On finding the surface admittance of an obstacle via the time domain enclosure method
Masaru Ikehata

TL;DR
This paper presents a method to determine the surface admittance and curvature of an unknown obstacle in electromagnetic scattering problems using time domain data from a single wave measurement.
Contribution
It introduces a novel approach to extract surface admittance and curvature information from finite time electromagnetic data using the enclosure method.
Findings
Surface admittance can be identified from observed data.
Curvature information at the closest surface points can be extracted.
A single wave measurement provides significant surface information.
Abstract
An inverse obstacle scattering problem for the electromagnetic wave governed by the Maxwell system over a finite time interval is considered. It is assumed that the wave satisfies the Leontovich boundary condition on the surface of an unknown obstacle. The condition is described by using an unknown positive function on the surface of the obstacle which is called the surface admittance. The wave is generated at the initial time by a volumetric current source supported on a very small ball placed outside the obstacle and only the electric component of the wave is observed on the same ball over a finite time interval. It is shown that from the observed data one can extract information about the value of the surface admittance and the curvatures at the points on the surface nearest to the center of the ball. This shows that a single shot contains a meaningful information about the…
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On finding the surface admittance of an obstacle via the time domain enclosure method
Masaru IKEHATA111 Laboratory of Mathematics, Graduate School of Engineering, Hiroshima University, Higashihiroshima 739-8527, JAPAN
Abstract
An inverse obstacle scattering problem for the electromagnetic wave governed by the Maxwell system over a finite time interval is considered. It is assumed that the wave satisfies the Leontovich boundary condition on the surface of an unknown obstacle. The condition is described by using an unknown positive function on the surface of the obstacle which is called the surface admittance. The wave is generated at the initial time by a volumetric current source supported on a very small ball placed outside the obstacle and only the electric component of the wave is observed on the same ball over a finite time interval. It is shown that from the observed data one can extract information about the value of the surface admittance and the curvatures at the points on the surface nearest to the center of the ball. This shows that a single shot contains a meaningful information about the quantitative state of the surface of the obstacle.
AMS: 35R30, 35L50, 35Q61, 78A46, 78M35
KEY WORDS: enclosure method, inverse obstacle scattering problem, electromagnetic wave, obstacle, Maxwell’s equations, surface admittance, Leontovich boundary condition
1 Introduction and statement of the results
In this paper, we pursue further the possibility of the time domain enclosure method [10] for the Maxwell system developed in [11, 12]. We consider an inverse obstacle scattering problem for the wave governed by the Maxwell system in the time domain, in particular, over a finite time interval unlike the time harmonic reduced case, see [5, 15, 18].
Let us formulate the problem more precisely. We denote by the unknown obstacle. We assume that is a non empty bounded open set of with -boundary such that is connected.
We assume that the electric field \mbox{\boldmathE}=\mbox{\boldmathE}(x,t) and magnetic field \mbox{\boldmathH}=\mbox{\boldmathH}(x,t) are generated only by the current density \mbox{\boldmathJ}=\mbox{\boldmathJ}(x,t) at the initial time located not far a way from the unknown obstacle. There should be several choices of current density as a model of antenna [2, 4]. In this paper, as considered in [11, 12] we assume that takes the form
[TABLE]
where is an arbitrary unit vector; is a (very small) open ball satisfying and denotes the characteristic function of ; with .
Let . In this paper, we assume that
Assumption 1.
(i) the pair (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t))\equiv(\mbox{\boldmathE}(\,\cdot\,,t),\mbox{\boldmathH}(\,\cdot\,,t)) belongs to as a function of ;
(ii) for each , the pair (\nabla\times\mbox{\boldmathE}(t),\nabla\times\mbox{\boldmathH}(t)) belongs to ;
(iii) it holds that
[TABLE]
(iv) for each , (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t)) satisfies, in the sense of trace [14]
[TABLE]
where and satisfies .
Note that denotes the unit outward normal to . The obstacle is embedded in a medium like air (free space) which has constant electric permittivity and magnetic permeability . The boundary condition (1.3) is called the Leontovich boundary condition ([1, 5, 15, 18]) and see also [16] for the case when is constant. The quantity is called the surface impedance, see [1] and thus is called the admittance. In what follows we use these equivalent forms without mentioning explicitly. The existence of the admittance causes the loss of the energy of the solution on the surface of the obstacle after stopping of the source supply.
In [14] it is stated that the existence of (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t)) satisfying (i)-(iv) can be derived from the theory of contraction semigroups [20]. However, therein the detailed proof is not given as pointed out in [12]. To make the logical relation clear, here we assume that our pair (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t)) satisfies (i)-(iv). This is our starting assumption. It should be pointed out that Assumption () in [12] implies the existence of such (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t)) which ensures that conditions (i)-(iv) has a sense.
We consider the following problem.
Problem. Fix a large (to be determined later) . Observe \mbox{\boldmathE}(t) on over the time interval . Extract information about the geometry of and the values of on from the observed data.
First of all let us recall the previous reslult on this problem. Denote the solution of the system (1.2) in the case when by (\mbox{\boldmathE}_{0}(t),\mbox{\boldmathH}_{0}(t)) with given by (1.1). Note that in this case, the solvabilty has been ensured by applying theory of contraction semigroups [20].
Define the indicator function
[TABLE]
where
[TABLE]
and
[TABLE]
And also, to describe another assumtion, we introduce here
[TABLE]
Using the same argument as that of [12] under Assumption 1, we know the following fatcts.
The pair (\mbox{\boldmathW}_{e},\mbox{\boldmathW}_{m}) belongs to with (\nabla\times\mbox{\boldmathW}_{e},\nabla\times\mbox{\boldmathW}_{m})\in L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3}\times L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3}.
We have
[TABLE]
The boundary condition (1.3) remains valid in the sense of the trace [14] as mentioned above if (\mbox{\boldmathE}(t),\mbox{\boldmathH}(t)) is replaced with (\mbox{\boldmathW}_{e},\mbox{\boldmathW}_{m}).
It holds that
[TABLE]
Note that, at this stage, each term on (1.3) does not have a point-wise meaning. What we know is: the left-hand side on (1.3) just belongs to the dual space of . In this paper, we introduce another assumption which states a regularity up to boundary.
Assumption 2. The functions \mbox{\boldmathW}_{e} and \mbox{\boldmathW}_{m} above belong to on the intersection of an open neighbourhhod of in with .
This assumption makes us possible to treate vector-valued functions appeared in a dual paring pointwise. Note that Assumption 2 is a special version of Assumption () introduced in [12] by virtue of (1.6). However, for our purpose, it suffices to assume Assumption 2 instead of Assumption (). We believe that Assumption 2 should be removed.
Now, by Assumption 2, we have that both \mbox{\boldmathW}_{e} and \mbox{\boldmathW}_{m} belong to in the intersection of an open neighbourhood of with . Then, we see that the boundary condition (1.3) is satisfied in the sense of the usual trace in :
[TABLE]
Note that this is equivalent to
[TABLE]
Moreover, note also that: since \mbox{\boldmathW}_{m}\in L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3} satifies \nabla\times\mbox{\boldmathW}_{m}\in L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3}, from the first equation on (1.6) and by applying Corollary 1.1 on page 212 and Remark 2 on page 213 in [6] one can conclude that \mbox{\boldmathW}_{m}\in H^{1}({\rm\bf R}^{3}\setminus\overline{D})^{3}.
Set
[TABLE]
As done in [11], we introduce two conditions (A.I) and (A.II) on listed below:
(A.I) for all ;
(A.II) for all .
Roughly speaking, we can say that: the condition (A.I)/(A.II) means that the admittance is greater/less than the special value which is the admittance of free space [1].
Define .
Under assumptions 1-2 we have already known that the following statement is true.
Theorem 1.1([12]).* Let \mbox{\boldmatha}_{j}, be two linearly independent unit vectors. Let \mbox{\boldmathJ}_{j}(x,t)=f(t)\chi_{B}(x)\mbox{\boldmatha}_{j} and satisfy*
[TABLE]
Then, we have:
[TABLE]
Moreover, if satisfies (A.I) or (A.II), then for all
[TABLE]
Remark 1.1. As described in Theorem 1.2 in [12], all the statements of Theorem 1.1 are valid if \mbox{\boldmathV}_{e} in I_{\mbox{\boldmathJ}}(\tau,T) is replaced with the unique weak solution \mbox{\boldmathV}\in L^{2}({\rm\bf R}^{3})^{3} with \nabla\times\mbox{\boldmathV}\in L^{2}({\rm\bf R}^{3})^{3} of
[TABLE]
In what follows, we denote by \mbox{\boldmathV}_{e}^{0} the weak solution. Roughly speaking, the reason why such a replacement is possible is the following. Introduce another indicator function by the formula
[TABLE]
Using the simple facts
[TABLE]
and
[TABLE]
one has
[TABLE]
Thus, one can transplant all the results in Theorem 1.1 into the case when the indicator function is given by (1.10). This version’s advantage is: no need of time domain computation of \mbox{\boldmathE}_{0} in \mbox{\boldmathV}_{e}.
Remark 1.2. From Theorem 1.1. one can obtain another formula which has a similarity to the original version of the enclosure method developed in [8]. See (15) in [12].
The main purpose of this paper is to go further beyond Theorem 1.1 under Assumptions 1 and 2. Especially, we consider how to extract quantitative information about the state of the surafce of an unknown obstacle using the time domain enclosure method. For the purpose, we clarify the leading profile of the indicator functions (1.4) or (1.10) as .
In what follows, we denote by the open ball centered at with radius . Set and . To describe the formula, we recall some notion in differential geometry. Let . Let and denote the shape operators (or Weingarten maps) at of and with respect to and , respectively (see [19] for the notion of the shape operator). Because attains the minimum of the function: , we have always as the quadratic form on the common tangent space at .
Now we are ready to state the main result in this paper.
Theorem 1.2.* Assume that is and . Assume that satisfies (A1) or (A2). Let satisfy (1.8) and . Assume that the set consists of finite points and*
[TABLE]
And also assume that \mbox{\boldmath\nu}_{q}\times\mbox{\boldmatha}\not=\mbox{\boldmath0} for some . Then, we have
[TABLE]
where
[TABLE]
and
[TABLE]
Note that |\mbox{\boldmath\nu}_{q}\times(\mbox{\boldmatha}\times\mbox{\boldmath\nu}_{q})|^{2}=|\mbox{\boldmath\nu}_{q}\times\mbox{\boldmatha}|^{2}=1-(\mbox{\boldmath\nu}_{q}\cdot\mbox{\boldmatha})^{2}.
Once we have the formula (1.13), as done in [13] for the scalar wave equation case, we immediately obtain the following corollary. To indicate the dependence of the indicator function on the surface admittance we write
[TABLE]
Corollary 1.1.* Assume that is . Let and belong to and satisfy (A1) or (A2). Let satisfy (1.8) and . Assume that the set consists of finite points and satisfies (1.12). And also assume that \mbox{\boldmath\nu}_{q}\times\mbox{\boldmatha}\not=\mbox{\boldmath0} for some . Then, we have*
[TABLE]
and its lower and upper estimates:
[TABLE]
In particulr, if consists of a single point , we have
[TABLE]
Estimates (1.14) and formula (1.15) are remarkable since they do not require information about the curvatures of the surface of the obstacle in advance. Note that if we know a point , then, all the intermediate points on the segment connecting and , satisfy and . Thus, one gets immediately the following corollary in which the set can be an infinite one, even, continuum.
Corollary 1.2.* Assume that is . Let and belong to and satisfy (A1) or (A2). Le be an arbitrary point in and . Let be an arbitrary point on the open segment and an open ball centered at satisfying . Let satisfy (1.8) and . Let \mbox{\boldmathJ}^{\prime} be the given by (1.1) in which is replaced with . And also assume that \mbox{\boldmath\nu}_{q}\times\mbox{\boldmatha}\not=\mbox{\boldmath0}.*
Then, we have
[TABLE]
Thus formula (1.16) can be used for monitoring of the quantitative state of the surface, that is, the change of to of the surface admittance at a given monitoting point on the surface.
All the results mentioned above can be transplanted as follows. Corollary 1.3.* Theorem 1.2 and Corollaries 1.1-1.2 remain valid if is replaced with .*
This can be seen as follows. From (1.8) we have
[TABLE]
Thus if satisfies , then (1.11) and (1.17) ensure both quantities
[TABLE]
and
[TABLE]
have the same leading profile as .
Finally, we show that Theorem 1.2 suggests us a procedure for finding curvatures and at an arbitrary point on . It is a translation of the procedure described in [13] in which the scalar wave equation is considered.
Step 1. Choose three points , on the segment connecting and . Denote by three open balls with very small radiuses centered at such that . Note that we have and .
Step 2. Fix and generate and on by the source \mbox{\boldmathJ}_{j}=f(t)\chi_{B_{j}}\mbox{\boldmatha} for a fixed unit vector with \mbox{\boldmatha}\times\mbox{\boldmath\nu}_{q}\not=\mbox{\boldmath0} and observe on over the time interval .
Step 3. Compute \tilde{I}_{\mbox{\boldmathJ}_{j}}(\tau,T) from the observation data in Step 2.
Step 4. Apply Theorem 1.2 to the case . Then, we have
[TABLE]
where
[TABLE]
Step 5. Use the expression
[TABLE]
where and denote the mean and Gauss curvatures at of with respect to \mbox{\boldmath\nu}_{q}. From we have
[TABLE]
Solving this linear system numerically, we may obtain and .
Step 6. From one has
[TABLE]
Step 7. From the signature of one of one can know whether or .
Step 8. From Steps 6 and 7 we may obtain .
This paper is organized as follows. In section 2, we give a proof of Theorem 1.2. The proof is based on a rough asymptotic formula of the indicator function as as stated in Lemma 2.1 which has been established in [12]. The formula consists of two terms and remainder. The treatement of the remainder is not a problem. And the first term is explicitly given by (2.6) as a Laplace type surface integral of \mbox{\boldmathV}_{e}^{0} and its rotation over . Thus the key point is the profile of the second term which is the energy integral of the so-called reflected solutions given by (2.7). Its asymptotic profile is stated as Theorem 2.1 which tells us that the leading profle is also given as a Laplace type surface integral of \mbox{\boldmathV}_{e}^{0} and its rotation. Then, using the leading profile of those two terms which is described in Lemma 2.2 as an application of the Laplace method, we obtain the reading profile of the indicator function as stated in Theorem 1.2.
The proof of Theorem 2.1 is given in section 3. First we construct a candidate of the leading term of the reflected solutions. For the purpose we employ a combination of the reflection principle which has been established in [12] and a cut-off argument in a neighbourhood of with a cut-off parameter . Then the first and second terms of integral (2.7) is extracted as (3.7) in Lemma 3.1. To show that the first term is the reading profile we have to prove that the second term is small compared with first term. We see that it is true if is properly chosen according to the size of . It’s essence is described as Lemma 3.2. The proof of Lemma 3.2 which is given in section 4, is a modification of the Lax-Phillips reflection argument [17] originally developed for the study of the leading singularity of the scattering kernel for the scalar wave equation in the context of the Lax-Phillips scattering theory, however, our version of the argument is rather straightforward.
2 Proof of Theorem 1.2
Define
[TABLE]
From this and (1.9) we have
[TABLE]
It is a due course to deduce that \mbox{\boldmathV}_{m}^{0}\in H^{1}({\rm\bf R}^{3})^{3} and \mbox{\boldmathV}_{e}^{0} belongs to in a neighbourhood of .
Define
[TABLE]
Note that (\mbox{\boldmathR}_{e},\mbox{\boldmathR}_{m}) belongs to with (\nabla\times\mbox{\boldmathR}_{e},\nabla\times\mbox{\boldmathR}_{m})\in\,L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3}\times L^{2}({\rm\bf R}^{3}\setminus\overline{D})^{3}; \mbox{\boldmathR}_{m}\in H^{1}({\rm\bf R}^{3}\setminus\overline{D})^{3} and \mbox{\boldmathR}_{e} belongs to in a neighbourhood of .
From (2.2) and (1.5) we see that \mbox{\boldmathR}_{e} and \mbox{\boldmathR}_{m} satisfy
[TABLE]
It follows from (1.7) that
[TABLE]
From [12], we have a rough asymptotic formula of the indicator function.
Lemma 2.1(****[12**]**).* We have, as *
[TABLE]
where
[TABLE]
and
[TABLE]
Thus, the essential part of the proof of Theorem 1.2 should be the study of the asymptotic behaviour of and as . The asymptotic behaviour of can be reduced to that of a Laplace-type integral [3]. See [12]. For that of , we have the following result, which enables us to make a reduction of the study to a Laplace-type integral.
Theorem 2.1.* Assume that is an . Assume that has a positive lower bound, the set consists of finite points, and (1.12) is satisfied; there exists a point such that and that*
[TABLE]
Let satisfy (1.8) and
[TABLE]
Then, we have
[TABLE]
where
[TABLE]
and
[TABLE]
The proof of Theorem 2.1 is given in Section 3. Assumption (2.8) means that vector is not parallel to \mbox{\boldmath\nu}_{q} at . Note that the factor in the restriction in Theorem 1.2 is dropped in (2.9). The quantity corresponds to the first arrival time of the wave generated at on and reached at firstly. The asymptotic formula (2.10) clarifies the effect on the leading profile of the energy of the reflected solutions \mbox{\boldmathR}_{e} and \mbox{\boldmathR}_{m} in terms of the deviation of th surface admittance from that of free-space admittance and the energy density of the incident wave.
To complete the proof of Theorem 1.2 we need the following asymptotic formulae of and as .
Lemma 2.2.* We have*
[TABLE]
and
[TABLE]
Proof. Using (2.1), (2.12) and a simple computation in vector analysis, one can rewrite the right-hand side on (2.6) as
[TABLE]
Set
[TABLE]
By (18) in [11] we have already shown that \mbox{\boldmathV}_{e}^{0} has the form
[TABLE]
where
[TABLE]
[TABLE]
and
[TABLE]
This yields
[TABLE]
and thus (2.1) gives
[TABLE]
A combination of (2.16) and (2.17) gives
[TABLE]
where means uniformly with respect to and
[TABLE]
Thus we obtain
[TABLE]
and (2.15) gives
[TABLE]
Note that if , then at coincides with -\mbox{\boldmath\omega}_{x}. Thus we have
[TABLE]
and hence
[TABLE]
It is well known that the Laplace method under the assumption that is finite and satisfies (1.12), yields
[TABLE]
where . See [3], for example. The point is that the Hessian matrix of the function at is given by the operator . See, for example, [9] for this point. Replacing above with , we obtain
[TABLE]
Note also that
[TABLE]
and thus
[TABLE]
Applying (2.22) to (2.20) and noting (2.21) and (2.23), we obtain
[TABLE]
This is nothing but (2.13). Similary, from (2.11), (2.19), (2.21), (2.22) and (2.23) we obtain (2.14).
Now applying (2.10), (2.13) and (2.14) to (2.5) and noting
[TABLE]
provided (1.8) is satisfied, we obtain (1.13). This completes the proof of Theorem 1.1.
3 Proof of Theorem 2.1
We denote by the reflection across of the point with for a sufficiently small . It is given by , where denotes the unique point on such that . Note that is for with if is (see [7]). Define for with . The function is therein and coincides with for .
Choose a cutoff function with which satisfies ; if ; if ; ; .
Using the reflection across the boundary , in [11] we have already constructed from \mbox{\boldmathV}_{e}^{0} in the vector field (\mbox{\boldmathV}_{e}^{0})^{*} for with and another one
[TABLE]
which satisfy
[TABLE]
and
[TABLE]
Define
[TABLE]
and
[TABLE]
The pair (\mbox{\boldmathR}_{e}^{0},\mbox{\boldmathR}_{m}^{0}) belongs to and depends on .
Define
[TABLE]
Since \mbox{\boldmathR}_{e} and \mbox{\boldmathR}_{m} satisfiy (2.4), we obtain
[TABLE]
Define
[TABLE]
It follows from (2.3) and (3.3) that \mbox{\boldmathR}_{e}^{1} and \mbox{\boldmathR}_{m}^{1} satisfy
[TABLE]
and
[TABLE]
Now we are ready to state an asymptotic formula of as which extracts the main term involving \mbox{\boldmath\nu}\times\mbox{\boldmathR}_{m}^{1} on .
Lemma 3.1.* We have, as *
[TABLE]
Proof. Recall (40) in [12]:
[TABLE]
It follows from this and (2.7) that
[TABLE]
From (2.4) we have
[TABLE]
This gives
[TABLE]
Substituting \mbox{\boldmathR}_{m}=\mbox{\boldmathR}_{m}^{0}+\mbox{\boldmathR}_{m}^{1} into the second term on this right-hand side and using (3.1) and (3.2), we obtain
[TABLE]
Thus (3.8) becomes
[TABLE]
By Lemma 3.2 in [12] we have
[TABLE]
Here we make use of the following asymptotic formula which can be shown similarily as formulae in Lemma 2.2 by using (2.18):
[TABLE]
Applying this to the right-hand side on (3.10), we obtain
[TABLE]
Now a combination of (3.9) and (3.12) yields (3.7).
Thus, the problem is: clarify the asymptotic behaviour of \mbox{\boldmath\nu}\times\mbox{\boldmathR}_{m}^{1} on as . The point is the choice of .
Lemma 3.2.* Choose . We have*
[TABLE]
The proof of Leema 3.2 is given in Section 4.
Now choose in the pair (\mbox{\boldmathR}_{e}^{0},\mbox{\boldmathR}_{m}^{0}) as that of Lemma 3.2.
Write
[TABLE]
Applying (2.14), (3.11) and (3.13) to this right-hand side, we obtain
[TABLE]
Write
[TABLE]
Note that, if and satisfiy (1.8) and (2.9), respectively, then we have, as
[TABLE]
Now, applying this to (3.15) with the help of (2.14), we see that the left-hand side on (3.15) converges to [math] as . Applying this and (3.14) to the right-hand side on (3.7), we obtain (2.10).
4 Proof of Lemma 3.2
In this section, we denote by several positive constants independen of and .
Lemma 4.1.* We have*
[TABLE]
where and
[TABLE]
Proof. Taking the inner product of the both sides of the first equation on (3.5) with \mbox{\boldmathR}_{m}^{1}, we obtain
[TABLE]
Taking the inner product of the both sides of the second equation on (3.5) with \mbox{\boldmathR}_{e}^{1}, we obtain
[TABLE]
By virtue of the fact that \mbox{\boldmathR}_{m}^{1}\in H^{1}({\rm\bf R}^{3}\setminus\overline{D})^{3} and \mbox{\boldmathR}_{e}^{1}\in H(\mbox{curl},{\rm\bf R}^{3}\setminus\overline{D}), we have
[TABLE]
where this right-hand side denotes the value of the bounded linear functional \mbox{\boldmathR}_{e}^{1}\times\mbox{\boldmath\nu} on of \mbox{\boldmath\nu}\times(\mbox{\boldmathR}_{m}^{1}\times\mbox{\boldmath\nu})\in H^{1/2}(\partial D)^{3}. However, \mbox{\boldmathR}_{e}^{1} belongs to in a neighbourhood of this coincides with the integral
[TABLE]
Note also that
[TABLE]
From these, (4.2), (4.3) and (4.4) we obtain
[TABLE]
Sine we have
[TABLE]
from (3.6) one gets
[TABLE]
Thus (4.5) becomes
[TABLE]
where
[TABLE]
Rewrite (4.6) further as
[TABLE]
This immediately yields
[TABLE]
Then, the boundary condition (3.6) yields (4.1).
In order to make use of the right-hand side on (4.1), we prepare the following two lemmas.
Lemma 4.2.* We have, as *
[TABLE]
Proof. From (2.12) and (3.4) we have the expression
[TABLE]
Thus (2.18) yields
[TABLE]
Note that the term is uniform with repect to . Since {\cal D}(x)|_{\lambda=\lambda_{0}}\mbox{\boldmatha}=\mbox{\boldmath0} for all , it follows from (2.22) that
[TABLE]
Then, from (2.23) we obtain the desired conclusion.
Lemma 4.3.* We have*
[TABLE]
and
[TABLE]
where
[TABLE]
Proof. This is an application of a reflection argument developed in [17]. First of all, we compute both \nabla\times(\mbox{\boldmathV}_{e}^{0})^{*} and \nabla\times(\mbox{\boldmathV}_{m}^{0})^{*}. From the definition we have
[TABLE]
and hence
[TABLE]
Define
[TABLE]
We have
[TABLE]
and from (4.11) one gets the expression
[TABLE]
This gives
[TABLE]
Using the change of variables , one has
[TABLE]
We have
[TABLE]
Thus, from (4.13), (4.14) and (4.15), we obtain (4.8).
From (1.9) we know that \mbox{\boldmathV}_{e}^{0} satisfies
[TABLE]
Applying Proposition 3 in [11] to this case, we have
[TABLE]
and all the coefficients in this right-hand side are independent of and continuous, in particular, the coefficients come from the second order terms are in a tubular neighbourhood of .
From (4.12) we have
[TABLE]
Thus (4.16) gives
[TABLE]
This yields
[TABLE]
From the form of and the cahnge of variables, we have
[TABLE]
From the definition of (\mbox{\boldmathV}_{m}^{0})^{*} and a change of variables we have
[TABLE]
Here we claim
[TABLE]
and
[TABLE]
The estimate (4.20) has been established as (27) of Lemma 2.2 in [11] since from (2.1) we have another expression
[TABLE]
The estimate (4.21) is proved using the explicit from (2.16) as follows. We have
[TABLE]
where and
[TABLE]
Then, from (2.16) we see that
[TABLE]
and hence, for
[TABLE]
Then, it is easy to see that, there exists a positive constant independent of such that, for all and , we have
[TABLE]
We know from (24) in [11] that, for all
[TABLE]
This yields
[TABLE]
Then, applying (4.15) and (4.20) to this right-hand side we obtain (4.21).
Now applying (4.15), estimates (4.20) and (4.21) to (4.18), one gets
[TABLE]
Then, this together with (4.17), (4.19) and (4.20) yields (4.9).
A combination of (2.2) in and (4.10), we have
[TABLE]
Since this last expreesion means that , similarly to (2.13), we have
[TABLE]
This gives, as
[TABLE]
From this together with (4.8) and (4.1), we have
[TABLE]
and hence
[TABLE]
Now choosing with , we have . Thus choosing , we have and (4.22) becomes
[TABLE]
Now applying this and (4.7) to the right-hand side on (4.1) together with (1.8) and (2.9), we obtain (3.13). This completes the proof of Lemma 3.2.
[TABLE]
Acknowledgments
The author was partially supported by Grant-in-Aid for Scientific Research (C)(No 17K05331) of Japan Society for the Promotion of Science.
[TABLE]
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