Abstract

The mathematical formulation for a quadratic optimal control problem governed by a linear quasiparabolic integrodifferential equation is studied. The control constrains are given in an integral sense: 𝑈𝑎𝑑={𝑢𝑋;Ω𝑈𝑢0,𝑡[0,𝑇]}. Then the a posteriori error estimates in 𝐿(0,𝑇;𝐻1(Ω))-norm and 𝐿2(0,𝑇;𝐿2(Ω))-norm for both the state and the control approximation are given.

1. Introduction

Integrodifferential equations of quasiparabolic and their control of this nature appear in applications such as biology mechanics, nuclear reaction dynamics, heat conduction in materials with memory, and viscoelasticity. All these models express a conservation of a certain quantity in any moment for any subdomain and the historical accumulation feature in the physical models. This in many applications is the most desirable feature of the approximation method when it comes to numerical solution of the corresponding initial boundary value problem. The existence and uniqueness of the solution of the quasiparabolic Integrodifferential equations has been studied in [1]. Finite element methods for quasiparabolic Integrodifferential equations problems with a smooth kernel have been discussed in Cui [2]. Although there is so much work for the finite element approximation of this problem, to our knowledge, there has been a lack of a posteriori error estimates for finite element approximation of any quasiparabolic Integrodifferential optimal control problem.

The finite element approximation of optimal control problems has been an important topic in engineering design works. There have been extensive theoretical and numerical studies for various optimal control problems, see, for instance, [311], although it is impossible to give even a very brief review here. And research on finite element approximation of parabolic optimal control problems can be found in, for example, [12, 13].

Among many finite element methods, the adaptive finite element method based on a posteriori error estimates has become a central theme in scientific and engineering computations for its high efficiency. In order to obtain a numerical solution of acceptable accuracy, it is essential for the adaptive finite element method to use a posteriori error estimate indicators to guide the mesh refinement procedure. We only need refine the area where the error indicators are larger, so that a higher density of nodes are distributed over the area where the solution is difficult to approximate. In this sense, adaptive finite element approximation relies very much on the error indicators used, which are often based on a posteriori error estimates of the solutions.

The purpose of this paper is to derive the a posteriori error estimates for the semidiscrete finite element approximation of a quadratic optimal control problem governed by a linear quasiparabolic Integrodifferential equation, which paves a way to derive the a posteriori error estimates for the full discrete finite element approximation for this control problem and thus to develop its adaptive finite element schemes. We extend the existing techniques and results in [1416] to the optimal control problem governed by the Integrodifferential equation of quasiparabolic type.

The outline of the paper is as follows. In Section 2, we first briefly introduce the optimal control problem and give the optimality conditions, then construct the finite element approximation schemes for the optimal control problem. In Section 3, we give the a posteriori error bounds in 𝐿(0,𝑇;𝐻1(Ω))-norm for the control problem. And the a posteriori error bounds in 𝐿2(0,𝑇;𝐿2(Ω))-norm for the control problem are derived in Section 4.

2. Optimal Control Problem and Its Finite Element Approximation

Let Ω and Ω𝑈 be bounded convex polygon domains in 𝑅𝑑 with Lipschitz boundary 𝜕Ω and 𝜕Ω𝑈. In this paper, we adopt the standard notation 𝑊𝑚,𝑞(Ω) for Sobolev spaces on Ω with norm 𝑚,𝑞,Ω, and seminorm  ||𝑚,𝑞,Ω. We set 𝑊0𝑚,𝑞(Ω)={𝑤𝑊𝑚,𝑞(Ω)𝑤|𝜕Ω=0}. We denote 𝑊𝑚,2(Ω)(𝑊0𝑚,2(Ω)) by 𝐻𝑚(Ω)(𝐻𝑚0(Ω)), with norm  𝑚,Ω, and seminorm  ||𝑚,Ω.

We denote by 𝐿𝑠(0,𝑇;𝑊𝑚,𝑞(Ω)) the Banach space of all 𝐿𝑠 integrable functions from (0,𝑇) into 𝑊𝑚,𝑞(Ω) with norm 𝑣𝐿𝑠(0,𝑇;𝑊𝑚,𝑞(Ω))=(𝑇0𝑣𝑠𝑊𝑚,𝑞(Ω)𝑑𝑡)1/𝑠 for 𝑠[1,) and the standard modification for 𝑠=. Similarly, one can define the spaces 𝐻1(0,𝑇;𝑊𝑚,𝑞(Ω)) and 𝐶𝑘(0,𝑇;𝑊𝑚,𝑞(Ω)). The details can be found in [17]. In addition, 𝑐 or 𝐶 denotes a general positive constant independent of the mesh size .

In the following, we will give semi-discrete finite element approximation schemes for the optimal control problem governed by a linear quasiparabolic Integrodifferential equation.

2.1. Model Problem and Its Weak Formulation

We will take the state space 𝑊=𝐿2(0,𝑇;𝑉) with 𝑉=𝐻10(Ω) and the control space 𝑋=𝐿2(0,𝑇;𝑈) with 𝑈=𝐿2(Ω𝑈). Let the observation space 𝑌=𝐿2(0,𝑇;𝐻) with 𝐻=𝐿2(Ω) and 𝑈𝑎𝑑𝑋 a convex subset.

We are interested in the following optimal control problem: min𝑢𝑈𝑎𝑑𝑋1𝐽(𝑢,𝑦(𝑢))=2𝑇0𝑦𝑧𝑑20,Ω𝑑𝑡+𝑇0𝑢20,Ω𝑈,𝑑𝑡(2.1) subject to 𝑦𝑡div𝐴𝑦𝑡+𝐷𝑦+𝑡0],[],𝐶(𝑡,𝜏)𝑦(𝑥,𝜏)𝑑𝜏=𝑓+𝐵𝑢,inΩ×(0,𝑇𝑦=0,on𝜕Ω×0,𝑇𝑦|𝑡=0=𝑦0,inΩ,(2.2) where 𝑢 is control, 𝑦 is state, 𝑧𝑑 is the observation, 𝑈𝑎𝑑 is a closed convex subset, 𝑓(𝑥,𝑡)𝐿2(0,𝑇;𝐿2(Ω)), and 𝑧𝑑 and 𝑦0𝐻1(Ω) are some suitable functions to be specified later. 𝐵 is a linear bounded operator from 𝐿2(Ω𝑈) to 𝐿2(Ω) independent of 𝑡. And 𝑎𝐴=𝐴(𝑥)=𝑖,𝑗()𝑛×𝑛𝐶Ω𝑛×𝑛𝑑,𝐷=𝐷(𝑥)=𝑖,𝑗()𝑛×𝑛𝐶Ω𝑛×𝑛,(2.3) such that there is a constant 𝑐>0 satisfying that for any vector 𝑋𝑅𝑛 as follows: 𝑋𝑡𝐴𝑋𝑐𝑋2𝑅𝑛,𝑋𝑡𝐷𝑋𝑐𝑋2𝑅𝑛,(2.4)𝐶=𝐶(𝑥,𝑡,𝜏)=(𝑐𝑖,𝑗(𝑥,𝑡,𝜏))𝑛×𝑛(𝐶(0,𝑇;𝐿2(Ω))𝑛×𝑛).

Let 𝑓1,𝑓2=Ω𝑓1𝑓2𝑓,1,𝑓2𝐻×𝐻,(𝑢,𝑣)𝑈=Ω𝑈𝑢𝑣,(𝑢,𝑣)𝑈×𝑈,𝑎(𝑧,𝜔)=(𝐴𝑧,𝜔),𝑑(𝑧,𝜔)=(𝐷𝑧,𝜔),𝑐(𝑡,𝜏;𝑧,𝜔)=(𝐶(𝑡,𝜏)𝑧,𝜔),𝑧,𝑤𝑉×𝑉.(2.5) In the case that 𝑓1𝑉 and 𝑓2𝑉, the dual pair (𝑓1,𝑓2) is understood as 𝑓1,𝑓2𝑉×𝑉.

Assume that there are constants 𝑐and 𝐶, such that for all 𝑡 and 𝜏 in [0,𝑇] as follows: (𝑎)𝑎(𝑧,𝑧)𝑐𝑧21,Ω,||||(b)𝑎(𝑧,𝑤)𝐶𝑧1,Ω𝑤1,Ω,||||𝑑(𝑧,𝑤)𝐶𝑧1,Ω𝑤1,Ω,(||||c)𝑐(𝑡,𝜏;𝑧,𝑤)𝐶𝑧1,Ω𝑤1,Ω.(2.6) for any 𝑧 and 𝑤 in 𝑉.

Then the weak form of the state equation reads as 𝑦𝑡𝑦,𝑤+𝑎𝑡,𝑤+𝑑(𝑦,𝑤)+𝑡0],𝑐(𝑡,𝜏;𝑦(𝜏),𝑤)𝑑𝜏=(𝑓+𝐵𝑢,𝑤)𝑤𝑉,𝑡(0,𝑇𝑦|𝑡=0=𝑦0.(2.7) It is well known (see, e.g., [1]) that the above weak formulation has at least one solution in  𝑦𝑊(0,𝑇)={𝑤𝐿(0,𝑇;𝐻1(Ω)),𝑤𝑡𝐿2(0,𝑇;𝐻1(Ω))}.

Therefore, the weak form of the control problem (2.1) and (2.2) reads as (OCP) min𝑢𝑈𝑎𝑑𝑦𝐽(𝑢,𝑦(𝑢)),𝑡𝑦,𝑤+𝑎𝑡,𝑤+𝑑(𝑦,𝑤)+𝑡0],𝑐(𝑡,𝜏;𝑦(𝜏),𝑤)𝑑𝜏=(𝑓+𝐵𝑢,𝑤)𝑤𝑉,𝑡(0,𝑇𝑦|𝑡=0=𝑦0.(2.8) In the following, we first give the existence and uniqueness of the solution of the system (2.8).

Theorem 2.1. Assume that the condition (2.6) (a)–(c) holds. There exists the unique solution (𝑢,𝑦) for the minimization problem (2.8) such that 𝑢𝐿2(0,𝑇;𝐿2(Ω𝑈)), 𝑦𝐿(0,𝑇;𝐻1(Ω)), and 𝑦𝑡𝐿2(0,𝑇;𝐻1(Ω)).

Proof. Let {(𝑢𝑛,𝑦𝑛)}𝑛=1 be a minimization sequence for the system (2.8), then the sequence {𝑢𝑛}𝑛=1 is bounded in 𝐿2(0,𝑇;𝐿2(Ω𝑈)). Thus there is a subsequence of {𝑢𝑛}𝑛=1 (still denote by {𝑢𝑛}𝑛=1 ) such that 𝑢𝑛 converges to 𝑢 weakly in 𝐿2(0,𝑇;𝐿2(Ω𝑈)). For the subsequence {𝑢𝑛}𝑛=1, we have 𝑦𝑛𝑡𝑦,𝑤+𝑎𝑛𝑡,𝑤+𝑑(𝑦𝑛,𝑤)+𝑡0𝑐(𝑡,𝜏;𝑦𝑛(𝜏),𝑤(𝑡))𝑑𝜏=(𝑓+𝐵𝑢𝑛].,𝑤)𝑤𝑉,𝑡(0,𝑇(2.9) By setting 𝑤=𝑦𝑛 and integrating from 0 to 𝑡 in (2.9), we give 𝑦𝑛(𝑡)21,Ω+𝑡0𝑦𝑛21,Ω𝑦𝑑𝜏𝐶01,Ω+𝐶𝑡0𝑓21,Ω+𝑢𝑛20,Ω𝑈𝑑𝑡+𝑡0𝜏0𝑦(𝑠)21,Ω.𝑑𝑠𝑑𝜏(2.10) Applying Gronwall's inequality to (2.10) yields 𝑦𝑛2𝐿0,𝑇;𝐻1(Ω)+𝑦𝑛2𝐿20,𝑇;𝐻1(Ω)𝑦𝐶021,Ω+𝑇0𝑓21,Ω+𝑢𝑛20,Ω𝑈.(2.11) So {𝑢𝑛}𝑛=1 is a bounded set in 𝐿2(0,𝑇;𝐿2(Ω𝑈)) and {𝑦𝑛}𝑛=1 is a bounded set in 𝐿(0,𝑇;𝐻1(Ω)). Thus 𝑢𝑛𝑢weaklyin𝐿20,𝑇;𝐿2Ω𝑈,𝑦𝑛𝑦weaklyin𝐿0,𝑇;𝐻1,𝑦(Ω)𝑛(𝑇)𝑦(𝑇)weaklyin𝐻1(Ω).(2.12) Let 𝑊={𝑤;𝑤𝐿(0,𝑇;𝐻1(Ω)),𝑤𝑡𝐿2(0,𝑇;𝐻1(Ω))}.
By integrating time from 0 to 𝑇 in (2.9) and taking limit as 𝑛, we obtain (𝑦(𝑇),𝑤(𝑇))+𝑎(𝑦(𝑇),𝑤(𝑇))𝑇0𝑦,𝑤𝑡+𝑎𝑦,𝑤𝑡++𝑑(𝑦,𝑤)𝑇0𝑡0=𝑦𝑐(𝑡,𝜏;𝑦(𝜏),𝑤(𝑡))𝑑𝜏𝑑𝑡0𝑦,𝑤(0)+𝑎0+,𝑤(0)𝑇0(𝑓+𝐵𝑢,𝑤),𝑤𝑊.(2.13) Then, 𝑦𝑡𝑦,𝑤+𝑎𝑡,𝑤+𝑑(𝑦,𝑤)+𝑡0].𝑐(𝑡,𝜏;𝑦(𝜏),𝑤)𝑑𝜏=(𝑓+𝐵𝑢,𝑤),𝑤𝑉,𝑡(0,𝑇(2.14) Furthermore, we have 𝑇0𝑦𝑡,𝑦𝑡𝑦+𝑎𝑡,𝑦𝑡+𝑑𝑦,𝑦𝑡+𝑡0𝑐𝑡,𝜏;𝑦(𝜏),𝑦𝑡(𝑡)𝑑𝜏𝑑𝑡=𝑇0𝑓+𝐵𝑢,𝑦𝑡.(2.15) Then, we get 𝑇0𝑦𝑡21,Ω𝐶𝑇0𝑓21,Ω+𝑢20,Ω𝑈+𝑦21,Ω+𝑡0𝑦21,Ω.𝑑𝜏(2.16) This means 𝑦𝑡𝐿2(0,𝑇;𝐻1(Ω)). So (𝑢,𝑦) is one solution of (2.8).
Since 𝑇0𝑦𝑧𝑑20,Ω is a convex function on space 𝐿2(0,𝑇;𝐿2(Ω)) and (𝛼/2)𝑇0𝑢20,Ω𝑈 is a strictly convex function on 𝑈, hence 𝐽(𝑢,𝑦(𝑢)) is a strictly convex function on 𝑈, so the minimization problem (2.8) has one unique solution.

2.2. Optimality Conditions and Their Finite Element Approximation

By the theory of optimal control problem (see [18]), we can similarly deduce the following optimality conditions of the problem (2.8).

Theorem 2.2. A pair (𝑦,𝑢)𝐿2(0,𝑇;𝐻10(Ω))×𝐿2(0,𝑇;𝐿2(Ω𝑈)) is the solution of the optimal control problem (2.8), if and only if there exists a costate 𝑝𝐿2(0,𝑇;𝐻10(Ω)) such that the triple (𝑦,𝑝,𝑢) satisfies the following optimality conditions: 𝑦𝑡𝑦,𝑤+𝑎𝑡,𝑤+𝑑(𝑦,𝑤)+𝑡0],𝑐(𝑡,𝜏;𝑦(𝜏),𝑤(𝑡))𝑑𝜏=(𝑓+𝐵𝑢,𝑤)𝑤𝑉,𝑡(0,𝑇𝑦|𝑡=0=𝑦0;(2.17)𝑞,𝑝𝑡𝑎𝑞,𝑝𝑡+𝑑(𝑞,𝑝)+𝑇𝑡𝑐(𝜏,𝑡;𝑞(𝑡),𝑝(𝜏))𝑑𝜏=𝑦𝑧𝑑[,𝑞𝑞𝑉,𝑡0,𝑇),𝑝|𝑡=𝑇=0;(2.18)𝑇0𝑢+𝐵𝑝,𝑣𝑢𝑈𝑑𝑡0,𝑣𝑈𝑎𝑑,(2.19) where 𝐵 is the adjoint operator of 𝐵.

Let us consider the semi-discrete finite element approximation of the control problem (2.8). Here, we only consider triangular and conforming elements.

Let Ω be a polygonal approximation to Ω with boundary  𝜕Ω. Let 𝑇 be a partitioning of Ω into disjoint regular 𝑛-simplices 𝜏, so that Ω=𝜏𝑇𝜏. Each element has at most one face on 𝜕Ω, and 𝜏 and 𝜏 have either only one common vertex or a whole edge or face if 𝜏 and 𝜏𝑇. We further require that 𝑃𝑖𝜕Ω𝑃𝑖𝜕Ω  where 𝑃𝑖(𝑖=1,,𝐽) is the vertex set associated with the triangulation 𝑇. As usual, denotes the diameter of the triangulation 𝑇. For simplicity, we assume that Ω is a convex polygon so that Ω=Ω.

Associated with 𝑇 is a finite-dimensional subspace 𝑆 of 𝐶(Ω), such that 𝜒|𝜏 are polynomials of order 𝑚(𝑚1) for all 𝜒𝑆 and 𝜏𝑇. Let 𝑉={𝑣𝑆𝑣(𝑃𝑖)=0(𝑖=1,,𝐽)},𝑊=𝐿2(0,𝑇;𝑉). Note that we do not impose a continuity requirement. It is easy to see that 𝑉𝑉,𝑊𝑊.

Let 𝑇𝑈 be a partitioning of Ω𝑈 into disjoint regular 𝑛-simplices 𝜏𝑈, so that Ω𝑈=𝜏𝑈𝑇𝑈𝜏𝑈. 𝜏𝑈 and 𝜏𝑈 have either only one common vertex or a whole edge or face if 𝜏𝑈 and 𝜏𝑈𝑇𝑈. We further require that 𝑃𝑖𝜕Ω𝑈𝑃𝑖𝜕Ω𝑈, where 𝑃𝑖(𝑖=1,,𝐽) is the vertex set associated with the triangulation 𝑇𝑈. For simplicity, we again assume that Ω𝑈 is a convex polygon so that Ω𝑈=Ω𝑈.

Associated with 𝑇𝑈 is another finite-dimensional subspace 𝑈 of 𝐿2(Ω𝑈), such that 𝜒|𝜏𝑈 are polynomials of order 𝑚(𝑚0) for all 𝜒𝑈 and 𝜏𝑈𝑇𝑈. Here there is no requirement for the continuity. Let 𝑋=𝐿2(0,𝑇;𝑈). It is easy to see that 𝑋𝑋. Let 𝜏(𝜏𝑈) denote the maximum diameter of the element 𝜏(𝜏𝑈) in 𝑇(𝑇𝑈).

Due to the limited regularity of the optimal control 𝑢 in general, there will be no advantage in considering higher-order finite element spaces than the piecewise constant space for the control. We therefore only consider the piecewise constant finite element space for the approximation of the control, though higher-order finite element spaces will be used to approximate the state and the co-state. Let 𝑃0(Ω) denote all the 0-order polynomial over Ω. Therefore, we always take 𝑋={𝑢𝑋𝑢(𝑥,𝑡)|𝑥𝜏𝑈𝑃0(𝜏𝑈),forall𝑡[0,𝑇]}. 𝑈𝑎𝑑 is a closed convex set in 𝑋. For ease of exposition, in this paper, we assume that 𝑈𝑎𝑑𝑈𝑎𝑑𝑋.

Then a possible semi-discrete finite element approximation of (OCP) is as follows (OCP)min𝑢𝑈𝑎𝑑𝐽𝑢,𝑦=12𝑇0𝑦𝑧𝑑20,Ω+𝑇0𝑢20,Ω𝑈,(2.20) such that 𝜕𝑦𝜕𝑡,𝑤+𝑎𝜕𝑦𝜕𝑡,𝑤𝑦+𝑑,𝑤+𝑡0𝑐𝑡,𝜏;𝑦(𝜏),𝑤(𝑡)𝑑𝜏=𝑓+𝐵𝑢,𝑤,𝑤𝑉],𝑦,𝑡(0,𝑇||𝑡=0=𝑦0,(2.21) where 𝑦𝑊 and 𝑦0𝑉 is the approximation of 𝑦0.

In the same way of proving Theorem 2.1, we can easily prove that the problem (2.20)-(2.21) has a unique solution (𝑦,𝑢)𝑊×𝑈𝑎𝑑.

It is well known (see [18]) that a pair (𝑦,𝑢)𝑊×𝑈𝑎𝑑 is a solution of (2.20)-(2.21), if and only if there exists a co-state 𝑝𝑊 such that the triple (𝑦,𝑝,𝑢) satisfies the following optimality conditions: 𝜕𝑦𝜕𝑡,𝑤+𝑎𝜕𝑦𝜕𝑡,𝑤𝑦+𝑑,𝑤+𝑡0𝑐𝑡,𝜏;𝑦(𝜏),𝑤(𝑡)𝑑𝜏=𝑓+𝐵𝑢,𝑤,𝑤𝑉,𝑦|𝑡=0=𝑦0,𝑞(2.22),𝜕𝑝𝑞𝜕𝑡𝑎,𝜕𝑝𝑞𝜕𝑡+𝑑,𝑝+𝑇𝑡𝑐𝜏,𝑡;𝑞,𝑝𝑦(𝜏)𝑑𝜏=𝑧𝑑,𝑞,𝑞𝑉,𝑝|𝑡=𝑇=0,(2.23)𝑇0𝑢+𝐵𝑝,𝑣𝑢𝑈𝑑𝑡0,𝑣𝑈𝑎𝑑.(2.24)

The optimality conditions in (2.22)–(2.24) are the semi-discrete approximation to the problem (2.17)–(2.19).

Introduce the local averaging operator 𝜋 given by 𝜋𝑤|𝜏𝑈=𝜏𝑈𝑤𝜏𝑈1,𝜏𝑈𝑇𝑈.(2.25) Then, we have Ω𝑈𝑤=Ω𝑈𝜋𝑤 for any 𝑤𝐿2(0,𝑇;𝐿2(Ω𝑈)),𝑡[0,𝑇] and (2.24) is equivalent to 𝑇0𝑢+𝜋𝐵𝑝,𝑣𝑢𝑈𝑑𝑡0,𝑣𝑈𝑎𝑑.(2.26) In the following, we derive the a posteriori error estimates for semi-discrete finite element approximation (2.22)–(2.24), allowing different meshes to be used for the state and the control.

The following lemmas are important in deriving the a posteriori error estimates of residual type.

Lemma 2.3 (see [19]). Let 𝜋 be the standard Lagrange interpolation operator. For 𝑚=0 or 1, 𝑞>𝑛/2 and 𝑣𝑊2,𝑞(Ω) as ||𝑣𝜋𝑣||𝑚,𝑞,Ω𝐶2𝑚|𝑣|2,𝑞,Ω.(2.27)

Lemma 2.4 (see [20]). Let 𝜋 be the average interpolation operator defined in (2.25). For 𝑚=0 or 1, 1𝑞 and forall𝑣𝑊1,𝑞(Ω) as ||𝑣𝜋𝑣||𝑚,𝑞,𝜏𝜏𝜏𝐶𝜏1𝑚|𝑣|1,𝑞,𝜏.(2.28)

Lemma 2.5 (see [21]). For all 𝑣𝑊1,𝑞(Ω),1𝑞< as 𝑣0,𝑞,𝜕𝜏𝐶𝜏1/𝑞𝑣0,𝑞,𝜏+𝜏11/𝑞|𝑣|1,𝑞,𝜏.(2.29)

3. A Posteriori Error Estimates in 𝐿(0,𝑇;𝐻1(Ω))-Norm

In this paper, the control constraints are given in an integral sense as follows: 𝑈𝑎𝑑=𝑣𝑋;Ω𝑈[].𝑣0,𝑡0,𝑇(3.1) The following lemma is the first step to derive the a posteriori error estimates of residual type.

Lemma 3.1. Let (𝑦,𝑝,𝑢) and (𝑦,𝑝,𝑢) be the solutions of (2.17)–(2.19) and (2.22)–(2.24). Then, we have 𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈𝐶𝜂21𝑝+𝐶𝑢𝑝2𝐿20,𝑇;𝐿2(Ω),(3.2) where 𝜂21=𝑇0𝜏𝑈𝜏𝑈𝐵𝑝𝑃𝐵𝑝2𝑑𝑡,(3.3)𝑃 is the 𝐿2-projection from 𝐿2(Ω) to 𝑈, and 𝑝(𝑢) is defined by the following system: 𝜕𝑦𝑢𝜕𝑡𝜕,𝜔+𝑎𝑦𝑢𝜕𝑡𝑦𝑢,𝜔+𝑑+,𝜔𝑡0𝑐𝑢𝑡,𝜏;𝑦(=𝜏),𝜔(𝑡)𝑑𝜏𝑓+𝐵𝑢𝑦𝑢,𝜔,𝜔𝑉,(0)=𝑦0(𝜕𝑥),𝑥Ω,(3.4)𝑞,𝑝𝑢𝜕𝑡𝜕𝑎𝑞,𝑝𝑢𝜕𝑡𝑢+𝑑𝑞,𝑝+𝑇𝑡𝑐𝑢𝜏,𝑡;𝑞(𝑡),𝑝=𝑦𝑢(𝜏)𝑑𝜏𝑧𝑑,𝑞,𝑞𝑉.(3.5)

Proof. From (2.19), we have 𝑢,𝑢𝑢𝑈𝐵𝑝,𝑢𝑢𝑈.(3.6) Then, by (2.24) and (3.6), we have 𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈=𝑇0𝑢,𝑢𝑢𝑈𝑢,𝑢𝑢𝑈𝑑𝑡=𝑇0𝐵𝑝+𝑢,𝑢𝑢𝑈𝑑𝑡=𝑇0𝐵𝑝+𝑢,𝑢𝑣𝑈𝑑𝑡𝑇0𝐵𝑝+𝑢,𝑣𝑢𝑈+𝑑𝑡𝑇0𝐵𝑝𝐵𝑝𝑢,𝑢𝑢𝑈𝑑𝑡+𝑇0𝐵𝑝𝑢𝐵𝑝,𝑢𝑢𝑈𝑑𝑡inf𝑣𝑈𝑎𝑑𝑇0𝐵𝑝+𝑢,𝑣𝑢𝑈+𝑑𝑡𝑇0𝐵𝑝𝑢𝑝,𝑢𝑢𝑈𝑑𝑡+𝑇0𝐵𝑝𝑢𝑝,𝑢𝑢𝑈𝑑𝑡=𝐼1+𝐼2+𝐼3.(3.7) Next, we will estimate 𝐼1,𝐼2,and𝐼3, respectively.
(1) We first estimate 𝐼1. Let 𝑃 be the 𝐿2-projection from 𝐿2(Ω) to 𝑈.
We have Ω𝑈𝑃𝑣𝑣𝜙=0,𝜙𝑋,𝑣𝑈𝑎𝑑].,𝑡(0,𝑇(3.8) Since 𝑣𝑈𝑎𝑑, so Ω𝑈𝑃𝑣0, then 𝑃𝑣𝑈𝑎𝑑. So that we can take 𝑣=𝑃𝑢 in 𝐼1.
For given 𝑡(0,𝑇], let 𝑢=𝑃𝐵𝑝+max0,Ω𝑈𝐵𝑝Ω𝑈1.(3.9) We have 𝑢𝑋. We will show that 𝑢 is the solution of the variational inequality in (2.24) assuming 𝑝 is known.
Since Ω𝑈[𝑃(𝐵𝑝+max{0,Ω𝑈𝐵𝑝/Ω𝑈1})(𝐵𝑝+max{0,Ω𝑈𝐵𝑝/Ω𝑈1})]=0, we have Ω𝑈𝑢=Ω𝑈𝐵𝑝+Ω𝑈max0,Ω𝑈𝐵𝑝Ω𝑈1=Ω𝑈𝐵𝑝,Ω𝑈𝐵𝑝<0,0,Ω𝑈𝐵𝑝0.(3.10) Thus, Ω𝑈𝑢0, we have 𝑢𝑈𝑎𝑑. Note that for all 𝑣𝑈𝑎𝑑,𝑡(0,𝑇], we have 𝑢+𝐵𝑝,𝑣𝑢𝑈=Ω𝑈𝑃𝐵𝑝+max0,Ω𝑈𝐵𝑝Ω𝑈1𝐵𝑝+max0,Ω𝑈𝐵𝑝Ω𝑈1+max0,Ω𝑈𝐵𝑝Ω𝑈1𝑣𝑢=Ω𝑈max0,Ω𝑈𝐵𝑝Ω𝑈1𝑣𝑢.(3.11) If Ω𝑈𝐵𝑝<0, then 𝑢+𝐵𝑝,𝑣𝑢𝑈=Ω𝑈𝑣0𝑢=0.(3.12) If Ω𝑈𝐵𝑝0, since Ω𝑈𝑢=Ω𝑈𝐵𝑝+max0,Ω𝑈𝐵𝑝Ω𝑈1=0.(3.13) we have 𝑢+𝐵𝑝,𝑣𝑢𝑈=Ω𝑈𝐵𝑝Ω𝑈1Ω𝑈𝑣𝑢=Ω𝑈𝐵𝑝Ω𝑈1Ω𝑈𝑣0.(3.14) From (3.11)–(3.14), we obtain 𝑢+𝐵𝑝,𝑣𝑢𝑈0,𝑣𝑈𝑎𝑑.(3.15) So 𝑢=𝑃(𝐵𝑝+max{0,Ω𝑈𝐵𝑝/Ω𝑈1}) is the solution of the variational inequality in (2.24) assuming 𝑝 is known.
Then, 𝐼1𝑇0𝐵𝑝+𝑢,𝑃𝑢𝑢𝑈=𝑑𝑡𝑇0𝜏𝑈𝜏𝑈𝑃𝐵𝑝+max0,Ω𝑈𝐵𝑝Ω𝑈1+𝐵𝑝𝑃𝑢𝑢𝑑𝑡.(3.16) Since 𝜏𝑈(𝑃𝑢𝑢)=0, we have 𝐼1𝑇0𝜏𝑈𝜏𝑈𝑃𝐵𝑝+𝐵𝑝𝑃=𝑢𝑢𝑑𝑡𝑇0𝜏𝑈𝜏𝑈𝑃𝐵𝑝+𝐵𝑝𝑃𝑢𝑢𝑢𝑢𝑑𝑡𝐶(𝛿)𝑇0𝜏𝑈𝜏𝑈𝑃𝐵𝑝+𝐵𝑝2𝑑𝑡+𝛿𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈=𝐶𝜂21+𝛿𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈.(3.17)(2) Consider 𝐼2=𝑇0𝐵𝑝𝑢𝑝,𝑢𝑢𝑈𝑝𝑑𝑡𝐶𝑢𝑝2𝐿20,𝑇;𝐿2(Ω)+𝛿𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈.(3.18)(3) By (3.4) and (2.17), we have for 𝑡(0,𝑇]𝜕𝑢𝜕𝑡𝑦𝑦𝜕,𝜔+𝑎𝑢𝜕𝑡𝑦𝑦𝑢,𝜔+𝑑𝑦𝑦+,𝑤𝑡0𝑐𝑢𝑡,𝜏;𝑦𝑦(𝐵𝜏),𝜔(𝑡)𝑑𝜏=𝑢𝑢,𝜔,𝜔𝑉,(3.19) and from (3.5) and (2.18), we have 𝜕𝑞,𝑢𝜕𝑡𝑝𝑝𝜕𝑎𝑞,𝑢𝜕𝑡𝑝𝑝𝑢+𝑑𝑞,𝑝𝑝+𝑇𝑡𝑐𝑢𝜏,𝑡;𝑞(𝑡),𝑝𝑝𝑢(𝜏)𝑑𝜏=𝑦𝑦,𝑞,𝑞𝑉.(3.20) Then, from (3.19), (3.20), and integrating by part we have 𝐼3=𝑇0𝐵𝑝𝑢𝑝,𝑢𝑢𝑈𝑑𝑡=𝑇0𝑝𝑢𝑝,𝐵𝑢𝑢𝑈=𝑑𝑡𝑇0𝜕𝑢𝜕𝑡𝑦𝑦𝑢,𝑝𝜕𝑝+𝑎𝑢𝜕𝑡𝑦𝑦𝑢,𝑝𝑢𝑝+𝑑𝑦𝑦𝑢,𝑝+𝑝𝑡0𝑐𝑢𝑡,𝜏;𝑦𝑦𝑝𝑢(𝜏),=𝑝(𝑡)𝑑𝜏𝑑𝑡𝑇0𝑢𝑦𝑦,𝜕𝑝𝑢𝜕𝑡𝑢𝑝𝑎𝑦𝑦,𝜕𝑝𝑢𝜕𝑡𝑢𝑝+𝑑𝑦𝑦𝑢,𝑝+𝑝𝑇𝑡𝑐𝑢𝜏,𝑡;𝑦𝑦(𝑝𝑢𝑡),(=𝑝𝜏)𝑑𝜏𝑑𝑡𝑇0𝑢𝑦𝑦𝑢,𝑦𝑦𝑑𝑡0.(3.21) Following from (3.17)–(3.21), let 𝛿 be small enough as 𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈𝐶𝜂21𝑝+𝐶𝑢𝑝2𝐿20,𝑇;𝐿2(Ω).(3.22) This completes the proof.

Lemma 3.2. Let (𝑦,𝑝,𝑢) and (𝑦,𝑝,𝑢) be the solutions of (2.17)–(2.19), and (2.22)–(2.24) respectively. Then, there hold the a posteriori error estimates as 𝑦𝑢𝑦2𝐿0,𝑇;𝐻1(Ω)+𝜕𝑦𝜕𝑡𝑢𝑦2𝐿20,𝑇;𝐻1(Ω)+𝑝𝑢𝑝2𝐿0,𝑇;𝐻1(Ω)+𝜕𝑝𝜕𝑡𝑢𝑝2𝐿20,𝑇;𝐻1(Ω)𝐶6𝑖=2𝜂2𝑖,(3.23) where 𝜂22=𝑇0𝜏2𝜏𝜏𝜕𝑝𝐴𝜕𝑡div𝜕𝑝𝐷𝜕𝑡+div𝑝+𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏+𝑦𝑧𝑑2𝜂𝑑𝜏𝑑𝑡,23=𝑇0𝜏𝑙𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝(𝜏)𝑛𝑑𝜏2𝜂𝑑𝑙𝑑𝑡,24=𝑇0𝜏2𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝑡,𝜏)𝑦(𝜏)𝑑𝜏𝑓𝐵𝑢2𝜂𝑑𝑡,25=𝑇0𝜏𝑙𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐴𝑦𝑛+𝑡0𝐶(𝑡,𝜏)𝑦(𝜏)𝑛𝑑𝜏2𝜂𝑑𝑙𝑑𝑡,26=𝑦0𝑦021,Ω,(3.24) where 𝑙 is a face of an element 𝜏, 𝑙 is the maximum diameter of 𝑙,  and  [𝑝𝑛] and [𝑦𝑛] are the normal derivative jumps over the interior face 𝑙 defined by 𝑝𝑛𝑙=𝑝|𝜏1𝑙𝑝|𝜏2𝑙𝑛,𝑦𝑛𝑙=𝑦|𝜏1𝑙𝑦|𝜏2𝑙𝑛,(3.25) where 𝑛 is the unit normal vector on 𝑙=𝜏1𝑙𝜏2𝑙 outwards 𝜏1𝑙. For later convenience, one can define [𝑝𝑛]𝑙=0 and [𝑦𝑛]𝑙=0 when 𝑙𝜕Ω.

Proof. Let 𝑅𝑢𝜕,𝑣=𝑣,𝑝𝜕𝑡𝑢𝑝𝜕𝑎𝑣,𝑝𝜕𝑡𝑢𝑝+𝑑𝑣,𝑝𝑢𝑝+𝑇𝑡𝑐𝑝𝜏,𝑡;𝑣(𝑡),𝑢𝑝(𝜏)𝑑𝜏,(3.26) and 𝜋 the average interpolation operator defined as in (2.25) and 𝑒=𝑝𝑝(𝑢). Then, it follows from (2.23) and (3.5) that 𝑞,𝜕𝑝𝜕𝑡𝑢𝑝𝑞𝑎,𝜕𝑝𝜕𝑡𝑢𝑝𝑞+𝑑,𝑝𝑢𝑝+𝑇𝑡𝑐𝜏,𝑡;𝑞𝑝(𝑡),𝑢𝑝𝑦(𝜏)𝑑𝜏=𝑢𝑦,𝑞,𝑞𝑉.(3.27) We have 𝑅𝑢,𝑣=𝑣𝜋𝜕𝑣,𝑝𝜕𝑡𝑢𝑝𝑎𝑣𝜋𝜕𝑣,𝑝𝜕𝑡𝑢𝑝+𝑑𝑣𝜋𝑣,𝑝𝑢𝑝+𝑇𝑡𝑐𝜏,𝑡;𝑣𝜋𝑣𝑝(𝑡),𝑢𝑝𝜋(𝜏)𝑑𝜏𝜕𝑣,𝑝𝜕𝑡𝑢𝑝𝜋𝑎𝜕𝑣,𝑝𝜕𝑡𝑢𝑝𝜋+𝑑𝑣,𝑝𝑢𝑝+𝑇𝑡𝑐𝜏,𝑡;𝜋𝑝𝑣(𝑡),𝑢𝑝(𝜏)𝑑𝜏=𝑣𝜋𝑣,𝜕𝑝𝜕𝑡𝑎𝑣𝜋𝑣,𝜕𝑝𝜕𝑡+𝑑𝑣𝜋𝑣,𝑝+𝑇𝑡𝑐𝜏,𝑡;𝑣𝜋𝑣(𝑡),𝑝𝑦𝑢(𝜏)𝑑𝜏𝑧𝑑,𝑣𝜋𝑣+𝑦𝑢𝑦,𝜋𝑣=𝜏𝜏𝜕𝑝𝐴𝜕𝑡+div𝜕𝑝𝐷𝜕𝑡div𝑝𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏𝑦+𝑧𝑑×𝑣𝜋𝑣+𝜏𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝×(𝜏)𝑛𝑑𝜏𝑣𝜋𝑣+𝑦𝑢𝑦,𝑣𝜏𝜏2𝜏𝜕𝑝𝐴𝜕𝑡+div𝜕𝑝𝐷𝜕𝑡div𝑝𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏𝑦+𝑧𝑑2+𝜏𝜕𝜏𝑙𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝(𝜏)𝑛𝑑𝜏21/2×𝑣1,Ω+𝑦𝑢𝑦.,𝑣(3.28) Taking 𝑣=𝑝𝑝(𝑢) in (3.28) and from (2.6), we have 12𝑑𝑝𝑑𝑡𝑝(𝑢)20,Ω12𝑑𝑎𝑝𝑑𝑡𝑢𝑝,𝑝𝑢𝑝𝑝+𝑐𝑢𝑝21,Ω𝜏𝜏2𝜏𝜕𝑝𝐴𝜕𝑡+div𝜕𝑝𝐷𝜕𝑡div𝑝𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏𝑦+𝑧𝑑2+𝜏𝜕𝜏𝑙𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛21/2×𝑝𝑢𝑝1,Ω+𝑦𝑢𝑦,𝑝𝑢𝑝𝑇𝑡𝑐𝑝𝜏,𝑡;𝑢𝑝𝑝(𝑡),𝑢𝑝(𝜏)𝑑𝜏.(3.29) Integrating time from 𝑡 to 𝑇 in (3.29) and by Schwartz inequality, Lemmas 2.4 and 2.5, we have 12𝑝𝑢𝑝20,Ω𝑝+𝑐𝑢𝑝21,Ω+𝑐𝑇𝑡𝑝𝑢𝑝21,Ω𝑑𝜏𝑇𝑡𝜏2𝜏×𝜏𝜕𝑝𝐴𝜕𝑡div𝜕𝑝𝐷𝜕𝑡+div𝑝+𝑇𝜏𝐶div(𝑠,𝜏)𝑝(𝑠)𝑑𝑠+𝑦𝑧𝑑2+𝑑𝜏𝑇𝑡𝜏𝑙𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝜏𝐶(𝑠,𝜏)𝑝(𝑠)𝑛𝑑𝑠2𝑑𝜏+𝛿𝑇𝑡𝑝𝑢𝑝21,Ω𝑑𝜏+𝐶𝑇𝑡𝑦𝑢𝑦20,Ω𝑑𝜏+𝐶𝑇𝑡𝑇𝜏𝑝𝑢𝑝(𝑠)21,Ω𝑑𝑠𝑑𝜏.(3.30) Letting 𝛿 be small enough, we have 𝑇𝑡𝑝𝑝(𝑢)21,Ω𝑑𝜏𝐶𝑇𝑡𝜏2𝜏𝜏𝜕𝑝𝐴𝜕𝑡div𝜕𝑝𝐷𝜕𝑡+div𝑝+𝑇𝜏𝐶div(𝑠,𝜏)𝑝(𝑠)𝑑𝑠+𝑦𝑧𝑑2𝑑𝜏+𝐶𝑇𝑡𝜏𝑙𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝+𝑛𝑇𝜏𝐶(𝑠,𝜏)𝑝(𝑠)𝑛𝑑𝑠2𝑑𝜏+𝐶𝑇𝑡𝑦𝑦(𝑢)20,Ω𝑑𝜏+𝐶𝑇𝑡𝑇𝜏𝑝𝑢𝑝(𝑠)21,Ω𝑑𝑠𝑑𝜏.(3.31) Then, from Gronwall inequality and (3.28)–(3.31) we have 𝑝𝑝(𝑢)2𝐿20,𝑇;𝐻1(Ω)𝐶𝜂22+𝐶𝜂23𝑦+𝐶𝑢𝑦2𝐿20,𝑇;𝐿2(Ω).(3.32) Similarly, 𝑝𝑢𝑝2𝐿(0,𝑇;𝐻1(Ω))𝜂𝐶22+𝜂23+𝑦𝑢𝑦2𝐿20,𝑇;𝐿2(Ω)+𝐶𝑇0𝑇𝑡𝑝𝑢𝑝(𝜏)21,Ω𝑑𝜏𝑑𝑡𝐶𝜂22+𝐶𝜂23𝑦+𝐶𝑢𝑦2𝐿20,𝑇;𝐿2(Ω).(3.33) In the same way of getting (3.32),by setting 𝑣=(𝜕/𝜕𝑡)(𝑝𝑝(𝑢)) in (3.28), we have 𝜕𝑝𝜕𝑡𝑢𝑝2𝐿20,𝑇;𝐻1(Ω)𝐶𝜂22+𝐶𝜂23𝑦+𝐶𝑢𝑦2𝐿20,𝑇;𝐿2(Ω).(3.34) Similarly analysis for 𝑦𝑦(𝑢)𝐿(0,𝑇;𝐻1(Ω)), we let 𝑄𝑢=𝜕,𝑣𝜕𝑡𝑦𝑢𝑦𝜕,𝑣+𝑎𝜕𝑡𝑦𝑢𝑦𝑦,𝑣+𝑑𝑢𝑦+,𝑣𝑡0𝑐𝑦𝑡,𝜏;𝑢𝑦(𝜏),𝑣(𝑡)𝑑𝜏.(3.35) From (2.22) and (3.4), we obtain 𝜔,𝜕𝑦𝜕𝑡𝑢𝑦𝜕+𝑎𝑦𝜕𝑡𝑢𝑦,𝜔𝑦+𝑑𝑢𝑦,𝜔+𝑡0𝑐𝑦𝑡,𝜏;𝑢𝑦(𝜏),𝜔(𝑡)𝑑𝜏=0,𝜔𝑉.(3.36) We have 𝑄𝑢=𝜕,𝑣𝑦𝜕𝑡𝑢𝑦,𝑣𝜋𝑣𝜕+𝑎𝑦𝜕𝑡𝑢𝑦,𝑣𝜋𝑣𝑦+𝑑𝑢𝑦,𝑣𝜋𝑣+𝑡0𝑐𝑦𝑡,𝜏;𝑢𝑦(𝜏),𝑣𝜋𝑣=(𝑡)𝑑𝜏𝜕𝑦𝜕𝑡,𝑣𝜋𝑣+𝑎𝜕𝑦𝜕𝑡,𝑣𝜋𝑣𝑦+𝑑,𝑣𝜋𝑣+𝑡0𝑐𝑡,𝜏;𝑦(𝜏),𝑣𝜋𝑣(𝑡)𝑑𝜏𝑓+𝐵𝑢,𝑣𝜋𝑣=𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝑡,𝜏)𝑦𝑑𝜏𝑓𝐵𝑢𝑣𝜋𝑣+𝜏𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝑡0𝐶(𝑡,𝜏)𝑦𝑛𝑑𝜏𝑣𝜋𝑣𝜏𝜏2𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝑡,𝜏)𝑦𝑑𝜏𝑓𝐵𝑢2+𝜏𝜕𝜏𝑙𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝑡0𝐶(𝑡,𝜏)𝑦𝑛𝑑𝜏21/2𝑣1,Ω.(3.37) By setting 𝑣=𝑦𝑦(𝑢) and Swartz inequality, we have 12𝑑𝑦𝑑𝑡𝑢𝑦20,Ω+12𝑑𝑎𝑦𝑑𝑡𝑢𝑦,𝑦𝑢𝑦𝑦+𝑐𝑦(𝑢)21,Ω𝜏𝜏2𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝑡,𝜏)𝑦𝑑𝜏𝑓𝐵𝑢2+𝜏𝜕𝜏𝑙𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝑡0𝐶(𝑡,𝜏)𝑦𝑛𝑑𝜏2𝑦+𝛿𝑢𝑦21,Ω𝑡0𝑐𝑦𝑡,𝜏;𝑢𝑦𝑦(𝜏),𝑢𝑦(𝑡)𝑑𝜏.(3.38) Integrating time from 0 to 𝑡 in (3.38), we obtain 𝑦𝑢𝑦21,Ω+𝑐𝑡0𝑦𝑢𝑦21,Ω𝑑𝜏𝐶𝑡0𝜏2𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝜏0div𝐶(𝜏,𝑠)𝑦𝑑𝑠𝑓𝐵𝑢2+𝑑𝜏𝑡0𝜏𝑙𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝜏0𝐶(𝜏,𝑠)𝑦𝑛𝑑𝑠2𝑑𝑡+𝛿𝑡0𝑦𝑢𝑦21,Ω𝑑𝜏+𝐶𝑡0𝜏0𝑦𝑢𝑦21,Ω𝑦𝑑𝑠𝑑𝜏+𝐶0𝑦021,Ω.(3.39) Since 𝛿 is small enough, then from (3.39) and Gronwall inequality, we have 𝑡0𝑦𝑢𝑦21,Ω𝑑𝑡𝐶𝑡0𝜏2𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝜏0div𝐶(𝜏,𝑠)𝑦𝑑𝑠𝑓𝐵𝑢2𝑑𝜏+𝐶𝑡0𝜏𝑙𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝜏0𝐶(𝜏,𝑠)𝑦𝑛𝑑𝑠2𝑦𝑑𝑡+𝐶0𝑦021,Ω.(3.40) Then, 𝑦𝑢𝑦2𝐿20,𝑇;𝐻1(Ω)𝜂𝐶24+𝜂25+𝜂26,𝑦𝑢𝑦2𝐿0,𝑇;𝐻1(Ω)𝜂𝐶24+𝜂25+𝜂26.(3.41) In the same way of getting (3.34), we can similarly obtain 𝜕𝑦𝜕𝑡𝑢𝑦2𝐿20,𝑇;𝐻1(Ω)𝜂𝐶24+𝜂25+𝜂26.(3.42) Then the desired results (3.23) follow from (3.32)–(3.34) and (3.41)-(3.42).

From Lemmas 3.1 and 3.2, we have the following results.

Theorem 3.3. Let(𝑦,𝑝,𝑢) and (𝑦,𝑝,𝑢) be the solutions of(2.17)–(2.19) and (2.22)–(2.24) respectively. Then, there hold the a posteriori error estimates as 𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈+𝑦𝑦2𝐿0,𝑇;𝐻1(Ω)+𝜕𝜕𝑡𝑦𝑦2𝐿20,𝑇;𝐻1(Ω)+𝑝𝑝2𝐿0,𝑇;𝐻1(Ω)+𝜕𝜕𝑡𝑝𝑝2𝐿20,𝑇;𝐻1(Ω)𝐶6𝑖=1𝜂2𝑖,(3.43) where 𝜂21 is defined in Lemma 3.1.

Proof. First,  from (3.27) and (3.36), and [2], we have the following stability results: 𝑢𝑦𝑦2𝐿0,𝑇;𝐻1(Ω)+𝜕𝑢𝜕𝑡𝑦𝑦2𝐿20,𝑇;𝐻1(Ω)𝐶𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈,𝑢𝑝𝑝2𝐿0,𝑇;𝐻1(Ω)+𝜕𝑢𝜕𝑡𝑝𝑝2𝐿20,𝑇;𝐻1(Ω)𝑢𝐶𝑦𝑦2𝐿20,𝑇;𝐿2(Ω)𝐶𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈.(3.44) Then, the desired results (3.43) follows from triangle inequality, (3.44) and Lemmas 3.1 and 3.2.
This completes the proof.

4. A Posteriori Error Estimates in 𝐿2(0,𝑇;𝐿2(Ω))-Norm

In the following, we will derive the a posteriori error estimates in 𝐿2(0,𝑇;𝐿2(Ω))-norm.

We will introduce the following dual equations.

For given 𝐹𝐿2(0,𝑇;𝐿2(Ω)), we have 𝜕𝜙𝜕𝑡div𝐴𝜕𝜙𝜕𝑡div(𝐷𝜙)𝑡0],𝜙div(𝐶(𝑡,𝜏)𝜙(𝜏))𝑑𝜏=𝐹,(𝑥,𝑡)Ω×(0,𝑇],𝜕Ω=0,𝑡(0,𝑇𝜙(𝑥,0)=0,𝑥Ω,(4.1) and its dual equation 𝜕𝜓𝐴𝜕𝑡+div𝜕𝜓𝐷𝜕𝑡div𝜓𝑇𝑡𝐶div],𝜓(𝜏,𝑡)𝜓(𝜏)𝑑𝜏=𝐹,(𝑥,𝑡)Ω×(0,𝑇],𝜕Ω=0,𝑡(0,𝑇𝜓(𝑥,𝑇)=0,𝑥Ω.(4.2) From [1, 2], we have the following stability results.

Lemma 4.1. Assume that Ω is a convex domain. Let 𝜙 and 𝜓 be the solution of (4.1) and (4.2), respectively. Then, 𝜙𝐿(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝜙𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝐷2𝜙𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝜕𝜙𝜕𝑡𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝜓𝐿(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝜓𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝐷2𝜓𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),𝜕𝜓𝜕𝑡𝐿2(0,𝑇;𝐿2(Ω))𝐶𝐹𝐿2(0,𝑇;𝐿2(Ω)),(4.3) where 𝐷2𝜙=𝜕2𝜙/𝜕𝑥𝑖𝜕𝑥𝑗,1𝑖,𝑗𝑛, and 𝐷2𝜓 is defined similarly.

Using Lemmas 3.1 and 4.1, we have the following upperbounds.

Lemma 4.2. Let (𝑦,𝑝,𝑢) and (𝑦,𝑝,𝑢) be the solutions of (2.17)–(2.19) and (2.22)–(2.24), respectively. Then, there hold the a posteriori error estimates as 𝑦𝑢𝑦2𝐿20,𝑇;𝐿2(Ω)+𝑝𝑝(𝑢)2𝐿20,𝑇;𝐿2(Ω)𝐶5𝑖=2𝜉2𝑖+𝜂26,(4.4) where 𝜂26 is defined in Lemma 3.2, and 𝜉22=𝑇0𝜏4𝜏𝜏𝜕𝑝𝐴𝜕𝑡div𝜕𝑝𝐷𝜕𝑡+div𝑝+𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏+𝑦𝑧𝑑2𝜉𝑑𝑡,23=𝑇0𝜏3𝑙𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝(𝜏)𝑛𝑑𝜏2𝜉𝑑𝑙𝑑𝑡,24=𝑇0𝜏4𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝑡,𝜏)𝑦(𝜏)𝑑𝜏𝑓𝐵𝑢2𝜉𝑑𝑡,25=𝑇0𝜏3𝑙𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛+𝑡0𝐶(𝑡,𝜏)𝑦(𝜏)𝑛𝑑𝜏2𝑑𝑙𝑑𝑡.(4.5)

Proof. We first estimate 𝑝𝑝(𝑢)2𝐿2(0,𝑇;𝐿2(Ω)).
Let 𝜙 be the solution of (4.1) with 𝐹=𝑝𝑝(𝑢),  and  𝜙𝐼=𝜋𝜙 the interpolation of 𝜙 in Lemma 2.3.
From (4.1), (3.27), and by integrating by parts we obtain 𝑝𝑢𝑝2𝐿20,𝑇;𝐿2(Ω)=𝑇0𝐹𝑝(𝑡),𝑢𝑝=(𝑡)𝑑𝑡𝑇0𝜕𝑝𝜕𝑡𝑢𝑝𝜕,𝜙𝑎𝜙,𝑝𝜕𝑡𝑢𝑝+𝑑𝜙,𝑝𝑢𝑝+𝑡0𝑐𝑝𝑡,𝜏;𝜙(𝜏),𝑢𝑝=(𝑡)𝑑𝜏𝑑𝑡𝑇0𝜕𝑝𝜕𝑡𝑢𝑝,𝜙𝜙𝐼𝑎𝜙𝜙𝐼,𝜕𝑝𝜕𝑡𝑢𝑝+𝑑𝜙𝜙𝐼,𝑝𝑢𝑝+𝑡0𝑐𝑡,𝜏;𝜙𝜙𝐼𝑝(𝜏),𝑢𝑝𝜕(𝑡)𝑑𝜏𝑝𝜕𝑡𝑢𝑝,𝜙𝐼𝜙𝑎𝐼,𝜕𝑝𝜕𝑡𝑢𝑝𝜙+𝑑𝐼,𝑝𝑢𝑝+𝑡0𝑐𝑡,𝜏;𝜙𝐼(𝑝𝜏),𝑢𝑝(=𝑡)𝑑𝜏𝑑𝑡𝑇0𝜕𝑝𝜕𝑡,𝜙𝜙𝐼𝑎𝜙𝜙𝐼,𝜕𝑝𝜕𝑡+𝑑𝜙𝜙𝐼,𝑝+𝑡0𝑐𝑡,𝜏;𝜙𝜙𝐼(𝜏),𝑝𝑢(𝑡)𝑑𝜏+𝜕𝑝𝜕𝑡,𝜙𝜙𝐼+𝑎𝜙𝜙𝐼,𝑢𝜕𝑝𝜕𝑡𝑑𝜙𝜙𝐼𝑢,𝑝𝑡0𝑐𝑡,𝜏;𝜙𝜙𝐼𝑢(𝜏),𝑝𝜕(𝑡)𝑑𝜏𝑝𝜕𝑡𝑢𝑝,𝜙𝐼𝜙𝑎𝐼,𝜕𝑝𝜕𝑡𝑢𝑝𝜙+𝑑𝐼,𝑝𝑢𝑝+𝑡0𝑐𝑡,𝜏;𝜙𝐼𝑝(𝜏),𝑢𝑝=(𝑡)𝑑𝜏𝑑𝑡𝑇0𝜕𝑝𝜕𝑡,𝜙𝜙𝐼𝑎𝜙𝜙𝐼,𝜕𝑝𝜕𝑡+𝑑𝜙𝜙𝐼,𝑝+𝑇𝑡𝑐𝜏,𝑡;𝜙𝜙𝐼(𝑡),𝑝+𝑢(𝜏)𝑑𝜏𝜕𝑝𝜕𝑡,𝜙𝜙𝐼+𝑎𝜙𝜙𝐼,𝑢𝜕𝑝𝜕𝑡𝑑𝜙𝜙𝐼𝑢,𝑝𝑇𝑡𝑐𝜏,𝑡;𝜙𝜙𝐼𝑢(𝑡),𝑝𝜕(𝜏)𝑑𝜏𝑝𝜕𝑡𝑢𝑝,𝜙𝐼𝜙𝑎𝐼,𝜕𝑝𝜕𝑡𝑢𝑝𝜙+𝑑𝐼,𝑝𝑢𝑝+𝑇𝑡𝑐𝜏,𝑡;𝜙𝐼(𝑝𝑡),𝑢𝑝(=𝜏)𝑑𝜏𝑑𝑡𝑇0𝜕𝑝𝜕𝑡,𝜙𝜙𝐼𝑎𝜙𝜙𝐼,𝜕𝑝𝜕𝑡+𝑑𝜙𝜙𝐼,𝑝+𝑇𝑡𝑐𝜏,𝑡;𝜙𝜙𝐼(𝑡),𝑝(𝜏)𝑑𝜏𝑑𝑡𝑇0𝑦𝑢𝑧𝑑,𝜙𝜙𝐼𝑑𝑡+𝑇0𝑦𝑢𝑦,𝜙𝐼=𝑑𝑡𝑇0𝜏𝜏𝜕𝑝𝐴𝜕𝑡+div𝜕𝑝𝐷𝜕𝑡div𝑝+𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏+𝑦𝑧𝑑𝜙𝜙𝐼+𝑑𝑡𝑇0𝜏𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝×(𝜏)𝑛𝑑𝜏𝜙𝜙𝐼𝑑𝑙𝑑𝑡+𝑇0𝑦𝑢𝑦,𝜙𝑑𝑡=𝐽1+𝐽2+𝐽3.(4.6) It follows from Lemmas 2.3, 2.5, and 4.1 that 𝐽1𝐶(𝛿)𝑇0𝜏4𝜏𝜏𝜕𝑝𝐴𝜕𝑡div𝜕𝑝𝐷𝜕𝑡+div𝑝+𝑇𝑡𝐶div(𝜏,𝑡)𝑝(𝜏)𝑑𝜏+𝑦𝑧𝑑2𝑑𝑡+𝛿𝑇0||𝜙||22,Ω𝑑𝑡𝐶(𝛿)𝜉22𝑝+𝛿𝑢𝑝2𝐿20,𝑇;𝐿2(Ω),𝐽2𝐶(𝛿)𝑇0𝜏3𝑙𝜕𝜏𝐴𝜕𝑝𝐷𝜕𝑡𝑛+𝑝𝑛+𝑇𝑡𝐶(𝜏,𝑡)𝑝(𝜏)𝑛𝑑𝜏2𝑑𝑙𝑑𝑡+𝛿𝑇0||𝜙||20,Ω𝑑𝑡𝐶(𝛿)𝜉23𝑝+𝛿𝑢𝑝2𝐿20,𝑇;𝐿2(Ω).(4.7) By Schwartz inequality, we have 𝐽3𝑦𝐶(𝛿)𝑢𝑦2𝐿20,𝑇;𝐿2(Ω)𝑝+𝛿𝑢𝑝2𝐿20,𝑇;𝐿2(Ω).(4.8) Letting 𝛿 be small enough, it follows from (4.6)–(4.8) that 𝑝𝑢𝑝2𝐿20,𝑇;𝐿2(Ω)𝐶3𝑖=2𝜉2𝑖𝑦+𝐶𝑢𝑦2𝐿20,𝑇;𝐿2(Ω).(4.9) Next, we estimate 𝑦𝑦(𝑢)2𝐿2(0,𝑇;𝐿2(Ω)). Similarly let 𝜓 be the solution of (4.2) with 𝐹=𝑦𝑦(𝑢),  and  𝜓𝐼=𝜋𝜓 the interpolation of 𝜓 in Lemma 2.3.
Then, it follows from (3.36) and integrating by parts that 𝑦𝑢𝑦2𝐿20,𝑇;𝐿2(Ω)=𝑇0𝐹𝑦(𝑡),𝑢𝑦=(𝑡)𝑑𝑡𝑇0𝜕𝑦𝜕𝑡𝑢𝑦𝜕,𝜓+𝑎𝑦𝜕𝑡𝑢𝑦𝑦,𝜓+𝑑𝑢𝑦+,𝜓𝑇𝑡𝑐𝑦𝜏,𝑡;𝑢𝑦𝑦(𝑡),𝜓(𝜏)𝑑𝜏𝑑𝑡+𝑎0𝑦0+𝑦,𝜓(0)0𝑦0=,𝜓(0)𝑇0𝜕𝑦𝜕𝑡𝑢𝑦,𝜓𝜓𝐼𝜕+𝑎𝑦𝜕𝑡𝑢𝑦,𝜓𝜓𝐼𝑦+𝑑𝑢𝑦,𝜓𝜓𝐼+𝑇𝑡𝑐𝑦𝜏,𝑡;𝑢𝑦(𝑡),𝜓𝜓𝐼+(𝜏)𝑑𝜏𝑑𝑡𝑇0𝜕𝑦𝜕𝑡𝑢𝑦,𝜓𝐼𝜕+𝑎𝑦𝜕𝑡𝑢𝑦,𝜓𝐼𝑦+𝑑𝑢𝑦,𝜓𝐼+𝑇𝑡𝑐𝑦𝜏,𝑡;𝑢𝑦(𝑡),𝜓𝐼𝑦(𝜏)𝑑𝜏𝑑𝑡+𝑎0𝑦0+𝑦,𝜓(0)0𝑦0=,𝜓(0)𝑇0𝜕𝑦𝜕𝑡,𝜓𝜓𝐼+𝑎𝜕𝑦𝜕𝑡,𝜓𝜓𝐼𝑦+𝑑,𝜓𝜓𝐼+𝑡0𝑐𝑡,𝜏;𝑦(𝜏),𝜓𝜓𝐼(𝑡)𝑑𝜏𝑑𝑡𝑇0𝑓+𝐵𝑢,𝜓𝜓𝐼𝑦𝑑𝑡+𝑎0𝑦0+𝑦,𝜓(0)0𝑦0=,𝜓(0)𝑇0𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝜏,𝑡)𝑦(𝜏)𝑑𝜏𝑓𝐵𝑢𝜓𝜓𝐼+𝑑𝑡𝑇0𝜏𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛𝑡0𝐶(𝑡,𝜏)𝑦(𝜏)𝑛𝑑𝜏𝜓𝜓𝐼𝑦𝑑𝑙𝑑𝑡+𝑎0𝑦0+𝑦,𝜓(0)0𝑦0,𝜓(0)=𝐷1+𝐷2+𝐷3+𝐷4.(4.10) Similarly, it follows from Lemmas 2.3,  2.5 and 4.1 that 𝐷1𝐶(𝛿)𝑇0𝜏4𝜏𝜏𝜕𝑦𝜕𝑡div𝐴𝜕𝑦𝜕𝑡div𝐷𝑦𝑡0div𝐶(𝜏,𝑡)𝑦(𝜏)𝑑𝜏𝑓𝐵𝑢2𝑑𝑡+𝛿𝑇0||𝜓||22,Ω𝑑𝑡𝐶𝜉24𝑦+𝛿𝑢𝑦2𝐿20,𝑇;𝐿2(Ω),𝐷2𝐶(𝛿)𝑇0𝜏3𝑙𝜕𝜏𝐴𝜕𝑦𝜕𝑡𝑛+𝐷𝑦𝑛𝑡0𝐶(𝑡,𝜏)𝑦(𝜏)𝑛2𝑑𝑙𝑑𝑡+𝛿𝑇0||𝜓||22,Ω𝑑𝑡𝐶𝜉25𝑦+𝛿𝑢𝑦2𝐿20,𝑇;𝐿2(Ω),𝐷3+𝐷4𝐶𝜂26𝑦+𝛿𝑦(𝑢)2𝐿20,𝑇;𝐿2(Ω).(4.11) Letting 𝛿 be small enough, then from (4.10)–(4.11), we have 𝑦𝑢𝑦2𝐿20,𝑇;𝐿2(Ω)𝜉𝐶24+𝜉25+𝜂26.(4.12) The desired results (4.4) follows from (4.9)–(4.12).This completes the proof.

Using Lemmas 3.1 and 4.2, we have the following upper bounds.

Theorem 4.3. Let (𝑦,𝑝,𝑢) and (𝑦,𝑝,𝑢) be the solutions of (2.17)–(2.19) and (2.22)–(2.24), respectively. Then, there hold the a posteriori error estimates as 𝑢𝑢2𝐿20,𝑇;𝐿2Ω𝑈+𝑦𝑦2𝐿20,𝑇;𝐿2(Ω)+𝑝𝑝2𝐿20,𝑇;𝐿2(Ω)𝜂𝐶21+5𝑖=2𝜉2𝑖+𝜂26.(4.13)

Proof. By triangle inequality, (3.44) and (3.38), Lemmas 3.1 and 4.2, we can easily prove (4.13) in the same way of getting (3.43).
This completes the proof.

5. Conclusion

In this paper, we study the semi-discrete adaptive finite element method for optimal control problem governed by a linear quasiparabolic Integrodifferential equation. We extend the existing methods in studying adaptive finite element approximation of optimal control governed by a parabolic Integrodifferential equation to the control governed by a quasiparabolic Integrodifferential equation. After presenting the weak form and the existence and uniqueness of the solution for the optimal control problem, the a posteriori error estimates for semi-discrete finite element approximations in 𝐿(0,𝑇;𝐻1(Ω))-norm and 𝐿2(0,𝑇;𝐿2(Ω))-norm are derived. The work will pave a way to derive the a posteriori error estimates of full discrete finite element approximations of this optimal control problem

Acknowledgments

This research was supported by Science and Technology Development Planning project of Shandong Province (no. 2011GGH20118), Shandong Province Natural Science Foundation (no. ZR2009AQ004), and National Natural Science Foundation of China (no. 11071141).