
The recent marine algae study was carried out in the coastal region of Maharashtra, which is a district of Ratnagiri, Sindhudurg between 2021 and 2022. Water and algae samples were collected between September to October, mainly because to availability of algae is maximum in this period. The sampling locations were decided based on both previous work performed by researchers and on a literature review. The sampling sites were fixed based on the size of study area, sampling site accessibility, availability of algae on surface and substratum of the rock or wall. The microalgae were collected and preserved in plastic jar containing 3% to 4% formalin. The water samples were collected and specific physical and chemical parameters such as pH with pH meter, dissolved oxygen (mg/L) by DO meter, and temperature (Celsius) by digital thermometer were analyzed in situ. The remaining physical and chemical parameters were analyzed in the departmental research laboratory using standard methods outlined by the American Public Health Association (APHA). The collected micro algae were identified by a standard microscopy method using key references and with the help of algae experts. The main objective of the present research was to conduct extensive research on the collection and identification of diverse algal species in a coastal region to determine algal diversity, to determine the water quality standard and to measure the occurrence of algae in water.
Citation: Smita M. Pore, Vinayak P. Dhulap. Identification of marine micro algae in correlation with water quality assessment of coastal region of Maharashtra, India[J]. Clean Technologies and Recycling, 2023, 3(4): 257-266. doi: 10.3934/ctr.2023016
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The recent marine algae study was carried out in the coastal region of Maharashtra, which is a district of Ratnagiri, Sindhudurg between 2021 and 2022. Water and algae samples were collected between September to October, mainly because to availability of algae is maximum in this period. The sampling locations were decided based on both previous work performed by researchers and on a literature review. The sampling sites were fixed based on the size of study area, sampling site accessibility, availability of algae on surface and substratum of the rock or wall. The microalgae were collected and preserved in plastic jar containing 3% to 4% formalin. The water samples were collected and specific physical and chemical parameters such as pH with pH meter, dissolved oxygen (mg/L) by DO meter, and temperature (Celsius) by digital thermometer were analyzed in situ. The remaining physical and chemical parameters were analyzed in the departmental research laboratory using standard methods outlined by the American Public Health Association (APHA). The collected micro algae were identified by a standard microscopy method using key references and with the help of algae experts. The main objective of the present research was to conduct extensive research on the collection and identification of diverse algal species in a coastal region to determine algal diversity, to determine the water quality standard and to measure the occurrence of algae in water.
Let Ω be a convex polygonal domain in R2. In this paper, we consider the following Dirichlet boundary optimal control problem,
min{q} J(y,q)=12‖y−ˆy‖2L2(Ω)+α2‖q‖2L2(Γ) | (1.1) |
subject to the advection-diffusion equation
−Δy(x)+→β(x)⋅∇y(x)+c(x)y(x)=f(x),x∈Ω, | (1.2a) |
y(x)=q(x),x∈Γ. | (1.2b) |
Here, y(x) denotes the state variable, ˆy(x) is the desired state, (1.2a) and (1.2b) are called the state equation, q(x) is the control, Γ=∂Ω.
We assume the given functions f(x),ˆy(x)∈L2(Ω), →β(x)∈[W1∞(Ω)]2, c(x)∈L∞(Ω) with the assumption
c(x)−12∇⋅→β(x)≥0, |
and α>0 is a given scalar.
This problem is important in many applications, for example distribution of pollution in air [1] or water [2] and for problems in computational electro-dynamics, gas and fluid dynamics [3]. However, there are several challenges involved in solving this problem numerically. One problem arises for higher order elements and nonsmooth Dirichlet data which can cause serious problems in using standard finite element methods (see [4,5]). Another difficulty lies in the fact that Dirichlet boundary conditions do not enter the bilinear form naturally and that causes problems for analyzing the finite element method (see [6,7,8,9,10] for further discussion).
One faces another challenge in the presence of layers which are the regions where the gradient of the solution is large. Usually, the boundary layers occur because of the fact that problem has reduced to the first order PDEs and requires boundary conditions on inflow part of the boundary only. In this case, standard Galerkin methods fail when h|→β|>1, where h is mesh size, producing highly oscillatory solutions. A lot of research has been done in last 40 years to address this difficulty (see [3,4,11,12,13]).
We have an example to illustrate this difficulty in the following simple example,
Example 1.1.
−ϵy″(x)+y′(x)=1,x∈(0,1),y(0)=y(1)=0. | (1.3) |
The Figure 1 shows nonphysical oscillations of the standard Galerkin solution for h=0.1 and ϵ=0.0025.
One way to solve this problem is to use stabilized methods (see [14]). We will mention some of them. One of the first stable method of arbitrary order is SUPG (Streamline Upwind Petrov Galerkin) [11,15,16]. In this method, the space of test function is different from the space of trial function and chosen such that the method is stable and consistent. Other stabilized methods where the space of trial and test functions are the same and used upwind stabilization are HDG (Hybridizable Discontinuous Galerkin), [17,18,19,20,21], SIPG (Symmetric Interior Petrov Galerkin) [5,7,10], and LDG (Local Discontinuous Galerkin) [22,23,24]. Another popular stabilized method where the space of trial and test functions are the same is edge stabilization [25,26].
DG methods are shown to be robust for the advection-diffusion-reaction problem (see [7,27]) even for the advection-dominated case. DG methods were not only analyzed for the advection-diffusion-reaction problem but also for the optimal control problem of the advection-diffusion-reaction equation [28], (see other stabilized methods for the optimal control problem of the advection-diffusion-reaction equation [26,29,30]). In addition to being stable, the discontinuous Galerkin methods, such as SIPG, usually treat the boundary conditions weakly. The SIPG method was also analyzed for distributed optimal control problems and optimal local and global error estimates were obtained (see [28] but not for the boundary control problems. We would like to investigate the performance of the SIPG method applied to Dirichlet boundary control problem (1.1), (1.2a) and (1.2b) and prove a priori error estimates. We would also like to perform a number of numerical experiments to confirm our theoretical result which is the main subject of the current work.
In this paper, we analyze the SIPG solution of Dirichlet boundary control problem and the difficulties with dealing with the stability issues as well as with the difficulty of the treatment of Dirichlet boundary conditions. This method has some attractive features and offers some advantages. This method is stable and accurate, can be of arbitrary order and has been shown analytically that the boundary layers do not pollute the solution into the subdomain of smoothness [28]. Another attractive feature of the method is that Dirichlet boundary conditions are enforced weakly through the penalty term and not through the finite dimensional subspace [25]. As a result of the weak treatment of the boundary conditions, Dirichlet boundary control enters naturally into the bilinear form and makes analysis more natural [6,7,8,31]. Finally, the SIPG method has the property that two strategies optimize-then-discretize and discretize-then-optimize produce the same discrete optimality system (see [10,23]), which is not the case for other stabilized methods, for example, SUPG method (see [15]).
Let us show some features of SIPG method with Figure 2 in the previous example. Consider the problem 1.3 in the example 1 with the much more smaller diffiusion parameter 10−9 instead of −0.0025. Figure 2 shows the behavior of the SIPG solution for h=0.1 and ϵ=1e−9. As one can see the solution is stable. The Dirichlet boundary condition at x=1 is almost ignored by the method as a result of weak treatment.
Our choice of this particular DG method was motivated by good approximation and stabilization properties of the method. Additional attractive feature of the method is the weak treatment of the boundary conditions which allows us to set Dirichlet optimal control problem in natural the finite element frame work and to prove optimal convergence rates for on general convex polygonal domain. Moreover, we state the main result of the paper is valid for any general convex domain, there exists a positive constant C independent of h for the error between exact solution of the control function ˉq and its approximation ˉqh such that
‖ˉq−ˉqh‖L2(Γ)≤Ch1/2(|ˉq|H1/2(Γ)+‖ˉy‖H1(Ω)+‖ˆy‖L2(Ω)), |
for h small enough. Also, we performed several numerical examples to support our theoretical results, and additionally when we investigate numerically performance of the method in the advection-dominated case.
Throughout the paper, we will use standard notation for spaces, completeness and norms. We will use the standard notation for Lebesgue and Sobolev space, their suitable norms, and L2- inner product. Thus,
● (u,v)Ω=∫Ωuvdx and ⟨u,v⟩Γ=∫Γuvds are the inner products on the domain Ω and its boundary Γ, respectively.
The corresponding norms respectively are
‖u‖L2(Ω)=(∫Ω|u|2dx)1/2,‖u‖L2(Γ)=(∫Γ|u|2)ds)1/2. |
● H1/2(Γ)={u∈L2(Γ)|∃˜u∈H1(Ω):u=tr(˜u)}.
● ‖u‖H1/2(Γ)=inf{‖˜u‖H1(Ω)|tr(˜u)=u}.
● |u|H1/2(Γ)=inf{|˜u|H1(Ω)|tr(˜u)=u}.
First, let us consider the state equation,
−Δy+→β⋅∇y+cy=fin Ω,y=qon Γ. | (2.1) |
We review some regularity results for various conditions on data which we will use later in the analysis. The first result is standard and found in [32].
Theorem 2.1. Let f∈H−1(Ω) and q∈H1/2(Γ). Then Eq (2.1) admits a unique solution y∈H1(Ω). Moreover, the following estimate holds
‖y‖H1(Ω)≤C(‖f‖H−1(Ω)+‖q‖H12(Γ)). |
In the case of q=0 on Γ, f∈L2(Ω), and convex Ω, we can obtain a higher regularity of the solution (see [33]).
Theorem 2.2. Let f∈L2(Ω) and q=0 on Γ. Then, the Eq (2.1) admits a unique solution y∈H2(Ω) and the following estimate holds
‖y‖H2(Ω)≤C‖f‖L2(Ω). |
Remark 2.1. Since the adjoint equation defined by
−Δz−∇⋅(→βz)+cz=y−ˆyin Ωz=0on Γ, |
it is also an advection-diffusion equation and the results of the above theorems are valid for the adjoint equation with similar estimates as well. Also, notice that −→β⋅∇z+(c−∇⋅→β)z=−∇⋅(→βz)+cz.
The theory in the case of q∈L2(Γ) is more technical and to obtain the desired regularity result, we use the transposition method [34], which we will briefly describe next.
Suppose q is smooth enough having continuous derivatives up to the desired order, ϕ∈L2(Ω) and let y1 and y2 be the solutions of the following equations,
−Δy1+→β⋅∇y1+cy1=0 in Ω,y1=qon Γ,and−Δy2−∇⋅(→βy2)+cy2=ϕin Ω,y2=0on Γ, |
respectively. Then, by the integration by parts and using the fact that y2=0 on Γ, we obtain
0=(−Δy1+→β⋅∇y1+cy1,y2)Ω=(∇y1,∇y2)Ω−⟨∂y1∂n,y2⟩Γ+⟨y1→β⋅→n,y2⟩Γ−(y1,∇⋅(→βy2))Ω+(cy1,y2)Ω=(∇y1,∇y2)Ω−(y1,∇⋅(→βy2))Ω+(y1,cy2)Ω=(y1,−Δy2)Ω+⟨y1,∂y2∂n⟩Γ−(y1,∇⋅(→βy2))Ω+(y1,cy2)Ω=(y1,−Δy2−∇⋅(→βy2)+cy2)Ω+⟨y1,∂y2∂n⟩Γ=(y1,ϕ)Ω+⟨q,∂y2∂n⟩Γ, |
where in the last step we use that −Δy2−∇⋅(→βy2)+cy2=ϕ in Ω and y1=q on Γ. Hence we obtain
(y1,ϕ)Ω=−⟨q,∂y2∂n⟩Γ. |
The above formula defines a mapping Λ:ϕ→−∂y2∂n that is linear and continuous from L2(Ω) to H1/2(Γ). Since the embedding H1/2(Γ)↪L2(Γ) is compact, Λ is a compact operator from L2(Ω) to L2(Γ). Hence, its adjoint Λ∗ is a compact operator from L2(Γ) to L2(Ω).
Since (y1,ϕ)Ω=−∫Γq∂y2∂n=⟨q,Λϕ⟩Γ and ⟨q,Λϕ⟩Γ=(Λ∗q,ϕ)Ω, we conclude that y1=Λ∗q. Using the above, we can define an "ultra-weak" solution for the Eq (2.1) for Dirichlet data in L2(Γ) as follows.
Definition 2.1. We say that y∈L2(Ω) is a unique ultra-weak solution of the Eq (2.1) if
∫Ωyϕ=(f,p)(H−1(Ω),H10(Ω))−∫Γq∂p∂n,∀ϕ∈L2(Ω), |
where p satisfies
−Δp−∇⋅(→βp)+cp=ϕin Ω,p=0 on Γ. |
Now we are ready to provide the following regularity result.
Theorem 2.3. For any f∈H−1(Ω) and q∈L2(Γ), the Eq (2.1) admits a unique ultra-weak solution y∈L2(Ω). Moreover, the following estimate holds,
‖y‖L2(Ω)≤C(‖f‖H−1(Ω)+‖q‖L2(Γ)). | (2.2) |
Proof. Existence follows from the Definition (2.1). For the uniqueness, we assume that y1 and y2 are distinct solutions of the Eq (2.1) and let u=y1−y2, then
−Δu−∇⋅(→βu)+cu=0in Ω,u=0on Γ. |
Since H1(Ω) is dense in L2(Ω), it is enough to consider u∈H1(Ω). By the Theorem (2.1), we have
‖u‖H1(Ω)=0. |
As a result u=0, hence y1=y2 and this contradiction proves the uniqueness.
To show the desired estimate (2.2), we use a duality argument. Let w be the solution of the problem
−Δw−∇⋅(→βw)+cw=yin Ω,w=0on Γ. |
By using the above duality argument and using integration by parts and the fact that w=0 on Γ, we obtain
‖y‖2L2(Ω)=(y,−Δw−∇⋅(→βw)+cw)Ω=(∇y,∇w)Ω−⟨y,∂w∂n⟩Γ−⟨y,w(→β⋅→n)⟩Γ+(→β⋅∇y,w)Ω+(y,cw)Ω=(−Δy,w)Ω+⟨∂y∂n,w⟩Γ−⟨y,∂w∂n⟩Γ−⟨y,w(→β⋅→n)⟩Γ+(→β⋅∇y,w)Ω+(y,cw)Ω=(−Δy+→β⋅∇y+cy,w)Ω−⟨y,∂w∂n⟩Γ=(f,w)Ω−⟨q,∂w∂n⟩Γ, |
where in the last step we use −Δy+→β⋅∇y+cy=f.
By the trace and the Cauchy-Schwarz inequalities, and by using the Theorem (2.2), we have the following estimate
‖y‖2L2(Ω)≤‖f‖H−1(Ω)‖w‖H1(Ω)+‖q‖L2(Γ)‖∂w∂n‖L2(Γ)≤C(‖f‖H−1(Ω)+‖q‖L2(Γ))‖w‖H2(Ω)≤C(‖f‖H−1(Ω)+‖q‖L2(Γ))‖y‖L2(Ω). |
Canceling ‖y‖L2(Ω) on both sides, we prove the desired estimate (2.2).
Next we will provide the first order optimality conditions for the problem (1.1)
Theorem 3.1. Assume that f,ˆy∈L2(Ω) and let (ˉy,ˉq) be the optimal solution of the Eq (2.1). Then, the optimal control ˉq is given by ∂ˉz∂n=αˉq, where ˉz is the unique solution of the equation,
−Δˉz−∇⋅(→βˉz)+cˉz=ˉy−ˆyin Ω,ˉz=0 on Γ. | (3.1) |
Proof. Let (ˉy,ˉq) be an optimal solution of the Eq (1.1). We set
F(q)=J(y(q),q), |
where y(q) is the solution of the Eq (2.1) for a given q∈L2(Γ). Let yq be the solution of the problem
−Δyq+→β⋅∇yq+cyq=f in Ω,yq=q+ˉqon Γ. |
By the optimality of (ˉy,ˉq) and convexity of Ω, we have that 1λ(F(ˉq+λq)−F(ˉq))≥0 for all q and λ∈(0,1] [35]. For λ=1, yq=q+ˉq, and so F(ˉq+q)−F(ˉq)≥0.
Equivalently, if F(ˉq+q)−F(ˉq)≥0 for all q in L2(Γ), then ˉq is an optimal solution of the problem. We find
F(ˉq+q)−F(ˉq)=J(yq,q+ˉq)−J(ˉy,ˉq)=12∫Ω(yq−ˉy)(yq+ˉy−2ˆy)+α2∫Γ(2qˉq+q2)=12∫Ω(yq−ˉy)2+α2∫Γq2+∫Ω(yq−ˉy)(ˉy−ˆy)+α∫Γqˉq. |
Let ˉz be the solution of the Eq (3.1). Then, we can estimate the third term of the right hand side by using the Green's formula and using the fact that yq=ˉq+q and ˉz=0 on Γ. Thus, we obtain
∫Ω(yq−ˉy)(ˉy−ˆy)=∫Ω(yq−ˉy)(−Δˉz−∇⋅(→βˉz)+cˉz)=−∫Γ∂ˉz∂n(yq−ˉq)+∫Ω∇ˉz⋅∇(yq−ˉy)−∫Γ(yq−ˉy)ˉz(→β⋅→n)+∫Ωˉz(→β⋅∇(yq−ˉy))+∫Ω(yq−ˉy)cˉz=−∫Γ∂ˉz∂n(ˉq+q−ˉq)+∫Ω∇ˉz⋅∇(yq−ˉy)+∫Ωˉz(→β⋅∇(yq−ˉy))+∫Ω(yq−ˉy)cˉz=−∫Γq∂ˉz∂n+(∂yq∂n−∂ˉy∂n)ˉz|Γ+∫Ωˉz(−Δ(yq−ˉy)+→β⋅∇(yq−ˉy)+c(yq−ˉy))⏟=0. |
Notice that ∫Ω∇ˉz⋅∇(yq−ˉy)=(∂yq∂n−∂ˉy∂n)ˉz|Γ−∫ΩˉzΔ(yq−ˉy) by using integration by parts. By setting ∂ˉz∂n=αˉq, we have
∫Ω(yq−ˉy)(ˉy−ˆy)=−∫Γq∂ˉz∂n=−α∫Γqˉq. |
Putting all results together, we have
F(ˉq+q)−F(ˉq)=12∫Ω(yq−ˉy)2+α2∫Γq2−α∫Γqˉq+α∫Γqˉq=12∫Ω(yq−ˉy)2+α2∫Γq2≥0, |
i.e., (ˉy,ˉq) is the optimal solution to the Eq (2.1) with ˉq=1α∂ˉz∂n where α>0 given any scalar in the problem (1.1)
The first order optimality conditions in the strong form are as the following
Adjoint equation{−Δz−→β⋅∇z+(c−∇⋅→β)z=y−ˆyinΩ,z=0 onΓ. | (3.2) |
Gradient equation{∂z∂n=αqonΓ, | (3.3) |
State equation{−Δy+→β⋅∇y+cy=finΩ,y=qonΓ. | (3.4) |
In the next theorem, we establish the regularity of the optimal solution of the problem (1.2a) and (1.2b).
Theorem 3.2. Let (ˉy,ˉq)∈L2(Ω)×L2(Γ) be the optimal solution to the optimization problem (1.1) subject to the problem (1.2a) and (1.2b), and ˉz be the optimal adjoint state (3.1). Then,
(ˉy,ˉq,ˉz)∈H1(Ω)×H1/2(Γ)×H2(Ω). |
Proof. For ˉq∈L2(Γ), from the state Eq (3.4), ˉy∈L2(Ω) holds by Theorem (2.3).
Since ˉy,ˆy∈L2(Ω) and Ω is a convex domain, from the adjoint Eq (3.2), ˉz∈H2(Ω) holds by Theorem (2.2).
Since ˉz∈H2(Ω), we have ∂ˉz∂n∈H1/2(Γ), from the gradient Eq (3.3), ∂ˉz∂n=αq implies ˉq∈H1/2(Γ).
Since ˉq∈H1/2(Γ), from the state Eq (3.4), ˉy∈H1(Ω) holds by Theorem (2.1).
Remark 3.1. Using regularity results, we can generalize the regularity which depends on the largest interior angle of the polygonal domain in R2 [36].
The idea of the FEM is to construct Vh and Qh defined on a finite dimensional space that is well approximate the solution spaces V and Q. The Galerkin FEM is to find yh∈Vh and qh∈Qh such that
ah(yh,vh)=ℓh(f;qh,vh),∀vh∈Vh, | (4.1) |
where Vh is a finite dimensional space and h is a discretization parameter. We can easily see that if ah(⋅,⋅) satisfies the conditions of Lax-Milgram Lemma, the Eq (4.1) has a unique solution for each h.
To construct Vh, we consider a family of conforming quasi-uniform shape regular triangulations Th of Ω such that ˉΩ=∪τi∈Thτi and τi∩τj=0 ∀τi,τj∈Th, i≠j with a mesh size
h=supτi∈Thdiam(τi). |
We define Eh as a collection of all edges Eh=E0h∪E∂h where E0h and E∂h are the collections of interior and boundary edges, respectively, and we decompose the boundary edges as
E∂h=E+−hh, | (4.2) |
where E−h:={e∈E∂h:e⊂{x∈Γ:→β(x)⋅→n(x)<0}} and E+h:=E∂h∖E−h i.e. these are the collections of the edges that belong to the inflow and outflow part of the boundary, respectively. In other words, for a given elements τ∈Th and nτ indicates the outward normal to τ, then we can decompose its boundary ∂τ as ∂τ−={x∈∂τ:→β(x)⋅→nτ(x)<0} and ∂τ+={x∈∂τ:→β(x)⋅→nτ(x)≥0}.
We define the standard jumps and averages on the set of interior edges by
{φ}=φ1+φ22,[[φ]]=φ1→n1+φ2→n2,{→ϕ}=→ϕ1+→ϕ22,[[→ϕ]]=→ϕ1⋅→n1+→ϕ2⋅→n2, |
where →n1 and →n2 are outward normal vectors at the common boundary edge of neighboring elements τ1 and τ2, respectively. If e∈E∂h, then {φ}=[[φ]]=φ|e [37,38]. Define the discrete state and control spaces as
Vh:={yh∈L2(Ω):yh|τ∈Pk(τ)∀τ∈Th}, | (4.3) |
Qh:={qh∈L2(Γ):qh|τ∈Pl(τ)∀τ∈E∂h}, | (4.4) |
respectively. We denote by Pk, Pl the space of polynomials of degree at most k on each element and at most l on each edge, respectively. In general, the state and control variables can be approximated by polynomials of different degrees k, l∈N.
Here, we use the symmetric interior penalty Galerkin (SIPG) method to approximate to the problem. In deriving the SIPG method, we use the following identity
∑τ∈Th(→ϕ⋅→n,φ)∂τ=∑e∈Eh({→ϕ},[[φ]])e+∑e∈E0h([[→ϕ]],{φ})e=∑e∈E0h({→ϕ},[[φ]])e+([[→ϕ]],{φ})e+∑e∈E∂h(→ϕ⋅→n,φ)e. |
The SIPG solutions qh∈Qh, yh∈Vh and a constant advection field →β satisfies the Eq (4.1) for all vh∈Vh where
ah(yh,vh)=∑τ∈Th(∇yh,∇vh)τ +∑τ∈Th(→β⋅∇yh+cyh,vh)τ+∑e∈Eh[γh([[yh]],[[vh]])e−({∇yh},[[vh]])e−([[yh]],{∇vh})e]+∑e∈E0h(y+h−y−h,|→n⋅→β|v+h)e+∑e∈E−h(y+h,v+h|→n⋅→β|)e, | (4.5) |
where γ is the penalty parameter, which should be chosen sufficiently large to ensure the stability of the SIPG scheme [37,39,40], and y−h=limζ→0+yh(x−ζ→β), y+h(x)=limζ→0+yh(x+ζ→β),
ℓh(f;qh,vh)=∑τ∈Th(f,vh)τ+∑e∈E∂h(γh(qh,[[vh]])e−(qh,{∇vh})e)+∑e∈E−h(qh,v+h|→n⋅→β|)e. | (4.6) |
Then, DG solution is defined as a solution of ah(yh,vh)=ℓh(f;qh,vh) for al all vh∈Vh, and mesh dependent norm
|||vh|||2=‖vh‖2h=∑τ∈Th‖∇vh‖2τ+‖vh‖2τ+∑e∈E∂hγh‖[[vh]]‖2e, |
which is equivalent to the energy norm [38].
It has been shown, for example [7], that the bilinear form (4.5) is coercive and bounded on Vh i.e., ah(vh,vh)≥C|||vh|||2 and ah(yh,vh)≤C|||yh||||||vh|||, respectively. Thus, Lax-Milgram Lemma guarantees the existence of a unique solution yh∈Vh of the Eq (4.1) for all vh∈Vh.
We apply the SIPG discretization to the optimal control problem (1.1). Now, define the discrete Lagrangian as
Lh(ˉyh,ˉqh,ˉzh)=J(ˉyh,ˉqh)+ah(ˉyh,ˉzh)−ℓh(f,ˉqh). |
Then, setting the partial Frechet derivatives with respect to yh,qh and zh to be zero, we obtain the discrete optimality system.Then, the discretized optimal control problem has a unique solution (yh,qh)∈VhxQh if only if there exists zh∈Vh holds the following system:
∂Lh∂ˉyhψh=0⇒ah(ψh,ˉzh)=ℓh(ˆy−ˉyh;0,ψh)∀ψh∈Vh, | (4.7) |
∂Lh∂ˉqhϕh=0⇒⟨∂ˉzh∂n,ϕh⟩Γ=−⟨αˉqh,ϕh⟩Γ+γh⟨ˉzh,ϕh⟩Γ+⟨ˉzh|→n⋅→β|,ϕh⟩Γ ∀ϕh∈Qh, | (4.8) |
∂Lh∂ˉzhφh=0⇒ah(φh,ˉyh)=ℓh(f;qh,φh)∀φh∈Vh. | (4.9) |
We will need some auxiliary estimates that we will use in the proof of the main result. First, we have some standard estimates which are trace and inverse inequalities and the proofs can be found in [41,42,43].
Lemma 5.1. There exist positive constants Ctr and Cinv independent of τ and h such that for ∀τ∈Th,
‖v‖∂τ≤Ctr(h−1/2‖v‖τ+h1/2‖∇v‖τ),∀v∈Hk+1(τ), | (5.1) |
‖∇vh‖τ≤Cinvh−1‖vh‖τ,∀vh∈Vh, | (5.2) |
for integer k≥0
Then, we need some basic estimates for L2-Projection where Ph:L2(Ω)→Vh is the orthogonal projection such that (Phv,χ)τ=(v,χ)τ for all v∈L2(τ) and χ∈Vh.
Lemma 5.2. Let Ph be L2-projection. Then, we have that ∃Ph:Hk+1→Vh such that for any τ∈Th,
‖v−Phv‖L2(τ)≤Chk+1‖v‖Hk+1(τ),∀v∈Hk+1(τ),‖∇(v−Phv)‖L2(τ)≤Chk‖v‖Hk+1(τ),∀v∈Hk+1(τ), |
where integer k≥0.
Proof. From Local Approximation used in [30], we know that there exists a local interpolant operator Ph:Hk+1→Vh such that for any τ∈Th and ∀v∈Hk+1(τ),
h‖∇(v−Ph(v))‖τ+‖v−Ph(v)‖τ≤Chk+1‖v‖Hk+1(τ). |
Since h‖∇(v−Ph(v))‖τ≤h‖∇(v−Ph(v))‖τ+‖v−Ph(v)‖τ≤Chk+1‖v‖Hk+1(τ), we have
h‖∇(v−Ph(v))‖τ≤Chk+1‖v‖Hk+1(τ). |
Thus,
‖∇(v−Phv)‖L2(τ)≤Chk‖v‖Hk+1(τ). |
Likewise, we obtain ‖v−Phv‖L2(τ)≤Chk+1‖v‖Hk+1(τ).
Now, we are ready to show the error estimate of SIPG solution in the energy norm.
Lemma 5.3. Let v be the unique solution of the Eq (2.1) to satisfy v∈Hk+1(Ω) and vh∈Vh be the SIPG solution of the discretized state equation with piecewise polynomials of degree k. Then,
|||v−vh|||≤Chk‖v‖Hk+1(Ω), |
for integer k≥0.
The proof can be easily seen by using the well-posedness of the bilinear form (4.5), Lemmas (5.1) and (5.2), and it can be also found for example in [44,45]. Next, we will need the estimate of L2-Projection on the boundary Γ where P∂h:L2(Γ)→Qh is defined by ⟨q−P∂hq,ϕh⟩e=0 for all ϕh∈Ps(e).
Lemma 5.4. Let P∂h be L2−projection defined on the boundary. Then, for any edge e∈E∂h,
‖q−P∂q‖L2(e)+hs‖q−P∂q‖Ws,p(e)≤hs|q|Ws,p(e)∀e∈E∂h, |
where E∂h is the set of boundary edges which is described in the Eq (4.2), q∈Ws,p(e), 0≤s≤1, and 1<p<∞.
The proof can be found in [6].
Note that Lemmas (5.1)–(5.4) state for general reqularity which depends on the polynomial degree k used in SIPG, the regularity on the solution of the optimal control problem is (ˉy,ˉq,ˉz)∈H1(Ω)×H1/2(Γ)×H2(Ω) by Theorem (3.2). Thus, the following estimates and the main result will be done by using the regularity on the solution of the problem in Theorem (3.2).
Since SIPG method treats the boundary conditions weakly, SIPG solution is not zero on the boundary even if its continuous solution z is. However, the following result says that the norm of SIPG solution zh on the boundary is rather small.
Lemma 5.5. Let us define auxiliary variable ˜z to be a solution of the Eq (3.2)
−Δ˜z−∇⋅(→β˜z)+c˜z=ˆy−yh in Ω˜z=0on Γ, |
and ˜zh∈Vh be the SIPG approximation solution. Then,
‖˜zh‖L2(Γ)≤Ch3/2‖ˆy−yh‖L2(Ω). |
Proof. Let ˜z be a solution to the Eq (3.2). Since
‖˜zh‖L2(Γ)=‖˜zh−˜z‖L2(Γ)=‖[[˜zh−˜z]]‖L2(Γ), |
we can estimated that
‖[[˜zh−˜z]]‖L2(Γ)≤Ch1/2|||˜zh−˜z|||, |
by using the definition of the energy norm. Thus, by Theorems (2.2), (3.2) and Lemma (5.3), we have that
‖˜zh‖L2(Γ)≤Ch1/2|||˜zh−˜z|||≤Ch1/2h‖˜z‖H2(Ω)≤Ch3/2‖ˆy−yh‖L2(Ω). |
The estimate of |||y−yh||| is more involved because (y−yh) does not satisfy the Galerkin orthogonality by (y−yh)∉Vh and ah(y−yh,vh)≠0 for vh∈Vh. First, we can show the following result.
Lemma 5.6. Let y and yh satisfy
ah(y,v)=ℓh(f;q,v), ∀v∈H1(Ω),ah(yh,χ)=ℓh(f;qh,χ),∀χ∈Vh. |
Then,
|||y−yh|||≤C(h−1/2‖q−qh‖L2(Γ)+‖y‖H1(Ω)). |
Proof. By the coersivity, adding and subtracting Phy, we have
|||y−yh|||2≤ah(y−yh,y−yh)=ah(y−yh,Phy−yh)⏟I+ah(y−yh,y−Phy)⏟II. |
II:
By using the boundedness of ah(.,.), Theorem (3.2) and Lemma (5.3), k=0 and we obtain
ah(y−yh,y−Phy)≤|||y−yh||||||y−Phy|||≤C|||y−yh|||‖y‖H1(Ω). |
I:
Since(Phy−yh)∈Vh, we have ah(y−yh,Phy−yh)=ℓh(0;q−qh,Phy−yh). Then, we have
ℓh(0;q−qh,Phy−yh)=∑e∈E∂h(γh(q−qh,[[Phy−yh]])e−(q−qh,{∇(Phy−yh)})e)+∑e∈E−h(q−qh,(Phy−yh)+|→n⋅→β|)e. |
By the definition of ℓh(,), we can see that ∑eγh(q−qh,[[Phy−yh]])e is the dominating term by being γh large. Using the fact that ‖[[Phy−yh]]‖L2(Γ) is a part of the energy norm and Lemma (5.3) for k=0 since y∈H1(Ω), we have
ℓh(0;q−qh,Phy−yh)≤C∑eγh(q−qh,[[Phy−yh]])e≤Ch−1(∑e‖q−qh‖2L2(e))1/2(∑e‖[[Phy−yh]]‖2L2(e))1/2≤Ch−1‖q−qh‖L2(Γ)‖[[Phy−yh]]‖L2(Γ)≤Ch−1‖q−qh‖L2(Γ)h1/2|||Phy−yh|||≤Ch−1/2‖q−qh‖L2(Γ)(|||Phy−y|||+|||y−yh|||)≤Ch−1/2‖q−qh‖L2(Γ)(‖y‖H1(Ω)+|||y−yh|||). |
The other terms in ℓh(0;q−qh,Phy−yh) can be estimated with the similar way. Thus,
|||y−yh|||2≤I+II≤C‖y‖H1(Ω)|||y−yh|||+Ch−12‖q−qh‖L2(Γ)|||y−yh|||+Ch−12‖q−qh‖L2(Γ)‖y‖H1(Ω)≤14|||y−yh|||2+Ch−1‖q−qh‖2L2(Γ)+C‖y‖2H1(Ω). |
By first taking the square root and then canceling |||y−yh|||, we obtain
|||y−yh|||≤C(h−1/2‖q−qh‖L2(Γ)+‖y‖H1(Ω)). |
Using a duality, we can show better estimate in L2 norm.
Lemma 5.7. Let y be the solution of the Eq (2.1) and yh in Vh satisfy the bilinear form (4.5). Then,
‖y−yh‖L2(Ω)≤C(h1/2‖q−qh‖L2(Γ)+h‖y‖H1(Ω)). |
Proof. Since yh is not a Galerkin projection of y, let us define ˜yh by ah(y−˜yh,χ)=0 for χ∈Vh. Then, by the triangle inequality, we have
‖y−yh‖2L2(Ω)≤‖y−˜yh‖2L2(Ω)⏟K1+‖˜yh−yh‖2L2(Ω)⏟K2. |
K1
Consider the following equation,
−Δt−∇⋅(→βt)+ct=y−˜yh in Ωt=0 on Γ. |
By the boundedness of the bilinear form and using the Galerkin orthogonality,
‖y−˜yh‖2L2(Ω)=ah(y−˜yh,t)=ah(y−˜yh,t−Pht)+ah(y−˜yh,Pht)⏟=0≤C|||t−Pht|||.|||y−˜yh|||≤Ch‖t‖H2(Ω)|||y−˜yh|||. |
By using Theorem (2.2) and Lemma (5.3), we obtain
K1≤Ch‖y−˜yh‖L2(Ω)‖y‖H1(Ω)≤14‖y−˜yh‖2L2(Ω)+Ch2‖y‖2H1(Ω). |
By canceling ‖y−˜yh‖2L2(Ω), we obtain that
K1≤Ch2‖y‖2H1(Ω). |
K2:
Let us define another dual equation,
−Δv−∇⋅(→βv)+cv=˜yh−yhin Ωv=0on Γ. |
‖˜yh−yh‖2L2(Ω)=ah(˜yh−yh,v)=ah(~yh−y,v)⏟K21+ah(y−yh,v)⏟K22. |
K21:
Likewise K1,
K21=ah(˜yh−y,v)=ah(˜yh−y,v−Phv)+ah(˜yh−y,Phv)⏟=0≤C|||v−Phv||||||˜yh−y|||≤Ch‖v‖H2(Ω)|||˜yh−y|||. |
By using Theorem (2.2) and Lemma (5.3), we obtain
K21≤Ch‖˜yh−yh‖L2(Ω)‖y‖H1(Ω). |
K22:
K22=ah(y−yh,v)=ah(y−yh,v−Phv)⏟K221+ah(y−yh,Phv)⏟K222.
By using the boundedness of the bilinear form, Theorem (2.2) and Lemma (5.3),
K221=ah(y−yh,v−Phv)≤C|||v−Phv||||||y−yh|||≤Ch‖v‖H2(Ω)|||y−yh|||≤Ch‖˜yh−yh‖L2(Ω)|||y−yh|||. |
By using Lemma (5.6), we obtain
K221≤Ch‖˜yh−yh‖L2(Ω)|||y−yh|||≤Ch‖˜yh−yh‖L2(Ω)(h−1/2‖q−qh‖L2(Γ)+‖y‖H1(Ω))≤C‖˜yh−yh‖L2(Ω)(h1/2‖q−qh‖L2(Γ)+h‖y‖H1(Ω)). |
K222:
Using the fact that v=0 on Γ, Theorems (2.2), (3.2) and Lemma (5.3), we have that
K222=ah(y−yh,Phv)=ℓh(0;q−qh,Phv)≤Ch−1‖q−qh‖L2(Γ)‖Phv‖L2(Γ)≤Ch−1‖q−qh‖L2(Γ)‖[[Phv−v]]‖L2(Γ)≤Ch−1‖q−qh‖L2(Γ)h1/2|||Phv−v|||≤Ch−1‖q−qh‖L2(Γ)h1/2h‖v‖H2(Ω)≤Ch−1‖q−qh‖L2(Γ)h3/2‖˜yh−yh‖L2(Ω). |
Then, we obtain
K222≤Ch1/2‖q−qh‖L2(Γ)‖˜yh−yh‖L2(Ω). |
Thus, we have
‖˜yh−yh‖2L2(Ω)≤K21+K22⏟K221+K222≤Ch2‖y‖H1(Ω)+C‖˜yh−yh‖L2(Ω)(h1/2‖q−qh‖L2(Γ)+h‖y‖H1(Ω))≤14‖˜yh−yh‖2L2(Ω)+Ch2‖y‖2H1(Ω)+Ch‖q−qh‖2L2(Γ). |
By canceling ‖˜yh−yh‖2L2(Ω), we obtain
‖˜yh−yh‖2L2(Ω)≤Ch2‖y‖2H1(Ω)+Ch‖q−qh‖2L2(Γ). |
Finally, we obtain
‖y−yh‖2L2(Ω)≤‖y−˜yh‖2L2(Ω)+‖˜yh−yh‖2L2(Ω)≤C(h‖q−qh‖2L2(Γ)+h2‖y‖2H1(Ω)). |
By taking the square root, we conclude
‖y−yh‖L2(Ω)≤C(h1/2‖q−qh‖L2(Γ)+h‖y‖H1(Ω)). |
Now, we are ready to prove the main result of the paper. We will state it in the next theorem.
Theorem 5.1. Let Ω be a convex polygonal domain, ˉq be the optimal control of the problem (1.1) and ˉqh be its optimal SIPG solution. Then, for h sufficiently small, there exists a positive constant C independent of h such that
‖ˉq−ˉqh‖L2(Γ)≤Ch1/2(|ˉq|H1/2(Γ)+‖ˉy‖H1(Ω)+‖ˆy‖L2(Ω)), | (5.3) |
where (ˉy,ˉq,ˉz)∈H1(Ω)×H1/2(Γ)×H2(Ω) and ˆy∈L2(Ω).
Proof. Since ˉq is the optimal solution of the problem (1.1) and ˉq satisfies the Eq (3.3), we have
α⟨ˉq,ϕh⟩Γ+⟨ϕh,∂ˉz∂n⟩Γ=0,∀ϕh∈Qh. | (5.4) |
Since ˉqh is the approximate solution of the problem (1.1) and ˉqh satisfies the Eq (4.8), we have
α⟨ˉqh,ϕh⟩Γ+⟨ϕh,∂ˉzh∂n⟩Γ−γh⟨ϕh,ˉzh⟩Γ−⟨ˉzh|→n⋅→β|,ϕh⟩Γ−=0,∀ϕh∈ Qh. | (5.5) |
Subtracting the Eq (5.4) from the Eq (5.5), for any ϕh∈Qh, we have
α⟨ˉq−ˉqh,ϕh⟩Γ+⟨ϕh,∂(ˉz−ˉzh)∂n⟩Γ+γh⟨ϕh,ˉzh⟩Γ+⟨ˉzh|→n⋅→β|,ϕh⟩Γ−=0. | (5.6) |
Taking ϕh=P∂h(ˉq−ˉqh)=P∂hˉq−P∂hˉqh=P∂hˉq−ˉqh in the Eq (5.6) and splitting
P∂hˉq−ˉqh=(P∂hˉq−ˉq)+(ˉq−ˉqh), |
we obtain
α‖ˉq−ˉqh‖2L2(Γ)=α⟨ˉq−ˉqh,ˉq−ˉqh⟩≤α⟨ˉq−ˉqh,P∂hˉq−ˉq⟩ΓJ1+⟨P∂hˉq−ˉq,∂(ˉz−ˉzh)∂n⟩ΓJ2+γh⟨P∂hˉq−ˉq,ˉzh⟩ΓJ3+⟨P∂hˉq−ˉq,ˉzh|→n⋅→β|⟩Γ−J4+⟨ˉq−ˉqh,∂(ˉz−ˉzh)∂n⟩ΓJ5+γh⟨ˉq−ˉqh,ˉzh⟩ΓJ6+⟨ˉq−ˉqh,ˉzh|→n⋅→β|⟩Γ−J7=J1+J2+J3+J4+J5+J6+J7. | (5.7) |
Now, we shall estimate each term separately. Most terms can be estimated by using the estimate of the L2-projection. However, the term (ˉz−ˉzh) in J2 and J5 is not in the discrete space, so additional arguments are needed to treat these terms.
Estimate for J1: By the Cauchy-Schwarz inequality and using Lemma (5.4),
J1=α⟨ˉq−ˉqh,P∂hˉq−ˉq⟩Γ≤α‖ˉq−ˉqh‖L2(Γ)‖P∂hˉq−ˉq‖L2(Γ)≤C1h1/2|ˉq|H1/2(Γ)‖ˉq−ˉqh‖L2(Γ), |
where C1 depends on α.
Estimates for J3 and J6: Using Lemma (5.5) to estimate ‖ˉzh‖L2(Γ), the Cauchy-Schwarz inequality, Lemma (5.7) and the regularity of ˉy, then we have
J3=γh⟨P∂hˉq−ˉq,ˉzh⟩Γ≤γh‖P∂hˉq−ˉq‖L2(Γ)‖ˉzh‖L2(Γ).≤C3h−1h1/2|ˉq|H1/2(Γ)h3/2‖ˆy−ˉyh‖L2(Ω)≤C3h|ˉq|H1/2‖ˆy−ˉyh‖L2(Ω)≤C3h|q|H1/2(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+‖ˉy−ˉyh‖L2(Ω))≤C3h|q|H1/2(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Likewise,
J6=γh⟨ˉq−ˉqh,ˉzh⟩Γ≤γh‖ˉq−ˉqh‖L2(Γ)‖ˉzh‖L2(Γ)≤C6h1/2‖ˉq−ˉqh‖L2(Γ)‖ˆy−ˉyh‖L2(Ω)≤C6h1/2‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+‖ˉy−ˉyh‖L2(Ω))≤C6h1/2‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)), |
where C3 and C6 depend on γ.
Estimates for J4 and J7: By using the Cauchy-Schwarz inequality, Lemmas (5.5) and (5.7), we have
J4=⟨P∂hˉq−ˉq,ˉzh|→n⋅→β|⟩Γ−≤C4h1/2|ˉq|H1/2(Γ)‖β‖1/2L∞(Γ)‖ˉzh‖L2(Γ)≤C4h2|q|H1/2(Γ)‖β‖1/2L∞(Γ)‖ˆy−ˉyh‖L2(Ω)≤C4h2|ˉq|H1/2(Γ)‖β‖1/2L∞(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+‖ˉy−ˉyh‖L2(Ω))≤C4h2|ˉq|H1/2(Γ)‖β‖1/2L∞(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Likewise,
J7=⟨ˉq−ˉqh,ˉzh|→n⋅→β|⟩Γ−≤C7‖β‖1/2L∞(Γ)‖ˉq−ˉqh‖L2(Γ)‖ˉzh‖L2(Γ)≤C7‖β‖1/2L∞(Γ)‖ˉq−ˉqh‖L2(Γ)h3/2‖ˆy−ˉyh‖L2(Ω)≤C7h3/2‖β‖1/2L∞(Γ)‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+‖ˉy−ˉyh‖L2(Ω))≤C7h3/2‖β‖1/2L∞(Γ)‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Estimate for J5: By the Cauchy-Schwarz inequality,
J5=⟨ˉq−ˉqh,∂(ˉz−ˉzh)∂n⟩Γ≤‖ˉq−ˉqh‖L2(Γ)‖∂(ˉz−ˉzh)∂n‖L2(Γ). |
Let us define ˜zh∈Vh to be the SIPG solution to ˉz i.e. ah(χ,˜zh)=(ˆy−ˉy,χ), ∀χ∈Vh.
In particular, ah(χ,ˉz−˜zh)=0 by the Galerkin orthogonality. Thus, we continue as following,
⟨ˉq−ˉqh,∂(ˉz−ˉzh)∂n⟩Γ≤‖ˉq−ˉqh‖L2(Γ)(‖∂(ˉz−˜zh)∂n‖L2(Γ)⏟J51+‖∂(˜zh−ˉzh)∂n‖L2(Γ)⏟J52). |
J51:
By the triangle inequality, we have
‖∂(ˉz−˜zh)∂n‖L2(Γ)≤‖∂(ˉz−Phˉz)∂n‖L2(Γ)⏟J511+‖∂(Phˉz−˜zh)∂n‖L2(Γ)⏟J512. |
J511:
By the trace inequality, Theorem (2.2) and Lemma (5.2), we obtain
J511=‖∂(ˉz−Phˉz)∂n‖2L2(Γ)=∑e∈Γ‖∂(ˉz−Phˉz)∂n‖2L2(e)≤∑τ∈Th(Ch−1‖ˉz−Phˉz‖2H1(τ)+Ch‖ˉz−Phˉz‖2H2(τ))≤∑τ∈ThCh‖ˉz‖2H2(τ)=Ch‖ˉz‖2H2(Ω)≤Ch‖ˆy−ˉy‖2L2(Ω). |
Thus,
J511=‖∂(ˉz−Phˉz)∂n‖L2(Γ)≤Ch1/2‖ˆy−ˉy‖L2(Ω). |
J512:
Since (Phˉz−˜zh)∈Vh, we can apply the trace theorem for discrete function and by using the inverse inequality and Lemma (5.2), we obtain that
‖∂(Phˉz−˜zh)∂n‖L2(Γ)≤Ch−1/2‖Phˉz−˜zh‖H1(Ω)≤Ch−1/2|||Phˉz−˜zh|||≤Ch−1/2(|||Phˉz−ˉz|||+|||ˉz−˜zh|||)≤Ch−1/2h‖ˉz‖H2(Ω)≤Ch1/2‖ˆy−ˉy‖L2(Ω), |
where we have used Lemma (5.3) for k=1 by Theorem (2.2) and Lemma (5.2).
Thus,
‖∂(Phˉz−˜zh)∂n‖L2(Γ)≤Ch1/2‖ˆy−ˉy‖L2(Ω). |
Since J51=J511+J512, we obtain
J51=‖∂(ˉz−˜zh)∂n‖L2(Γ)≤Ch1/2‖ˆy−ˉy‖L2(Ω)≤Ch1/2(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)). |
J52:
Since we have
ah(χ,ˉzh)=(ˆy−ˉyh,χ),ah(χ,˜zh)=(ˆy−ˉy,χ), |
where ∀χ∈Vh. We obtain
ah(χ,˜zh−ˉzh)=(ˉyh−ˉy,χ),∀χ∈Vh. | (5.8) |
Now, let us define the following equation
−Δw−∇⋅(→βw)+cw=ˉyh−ˉyin Ωw=0on Γ. |
By using the Eq (5.8),
ah(χ,˜zh−ˉzh)=ah(χ,˜zh)−ah(χ,ˉzh)=(ˆy−ˉy,χ)−(ˆy−ˉyh,χ)=(ˉyh−ˉy,χ)=ah(χ,wh). |
The above equality shows that wh=˜zh−ˉzh.
Now, using the inverse inequality and the fact that w=0 on Γ, we obtain
‖∂(˜zh−ˉzh)∂n‖L2(Γ)≤Ch−1‖˜zh−ˉzh‖L2(Γ)=Ch−1‖˜zh−ˉzh−w‖L2(Γ)≤Ch−1h1/2|||(˜zh−ˉzh)−w|||≤Ch−1/2|||wh−w|||≤Ch−1/2h‖w‖H2(Ω)≤Ch1/2‖ˉyh−ˉy‖L2(Ω)≤Ch1/2(h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)), |
where we have used Theorem (2.2) and Lemma (5.3) for k=1 by Lemmas (5.2) and (5.7) in the last step.
Thus,
J52=‖∂(˜zh−ˉzh)∂n‖L2(Γ)≤Ch1/2(h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Finally, we obtain
J5≤‖ˉq−ˉqh‖L2(Γ)(J51+J52)≤C5h1/2‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Estimate for J2: By using the the estimation of ‖∂(ˉz−ˉzh)∂n‖L2(Γ) in J5, Cauchy-Schwarz inequality and Lemma (5.4), we have
J2=⟨P∂hˉq−ˉq,∂(ˉz−ˉzh)∂n⟩Γ≤‖P∂hˉq−ˉq‖L2(Γ)‖∂(ˉz−ˉzh)∂n‖L2(Γ)≤C2h1/2|ˉq|H1/2(Γ)‖∂(ˉz−ˉzh)∂n‖L2(Γ)≤C2h1/2|ˉq|H1/2(Γ)h1/2(‖ˆy‖L(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))=C2h|ˉq|H1/2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Thus,
J2≤C2h|q|H1/2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
After using Lemma (5.7) to estimate ‖ˉy−ˉyh‖L2(Ω) and combining J1,J2,J3,J4,J5,J6,J7 in the Eq (5.7), we obtain
α‖ˉq−ˉqh‖2L2(Ω)≤J1+J2+J3+J4+J5+J6+J7≤C1h12|ˉq|H1/2(Γ)‖ˉq−ˉqh‖L2(Γ)+C2h|ˉq|H1/2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))+C3h|ˉq|H1/2(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))+C4h2|ˉq|H1/2(Γ)‖β‖12L∞(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))+C5h12‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖H1(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))+C6h12‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖H1(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))+C7h32‖β‖12L∞(Γ)‖ˉq−ˉqh‖L2(Γ)(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω)). |
Notice that we can rewrite the above inequality as
α‖ˉq−ˉqh‖2L2(Γ)≤CIh|ˉq|2H1/2(Γ)+α4‖ˉq−ˉqh‖2L2(Γ)+CIIh(‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)+h1/2‖ˉq−ˉqh‖L2(Γ)+h‖ˉy‖H1(Ω))2+α4‖ˉq−ˉqh‖2L2(Γ)+CIIIh‖ˉq−ˉqh‖2L2(Γ). |
After all simplification, we obtain
α‖ˉq−ˉqh‖2L2(Γ)≤Ch(|ˉq|H1/2(Γ)+‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω))2+C′h‖ˉq−ˉqh‖2L2(Γ), |
where h is sufficiently small such that C′h≤α2 to absorb C′h‖ˉq−ˉqh‖2L2(Γ) to the left hand side. Thus, we conclude that there exists a positive constant C such that
‖ˉq−ˉqh‖L2(Γ)≤Ch1/2(|ˉq|H1/2(Γ)+‖ˆy‖L2(Ω)+‖ˉy‖H1(Ω)), |
provided h is sufficiently small.
In this section, we show the features of the method and some numerical examples to support our theoretical results by the method described for the main problem (1.1), (1.2a) and (1.2b). Here, we present numerical results depending on different kinds of domain as the following.
Since the domain is one dimensional and the boundary is consisting of two points, there is no regularity limitation due to geometry restriction. Thus, we do not expect an optimal convergence rate, but we observe that the method is still stable and convergent in Tables 1–3 and Figures 3–4.
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 1.959 | 1.002 | 2.007 | 1.965 |
2.50e-01 | 1.979 | 1.001 | 2.006 | 1.982 |
1.25e-01 | 1.990 | 1.001 | 2.004 | 1.991 |
6.25e-02 | 1.995 | 1.000 | 2.002 | 1.996 |
3.12e-02 | 1.997 | 1.001 | 2.001 | 1.998 |
1.56e-03 | 1.999 | 1.000 | 2.001 | 1.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 2.999 | 2.013 | 2.025 | 2.982 |
2.50e-01 | 2.999 | 2.007 | 2.683 | 2.991 |
1.25e-01 | 3.000 | 2.004 | 2.864 | 2.996 |
6.25e-02 | 3.000 | 2.002 | 2.937 | 2.998 |
3.12e-02 | 2.998 | 2.001 | 2.969 | 2.999 |
1.56e-03 | 1.938 | 2.001 | 2.985 | 2.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 4.436 | 2.436 | 3.970 | 3.866 |
2.50e-01 | 4.425 | 3.423 | 3.985 | 3.983 |
1.25e-01 | 4.380 | 3.385 | 3.992 | 3.991 |
6.25e-02 | 1.188 | 3.320 | 3.996 | 3.996 |
3.12e-02 | -0.777 | 3.223 | 3.998 | 3.998 |
1.56e-03 | -1.119 | 1.268 | 3.999 | 3.999 |
By setting Ω=[0,1], ϵ=1, α=1, →β=[1], ˉq=(1−x)2(x2), c=0, ˉy=x4−ex−1ϵ−e−1ϵ1−e−1ϵ, and ˉz=αϵ(1−x)2x2.
By setting the problem as the following,
Ω=[0,1]×[0,1], →β=[1;1], c=1,α=1, ˉq=−1ϵ(x(1−x)+y(1−y)),ˉy=−1ϵ(x(1−x)+y(1−y)), ˉz=αϵ(xy(1−x)(1−y)). |
Here, we consider piecewise linear continuous functions to approximate the optimal control.
The first order conditions allow us deduce the regularity results of the optimal control and so the expected convergence rate has agreed well with the rate in [6] as ‖ˉq−ˉqh‖L2(Γ)≤Ch by the square domain with the largest interior angle wmax=π2.
Lemma (5.7) and ‖ˉq−ˉqh‖L2(Γ)≤Ch yield ‖ˉy−ˉyh‖L2(Ω)≤Ch3/2. Since the power of h on the right-hand side drops for one for each derivative of the error (ˉy−ˉyh), ‖ˉy−ˉyh‖H1(Ω)≤Ch1/2 by Lemma (5.2). Likewise, From Lemma (5.2) and z∈H2, ‖ˉz−ˉzh‖L2(Ω)≤Ch2, and so ‖ˉz−ˉzh‖H1(Ω)≤Ch as our expected convergence rates indicated in Tables 4 and 5. Also, the expected rates have agreed well with the rates for the different densities of the meshes in [6]. Also, we can see the stability of the method in Figure 5.
h | ‖ˉy−ˉyh‖L2 | ‖ˉy−ˉyh‖H1 | ‖ˉq−ˉqh‖L2 | ‖ˉz−ˉzh‖L2 | ‖ˉz−ˉzh‖H1 |
5.00e-01 | 1.92e-01 | 3.91e+00 | 1.07e+00 | 4.31e-02 | 9.19e-01 |
2.50e-01 | 8.44e-02 | 2.25e+00 | 4.86e-01 | 1.38e-02 | 5.06e-01 |
1.25e-01 | 3.14e-02 | 1.27e+00 | 2.29e-01 | 4.21e-03 | 2.62e-01 |
6.25e-02 | 1.10e-02 | 7.33e-01 | 1.09e-01 | 1.22e-03 | 1.32e-01 |
3.12e-02 | 3.80e-03 | 4.49e-01 | 5.20e-02 | 3.32e-04 | 6.66e-02 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.19 | 0.80 | 1.13 | 1.64 | 0.86 |
1.25e-01 | 1.43 | 0.83 | 1.08 | 1.72 | 0.95 |
6.25e-02 | 1.51 | 0.79 | 1.08 | 1.79 | 0.98 |
3.12e-02 | 1.53 | 0.71 | 1.06 | 1.87 | 0.99 |
expected | 1.50 | 0.50 | 1.00 | 2.00 | 1.00 |
Since ϵ is too small for this case such as ϵ=10−5, h|→β|ϵ>1 which means the advection-diffusion dominated case occurs. The norm of y depends on ϵ such that ‖ˉy‖Hk+1(Ω)≤Cϵk+1/2. Since the convergence rate of ˉq depends on data of ˉy from the main result, we do not expect any convergence rate and so this case does not contradict with our main result. Also, the feature of the method shows itself that Dirichlet boundary condition is almost ignored by the method as a result of weak treatment and it does not resolve the layers and causes oscillations on the boundary. It can be seen in Figure 6 and Tables 6 and 7 that some oscillatory solutions and non-convergent rate of q appear on the inflow boundary, caused by non-stabilized terms of boundary edges E∂h represented by E−h in the bilinear form (4.6) and (4.5), whereas it is stable on both the interior edges E0h and the stabilized boundary edges E∂h by the penalty term in the form.
h | ‖ˉy−ˉyh‖L2 | ‖ˉy−ˉyh‖H1 | ‖ˉq−ˉqh‖L2 | ‖ˉz−ˉzh‖L2 | ‖ˉz−ˉzh‖H1 |
5.00e-01 | 4.29e+00 | 2.68e+01 | 8.15e+00 | 5.66e+01 | 9.52e+02 |
2.50e-01 | 7.69e-01 | 1.32e+01 | 2.22e+00 | 1.51e+01 | 5.15e+02 |
1.25e-01 | 4.72e-01 | 1.58e+01 | 9.70e-01 | 3.85e+00 | 2.63e+02 |
6.25e-02 | 3.78e-01 | 2.36e+01 | 6.66e-01 | 9.64e-01 | 1.32e+02 |
3.12e-02 | 2.55e-01 | 2.88e+01 | 6.37e-01 | 2.40e-01 | 6.62e+01 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 2.48 | 1.02 | 1.87 | 1.91 | 0.89 |
1.25e-01 | 0.71 | -0.26 | 1.20 | 1.97 | 0.97 |
6.25e-02 | 0.32 | -0.58 | 0.54 | 2.00 | 0.99 |
3.12e-02 | 0.57 | -0.28 | 0.06 | 2.01 | 1.00 |
By a transformation from the unit square domain to obtain a diamond shaped domain Ω with π4, π8 and π10 angles, while the angle of the domain is getting smaller, we expect that the error rate is getting close to the predicted optimal error rate.
After the transformation from the unit square domain to obtain a diamond shaped domain Ω with π4, π8 and π10 angles, we can observe from tables 8–10 that the regularity of the state is reducing sharply close to 1 and that we will obtain the predicted rate i.e., ‖ˉq−ˉqh‖L2(Γ)≤Ch1/2 yields ‖ˉy−ˉyh‖L2(Ω)≤Ch1 by Theorem (5.7). There are many researches, see [6,31,46], which obtained an error estimate for the optimal control of order depends on the largest angle of the boundary polygon. Also, we can see the stable behavior of the method in Figures 7–9.
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.51 | 0.80 | 0.65 | 1.43 | 1.78 |
1.25e-01 | 1.47 | 0.84 | 0.96 | 1.75 | 1.91 |
6.25e-02 | 1.69 | 0.85 | 1.05 | 1.89 | 1.96 |
3.12e-02 | 1.75 | 0.81 | 1.05 | 1.95 | 1.98 |
1.56e-02 | 1.73 | 0.74 | 1.03 | 1.97 | 1.99 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.75 | 0.72 | 0.32 | 1.11 | 0.76 |
1.25e-01 | 1.16 | 0.41 | 0.72 | 1.63 | 0.95 |
6.25e-02 | 1.60 | 0.50 | 0.97 | 1.88 | 0.99 |
3.12e-02 | 1.70 | 0.55 | 1.01 | 1.96 | 1.00 |
1.56e-02 | 1.66 | 0.53 | 1.02 | 1.99 | 1.00 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 0.85 | 0.17 | 0.17 | 1.03 | 0.61 |
1.25e-01 | 0.92 | 0.17 | 1.59 | 1.60 | 1.04 |
6.25e-02 | 1.32 | 0.26 | 0.90 | 1.89 | 1.14 |
3.12e-02 | 1.50 | 0.42 | 1.00 | 1.98 | 1.10 |
1.56e-02 | 1.55 | 0.50 | 1.02 | 2.00 | 1.05 |
While the method still works, likewise the frame in the unit square domain, it can be seen in Figure 10 and Table 11 that some oscillatory solutions and non-convergent rate of q appear on the inflow boundary whereas it is stable on the interior edges and the stabilized boundary edges as a result of weak treatment because of not resolving the layers and causing oscillations on the boundary.
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 3.35 | 2.45 | 3.36 | 2.87 | 1.89 |
1.25e-01 | 0.31 | 0.23 | 1.41 | 2.96 | 1.97 |
6.25e-02 | -0.01 | -0.64 | 0.81 | 2.97 | 1.99 |
3.12e-02 | 0.01 | -0.68 | 0.45 | 2.45 | 2.00 |
In this paper, we consider Dirichlet boundary optimal control problem governed by the advection-diffusion equation and apply the DG methods to the problem. We show some attractive features of the method such as the stable behavior of the SIPG method into the domain of the smoothness and for the advection dominated case except on the boundary as a result of the boundary weak treatments. We have proven that the convergence rate for the SIPG method is optimal in the interior of the general convex domain. However, all convergence rates in numerical examples are higher than predicted by the main result because the predicted order exists for general convex domain, but obtaining the predicted optimal convergence rate depends on the maximal angle of the domain because of the regularity [6,36,47], which is an interesting topic for future work. Also, for general polygonal domains and Laplace equations it has been shown [6] that
‖ˉq−ˉqh‖L2(Γ)≤Ch1−1p, |
where p>2 depends on the largest angle, and obtaining optimal convergence rates for the p=2 case is another interesting topic for future work.
I would like to thank to Prof. Dmitriy Leykekhman, my thesis advisor, for helpful discussions and his advisement on my academic journey.
The author declares no conflict of interest.
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1. | Divay Garg, Kamana Porwal, Unified discontinuous Galerkin finite element methods for second order Dirichlet boundary control problem, 2023, 185, 01689274, 336, 10.1016/j.apnum.2022.12.001 | |
2. | Kumar Rajeev Ranjan, S. Gowrisankar, Error analysis of discontinuous Galerkin methods on layer adapted meshes for two dimensional turning point problem, 2024, 70, 1598-5865, 2453, 10.1007/s12190-024-02054-y |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 1.959 | 1.002 | 2.007 | 1.965 |
2.50e-01 | 1.979 | 1.001 | 2.006 | 1.982 |
1.25e-01 | 1.990 | 1.001 | 2.004 | 1.991 |
6.25e-02 | 1.995 | 1.000 | 2.002 | 1.996 |
3.12e-02 | 1.997 | 1.001 | 2.001 | 1.998 |
1.56e-03 | 1.999 | 1.000 | 2.001 | 1.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 2.999 | 2.013 | 2.025 | 2.982 |
2.50e-01 | 2.999 | 2.007 | 2.683 | 2.991 |
1.25e-01 | 3.000 | 2.004 | 2.864 | 2.996 |
6.25e-02 | 3.000 | 2.002 | 2.937 | 2.998 |
3.12e-02 | 2.998 | 2.001 | 2.969 | 2.999 |
1.56e-03 | 1.938 | 2.001 | 2.985 | 2.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 4.436 | 2.436 | 3.970 | 3.866 |
2.50e-01 | 4.425 | 3.423 | 3.985 | 3.983 |
1.25e-01 | 4.380 | 3.385 | 3.992 | 3.991 |
6.25e-02 | 1.188 | 3.320 | 3.996 | 3.996 |
3.12e-02 | -0.777 | 3.223 | 3.998 | 3.998 |
1.56e-03 | -1.119 | 1.268 | 3.999 | 3.999 |
h | ‖ˉy−ˉyh‖L2 | ‖ˉy−ˉyh‖H1 | ‖ˉq−ˉqh‖L2 | ‖ˉz−ˉzh‖L2 | ‖ˉz−ˉzh‖H1 |
5.00e-01 | 1.92e-01 | 3.91e+00 | 1.07e+00 | 4.31e-02 | 9.19e-01 |
2.50e-01 | 8.44e-02 | 2.25e+00 | 4.86e-01 | 1.38e-02 | 5.06e-01 |
1.25e-01 | 3.14e-02 | 1.27e+00 | 2.29e-01 | 4.21e-03 | 2.62e-01 |
6.25e-02 | 1.10e-02 | 7.33e-01 | 1.09e-01 | 1.22e-03 | 1.32e-01 |
3.12e-02 | 3.80e-03 | 4.49e-01 | 5.20e-02 | 3.32e-04 | 6.66e-02 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.19 | 0.80 | 1.13 | 1.64 | 0.86 |
1.25e-01 | 1.43 | 0.83 | 1.08 | 1.72 | 0.95 |
6.25e-02 | 1.51 | 0.79 | 1.08 | 1.79 | 0.98 |
3.12e-02 | 1.53 | 0.71 | 1.06 | 1.87 | 0.99 |
expected | 1.50 | 0.50 | 1.00 | 2.00 | 1.00 |
h | ‖ˉy−ˉyh‖L2 | ‖ˉy−ˉyh‖H1 | ‖ˉq−ˉqh‖L2 | ‖ˉz−ˉzh‖L2 | ‖ˉz−ˉzh‖H1 |
5.00e-01 | 4.29e+00 | 2.68e+01 | 8.15e+00 | 5.66e+01 | 9.52e+02 |
2.50e-01 | 7.69e-01 | 1.32e+01 | 2.22e+00 | 1.51e+01 | 5.15e+02 |
1.25e-01 | 4.72e-01 | 1.58e+01 | 9.70e-01 | 3.85e+00 | 2.63e+02 |
6.25e-02 | 3.78e-01 | 2.36e+01 | 6.66e-01 | 9.64e-01 | 1.32e+02 |
3.12e-02 | 2.55e-01 | 2.88e+01 | 6.37e-01 | 2.40e-01 | 6.62e+01 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 2.48 | 1.02 | 1.87 | 1.91 | 0.89 |
1.25e-01 | 0.71 | -0.26 | 1.20 | 1.97 | 0.97 |
6.25e-02 | 0.32 | -0.58 | 0.54 | 2.00 | 0.99 |
3.12e-02 | 0.57 | -0.28 | 0.06 | 2.01 | 1.00 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.51 | 0.80 | 0.65 | 1.43 | 1.78 |
1.25e-01 | 1.47 | 0.84 | 0.96 | 1.75 | 1.91 |
6.25e-02 | 1.69 | 0.85 | 1.05 | 1.89 | 1.96 |
3.12e-02 | 1.75 | 0.81 | 1.05 | 1.95 | 1.98 |
1.56e-02 | 1.73 | 0.74 | 1.03 | 1.97 | 1.99 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.75 | 0.72 | 0.32 | 1.11 | 0.76 |
1.25e-01 | 1.16 | 0.41 | 0.72 | 1.63 | 0.95 |
6.25e-02 | 1.60 | 0.50 | 0.97 | 1.88 | 0.99 |
3.12e-02 | 1.70 | 0.55 | 1.01 | 1.96 | 1.00 |
1.56e-02 | 1.66 | 0.53 | 1.02 | 1.99 | 1.00 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 0.85 | 0.17 | 0.17 | 1.03 | 0.61 |
1.25e-01 | 0.92 | 0.17 | 1.59 | 1.60 | 1.04 |
6.25e-02 | 1.32 | 0.26 | 0.90 | 1.89 | 1.14 |
3.12e-02 | 1.50 | 0.42 | 1.00 | 1.98 | 1.10 |
1.56e-02 | 1.55 | 0.50 | 1.02 | 2.00 | 1.05 |
h | L2−yrate | H1−yrate | L2−qrate | L2−zrate | H1−zrate |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 3.35 | 2.45 | 3.36 | 2.87 | 1.89 |
1.25e-01 | 0.31 | 0.23 | 1.41 | 2.96 | 1.97 |
6.25e-02 | -0.01 | -0.64 | 0.81 | 2.97 | 1.99 |
3.12e-02 | 0.01 | -0.68 | 0.45 | 2.45 | 2.00 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 1.959 | 1.002 | 2.007 | 1.965 |
2.50e-01 | 1.979 | 1.001 | 2.006 | 1.982 |
1.25e-01 | 1.990 | 1.001 | 2.004 | 1.991 |
6.25e-02 | 1.995 | 1.000 | 2.002 | 1.996 |
3.12e-02 | 1.997 | 1.001 | 2.001 | 1.998 |
1.56e-03 | 1.999 | 1.000 | 2.001 | 1.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 2.999 | 2.013 | 2.025 | 2.982 |
2.50e-01 | 2.999 | 2.007 | 2.683 | 2.991 |
1.25e-01 | 3.000 | 2.004 | 2.864 | 2.996 |
6.25e-02 | 3.000 | 2.002 | 2.937 | 2.998 |
3.12e-02 | 2.998 | 2.001 | 2.969 | 2.999 |
1.56e-03 | 1.938 | 2.001 | 2.985 | 2.999 |
h | L2−yrate | H1−yrate | Left−qrate | Right−qrate |
5.00e-01 | 4.436 | 2.436 | 3.970 | 3.866 |
2.50e-01 | 4.425 | 3.423 | 3.985 | 3.983 |
1.25e-01 | 4.380 | 3.385 | 3.992 | 3.991 |
6.25e-02 | 1.188 | 3.320 | 3.996 | 3.996 |
3.12e-02 | -0.777 | 3.223 | 3.998 | 3.998 |
1.56e-03 | -1.119 | 1.268 | 3.999 | 3.999 |
h | ‖ˉy−ˉyh‖L2 | ‖ˉy−ˉyh‖H1 | |||
5.00e-01 | 1.92e-01 | 3.91e+00 | 1.07e+00 | 4.31e-02 | 9.19e-01 |
2.50e-01 | 8.44e-02 | 2.25e+00 | 4.86e-01 | 1.38e-02 | 5.06e-01 |
1.25e-01 | 3.14e-02 | 1.27e+00 | 2.29e-01 | 4.21e-03 | 2.62e-01 |
6.25e-02 | 1.10e-02 | 7.33e-01 | 1.09e-01 | 1.22e-03 | 1.32e-01 |
3.12e-02 | 3.80e-03 | 4.49e-01 | 5.20e-02 | 3.32e-04 | 6.66e-02 |
h | |||||
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.19 | 0.80 | 1.13 | 1.64 | 0.86 |
1.25e-01 | 1.43 | 0.83 | 1.08 | 1.72 | 0.95 |
6.25e-02 | 1.51 | 0.79 | 1.08 | 1.79 | 0.98 |
3.12e-02 | 1.53 | 0.71 | 1.06 | 1.87 | 0.99 |
expected | 1.50 | 0.50 | 1.00 | 2.00 | 1.00 |
h | |||||
5.00e-01 | 4.29e+00 | 2.68e+01 | 8.15e+00 | 5.66e+01 | 9.52e+02 |
2.50e-01 | 7.69e-01 | 1.32e+01 | 2.22e+00 | 1.51e+01 | 5.15e+02 |
1.25e-01 | 4.72e-01 | 1.58e+01 | 9.70e-01 | 3.85e+00 | 2.63e+02 |
6.25e-02 | 3.78e-01 | 2.36e+01 | 6.66e-01 | 9.64e-01 | 1.32e+02 |
3.12e-02 | 2.55e-01 | 2.88e+01 | 6.37e-01 | 2.40e-01 | 6.62e+01 |
h | |||||
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 2.48 | 1.02 | 1.87 | 1.91 | 0.89 |
1.25e-01 | 0.71 | -0.26 | 1.20 | 1.97 | 0.97 |
6.25e-02 | 0.32 | -0.58 | 0.54 | 2.00 | 0.99 |
3.12e-02 | 0.57 | -0.28 | 0.06 | 2.01 | 1.00 |
h | |||||
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.51 | 0.80 | 0.65 | 1.43 | 1.78 |
1.25e-01 | 1.47 | 0.84 | 0.96 | 1.75 | 1.91 |
6.25e-02 | 1.69 | 0.85 | 1.05 | 1.89 | 1.96 |
3.12e-02 | 1.75 | 0.81 | 1.05 | 1.95 | 1.98 |
1.56e-02 | 1.73 | 0.74 | 1.03 | 1.97 | 1.99 |
h | |||||
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 1.75 | 0.72 | 0.32 | 1.11 | 0.76 |
1.25e-01 | 1.16 | 0.41 | 0.72 | 1.63 | 0.95 |
6.25e-02 | 1.60 | 0.50 | 0.97 | 1.88 | 0.99 |
3.12e-02 | 1.70 | 0.55 | 1.01 | 1.96 | 1.00 |
1.56e-02 | 1.66 | 0.53 | 1.02 | 1.99 | 1.00 |
h | |||||
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 0.85 | 0.17 | 0.17 | 1.03 | 0.61 |
1.25e-01 | 0.92 | 0.17 | 1.59 | 1.60 | 1.04 |
6.25e-02 | 1.32 | 0.26 | 0.90 | 1.89 | 1.14 |
3.12e-02 | 1.50 | 0.42 | 1.00 | 1.98 | 1.10 |
1.56e-02 | 1.55 | 0.50 | 1.02 | 2.00 | 1.05 |
5.00e-01 | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
2.50e-01 | 3.35 | 2.45 | 3.36 | 2.87 | 1.89 |
1.25e-01 | 0.31 | 0.23 | 1.41 | 2.96 | 1.97 |
6.25e-02 | -0.01 | -0.64 | 0.81 | 2.97 | 1.99 |
3.12e-02 | 0.01 | -0.68 | 0.45 | 2.45 | 2.00 |