𝑑 ) 𝑑 𝑉 𝑑 𝑑 β‰₯ 0 , ( 2 . 3 ) where πœ‡ , 𝛾 are deterministic bounded continuous functions on time 𝑑 , and 𝑉 𝑑 is a Brownian motion independent of π‘Š 𝑑 .

Now, our aim is to estimate πœƒ in (2.2) based on the observation of (2.3). First, we can use Bayesian analysis to deal with the unknown parameter πœƒ . We model πœƒ as a random variable and denoted it as πœƒ 0 . We assume πœƒ 0 normally distributed and independent of 𝜎 ( π‘Š 𝑑 , 𝑉 𝑑 , 𝑑 β‰₯ 0 ) . Then, we can rewrite (2.2) as a two-component system for ( 𝑋 𝑑 , πœƒ 𝑑 ) as follows: βŽ› ⎜ ⎜ ⎝ 𝑑 𝑋 𝑑 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎝ ⎞ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ 𝑋 𝛽 ( 𝑑 ) 𝛼 ( 𝑑 ) 0 0 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ 0 ⎞ ⎟ ⎟ ⎠ 𝑑 𝑑 + 𝜎 ( 𝑑 ) 𝑑 π‘Š 𝑑 𝑑 β‰₯ 0 . ( 2 . 4 ) Similarly, filtering observations system (2.3) can be expressed as follows: 𝑑 π‘Œ 𝑑 = ξ‚€  βŽ› ⎜ ⎜ ⎝ 𝑋 πœ‡ ( 𝑑 ) 0 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ 𝑑 𝑑 + 𝛾 ( 𝑑 ) 𝑑 𝑉 𝑑 𝑑 β‰₯ 0 . ( 2 . 5 ) Therefore, we can use the Kalman-Bucy linear filtering theory to estimate πœƒ 0 as follows: Μ‚ πœƒ 𝑑 ξ€Ί πœƒ = 𝔼 0 ∣ π‘Œ 𝑠 ξ€» , , 0 ≀ 𝑠 ≀ 𝑑 ( 2 . 6 ) and moreover, we also have  𝑋 𝑑 = 𝔼 [ 𝑋 𝑑 | π‘Œ 𝑠 , 0 ≀ 𝑠 ≀ 𝑑 ] .

For given Gaussian initial conditions 𝑋 0 and πœƒ 0 , it is well known from Kalman-Bucy linear filtering theory that error covariance matrix 𝑆 ( 𝑑 ) satisfies the following Riccati equation: Μ‡ 𝑆 ( 𝑑 ) = 𝐴 𝑆 + 𝑆 𝐴 𝑇 βˆ’ 𝑆 𝐢 𝑇 ξ€· 𝐷 𝐷 𝑇 ξ€Έ βˆ’ 1 𝐢 𝑆 + 𝐡 𝐡 𝑇 , ( 2 . 7 ) where ξ€· 𝐴 = 𝛽 ( 𝑑 ) 𝛼 ( 𝑑 ) 0 0 ξ€Έ ξ€· , 𝐡 = 0 𝜎 ( 𝑑 ) ξ€Έ , 𝐢 = ( πœ‡ ( 𝑑 ) 0 ) , 𝐷 = 𝛾 ( 𝑑 ) , and as we all know the error covariance matrix 𝑆 ( 𝑑 ) is defined as follows: βŽ› ⎜ ⎜ ⎝ 𝑆 𝑆 ( 𝑑 ) = π‘₯ π‘₯ ( 𝑑 ) 𝑆 π‘₯ πœƒ 𝑆 ( 𝑑 ) πœƒ π‘₯ ( 𝑑 ) 𝑆 πœƒ πœƒ ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎝ 𝔼 ξ‚Έ ξ‚€ 𝑋 ( 𝑑 ) 𝑑 βˆ’  𝑋 𝑑  2 ξ‚Ή 𝔼 𝑋  ξ‚€ 𝑑 βˆ’  𝑋 𝑑  ξ€· πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 ξ€Έ ξ‚„ 𝔼 𝑋  ξ‚€ 𝑑 βˆ’  𝑋 𝑑  ξ€· πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 ξ€Έ ξ‚„ 𝔼  ξ€· πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 ξ€Έ 2 ξ‚„ ⎞ ⎟ ⎟ ⎟ ⎠ . ( 2 . 8 ) Set π‘Ž = 𝑆 π‘₯ π‘₯ , 𝑏 = 𝑆 π‘₯ πœƒ = 𝑆 πœƒ π‘₯ , and 𝑐 = 𝑆 πœƒ πœƒ . From Riccati equation (2.7), one can get the following system: Μ‡ π‘Ž = 2 𝛽 π‘Ž + 2 𝛼 𝑏 + 𝜎 2 βˆ’ πœ‡ 2 𝛾 2 π‘Ž 2 , Μ‡ πœ‡ 𝑏 = 𝛽 𝑏 + 𝛼 𝑐 βˆ’ 2 𝛾 2 πœ‡ π‘Ž 𝑏 , Μ‡ 𝑐 = βˆ’ 2 𝛾 2 𝑏 2 . ( 2 . 9 )

Remark 2.1. Equation (2.9) is a nontrivial nonlinear ordinary differential equation system, and it is well known from the Kalman-Bucy linear filtering theory that such Riccati equations have unique solutions for all 𝑑 ∈ ℝ + .

Remark 2.2. From the equation Μ‡ 𝑐 = βˆ’ ( πœ‡ 2 / 𝛾 2 ) 𝑏 2 , we can see that the error variance 𝔼 [ ( πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 ) 2 ] is monotonically decreasing.

3. Asymptotic Convergence Analysis

Assume that the initial conditions 𝑋 0 and πœƒ 0 are independent and have nonvariances, so that 𝑏 ( 0 ) = 0 and π‘Ž ( 0 ) = 𝔼 [ 𝑋 2 0 ] > 0 , 𝑐 ( 0 ) = 𝔼 [ πœƒ 2 0 ] > 0 ; thus, 𝑆 ( 0 ) is a regular matrix. For the property of continuity of 𝑆 ( 𝑑 ) , 𝑆 βˆ’ 1 ( 𝑑 ) exists at least for small times. In order to obtain the rate of convergence of the estimator, 𝑆 ( 𝑑 ) should satisfy the regularity conditions. The following Theorem certifies the regularity of 𝑆 ( 𝑑 ) .

Theorem 3.1.  (a1) Assume the initial conditions 𝑋 0 and πœƒ 0 for system (2.2) are independent and have nonvanishing variances.
  (a2) Let 𝛼 ( 𝑑 ) , 𝛽 ( 𝑑 ) , 𝜎 ( 𝑑 ) , πœ‡ ( 𝑑 ) , 𝛾 ( 𝑑 ) ∈ 𝐢 ( ℝ + ) .
 Then, the error covariance matrix 𝑆 ( 𝑑 ) satisfies d e t ( S(t) ) > 0 for all 𝑑 β‰₯ 0 , and 𝑆 π‘₯ π‘₯ ( 𝑑 ) > 0 , 𝑆 πœƒ πœƒ ( 𝑑 ) > 0 βˆ€ 𝑑 β‰₯ 0 . ( 3 . 1 )

Proof. By Kalman-Bucy linear filtering theory, we know that d e t ( 𝑆 ( 𝑑 ) ) > 0 for all 𝑑 β‰₯ 0 . Furthermore, it is not difficult to show that (3.1) holds for all 𝑑 β‰₯ 0 .
Since d e t ( 𝑆 ( 𝑑 ) ) > 0 , it follows that 𝑆 βˆ’ 1 ( 𝑑 ) exists. Set 𝑅 ( 𝑑 ) = 𝑆 βˆ’ 1 βŽ› ⎜ ⎜ ⎝ ⎞ ⎟ ⎟ ⎠ ( 𝑑 ) = 𝑒 ( 𝑑 ) 𝑓 ( 𝑑 ) 𝑓 ( 𝑑 ) 𝑔 ( 𝑑 ) . ( 3 . 2 ) As we know that 𝑅 = 1 / 𝑆 implies that Μ‡ 𝑅 = βˆ’ ( 1 / 𝑆 2 ) Μ‡ 𝑆 , one can easily have that Μ‡ Μ‡ 𝑅 = βˆ’ 𝑅 𝑆 𝑅 . ( 3 . 3 ) It follows readily form (2.9) and (3.3) that Μ‡ 𝑅 = βˆ’ 𝑅 𝐴 βˆ’ 𝐴 𝑇 𝑅 + 𝐢 𝑇 ξ€· 𝐷 𝐷 𝑇 ξ€Έ βˆ’ 1 𝐢 βˆ’ 𝑅 𝐡 𝐡 𝑇 𝑅 . ( 3 . 4 ) Using a similar computation as (2.9), we can get πœ‡ Μ‡ 𝑒 = 2 𝛾 2 βˆ’ 2 𝛽 𝑒 βˆ’ 𝜎 2 𝑒 2 , Μ‡ 𝑓 = βˆ’ 𝛼 𝑒 βˆ’ 𝛽 𝑓 βˆ’ 𝜎 2 𝑒 𝑓 , Μ‡ 𝑔 = βˆ’ 2 𝛼 𝑓 βˆ’ 𝜎 2 𝑓 2 . ( 3 . 5 ) The condition (a1) shows that π‘Ž ( 0 ) > 0 , 𝑏 ( 0 ) = 0 , and 𝑐 ( 0 ) > 0 , which implies that 𝑒 ( 0 ) > 0 , 𝑓 ( 0 ) = 0 , and 𝑔 ( 0 ) > 0 . Since the Riccati equations (2.9) have unique solutions on 𝑅 + , thus the nonlinear system (3.5) has a unique solution on ℝ + . Furthermore, the first equation Μ‡ 𝑒 = πœ‡ 2 / 𝛾 2 βˆ’ 2 𝛽 𝑒 βˆ’ 𝜎 2 𝑒 2 with initial condition 𝑒 ( 0 ) > 0 has a unique solution on a maximal time interval [ 0 , 𝑇 ) , where 𝑇 ∈ ℝ + . Assume that there exists a smallest time βˆ’ 𝑑 ∈ ( 0 , 𝑇 ) such that 𝑒 ( βˆ’ 𝑑 ) = 0 . By the property of continuity of 𝑒 ( 𝑑 ) , we have 𝑒 ( 𝑑 ) > 0 , for 0 ≀ 𝑑 < βˆ’ 𝑑 . Thus, Μ‡ 𝑒 ( 𝑑 ) = l i m Ξ” 𝑑 β†’ 0 𝑒 ξ‚€ βˆ’ 𝑑  ξ‚€ βˆ’ 𝑒 βˆ’ 𝑑  βˆ’ Ξ” 𝑑 Ξ” 𝑑 < 0 , ( 3 . 6 ) this contradicts with Μ‡ 𝑒 ( 𝑑 ) = πœ‡ 2 ( βˆ’ 𝑑 ) / 𝛾 2 ( βˆ’ 𝑑 ) βˆ’ 2 𝛽 ( βˆ’ 𝑑 ) 𝑒 ( βˆ’ 𝑑 ) βˆ’ 𝜎 2 ( βˆ’ 𝑑 ) 𝑒 2 ( βˆ’ 𝑑 ) ≀ πœ‡ 2 ( βˆ’ 𝑑 ) / 𝛾 2 ( βˆ’ 𝑑 ) for all 𝑑 ∈ [ 0 , 𝑇 ) . Therefore, 𝑒 ( 𝑑 ) > 0 , for 𝑑 ∈ [ 0 , 𝑇 ) .
As long as Μ‡ 𝑒 ( 𝑑 ) = πœ‡ 2 ( βˆ’ 𝑑 ) / 𝛾 2 ( βˆ’ 𝑑 ) βˆ’ 2 𝛽 ( βˆ’ 𝑑 ) 𝑒 ( βˆ’ 𝑑 ) βˆ’ 𝜎 2 ( βˆ’ 𝑑 ) 𝑒 2 ( βˆ’ 𝑑 ) ≀ πœ‡ 2 ( βˆ’ 𝑑 ) / 𝛾 2 ( βˆ’ 𝑑 ) for all 𝑑 ∈ [ 0 , 𝑇 ) and πœ‡ ( 𝑑 ) , 𝛾 ( 𝑑 ) are bounded, we have Μ‡ 𝑒 ( 𝑑 ) ≀ 𝐢 , where 𝐢 is a constant. So that 𝑒 ( 𝑑 ) is bounded from below by 0 and from above by 𝑒 ( 0 ) + 𝑑 , which implies that 𝑒 ( 𝑑 ) cannot explode in finite time, thus 𝑇 = + ∞ . This shows that system (3.5) has a unique solution on ℝ + because the second equation is a linear equation for 𝑓 which can be solved analytically on ℝ + , and 𝑔 can get by integration.
Define β„Ž ( 𝑑 ) ∢ = d e t ( 𝑅 ( 𝑑 ) ) = 𝑒 ( 𝑑 ) 𝑔 ( 𝑑 ) βˆ’ 𝑓 2 ( 𝑑 ) . Since d e t ( 𝑆 ( 𝑑 ) ) > 0 for all 𝑑 β‰₯ 0 , thus β„Ž ( 𝑑 ) = d e t ( 𝑅 ( 𝑑 ) ) = 1 / d e t ( 𝑆 ( 𝑑 ) ) > 0 for all 𝑑 β‰₯ 0 , moreover, 𝑆 πœƒ πœƒ > 0 for all 𝑑 β‰₯ 0 . Finally, we assume that there exists 𝑑 0 such that, 𝑆 π‘₯ π‘₯ ( 𝑑 0 ) = 0 , then 𝑔 ( 𝑑 0 ) = 𝑆 π‘₯ π‘₯ ( 𝑑 0 ) β„Ž ( 𝑑 0 ) = 0 , so that β„Ž ( 𝑑 0 ) = 𝑒 ( 𝑑 0 ) 𝑔 ( 𝑑 0 ) βˆ’ 𝑓 2 ( 𝑑 0 ) ≀ 0 , and this contradicts β„Ž ( 𝑑 0 ) > 0 . Hence, 𝑆 π‘₯ π‘₯ > 0 for all 𝑑 β‰₯ 0 .
The proof is complete.

In order to obtain the convergence rate, the Riccati equation must be solved, and we just need the solution of (3.5). Now, we solve the equation Μ‡ 𝑒 = πœ‡ 2 / 𝛾 2 βˆ’ 2 𝛽 𝑒 βˆ’ 𝜎 2 𝑒 2 when 𝛽 , 𝜎 , πœ‡ , 𝛾 are equal to constants.

In the case 𝑒 ( 0 ) β‰  𝑙 2 , we get 𝑒 𝑙 ( 𝑑 ) = 1 + 𝑙 2 𝑙 𝐿 e x p ξ€Ί ξ€· 1 + 𝑙 2 ξ€Έ 𝜎 2 𝑑 ξ€» 𝑙 𝐿 e x p ξ€Ί ξ€· 1 + 𝑙 2 ξ€Έ 𝜎 2 𝑑 ξ€» , βˆ’ 1 ( 3 . 7 ) where 𝐿 = ( 𝑒 ( 0 ) + 𝑙 1 ) / ( 𝑒 ( 0 ) βˆ’ 𝑙 2 ) , 𝑙 1 = ( 2 𝛽 / 𝜎 2 + √ 4 𝛽 2 / 𝜎 4 + 4 πœ‡ 2 / 𝜎 2 𝛾 2 ) / 2 , 𝑙 2 = ( βˆ’ ( 2 𝛽 / 𝜎 2 √ ) + 4 𝛽 2 / 𝜎 4 + 4 πœ‡ 2 / 𝜎 2 𝛾 2 ) / 2 .

In the other case 𝑒 ( 0 ) = 𝑙 2 , the solution shows that 𝑒 ( 𝑑 ) = 𝑙 2 for all 𝑑 β‰₯ 0 .

Thus, for each 𝛼 > 0 , 𝛽 > 0 , 𝜎 > 0 , πœ‡ > 0 , 𝛾 > 0 , the solution 𝑒 ( 𝑑 ) obviously satisfies 𝑒 ( 𝑑 ) ⟢ 𝑙 2 a s 𝑑 ⟢ + ∞ . ( 3 . 8 )

The convergence rate of the estimator is given by following theorem.

Theorem 3.2. Assume that 𝛼 , 𝛽 , 𝜎 , πœ‡ , 𝛾 ∈ 𝐢 ( ℝ + ) , are all bounded, and there are constants 𝛼 1 , 𝛼 2 , 𝛽 1 , 𝛽 2 , 𝜎 1 , 𝜎 2 , πœ‡ 1 , πœ‡ 2 , 𝛾 1 , 𝛾 2 , and 𝑑 0 , such that(b1): 0 < 𝛼 1 ≀ | 𝛼 ( 𝑑 ) | ≀ 𝛼 2 for all 𝑑 β‰₯ 𝑑 0 ;(b2): 0 < 𝛽 1 ≀ | 𝛽 ( 𝑑 ) | ≀ 𝛽 2 for all 𝑑 β‰₯ 𝑑 0 ;(b3): 0 < 𝜎 1 ≀ | 𝜎 ( 𝑑 ) | ≀ 𝜎 2 for all 𝑑 β‰₯ 𝑑 0 ;(b4): 0 < πœ‡ 2 ≀ | πœ‡ ( 𝑑 ) | ≀ πœ‡ 1 for all 𝑑 β‰₯ 𝑑 0 ;(b5): 0 < 𝛾 1 ≀ | 𝛾 ( 𝑑 ) | ≀ 𝛾 2 for all 𝑑 β‰₯ 𝑑 0 ;(b6): 2 𝛼 1 ( 𝛽 1 + 𝜎 2 1 𝑙 2 2 ) > 𝜎 2 2 𝑙 2 1 where 𝑙 2 𝑖 = ( βˆ’ 2 𝛽 𝑖 / 𝜎 2 𝑖 +  ( 4 𝛽 2 𝑖 ) / ( 𝜎 4 𝑖 ) + ( 4 πœ‡ 2 𝑖 ) / ( 𝜎 2 𝑖 𝛾 2 𝑖 ) ) / 2 , 𝑖 = 1 , 2 .
Then, for arbitrary πœ– > 0 and 𝑇 > 0 , we have 𝑃 ξ€· | | πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 | | ξ€Έ ≀ 1 > πœ– πœ– 2 𝐢 𝑇 βˆ’ 1 , ( 3 . 9 ) where 𝐢 is a positive constant independent of πœ– and 𝑇 .

Proof. Let 𝑒 𝑖 be the solution to Μ‡ 𝑒 𝑖 = πœ‡ 2 𝑖 / 𝛾 2 𝑖 βˆ’ 2 𝛽 𝑖 𝑒 𝑖 βˆ’ 𝜎 2 𝑖 𝑒 2 𝑖 , 𝑖 = 1 , 2 , and 𝑒 𝑖 ( 𝑑 0 ) = 𝑒 ( 𝑑 0 ) .
Since πœ‡ 2 2 / 𝛾 2 2 βˆ’ 2 𝛽 2 𝑒 βˆ’ 𝜎 2 2 𝑒 2 ≀ Μ‡ 𝑒 = πœ‡ 2 / 𝛾 2 βˆ’ 2 𝛽 𝑒 βˆ’ 𝜎 2 𝑒 2 ≀ πœ‡ 2 1 / 𝛾 2 1 βˆ’ 2 𝛽 1 𝑒 βˆ’ 𝜎 2 1 𝑒 2 for all 𝑑 β‰₯ 𝑑 0 , by the comparison theorem [2, 36], we obtain that 𝑒 2 ( 𝑑 ) ≀ 𝑒 ( 𝑑 ) ≀ 𝑒 1 ( 𝑑 ) βˆ€ 𝑑 β‰₯ 𝑑 0 . ( 3 . 1 0 ) It follows from (3.7) that 𝑒 is bounded, and for any given 𝛿 ∈ ( 0 , 1 ) , there is a 𝑑 1 β‰₯ 𝑑 0 such that 0 < 𝑙 2 2 ( 1 βˆ’ 𝛿 ) ≀ 𝑒 ( π‘Ÿ ) ≀ 𝑙 2 1 ( 1 + 𝛿 ) βˆ€ π‘Ÿ β‰₯ 𝑑 1 . ( 3 . 1 1 ) For 𝑑 β‰₯ 𝑑 1 , we can obtain from (3.5) and 𝑓 ( 0 ) = 0 that ξ€œ 𝑓 ( 𝑑 ) = βˆ’ 𝑑 0 ξ‚Έ βˆ’ ξ€œ e x p 𝑑 𝑠 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ( ξ€Έ ξ‚Ή ξ‚Έ βˆ’ ξ€œ π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝛼 ( 𝑠 ) 𝑒 ( 𝑠 ) 𝑑 𝑠 = βˆ’ e x p 𝑑 0 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ( ξ€Έ ξ‚Ή ξ€œ π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝑑 1 0 ξ‚Έ ξ€œ e x p 𝑠 0 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ( ξ€Έ ξ‚Ή βˆ’ ξ€œ π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝛼 ( 𝑠 ) 𝑒 ( 𝑠 ) 𝑑 𝑠 𝑑 𝑑 1 ξ‚Έ βˆ’ ξ€œ e x p 𝑑 𝑠 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ξ€Έ ξ‚Ή ( π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝛼 ( 𝑠 ) 𝑒 ( 𝑠 ) 𝑑 𝑠 . ( 3 . 1 2 ) As 𝛽 ( π‘Ÿ ) + 𝜎 2 ( π‘Ÿ ) 𝑒 ( π‘Ÿ ) β‰₯ 𝛽 1 + 𝜎 2 1 𝑙 2 2 ( 1 βˆ’ 𝛿 ) holds for all 𝑑 β‰₯ 𝑑 1 , thus, the first term in (3.12) goes to 0 as 𝑑 β†’ ∞ . For the second term in (3.12), we have | | | | ξ€œ 𝑑 𝑑 1 ξ‚Έ βˆ’ ξ€œ e x p 𝑑 𝑠 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ξ€Έ ξ‚Ή | | | | ≀ ξ€œ ( π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝛼 ( 𝑠 ) 𝑒 ( 𝑠 ) 𝑑 𝑠 𝑑 0 ξ€Ί βˆ’ ξ€· 𝛽 e x p 1 + 𝜎 2 1 𝑙 2 2 ξ€Έ ξ€» 𝑙 ( 1 βˆ’ 𝛿 ) ( 𝑑 βˆ’ 𝑠 ) 2 1 = 𝑙 ( 1 + 𝛿 ) 𝑑 𝑠 2 1 ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 ξ€œ ( 1 βˆ’ 𝛿 ) 𝑑 0 ξ€Ί βˆ’ ξ€· 𝛽 e x p 1 + 𝜎 2 1 𝑙 2 2 ξ€Έ ξ€» 𝑑 ξ€· 𝛽 ( 1 βˆ’ 𝛿 ) ( 𝑑 βˆ’ 𝑠 ) 1 + 𝜎 2 1 𝑙 2 2 ξ€Έ 𝑠 = 𝑙 ( 1 βˆ’ 𝛿 ) 2 1 ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 ξ€· ξ€Ί βˆ’ ξ€· 𝛽 ( 1 βˆ’ 𝛿 ) 1 βˆ’ e x p 1 + 𝜎 2 1 𝑙 2 2 ξ€Έ 𝑑 ≀ 𝑙 ( 1 βˆ’ 𝛿 ) ξ€» ξ€Έ 2 1 ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 . ( 1 βˆ’ 𝛿 ) ( 3 . 1 3 ) By similar arguments, we obtain that | | | | ξ€œ 𝑑 𝑑 1 ξ‚Έ βˆ’ ξ€œ e x p 𝑑 𝑠 ξ€· 𝛽 ( π‘Ÿ ) + 𝜎 2 ξ€Έ ξ‚Ή | | | | β‰₯ 𝑙 ( π‘Ÿ ) 𝑒 ( π‘Ÿ ) 𝑑 π‘Ÿ 𝛼 ( 𝑠 ) 𝑒 ( 𝑠 ) 𝑑 𝑠 2 2 ( 1 βˆ’ 𝛿 ) 𝛽 2 + 𝜎 2 2 𝑙 2 1 . ( 1 + 𝛿 ) ( 3 . 1 4 ) Therefore, for any πœ‰ > 0 , there exists 𝑑 ( πœ‰ ) > 0 such that 𝑙 2 2 ( 1 βˆ’ 𝛿 ) 𝛽 2 + 𝜎 2 2 𝑙 2 1 ≀ | | | | ≀ 𝑙 ( 1 + 𝛿 ) 𝑓 ( 𝑑 ) 2 1 ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 ( 1 βˆ’ 𝛿 ) βˆ€ 𝑑 β‰₯ 𝑑 ( πœ‰ ) . ( 3 . 1 5 ) For all 𝑑 β‰₯ 𝑑 ( πœ‰ ) , we can get from (3.5) that ξ€· Μ‡ 𝑔 = 2 | 𝛼 | βˆ’ 𝜎 2 | | 𝑓 | | ξ€Έ | | 𝑓 | | β‰₯  2 𝛼 1 βˆ’ 𝜎 2 2 𝑙 2 1 ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 ξƒͺ 𝑙 ( 1 βˆ’ 𝛿 ) 2 2 ( 1 βˆ’ 𝛿 ) 𝛽 2 + 𝜎 2 2 𝑙 2 1 =  ( 1 + 𝛿 ) 2 𝛼 1 ξ€· 𝛽 1 + 𝜎 2 1 𝑙 2 2 ξ€Έ βˆ’ 𝜎 2 2 ξ€· 𝑙 2 1 ξ€Έ ( 1 + 𝛿 ) 𝛽 1 + 𝜎 2 1 𝑙 2 2 ( ξƒͺ 𝑙 1 βˆ’ 𝛿 ) 2 2 ( 1 βˆ’ 𝛿 ) 𝛽 2 + 𝜎 2 2 𝑙 2 1 ( . 1 + 𝛿 ) ( 3 . 1 6 ) By assumption (b6), we get Μ‡ 𝑔 > 0 for a sufficiently small πœ‰ > 0 . This implies that 𝑔 ( 𝑑 ) goes to infinity at least as a linear function. Thus, there exists a constant 𝐢 > 0 , such that 𝔼 ξ€· πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 ξ€Έ 2 = 𝑆 πœƒ πœƒ = 𝑒 β„Ž ≀ 𝐢 𝑑 βˆ’ 1 . ( 3 . 1 7 ) Hence, for arbitrary πœ– > 0 and all 𝑇 > 0 , it follows from Chebyshev’s inequality that 𝑃 ξ€· | | πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 | | ξ€Έ ≀ 1 > πœ– πœ– 2 𝐢 𝑇 βˆ’ 1 . ( 3 . 1 8 )
The proof is complete.

Remark 3.3. From the proof of Theorem 3.2, we can see that πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 goes to 0 in 𝐿 2 -sense under the given conditions. In other words, Μ‚ πœƒ 𝑑 is asymptotically unbiased.

Remark 3.4. It is well known that Kalman-Bucy linear filtering theory remains valid if one replaces the Brownian motion ( π‘Š 𝑑 , 𝑉 𝑑 ) in systems (2.2) and (2.3) by an arbitrary centered orthogonal increment process of the same covariance structure. Thus, Theorem 3.2 remains valid under this replacement.

4. Strong Consistency

In last section, we give the conditions for the convergence rate of the estimator. Furthermore, we use the comparison theorem to proof the strong consistency in this section. As we all know, if the parameter πœƒ is, a genuine Gaussian random variable, then we can have a clear statistical interpretation for the convergence rate. Firstly, we pick πœƒ 0 at random; secondly, let system (2.2) run up to time 𝑑 and simultaneously observe π‘Œ by system (2.3); finally, compute Μ‚ πœƒ 𝑑 as the following form.

The Kalman-Bucy linear filtering theory shows us βŽ› ⎜ ⎜ ⎝ 𝑑 𝑋 𝑑 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = ξ‚΅ 𝐢 𝐴 ( 𝑑 ) βˆ’ 𝑇 ( 𝑑 ) 𝐢 ( 𝑑 ) 𝐷 2 ξ‚Ά βŽ› ⎜ ⎜ ⎝ 𝑋 ( 𝑑 ) 𝑆 ( 𝑑 ) 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ 𝑑 𝑑 + 𝐢 ( 𝑑 ) 𝐷 2 ( 𝑑 ) 𝑆 ( 𝑑 ) 𝑑 π‘Œ 𝑑 = βŽ› ⎜ ⎜ ⎜ ⎝ πœ‡ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ βˆ’ πœ‡ ( 𝑑 ) 𝛼 ( 𝑑 ) 2 ( 𝑑 ) 𝛾 2 ( 𝑆 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ 𝑋 ( 𝑑 ) 0 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ πœ‡ 𝑑 𝑑 + 2 ( 𝑑 ) 𝛾 2 βŽ› ⎜ ⎜ ⎝ 𝑆 ( 𝑑 ) π‘₯ π‘₯ 𝑆 ( 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎠ ( 𝑑 ) 𝑑 π‘Œ 𝑑 ( 4 . 1 ) with initial conditions  𝑋 0 = 𝔼 [ 𝑋 0 ] and Μ‚ πœƒ 0 = 𝔼 [ πœƒ 0 ] . If we denote that Ξ¦ ( 𝑑 ) is the matrix fundamental solution of the deterministic linear system βŽ› ⎜ ⎜ ⎝ Μ‡ π‘₯ 𝑑 Μ‡ 𝑦 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎝ πœ‡ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ βˆ’ πœ‡ ( 𝑑 ) 𝛼 ( 𝑑 ) 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ ⎞ ⎟ ⎟ ⎠ ( 𝑑 ) 0 π‘₯ ( 𝑑 ) 𝑦 ( 𝑑 ) , ( 4 . 2 ) then the solution to (4.1) is given by βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = Ξ¦ ( 𝑑 ) Ξ¦ βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝔼 ξ€Ί 𝑋 ( 0 ) 0 ξ€» 𝔼 ξ€Ί πœƒ 0 ξ€» ⎞ ⎟ ⎟ ⎠ + ξ€œ 𝑑 0 Ξ¦ ( 𝑑 ) Ξ¦ βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝑆 ( 𝑠 ) π‘₯ π‘₯ 𝑆 ( 𝑑 ) πœƒ π‘₯ ( ⎞ ⎟ ⎟ ⎠ 𝑑 ) 𝑑 π‘Œ 𝑠 . ( 4 . 3 ) And for every particular experiment πœ” , the quantity ( πœƒ 0 Μ‚ πœƒ ( πœ” ) βˆ’ 𝑑 ( πœ” ) ) 2 would be the squared estimation error.

But in this paper πœƒ is a fixed parameter, so we can only choose πœƒ 0 ( πœ” ) = πœƒ , and then the statistical mean over different values of πœƒ 0 ( πœ” ) has no experimental meaning. The true estimation error is given by Μ‚ πœƒ πœƒ βˆ’ 𝑑 , not πœƒ 0 βˆ’ Μ‚ πœƒ 𝑑 . It is therefore desirable that estimator Μ‚ πœƒ 𝑑 converges to πœƒ 0 for “all fixed values 𝜐 = πœƒ 0 " a.s. To establish such an assertion we work with a product space ( 𝑅 Γ— Ξ© , ℬ ( 𝑅 ) βŠ— β„± , πœ‚ βŠ— 𝑃 ) , where πœ‚ denotes the law of πœƒ 0 , and ( Ξ© , β„± , 𝑃 ) is the underlying probability space for Brownian motion ( π‘Š 𝑑 , 𝑉 𝑑 ) 𝑑 β‰₯ 0 . This space is most appropriate because one can make 𝑃 a.s. statements for fixed 𝜐 ∈ ℝ . Notice that in this representation we have πœƒ 0 ( 𝜐 , πœ” ) = 𝜐 for all ( 𝜐 , πœ” ) ∈ ℝ Γ— Ξ© . Assuming this underlying probability space, we use the comparison theorem to get the following consistency result.

In the proof of Theorem 3.2, we know that 𝑒 , 𝑓 is bonded and 𝑔 is monotonically increasing, moreover, 𝑆 π‘₯ π‘₯ ( 𝑑 ) = π‘Ž = 𝑔 / β„Ž = 𝑔 / ( 𝑒 𝑔 βˆ’ 𝑓 2 ) = ( 𝑔 βˆ’ 𝑓 2 / 𝑒 + 𝑓 2 / 𝑒 ) / ( 𝑒 𝑔 βˆ’ 𝑓 2 ) = 1 / 𝑒 + 𝑓 2 / 𝑒 ( 𝑒 𝑔 βˆ’ 𝑓 2 ) and 𝑆 πœƒ π‘₯ ( 𝑑 ) = 𝑏 = 𝑓 / β„Ž = 𝑓 / ( 𝑒 𝑔 βˆ’ 𝑓 2 ) . Thus, there exist positive constants π‘Ž 1 , π‘Ž 2 , 𝑏 1 , and 𝑏 2 such that π‘Ž 1 ≀ π‘Ž ≀ π‘Ž 2 and 𝑏 1 ≀ 𝑏 ≀ 𝑏 2 .

Theorem 4.1. Assume that the following two conditions are satisfied:(c1): Μ‚ πœƒ 𝑑 converges to πœƒ 0 in 𝐿 2 ( πœ‚ βŠ— 𝑃 ) ;(c2): 𝛽 2 βˆ’ πœ‡ 2 2 / 𝛾 2 2 < 0 ;(c3): ( 𝛽 2 βˆ’ ( πœ‡ 2 2 / 𝛾 2 2 ) π‘Ž 2 ) 2 βˆ’ 4 𝛼 2 ( πœ‡ 2 2 / 𝛾 2 2 ) 𝑏 2 < 0 .
Then, for all fixed 𝜐 ∈ ℝ , we have Μ‚ πœƒ 𝑑 ( 𝜐 , β‹… ) ⟢ 𝜐 , 𝑃 - π‘Ž . 𝑠 . , π‘Ž 𝑠 𝑑 ⟢ ∞ . ( 4 . 4 )

Proof. We will show that (4.4) holds for all 𝜐 ∈ 𝑁 𝑐 , where πœ‚ ( 𝑁 ) = 0 .
By Kalman-Bucy linear filtering theory, we know βŽ› ⎜ ⎜ ⎝ 𝑑 𝑋 𝑑 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = ξ‚΅ 𝐢 𝐴 ( 𝑑 ) βˆ’ 𝑇 ( 𝑑 ) 𝐢 ( 𝑑 ) 𝐷 2 ξ‚Ά βŽ› ⎜ ⎜ ⎝ 𝑋 ( 𝑑 ) 𝑆 ( 𝑑 ) 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ 𝑑 𝑑 + 𝐢 ( 𝑑 ) 𝐷 2 ( 𝑑 ) 𝑆 ( 𝑑 ) 𝑑 π‘Œ 𝑑 = βŽ› ⎜ ⎜ ⎜ ⎝ πœ‡ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ βˆ’ πœ‡ ( 𝑑 ) 𝛼 ( 𝑑 ) 2 ( 𝑑 ) 𝛾 2 ( 𝑆 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ 𝑋 ( 𝑑 ) 0 𝑑 πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ πœ‡ 𝑑 𝑑 + 2 ( 𝑑 ) 𝛾 2 βŽ› ⎜ ⎜ ⎝ 𝑆 ( 𝑑 ) π‘₯ π‘₯ 𝑆 ( 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎠ ( 𝑑 ) 𝑑 π‘Œ 𝑑 ( 4 . 5 ) with initial conditions  𝑋 0 = 𝔼 [ 𝑋 0 Μ‚ πœƒ ] a n d 0 = 𝔼 [ πœƒ 0 ] = 𝔼 [ 𝜐 ] = 𝜐 .
Since the following linear equations: βŽ› ⎜ ⎜ ⎝ Μ‡ π‘₯ 𝑑 Μ‡ 𝑦 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎝ πœ‡ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ βˆ’ πœ‡ ( 𝑑 ) 𝛼 ( 𝑑 ) 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) πœƒ π‘₯ ⎞ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ ⎞ ⎟ ⎟ ⎠ ( 𝑑 ) 0 π‘₯ ( 𝑑 ) 𝑦 ( 𝑑 ) ( 4 . 6 ) equal to Μ‡ π‘₯ 𝑑 = ξ‚Έ πœ‡ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ ξ‚Ή ( 𝑑 ) π‘₯ ( 𝑑 ) + 𝛼 ( 𝑑 ) π‘Œ ( 𝑑 ) , Μ‡ 𝑦 𝑑 πœ‡ = βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) πœƒ π‘₯ ( 𝑑 ) π‘₯ ( 𝑑 ) , ( 4 . 7 ) it follows from (c1)–(c3) that 𝛽 1 βˆ’ πœ‡ 2 1 𝛾 2 1 π‘Ž 1 πœ‡ ≀ 𝛽 ( 𝑑 ) βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) π‘₯ π‘₯ ( 𝑑 ) ≀ 𝛽 2 βˆ’ πœ‡ 2 2 𝛾 2 2 π‘Ž 2 𝛼 < 0 , 1 ≀ 𝛼 ( 𝑑 ) ≀ 𝛼 2 , βˆ’ πœ‡ 2 1 𝛾 2 1 𝑏 1 πœ‡ ≀ βˆ’ 2 ( 𝑑 ) 𝛾 2 𝑆 ( 𝑑 ) πœƒ π‘₯ πœ‡ ( 𝑑 ) ≀ βˆ’ 2 2 𝛾 2 2 𝑏 2 . ( 4 . 8 ) For linear equations: βŽ› ⎜ ⎜ ⎝ Μ‡ π‘₯ 𝑑 Μ‡ 𝑦 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ 𝛽 1 βˆ’ πœ‡ 2 1 𝛾 2 1 π‘Ž 1 𝛼 1 βˆ’ πœ‡ 2 1 𝛾 2 1 𝑏 1 0 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ ⎞ ⎟ ⎟ ⎠ , βŽ› ⎜ ⎜ ⎝ π‘₯ ( 𝑑 ) 𝑦 ( 𝑑 ) Μ‡ π‘₯ 𝑑 Μ‡ 𝑦 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ 𝛽 2 βˆ’ πœ‡ 2 2 𝛾 2 2 π‘Ž 2 𝛼 2 βˆ’ πœ‡ 2 2 𝛾 2 2 𝑏 2 0 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝ π‘₯ ⎞ ⎟ ⎟ ⎠ , ( 𝑑 ) 𝑦 ( 𝑑 ) ( 4 . 9 ) if we set Ξ¦ 1 ( 𝑑 ) and Ξ¦ 2 ( 𝑑 ) that are the matrix fundamental solution of (4.9), we can obtain from the comparison theorem that Ξ¦ 1 ( 𝑑 ) ≀ Ξ¦ ( 𝑑 ) ≀ Ξ¦ 2 ( 𝑑 ) . ( 4 . 1 0 )
It is not difficult to explore (4.9), and get Ξ¦ 1 βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ βˆ’ πœ† ( 𝑑 ) = ξ…ž 1 𝑁 2 1 𝑒 πœ† β€² 1 𝑑 βˆ’ πœ† ξ…ž 2 𝑁 2 1 𝑒 πœ† β€² 2 𝑑 𝑒 πœ† β€² 1 𝑑 𝑒 πœ† β€² 2 𝑑 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ , Ξ¦ 2 βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ βˆ’ πœ† ( 𝑑 ) = 1 𝑀 2 1 𝑒 πœ† 1 𝑑 βˆ’ πœ† 2 𝑀 2 1 𝑒 πœ† 2 𝑑 𝑒 πœ† 1 𝑑 𝑒 πœ† 2 𝑑 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ , Ξ¦ 1 βˆ’ 1 ( βŽ› ⎜ ⎜ ⎜ ⎜ ⎜ ⎝ βˆ’ 𝑁 𝑑 ) = 2 1 πœ† ξ…ž 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† β€² 1 𝑑 βˆ’ πœ† ξ…ž 2 πœ† ξ…ž 1 βˆ’ πœ† ξ…ž 2 𝑒 βˆ’ πœ† β€² 1 𝑑 𝑁 2 1 πœ† ξ…ž 1 βˆ’ πœ† ξ…ž 2 𝑒 βˆ’ πœ† β€² 2 𝑑 πœ† ξ…ž 1 πœ† ξ…ž 1 βˆ’ πœ† ξ…ž 2 𝑒 βˆ’ πœ† β€² 2 𝑑 ⎞ ⎟ ⎟ ⎟ ⎟ ⎟ ⎠ , Ξ¦ 2 βˆ’ 1 ( βŽ› ⎜ ⎜ ⎜ ⎜ ⎜ ⎝ βˆ’ 𝑀 𝑑 ) 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 1 𝑑 βˆ’ πœ† 2 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 1 𝑑 𝑀 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 πœ† 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 ⎞ ⎟ ⎟ ⎟ ⎟ ⎟ ⎠ , ( 4 . 1 1 ) where 𝑁 1 1 = 𝛽 1 βˆ’ ( πœ‡ 2 1 / 𝛾 2 1 ) π‘Ž 1 , 𝑁 1 2 = 𝛼 1 , 𝑁 2 1 = ( πœ‡ 2 1 / 𝛾 2 1 ) 𝑏 1 , πœ† ξ…ž 1 = ( 𝑁 1 1 +  𝑁 2 1 1 βˆ’ 4 𝑁 1 2 𝑁 2 1 ) / 2 , πœ† ξ…ž 2 = ( 𝑁 1 1 βˆ’  𝑁 2 1 1 βˆ’ 4 𝑁 1 2 𝑁 2 1 ) / 2 , 𝑀 1 1 = 𝛽 2 βˆ’ ( πœ‡ 2 2 / 𝛾 2 2 ) π‘Ž 2 , 𝑀 1 2 = 𝛼 2 , 𝑀 2 1 = ( πœ‡ 2 2 / 𝛾 2 2 ) 𝑏 2 , πœ† 1 = ( 𝑀 1 1 +  𝑀 2 1 1 βˆ’ 4 𝑀 1 2 𝑀 2 1 ) / 2 , πœ† 2 = ( 𝑀 1 1 βˆ’  𝑀 2 1 1 βˆ’ 4 𝑀 1 2 𝑀 2 1 ) / 2 .
By assumption (c2) and (c3), we know that πœ† ξ…ž 1 < 0 , πœ† ξ…ž 2 < 0 , πœ† 1 < 0 , and πœ† 2 < 0 .
By the ODE theory [37, 38] and above discussion, we know that the solution of (4.1) is given by βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = Ξ¦ ( 𝑑 ) Ξ¦ βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝔼 ξ€Ί 𝑋 ( 0 ) 0 ξ€» 𝔼 ξ€Ί πœƒ 0 ξ€» ⎞ ⎟ ⎟ ⎠ + ξ€œ 𝑑 0 Ξ¦ ( 𝑑 ) Ξ¦ βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝑆 ( 𝑠 ) π‘₯ π‘₯ 𝑆 ( 𝑑 ) πœƒ π‘₯ ( ⎞ ⎟ ⎟ ⎠ 𝑑 ) 𝑑 π‘Œ 𝑠 . ( 4 . 1 2 ) Using the similar method, we can also obtain the solutions for the following two equations: βŽ› ⎜ ⎜ ⎝ 𝑑  𝑋 𝑑 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ 𝛽 1 βˆ’ πœ‡ 2 1 𝛾 2 1 π‘Ž 1 𝛼 1 βˆ’ πœ‡ 2 1 𝛾 2 1 𝑏 1 0 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ πœ‡ 𝑑 𝑑 + 1 𝛾 1 βŽ› ⎜ ⎜ ⎝ π‘Ž 1 𝑏 1 ⎞ ⎟ ⎟ ⎠ 𝑑 π‘Œ 𝑑 βŽ› ⎜ ⎜ ⎝ 𝑑  𝑋 , ( 4 . 1 3 ) 𝑑 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = βŽ› ⎜ ⎜ ⎜ ⎜ ⎝ 𝛽 2 βˆ’ πœ‡ 2 2 𝛾 2 2 π‘Ž 2 𝛼 2 βˆ’ πœ‡ 2 2 𝛾 2 2 𝑏 2 0 ⎞ ⎟ ⎟ ⎟ ⎟ ⎠ βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ πœ‡ 𝑑 𝑑 + 2 𝛾 2 βŽ› ⎜ ⎜ ⎝ π‘Ž 2 𝑏 2 ⎞ ⎟ ⎟ ⎠ 𝑑 π‘Œ 𝑑 , ( 4 . 1 4 ) where  𝑋 0 = 𝔼 [ 𝑋 0 ] and Μ‚ πœƒ 0 = 𝔼 [ πœƒ 0 ] = 𝔼 [ 𝜐 ] = 𝜐 .
The solutions of the two equations are explored as the following form: βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = Ξ¦ 1 ( 𝑑 ) Ξ¦ 1 βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝔼 ξ€Ί 𝑋 ( 0 ) 0 ξ€» 𝔼 ξ€Ί πœƒ 0 ξ€» ⎞ ⎟ ⎟ ⎠ + ξ€œ 𝑑 0 Ξ¦ 1 ( 𝑑 ) Ξ¦ 1 βˆ’ 1 βŽ› ⎜ ⎜ ⎝ π‘Ž ( 𝑠 ) 1 𝑏 1 ⎞ ⎟ ⎟ ⎠ 𝑑 π‘Œ 𝑠 , βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = Ξ¦ 2 ( 𝑑 ) Ξ¦ 2 βˆ’ 1 ( βŽ› ⎜ ⎜ ⎝ 𝔼 ξ€Ί 𝑋 0 ) 0 ξ€» 𝔼 ξ€Ί πœƒ 0 ξ€» ⎞ ⎟ ⎟ ⎠ + ξ€œ 𝑑 0 Ξ¦ 2 ( 𝑑 ) Ξ¦ 2 βˆ’ 1 ( βŽ› ⎜ ⎜ ⎝ π‘Ž 𝑠 ) 2 𝑏 2 ⎞ ⎟ ⎟ ⎠ 𝑑 π‘Œ 𝑠 . ( 4 . 1 5 )
For (4.14), we have that βŽ› ⎜ ⎜ ⎝  𝑋 𝑑 Μ‚ πœƒ 𝑑 ⎞ ⎟ ⎟ ⎠ = Ξ¦ 2 ( 𝑑 ) Ξ¦ 2 βˆ’ 1 βŽ› ⎜ ⎜ ⎝ 𝔼 ξ€Ί 𝑋 ( 0 ) 0 ξ€» 𝔼 ξ€Ί πœƒ 0 ξ€» ⎞ ⎟ ⎟ ⎠ + ξ€œ 𝑑 0 Ξ¦ 2 ( 𝑑 ) Ξ¦ 2 βˆ’ 1 βŽ› ⎜ ⎜ ⎝ π‘Ž ( 𝑠 ) 2 𝑏 2 ⎞ ⎟ ⎟ ⎠ 𝑑 π‘Œ 𝑠 ( 4 . 1 6 ) yields that Μ‚ πœƒ 𝑑 = ξ€œ 𝑑 0 ξ‚Έ π‘Ž 2 ξ‚΅ 𝑀 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 ( 𝑑 βˆ’ 𝑠 ) βˆ’ 𝑀 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 ( 𝑑 βˆ’ 𝑠 ) ξ‚Ά + 𝑏 2 ξ‚΅ πœ† 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 ( 𝑑 βˆ’ 𝑠 ) βˆ’ πœ† 2 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 ( 𝑑 βˆ’ 𝑠 ) ξ‚Ά ξ‚Ή 𝑑 π‘Œ 𝑠 + ξ‚΅ 𝑀 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 βˆ’ 𝑀 2 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 ξ‚Ά 𝑋 0 + ξ‚΅ πœ† 1 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 βˆ’ πœ† 2 πœ† 1 βˆ’ πœ† 2 𝑒 βˆ’ πœ† 2 𝑑 ξ‚Ά πœƒ 0 . ( 4 . 1 7 ) Since πœ† 1 < 0 and πœ† 2 < 0 , it is easy to get Μ‚ πœƒ 𝑑 ( 𝜐 , β‹… ) ⟢ 𝜐 , 𝑃 - a . s . , a s 𝑑 ⟢ ∞ . ( 4 . 1 8 ) For (4.13), we can also get Μ‚ πœƒ 𝑑 ( 𝜐 , β‹… ) ⟢ 𝜐 , 𝑃 - a . s . , a s 𝑑 ⟢ ∞ . ( 4 . 1 9 ) Hence, for (4.1), we can get the following result: Μ‚ πœƒ 𝑑 ( 𝜐 , β‹… ) ⟢ 𝜐 , 𝑃 - a . s . , a s 𝑑 ⟢ ∞ . ( 4 . 2 0 ) The proof is complete.

Remark 4.2. Under the probability space used in this paper, we can see that Theorem 3.2 is the particular form of Theorem 4.1 if we use Chebyshev’s inequality on the result of Theorem 4.1.

Remark 4.3. The strong consistency in Deck [30] requires that Μ‚ πœƒ 𝑑 is a martingale, while, in our result, Μ‚ πœƒ 𝑑 can be not a martingale. Furthermore, when Μ‚ πœƒ 𝑑 is a martingale, our result is more strong than Deck’s, so in that case we can relax the conditions as Deck.

5. Conclusions

In this paper, we have investigated the parameter estimation problem for a class of linear stochastic systems called Hull-White stochastic differential equations which are important models in finance. Firstly, Bayesian viewpoint is first chosen to analyze the parameter estimation problem based on Kalman-Bucy linear filtering theory. Secondly, some sufficient conditions on coefficients are given to study the asymptotic convergence problem. Finally, the strong consistent property of estimator is discussed by Kalman-Bucy linear filtering theory and comparison theorem.

Acknowledgments

This work was supported by the National Nature Science Foundation of China under Grant no. 60974030 and the Science and Technology Project of Education Department in Fujian Province JA11211.

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