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Article

Non-Singular Generalized RBF Solution and Weaker Singularity MFS: Laplace Equation and Anisotropic Laplace Equation

1
Center of Excellence for Ocean Engineering, National Taiwan Ocean University, Keelung 202301, Taiwan
2
Department of Applied Artificial Intelligence, Ming Chuan University, Taoyuan 333321, Taiwan
*
Author to whom correspondence should be addressed.
Mathematics 2025, 13(22), 3665; https://doi.org/10.3390/math13223665
Submission received: 23 October 2025 / Revised: 7 November 2025 / Accepted: 13 November 2025 / Published: 15 November 2025

Abstract

This paper introduces a singular distance function rs in terms of a symmetric non-negative metric tensor S. If S satisfies a quadratic matrix equation involving a parameter β, then for the Laplace equation r s β is a non-singular generalized radial basis function solution if 2 > β > 0, and a weaker singularity fundamental solution if −1 < β < 0. With a unit vector as a medium to express S, we can derive the metric tensor in closed form and prove that S is a singular projection operator. For the anisotropic Laplace equation, the corresponding closed-form representation of S is also derived. The concept of non-singular generalized radial basis function solution for the Laplace-type equations is novel and useful, which has not yet appeared in the literature. In addition, a logarithmic type method of fundamental solutions is developed for the anisotropic Laplace equation. Owing to non-singularity and weaker singularity of the bases of solutions, numerical experiments verify the accuracy and efficiency of the proposed methods.

1. Introduction

Since the work of Kupradze [1], there have appeared numerous discussions of the method of fundamental solutions (MFS) for the purpose of an easy computation of engineering problems. The fundamental solutions for the commonly used linear partial differential equations (PDEs) are listed in text books [2,3]. A review of the MFS for elliptic type PDEs up to 1998 was given in [4]. More topics for the MFS were issued in [5].
It is known that 1 / r is a fundamental solution of the 3D Laplace equation:
Δ u ( x ) = 0 , x Ω R 3 ,
u ( x ) | x Γ = f ( x ) ,
satisfying
Δ 1 r = · 1 r = · r r 3 = δ ( r ) ,
where δ is the Dirac delta function, due to r 3 0 when x x s ; r = r = x x s , and x s is a source point. It is evident from Equation (3) that 1 / r ( x ) is a fundamental solution of Equation (1), whose order of singularity is one. The derivation of Equation (3) is relegated into Appendix A.
In the whole paper the domain Ω of the problem considered is supposed to be bounded, and its boundary is continuous and piecewise smooth.
The singularity of MFS occurs as x = x s where 1 / r grows to infinity. One of the issues to reduce the ill-posedness due to the singularity is a proper selection of source points to improve the performance of MFS [6,7,8]. Wang et al. [9] proposed a novel adaptive method of fundamental solutions with physics-informed neural networks to determine the source points.
As noted in [3] the functions expressed in terms of the Euclidean distance belong to the radial basis function (RBF). For the linear PDEs the radially symmetric fundamental solutions have the radial form to be radial functions. For this reason Golberg and Chen [10] categorized the MFS into the class of the methods of RBFs. The MFS exhibits singularities at source points, where special treatment of these singularities should be handled numerically. To overcome the singularity of MFS, the RBF general solutions were proposed in [11] for varied orders of the vibrational thin, the Berger, and the Winkler plates, in [12] for the boundary particle method, and in [13,14] for the boundary knot method. These papers proposed non-singular radial functions as the bases of solutions. To further overcome the ill-posedness, there were some discussions on the improvements of the boundary knot method [15,16].
The boundary knot method (BKM) was developed by Chen and Tanaka [12], and it synergistically combines the merits of MFS and RBF techniques. Later many applications of BKM can be seen in the literature, such as the solution of two-dimensional advection reaction–diffusion and Brusselator equations [17], the 2D and 3D Helmholtz and convection–diffusion problems under complicated geometry [18], the inverse problems associated with the Helmholtz equation [19], with fictitious sources for solving Helmholtz-type equations [20], and the modified boundary knot method for multi-dimensional harmonic-type equations [21].
The non-singular RBF general solutions utilized for some commonly used linear PDEs were listed in Table 2.7 of [3]. Unfortunately the non-singular RBF solution for the Laplace equation is a constant, which is not suitable to be the basis of solution. The lack of non-singular RBF solutions for the Laplace-type equations motivates us to develop the non-singular generalized RBF solution (NSGRBF) in the present paper.
Chen et al. [11] used the non-singular RBF solutions of Helmholtz-like equation with a small characteristic parameter to overcome this difficulty. However, when the characteristic parameter should generally be small to get an accurate solution of the Laplace equation, the accuracy of numerical solution is very sensitive to the domain geometry. In this paper we generalize the radial function in terms of a singular distance function r s ( x , y ) = r T S r , where r = x y , and S 0 with det ( S ) = 0 is a singular symmetric tensor. If one takes S = I 3 , r s recovers to the usual Euclidean distance function r ( x , y ) = r . r s possesses the following properties: (i) r s ( x , y ) 0 , (ii) r s ( x , y ) = r s ( y , x ) , and (iii) r s ( x , z ) r s ( x , y ) + r s ( y , z ) . In addition to these properties, r ( x , y ) possesses an extra property of r ( x , y ) = 0 iff x = y . This property does not hold for r s ( x , y ) because, when r 0 lies in the null space of S , we have r s ( x , y ) = 0 even for x y .
The new solution in terms of r s will be called the generalized RBF solution, in contrast to the r-dependent RBF solution. Then we will extend the non-singular generalized RBF solution for the Laplace equation to the anisotropic Laplace equation:
· [ K u ( x ) ] = 0 , x Ω R 3 ,
where K is a positive-definite and symmetric anisotropic tensor.
For the anisotropic Laplace equation, the domain mapping method was derived in [22], and the boundary knot method based on geodesic distance was proposed in [23]. The newly defined generalized RBF solutions can be adopted as alternative and effective bases to find the numerical solutions of the Laplace equation and anisotropic Laplace equation.
The work on generalized operators in [24] can provide insights into extending the RBF framework to more complex approximations. On the other hand the methods for fractional systems in [25] may inspire analogous approaches for singular and non-singular solutions in PDEs.
By applying the MFS to solve the Laplace-type PDEs, it is utmost important, by using the de-singularized technique, to reduce the ill-conditioned behavior and then raise the computational efficiency and accuracy. The novel contributions of the present paper for solving the 3D Laplace equation and anisotropic Laplace equation are summarized as follows:
  • The extension from the original MFS to the non-singular generalized RBF (NSGRBF) using the novel bases can be carried out to improve the ill-posedness of the original MFS and enhance the accuracy of numerical solutions.
  • The de-singularized technique is simple and efficient.
  • The NSGRBF solution bases were derived at the first time for both the Laplace equation and anisotropic Laplace equation.

2. Generalized RBF Solution

The following vector notations can facilitate the proofs of the new results:
x : = x y z , x s : = x s y s z s , r : = x x s y y s z z s ,
where x Ω ¯ : = Ω Γ , and x s Ω ¯ c : = R 3 Ω ¯ is a source point. Hence,
r ( x ) = r ( x ) = r T ( x ) r ( x )
is a positive distance function of Euclidean type. We define a singular distance function:
r s ( x ) = r T ( x ) S r ( x ) ,
where the 3 × 3 matrix S is a symmetric non-negative metric tensor; the subscript s means that r s is a singular distance function. Later we will prove that S is a continuous quadratic function of a unit vector.
According to Equation (7), we have
r s ( x ) = S r ( x ) r s ( x ) .
Now we attempt to get rid of the singularity in Equation (3) as follows, which is an extension of Theorem 3 in [26].
Theorem 1. 
For the Laplace equation, if the 3 × 3 symmetric matrix S satisfies
S 2 = t r ( S ) 2 β S ,
where t r ( S ) > 0 is the trace of S , then
U ( x ) = r s β ( x ) = [ r T ( x ) S r ( x ) ] β / 2
satisfies Equation (1):
· [ U ( x ) ] = Δ U ( x ) = 0 .
When 2 > β > 0 , U ( x ) is a generalized RBF solution without having singularity; when 1 < β < 0 , U ( x ) is a singular solution with the order of singularity being β .
Proof. 
First we clarify the range of β . β = 2 is a singular point, which leads to the failure of Equation (9); hence, β < 2 is required. In Equation (10), β = 0 renders a constant value of U = 1 , which is not interesting. Therefore, the range of β is 2 > β > 0 for the non-singular solution U in Equation (10). In MFS the singular solution U = 1 / r has a singularity order β = 1 . For a less singular solution U in Equation (10), we take β > 1 . Therefore, the range of β is 1 < β < 0 for the singular solution U in Equation (10).
It follows from Equation (10) that
U = β r s β 1 r s .
Then by means of Equations (12) and (8), one has
U = β r s β 1 r s = β r s β 1 S r r s = β r s β 2 S r .
We have
· ( S r ) = · [ S ( x x s ) ] = · ( S x ) = t r ( S ) ,
because S is a constant matrix and x s is a constant vector.
Taking the divergence on both sides of Equation (13) and using Equation (14) yields
· ( U ) = β · ( r s β 2 S r ) = β r s β 2 · ( S r ) + β ( r s β 2 ) · ( S r ) = β r s β 2 t r ( S ) + β ( β 2 ) r s β 3 r s · ( S r ) .
Using Equations (7), (8) and (15)yields
· ( U ) = β r s β 2 t r ( S ) + β ( β 2 ) r s β 3 S r r s · ( S r ) = β r s β 2 t r ( S ) + β ( β 2 ) r s β 4 r T S T S r = β r s β 2 t r ( S ) + β ( β 2 ) r s β 4 r T S 2 r = β r s β 4 [ r s 2 t r ( S ) + ( β 2 ) r T S 2 r ] = β r s β 4 r T t r ( S ) S ( 2 β ) S 2 r ,
where S T S = S 2 was used owing to the symmetry of S . If Equation (9) holds, Equation (11) follows immediately. □
Satisfying Equation (9) by S , a generalized RBF solution (10) for U ( x ) of the Laplace equation is obtained. If β > 0 , the singularity of r s β is zero; when 1 < β < 0 , the singularity of U ( x ) with the order β is weaker than 1 / r of the original MFS as shown in Equation (3). For the special case with β = 0 , Equation (10) is a non-sense constant solution. Rather than a constant solution the logarithmic singular solution U ( x ) = ln r s ( x ) was already derived in [26], if we set β = 0 in Equation (9).
Notice that Theorem 1 involves the fundamental solution 1 / r ( x ) as a special case. Taking β = 1 , S = I 3 is a solution of Equation (9). Then U ( x ) in Equation (10) reduces to U ( x ) = 1 / r ( x ) .
Equation (9) is an operator equation as a projective constraint of S . Applying it to any nonzero vector b we have
b T S S t r ( S ) 2 β I 3 b = 0 .
Because S is symmetric, Equation (17) indicates that S b is perpendicular to [ S t r ( S ) 2 β I 3 ] b .
Theorem 2. 
No solution of Equation (9) with S > 0 exists. If a is a unit vector with a = 1 , then
S ˜ = I 3 a a T
satisfies
S ˜ 2 = S ˜ ,
where S ˜ 0 with det( S ˜ ) = 0 is a singular projection operator. Moreover, S with t r ( S ) > 0 can be derived as follows:
S = 2 β 2 S ˜ = 2 β 2 ( I 3 a a T ) .
Proof. 
We prove the first statement by a contradiction method. If S > 0 then S 1 exists. Multiplying both sides of Equation (9) by S 1 leads to
S = t r ( S ) 2 β I 3 ;
hence, S is proportional to I 3 . Let
S = γ I 3 , γ 0 ,
where γ is a proportional factor; by means of Equation (21), it induces a contradiction:
γ I 3 = 3 γ 2 β I 3 .
Given β < 2 , there exists no such a value of γ to satisfy the above equation.
Taking the determinant of both sides of Equation (9) makes
det ( S ) det ( S ) t r 3 ( S ) ( 2 β ) 3 = 0 .
Either det( S ) = 0 or det( S ) = t r 3 ( S ) / ( 2 β ) 3 . The latter one rendering det ( S ) > 0 and thus S 1 existing contradicts the non-existence of S 1 . Consequently, S 0 with det( S ) = 0 is a singular matrix.
Next we prove Equation (18), whose trace leads to
t r ( S ˜ ) = 2 ,
owing to a = 1 . Squaring Equation (18) and using a 2 = 1 leads to
S ˜ 2 = ( I 3 a a T ) ( I 3 a a T ) = I 3 a a T a a T + a 2 a a T = I 3 a a T = S ˜ .
Hence, S ˜ is a singular projection operator.
We can observe that Equation (9) is scaling invariant; hence, α S , α 0 is a solution when S is a solution. We can choose α , such that
t r ( S ) 2 β = 1 .
We take
S = α S ˜ ,
and because of tr( S ˜ ) = 2 and tr ( S ) = 2 β by Equation (24), α is obtained by taking the trace of Equation (25):
α = 2 β 2 .
The combination of Equations (18), (25) and (26) leads to Equation (20). □
From Equation (9) we can observe that S = 0 is a trivial solution. In order to avoid the trivial solution and using the scale invariance of S , we may fix S by an extra condition:
t r ( S ) = a 0 > 0 ,
where a 0 is a constant. Hence, S 0 . We can prove the following result.
Theorem 3. 
If S satisfies Equation (27), then the eigenvalues of S involve double zeros and a non-zero one λ = 1 β / 2 .
Proof. 
Let
λ : = t r ( S ) 2 β = a 0 2 β ,
which is combined to Equation (9) to generate an eigenvalue problem
( S λ I 3 ) S = 0 .
For a non-trivial solution of S , we ask
det ( S λ I 3 ) = 0 .
Since det ( S ) = 0 as shown in Theorem 2, λ = 0 is an eigenvalue of S . Therefore, we come to a quadratic characteristic equation:
λ 2 a 0 λ + A 0 = 0 ,
where
A 0 = s 11 s 22 + s 11 s 33 + s 22 s 33 s 12 2 s 13 2 s 23 2 ,
where s i j are the components of S .
From Equation (20) it follows that
S = 1 β 2 1 a 1 2 a 1 a 2 a 1 a 3 a 1 a 2 1 a 2 2 a 2 a 3 a 1 a 3 a 2 a 3 1 a 3 2 ,
where a = ( a 1 , a 2 , a 3 ) T is a unit vector satisfying
a 1 2 + a 2 2 + a 3 2 = 1 .
Equations (27), (33) and (34) lead to
a 0 = 2 β .
Inserting Equation (20) into Equation (32) and using Equation (34) yields
A 0 = 1 β 2 2 [ 1 a 1 2 a 2 2 + a 1 2 a 2 2 + 1 a 1 2 a 3 2 + a 1 2 a 3 2 + 1 a 2 2 a 3 2 + a 2 2 a 3 2 a 1 2 a 2 2 a 1 2 a 3 2 a 2 2 a 3 2 ] = 1 β 2 2 > 0
Therefore, by means of Equations (31) and (35), we have
λ 2 ( 2 β ) λ + 1 β 2 2 = 0 ,
whose roots are given by λ = 0 and λ = 1 β / 2 . □

3. Non-Singular Generalized RBF Solution of Anisotropic Laplace Equation

We extend Theorem 1 to the anisotropic Laplace Equation (4) as follows.
Theorem 4. 
For the anisotropic Laplace Equation (4), if the 3 × 3 symmetric matrix S satisfies
S K S = t r ( K S ) 2 β S ,
then
U ( x ) = r s β ( x ) = [ r T ( x ) S r ( x ) ] β / 2
satisfies Equation (4).
Proof. 
The existence of the solution S of Equation (38) will be given in Theorem 5. It follows from Equation (13) that
K U = β r s β 2 K S r .
Taking the divergence on both sides and using Equations (7) and (8) generates
· ( K U ) = β · ( r s β 2 K S r ) = β r s β 2 · ( K S r ) + β ( r s β 2 ) · ( K S r ) = β r s β 2 t r ( K S ) + β ( β 2 ) r s β 3 r T S K S r r s = β r s β 4 [ r s 2 t r ( K S ) + ( β 2 ) r T S K S r ] = β r s β 4 r T t r ( K S ) S ( 2 β ) S K S r .
If Equation (38) holds, then Equation (4) is proved for U ( x ) in Equation (39). □
A special case of Equation (38) is that
S = K 1 , β = 1 ;
in view of Equation (39),
U ( x ) = 1 r ( x ) , r ( x ) = r T ( x ) K 1 r ( x )
is the fundamental solution of Equation (4).
If we take K = I 3 , Equation (4) reduces to the Laplace Equation (1); meanwhile, Equation (43) is the fundamental solution of Equation (1).
The solution of S in Equation (38) can be proved as follows.
Theorem 5. 
If a is a unit vector with a = 1 , then S satisfying Equation (38) is given by
S = 2 β 2 ( K 1 K 1 a a T ) .
Proof. 
Equation (38) multiplying by K generates
H 2 = t r ( H ) 2 β H ,
where
H = K S .
It can be seen that Equation (45) for H is the same to Equation (9) for S . Then by means of Equations (20) and (46), we can derive Equation (44). □
In practical computation of S , we employ Equation (44), which is simple after giving K 1 and the unit vector a , given by
S = 1 β 2 K 1 1 a 1 2 a 1 a 2 a 1 a 3 a 1 a 2 1 a 2 2 a 2 a 3 a 1 a 3 a 2 a 3 1 a 3 2 .
Rather than the usual fundamental solution given in Equation (43), we can prove a weaker singular solution as follows:
Theorem 6. 
For the anisotropic Laplace Equation (4), if the 3 × 3 symmetric matrix S satisfies
S K S = t r ( K S ) 2 S ,
then
U ( x ) = ln r s ( x )
is a weaker singular fundamental solution of Equation (4).
Proof. 
One has
U = r s 2 S r
by means of Equations (8) and (49). Then,
K U = r s 2 K S r .
The divergence on both sides and the use of Equations (7) and (8) yields
· ( K U ) = · ( r s 2 K S r ) = r s 2 · ( K S r ) + ( r s 2 ) · ( K S r ) = r s 2 t r ( K S ) 2 r s 3 r T S K S r r s = β r s 4 ( r s 2 t r ( K S ) 2 r T S K S r ) = r s 4 r T t r ( K S ) S 2 S K S r .
If Equation (48) holds, then Equation (4) is proven for U ( x ) given in Equation (49). □
We cannot take S = I 3 ; there exists no proper K that can satisfy Equation (48), because we encounter the following contradiction:
K = t r ( K ) 2 I 3 ,
which is not an anisotropic tensor.
Table 1 summarizes S and U for different values of β for the anisotropic Laplace equation. If we take K = I 3 , the results reduce to that for the 3D Laplace equation.

4. A Non-Singular Generalized RBF and a Weaker Singularity MFS

We may call the newly constructed solution U of Equation (1) as shown in Equation (10) as a singular fundamental solution if β < 0 . When β > 0 it is a non-singular RBF solution. No matter which case is used, the present numerical method is novel for solving the Laplace equation, and we will name the new numerical method a weaker singular MFS (WSMFS) if β < 0 , and a non-singular generalized RBF solution method (NSGRBF) if β > 0 .
Inserting Equation (20) into Equation (7) yields
r s ( x ) = 2 β 2 [ ( x x s ) 2 + ( y y s ) 2 + ( z z s ) 2 ] 2 β 2 [ a 1 ( x x s ) + a 2 ( y y s ) + a 3 ( z z s ) ] 2 1 / 2 .
We project x s into two vectors:
y s = ( x s , 0 , z s ) T , z s = ( x s , y s , 0 ) T ,
and then to construct the unit vector a we take
a = y s × z s y s × z s = ( y s z s , x s z s , x s y s ) T ( x s y s ) 2 + ( x s z s ) 2 + ( y s z s ) 2 .
Hence, by using the NSGRBF the solution of Equation (1) is taken to be
u ( x , y , z ) = j = 1 n c j 2 β 2 [ ( x x j s ) 2 + ( y y j s ) 2 + ( z z j s ) 2 ] 2 β 2 [ a 1 ( x x j s ) + a 2 ( y y j s ) + a 3 ( z z j s ) ] 2 β / 2 ,
where
( a 1 , a 2 , a 3 ) = ( y j s z j s , x j s z j s , x j s y j s ) ( x j s y j s ) 2 + ( x j s z j s ) 2 + ( y j s z j s ) 2 .
The source points are given by
( x j s , y j s , z j s ) = [ ( D + ρ ( θ j , ϕ j ) ) cos θ j sin ϕ j , ( D + ρ ( θ j , ϕ j ) ) sin θ j sin ϕ j , ( D + ρ ( θ j , ϕ j ) ) cos ϕ j ] ,
where ρ ( θ , ϕ ) is a radius function for Γ , and D is an offset.
A compact vector form of Equation (57) reads as
u ( x ) = j = 1 n c j 2 β 2 x x j s 2 2 β 2 a · ( x x j s ) β / 2 ,
where x j s is the jth source point.
To be a well-defined basis of r s , the following cone condition must be satisfied:
r s ( x ) > 0 , x Ω ,
which indicates that the orientation vector a must point out from the cone. The cone consists of all straight lines passing through the vertex point x s and having at least one intersection point with the domain Ω ¯ . If a lies in the cone, there are some field points x with r = x x s = α a , which leads to r T S r = 0 , since S r = α S a = 0 .
In this situation, r s ( x ) = 0 in view of Equation (7), which is an ineffective basis, and we must get it rid of it. In our experience when the value of D is taken sufficiently large, r s ( x ) > 0 , x Ω .
It follows from Equations (1), (2) and (57) that a linear system
A c = b ,
where c : = ( c 1 , , c n ) T are unknown coefficients, b : = ( b 1 , , b n q ) T are the data on the right-hand side, and the components a i j of A with dimension n q × n can be derived. Equation (62) is scaled by a constant column norm with R 0 [6].
To raise the accuracy we consider a combination of Equation (57) and the traditional MFS:
u ( x , y , z ) = j = 1 m c j 2 β 2 [ ( x x j s ) 2 + ( y y j s ) 2 + ( z z j s ) 2 ] 2 β 2 [ a 1 ( x x j s ) + a 2 ( y y j s ) + a 3 ( z z j s ) ] 2 β / 2 + j = 1 m d j r j ( x , y , z ) .
Now the number of unknown coefficients is n = 2 m .
By means of Equations (5), (7) and (43), the solution of Equation (4) is given by
u ( x ) = j = 1 m c j [ r j T ( x ) S r j ( x ) ] β / 2 + j = 1 m d j r j T ( x ) K 1 r j ( x )
where r j = x x j s , S is given by Equation (44), and a is defined by Equation (58).
Using the logarithmic MFS in Theorem 6, the solution of Equation (4) is given by
u ( x ) = j = 1 m c j ln r j T ( x ) S r j ( x ) + j = 1 m d j r j T ( x ) K 1 r j ( x )
where S is given by Equation (44) with β = 0 , and a is defined by Equation (58).

5. Results and Discussions

Now the numerical solutions of the Laplace equation can be carried out by using the proposed NSGRBF or WSMFS depending on the value of the parameter β .

5.1. Example 1

Consider the boundary value problem by giving
u ( x , y , z ) = x y z + x 2 y 2 + z 2 2 ,
which is defined in a domain Ω with the boundary:
Γ = { ( x , y , z ) | x = ρ cos θ , y = ρ sin θ sin ϕ , z = ρ sin θ cos ϕ , 0 θ 2 π , 0 ϕ π } ,
where
ρ ( θ ) = cos ( 3 θ ) + 8 sin 2 ( 3 θ ) 1 3 .
For Equation (57) a weaker singularity MFS (WSMFS) can be obtained whose order of singularity is β if β < 0 . Under n = 400 , n q = 1600 , R 0 = 0.01 , and D = 0.8 , we compare the results using different β in Table 2.
We take a constant D = 7 for the offset. The value of D is taken by some trial tests, and among the testing values we take the optimal one.
With n = 100 , n q = 1600 , the maximum error (ME) = 2.34 × 10 5 and the root-mean-square-error (RMSE) = 1.44 × 10 5 are obtained on the surface S = Γ / 2 by using the original MFS.
On the curve C = { r = ρ / 2 , ϕ = π / 4 , 0 θ 2 π } , the numerical solution obtained by MFS is compared to the exact one in Figure 1a, whose error is shown in Figure 1b with ME = 2.18 × 10 5 .
By using Equation (63) under n = 1250 , n q = 1600 , R 0 = 0.01 , and D = 7 , we compare the results using different β in the NSGRBF in Table 3. For β = 0.0001 the improvement of accuracy comparing to MFS is about three orders. The accuracy is competitive to that computed in [26], which used the method of anisotropic fundamental solution (MAFS) with an optimal value of D; ME = 6.91 × 10 8 and RMSE = 3.08 × 10 8 were obtained.
When the parameter β is near to −1, say β = 0.999 , NSGRBF would lead to worse results of ME = 2.04 × 10 4 and RMSE = 8.66 × 10 5 ; comparing to Cond = 4.66 × 10 10 obtained for β = 0.0001 it with a large condition number Cond = 4.15 × 10 13 presents the ill-posedness of the linear system.
On the curve C , the numerical solution obtained by NSGRBF with β = 0.0001 is compared to the exact one in Figure 1a, whose error is shown in Figure 1b with ME = 3.81 × 10 8 , which is much accurate than that obtained by MFS. We have computed the condition number for NSGRBF, which is Cond = 4.66 × 10 10 . For MFS we have Cond = 2.75 × 10 11 , which is larger than that of NSGRBF, even n = 100 is much smaller than n = 1250 used in NSGRBF. In MFS if we take a near value of n = 1225 , the condition number increases to Cond = 6.02 × 10 16 , which is much large than Cond = 4.66 × 10 10 ; ME = 6.63 × 10 8 obtained by MFS is still larger than ME = 3.81 × 10 8 obtained by NSGRBF. So one major advantage of the NSGRBF is that the resulting linear system is less ill-conditioned that that of MFS and the accuracy of NSGRBF is better than MFS.
To observe the convergence behavior of NSGRBF, we take a different value of m in Equation (63) and list ME and RMSE in Table 4, where n q = 1600 , R 0 = 0.01 , D = 7 , and β = 0.0001 were fixed. It can be seen that the solution is convergent very fast when m increases from 25 to 400.
To test the sensitivity of NSGRBF with respect to β , the RMSE is plotted in Figure 2, where we can observe that when β nears zero the best value of RMSE can be obtained. With β < 0 the basis is singular, which is, in principle, less accurate than that with the non-singular basis with β > 0 .

5.2. Example 2

In this and next examples, we consider the anisotropic Laplace equation:
k 11 u x x ( x , y , z ) + k 22 u y y ( x , y , z ) + k 33 u z z ( x , y , z ) + 2 k 12 u x y ( x , y , z ) + 2 k 13 u x z ( x , y , z ) + 2 k 23 u y z ( x , y , z ) = 0 , ( x , y , z ) Ω R 3 ,
where the coefficients are subjected to the following constraints [22]:
k 11 > 0 , k 22 > 0 , k 33 > 0 , k 11 k 22 k 12 2 > 0 , k 11 k 33 k 13 2 > 0 , k 22 k 33 k 23 2 > 0 .
The numerical solutions of the anisotropic Laplace equation can be carried out by using the proposed NSGRBF or WSMFS depending on the value of the parameter β .
As an example we take k 11 = 1 , k 22 = 1 , k 33 = 1 / 2 and k 23 = 1 / 2 , and the exact solution is given by
u ( x , y , z ) = x 2 y 2 2 y z 2 z 2 .
We can derive
K 1 = 1 0 0 0 2 2 0 2 4 .
We can apply the original MFS with
u ( x ) = j = 1 m e j r j T ( x ) K 1 r j ( x ) ,
to solve Equation (69). Under n = m 2 = 625 , n q = 1600 , R 0 = 0.01 , and with the optimal value of D = 9.45 , we obtain ME = 1.58 × 10 5 and RMSE = 2.41 × 10 6 . They are used as referenced values to evaluate the accuracy of the newly proposed methods.
Under n = 1250 , n q = 1600 , R 0 = 0.01 , and D = 7 , we compare the results computed by Equation (64) using different β in Table 5. ME and RMSE are given in the whole domain with 12,500 testing points.
On the curve C = { r = ρ / 2 , ϕ = π / 4 , 0 θ 2 π } , the numerical solution obtained by MFS is compared to the exact one in Figure 3a, whose error is shown in Figure 3b with ME = 2.01 × 10 6 .
On the curve C , the numerical solution obtained by NSGRBF with β = 0.0001 is compared to the exact one in Figure 3a, whose error is shown in Figure 3b with ME = 1.28 × 10 6 , which is more accurate than that obtained by MFS. The condition number for NSGRBF with n = 1250 is Cond = 6.60 × 10 10 . For MFS we have Cond = 2.06 × 10 9 , of which n = 625 is smaller than n = 1250 used in NSGRBF. One major advantage of the NSGRBF is that the resulting linear system is less ill-conditioned that that of MFS and the accuracy of NSGRBF is better than MFS.
To observe the convergence behavior of NSGRBF, we take different values of m in Equation (64) and list ME and RMSE in Table 6, where n q = 1600 , R 0 = 0.01 , D = 7 , and β = 0.0001 were fixed. It can be seen that the solution is convergent very fast when m increases from 25 to 400.
The logarithmic MFS (LMFS) is also used to solve the anisotropic Laplace equation. Under n = 625 , n q = 1600 , R 0 = 0.01 , and D = 15 , ME = 1.35 × 10 3 and RMSE = 5.28 × 10 4 are obtained by LMFS.
To enhance the accuracy the LMFS revealed in Equation (65) is employed to solve this problem. Under n = 1250 , n q = 1600 , R 0 = 0.01 , we compare the results computed by Equation (65) using different D in Table 7. ME and RMSE are given in the whole domain with 12,500 testing points. Comparing to Table 5, LMFS is less accurate than the results obtained by NSGRBF and WSMFS.

5.3. Example 3

Next we consider a more complicated exact solution:
u ( x , y , z ) = x e x cos ( y + 2 z ) e x ( y + 2 z ) sin ( y + 2 z ) ,
with the same k 11 = 1 , k 22 = 1 , k 33 = 1 / 2 and k 23 = 1 / 2 .
Under n = 1250 , n q = 1600 , R 0 = 0.01 , and D = 7 , we compare the results computed by Equation (64) using different β in Table 8. ME and RMSE are given in the whole domain with 12,500 testing points.
When the parameter β is near to −1, say β = 0.99 , it would lead to the failure of NSGRBF as shown in Table 8, where ME = 1.997 and RMSE = 0.708 are incorrect, with a large condition number Cond = 2.13 × 10 13 to present the ill-posedness of the linear system. Similarly for β = 1.99 , ME = 0.645 and RMSE = 0.478 are incorrect, which are with a large condition number Cond = 9.27 × 10 18 to show that the linear system is highly ill-posed.
To test the sensitivity of NSGRBF with respect to β , the RMSE is plotted in Figure 4, where we can observe that when β nears to zero the best value of RMSE can be obtained.
Under n = 1250 , n q = 1600 , R 0 = 0.01 , we compare the results computed by Equation (64) using different D and the optimal β in Table 9. ME and RMSE are given in the whole domain with 12,500 testing points.
Using D = 2 and β = 3.82 × 10 3 , ME = 1.19 × 10 4 and RMSE = 2.70 × 10 5 can be obtained by NSGRBF. Notice that the original MFS in Equation (73) with the optimal value of D = 4.8263 , ME = 7.50 × 10 4 and RMSE = 1.39 × 10 4 can be obtained, which is less accurate than the present method of NSGRBF.
Rather than the smooth domain in Equations (67) and (68), we consider a unit cube that has eight corners. Let F = x e x cos ( y + 2 z ) e x ( y + 2 z ) sin ( y + 2 z ) be the exact solution in Equation (74). We impose the following boundary conditions:
u ( x , y , 0 ) = F ( x , y , 0 ) , u ( x , y , 1 ) = F ( x , y , 1 ) , u ( 0 , y , z ) = F ( 0 , y , z ) , u ( 1 , y , z ) = F ( 1 , y , z ) , u ( x , 0 , z ) = F ( x , 0 , z ) , u ( x , 1 , z ) = F ( x , 1 , z ) .
Under n = 300 , n q = 600 , R 0 = 0.01 , and D = 10 , we compare the results computed by Equation (64) using different β in Table 10. ME and RMSE are given in the whole domain with 8000 testing points. It can be seen that ME and RMSE are not sensitive to β ; β = 0.5 leads to a slightly worse value of RMSE.

6. Conclusions

This paper proposed an order reduction singular MFS to treat the boundary value problems of Laplace equation and anisotropic Laplace equation. The weaker singularity method of fundamental solutions (WSMFS) is endowed with a weaker singularity to raise the accuracy and increase the efficiency due to the reduction of a strong singularity of the original MFS. The non-singular generalized RBF (NSGRBF) solutions were first derived in the literature for both the Laplace equation and anisotropic Laplace equation. The combination of the proposed methods to the traditional MFS can raise the accuracy of the solutions. Numerical experiments assured the efficiency and accuracy of the WSMFS and NSGRBF.
The present paper is equipped with several novelties and significant contributions with a sound mathematical analysis.
1.
We introduced a new idea of singular distance function in terms of a singular projection operator equipped with a parameter β .
2.
The singular projection operators were derived in closed form for the Laplace equation and anisotropic Laplace equation.
3.
When 2 > β > 0 the generalized RBF solutions were obtained, which are non-singular.
4.
When 1 < β < 0 the generalized RBF solutions were obtained, which are singular with the order of singularity being β .
5.
The non-singular generalized RBF (NSGRBF) solutions were derived for the Laplace equation and anisotropic Laplace equation.
6.
The solutions of weaker singularity MFS (WSMFS) were derived for the Laplace equation and anisotropic Laplace equation.
In the future we may extend the present approach of the NSGRBF to other type linear PDEs. For instance U = cos λ r / r is the fundamental solution of the 3D Helmholtz equation Δ u + λ 2 u = 0 . We may modify the part 1 / r by the non-singular solution r s β . However, there is still much room to carry out these studies in the future.

Author Contributions

Conceptualization, C.-S.L.; methodology, C.-S.L.; validation, C.-L.K.; formal analysis, C.-L.K.; investigation, C.-S.L. and C.-L.K.; writing—original draft, C.-S.L.; writing—review and editing, C.-L.K. All authors have read and agreed to the published version of this manuscript.

Funding

The NSTC 113-2221-E-019-043-MY3 granted by the National Science and Technology Council, who partially supported this study, is gratefully acknowledged.

Data Availability Statement

No new data were created or analyzed in this study.

Conflicts of Interest

The authors declare no conflicts of interest.

Appendix A

In this appendix we derive Equation (3); refer to [27] for a detailed discussion of fundamental solution of the Laplace equation from the theory of distribution.
In the radial coordinate the 3D Laplace equation is written as
Δ Ψ = Ψ ( r ) + 2 r Ψ ( r ) = 0 ,
where the prime denotes the differential with respect to r. The general solution of Equation (A1) is
Ψ ( r ) = c 1 + c 2 r 1
where c 1 and c 2 are constants. Due to Ψ ( r ) 0 as r , c 1 = 0 is taken. To satisfy
Δ Ψ = δ ( x ) ,
we can determine c 2 .
For v C 0 ,
R 3 Ψ ( x ) Δ v ( x ) d x = v ( 0 )
holds in the sense of distribution. We omit c 2 in Equation (A2), and, thus, we can derive Equation (3).

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Figure 1. For example 1 (a) comparing numerical solutions obtained by MFS and NSGRBF with exact one and (b) numerical errors.
Figure 1. For example 1 (a) comparing numerical solutions obtained by MFS and NSGRBF with exact one and (b) numerical errors.
Mathematics 13 03665 g001
Figure 2. For example 1 showing the sensitivity of RMSE obtained by NSGRBF with respect to β .
Figure 2. For example 1 showing the sensitivity of RMSE obtained by NSGRBF with respect to β .
Mathematics 13 03665 g002
Figure 3. For example 3 (a) comparing numerical solutions obtained by MFS and NSGRBF with exact one and (b) numerical errors.
Figure 3. For example 3 (a) comparing numerical solutions obtained by MFS and NSGRBF with exact one and (b) numerical errors.
Mathematics 13 03665 g003
Figure 4. For example 3 showing the sensitivity of RMSE obtained by NSGRBF with respect to β .
Figure 4. For example 3 showing the sensitivity of RMSE obtained by NSGRBF with respect to β .
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Table 1. Comparing S , U and singularity for different values of β for the anisotropic Laplace equation.
Table 1. Comparing S , U and singularity for different values of β for the anisotropic Laplace equation.
β 1 1 < β < 0 0 0 < β < 2
S K 1 ( 1 β / 2 ) K 1 ( I 3 a a T ) K 1 ( I 3 a a T ) ( 1 β / 2 ) K 1 ( I 3 a a T )
U 1 / r r s β ln r s r s β
Singularityone order β orderweaknon-singular
Table 2. For example 1 comparing ME and RMSE using different β .
Table 2. For example 1 comparing ME and RMSE using different β .
β 0.01 0.005 0.001 0.0010.0050.01
ME 9.66 × 10 4 4.66 × 10 4 8.90 × 10 5 8.02 × 10 5 4.80 × 10 4 9.60 × 10 4
RMSE 4.63 × 10 4 2.26 × 10 4 4.89 × 10 5 3.97 × 10 5 2.31 × 10 4 4.61 × 10 4
Table 3. Solving example 1 by Equation (63); ME and RMSE using different β .
Table 3. Solving example 1 by Equation (63); ME and RMSE using different β .
β 0.00010.81.01.51.951.999
ME 6.91 × 10 8 5.11 × 10 5 5.70 × 10 5 8.02 × 10 5 3.56 × 10 5 1.03 × 10 6
RMSE 2.99 × 10 8 2.48 × 10 5 5.70 × 10 5 3.76 × 10 5 2.07 × 10 5 6.76 × 10 7
Table 4. Solving example 1 by Equation (63); ME and RMSE using different m.
Table 4. Solving example 1 by Equation (63); ME and RMSE using different m.
m2564100144225400625
ME 2.61 × 10 1 8.18 × 10 4 1.09 × 10 5 1.67 × 10 6 8.48 × 10 8 6.85 × 10 8 6.91 × 10 8
RMSE 1.18 × 10 1 2.65 × 10 4 3.38 × 10 6 5.44 × 10 7 4.72 × 10 8 2.80 × 10 8 2.99 × 10 8
Table 5. Solving example 2 by Equation (64); ME and RMSE using different β .
Table 5. Solving example 2 by Equation (64); ME and RMSE using different β .
β 0.0001 0.00010.00050.01
ME 6.79 × 10 6 5.94 × 10 6 7.30 × 10 6 2.64 × 10 5
RMSE 1.29 × 10 6 1.12 × 10 6 2.31 × 10 6 1.94 × 10 5
Table 6. Solving example 1 by Equation (64); ME and RMSE using different m.
Table 6. Solving example 1 by Equation (64); ME and RMSE using different m.
m2564144225400625
ME 7.64 × 10 2 2.90 × 10 4 5.01 × 10 5 2.42 × 10 5 7.94 × 10 6 5.94 × 10 6
RMSE 5.65 × 10 2 1.33 × 10 4 5.56 × 10 6 2.85 × 10 6 1.57 × 10 6 1.12 × 10 6
Table 7. Solving example 2 by Equation (65); ME and RMSE using different D.
Table 7. Solving example 2 by Equation (65); ME and RMSE using different D.
D467101520
ME 1.12 × 10 3 1.07 × 10 3 1.19 × 10 3 4.97 × 10 4 2.90 × 10 4 9.19 × 10 4
RMSE 8.47 × 10 4 7.06 × 10 4 7.68 × 10 4 3.79 × 10 4 1.72 × 10 4 4.36 × 10 4
Table 8. Solving example 3 by Equation (64); ME and RMSE using different β .
Table 8. Solving example 3 by Equation (64); ME and RMSE using different β .
β 0.99 0.01 0.00050.0010.011.99
ME1.997 5.53 × 10 2 7.62 × 10 3 7.52 × 10 3 5.28 × 10 2 0.645
RMSE0.708 4.06 × 10 2 1.40 × 10 3 1.34 × 10 3 3.87 × 10 2 0.478
Cond 2.13 × 10 13 1.49 × 10 12 1.32 × 10 10 2.56 × 10 11 2.53 × 10 9 9.27 × 10 18
Table 9. Solving example 3 by Equation (64); ME and RMSE using different D.
Table 9. Solving example 3 by Equation (64); ME and RMSE using different D.
D1.5234567
β 6.18 × 10 3 3.82 × 10 3 3.82 × 10 3 6.18 × 10 3 2.36 × 10 3 3.82 × 10 3 6.18 × 10 4
ME 1.33 × 10 4 1.19 × 10 4 1.98 × 10 4 6.65 × 10 4 9.46 × 10 4 4.36 × 10 3 6.70 × 10 3
RMSE 2.64 × 10 5 2.70 × 10 5 1.17 × 10 4 4.91 × 10 4 1.82 × 10 4 2.34 × 10 3 1.15 × 10 3
Table 10. Solving example 3 in a unit cube by Equation (64); ME and RMSE using different β .
Table 10. Solving example 3 in a unit cube by Equation (64); ME and RMSE using different β .
β 0.99 0.05 0.0010.51.99
ME 2.16 × 10 2 2.24 × 10 2 2.61 × 10 2 2.82 × 10 2 2.60 × 10 2
RMSE 9.20 × 10 3 5.93 × 10 3 4.56 × 10 3 1.07 × 10 2 6.17 × 10 3
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Liu, C.-S.; Kuo, C.-L. Non-Singular Generalized RBF Solution and Weaker Singularity MFS: Laplace Equation and Anisotropic Laplace Equation. Mathematics 2025, 13, 3665. https://doi.org/10.3390/math13223665

AMA Style

Liu C-S, Kuo C-L. Non-Singular Generalized RBF Solution and Weaker Singularity MFS: Laplace Equation and Anisotropic Laplace Equation. Mathematics. 2025; 13(22):3665. https://doi.org/10.3390/math13223665

Chicago/Turabian Style

Liu, Chein-Shan, and Chung-Lun Kuo. 2025. "Non-Singular Generalized RBF Solution and Weaker Singularity MFS: Laplace Equation and Anisotropic Laplace Equation" Mathematics 13, no. 22: 3665. https://doi.org/10.3390/math13223665

APA Style

Liu, C.-S., & Kuo, C.-L. (2025). Non-Singular Generalized RBF Solution and Weaker Singularity MFS: Laplace Equation and Anisotropic Laplace Equation. Mathematics, 13(22), 3665. https://doi.org/10.3390/math13223665

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