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Article

Novel Formulas of Specific Non-Symmetric Jacobi Polynomials with an Application in Numerical Analysis

by
Waleed Mohamed Abd-Elhameed
1,*,
Mohamed A. Abdelkawy
2,
Naher Mohammed A. Alsafri
3 and
Ahmed Gamal Atta
4
1
Department of Mathematics, Faculty of Science, Cairo University, Giza 12613, Egypt
2
Department of Mathematics and Statistics, College of Science, Imam Mohammad Ibn Saud Islamic University (IMSIU), Riyadh 11623, Saudi Arabia
3
Department of Mathematics and Statistics, College of Science, University of Jeddah, Jeddah 23831, Saudi Arabia
4
Department of Mathematics, Faculty of Education, Ain Shams University, Roxy, Cairo 11341, Egypt
*
Author to whom correspondence should be addressed.
Symmetry 2025, 17(9), 1440; https://doi.org/10.3390/sym17091440
Submission received: 29 July 2025 / Revised: 21 August 2025 / Accepted: 25 August 2025 / Published: 3 September 2025

Abstract

This paper introduces new formulas for non-symmetric Jacobi polynomials of specific parameters, focusing specifically on the subclasses where the difference between the two parameters of Jacobi polynomials is two or three. First, several key expressions of these polynomials are established, such as the power form expression and its inverse expression. After that, further essential formulas such as the derivatives of moments, linearization and connection formulas, and a formula for the repeated integrals are developed. Symbolic algebra is pivotal for summing some sums in closed forms. An application of some of the introduced formulas is included. The FitzHugh–Nagumo equation—a nonlinear differential equation arising in neuroscience—is solved using the collocation method. The presented numerical examples demonstrate the accuracy and efficiency of the proposed algorithm.

1. Introduction

Due to their unique properties and diverse applications, orthogonal polynomials are essential in pure and applied mathematics. These polynomials have imperative properties, including generating functions, recurrence relations, and differential equations (DEs). The Jacobi, Hermite, and Laguerre polynomials are examples of classical families of orthogonal polynomials. These polynomials are important in approximation theory because they are the building blocks of Fourier-like expansions of functions. These expansions make it possible to use fast numerical methods for function interpolation and spectral approximations. Some uses of orthogonal polynomials may be found in [1,2,3,4].
Investigating the sequences of polynomials is an important topic that has caught the attention of many authors due to their wide applications in several disciplines. We can categorize the sequences of polynomials into orthogonal polynomials and nonorthogonal ones. Each of the two categories has been investigated from both theoretical and practical points of view. Regarding the nonorthogonal polynomials, for example, the authors of [5] developed novel formulas regarding some Jacobsthal-type polynomials. In [6], some formulas of generalized Apostol-type polynomials were developed. Vieta Fibonacci polynomials were utilized in [7] to solve generalized Caputo fractal-fractional DEs. In [8], some explicit formulas for certain multi-poly-Bernoulli polynomials were developed. Vieta–Lucas polynomials were used in [9] to solve systems of some fractional DEs. Convolved Fermat polynomials were used in [10] to treat other fractional differential equations (FDEs). The authors of [11,12,13] investigated many polynomial sequences and introduced some applications. Some other contributions can be found in [14,15].
Many generalizations of classical orthogonal polynomials have been employed to solve differential equations. For example, some orthogonal combinations of Chebyshev polynomials were introduced in [16] and utilized for numerically treating the fractional Rayleigh–Stokes problem. The orthogonal Gegenbauer polynomials were employed in [17] to treat the time-fractional Black–Scholes model. New kinds of Chebyshev polynomials were introduced and used to solve some FDEs in [18,19].
The Jacobi polynomials (JPs) family is one of the most important families of classical orthogonal polynomials. These polynomials involve two parameters, so they generalize many well-known orthogonal sequences, such as Chebyshev and Legendre polynomials. A Sturm–Liouville-type second-order linear differential equation is satisfied by the JPs. The symmetric Jcobi polynomials are the Jacobi polynomials with identical parameters, while the non-symmetric Jacobi polynomials are polynomials with non-equal parameters. Of the most essential non-symmetric polynomials, the airfoil polynomials, also called Chebyshev polynomials of the third and fourth kinds, are the most important. These polynomials are useful when singularities occur at one endpoint, not at the other [20]. Due to the non-similarity of the parameters in the case of non-symmetric polynomials, the derivations of their formulas are more difficult than those of symmetric polynomials. The authors of [21] developed new formulas of certain non-symmetric Jacobi polynomials that generalize the third kind of Chebyshev polynomials and employed them to solve some even-order BVPs that arise in many applied sciences. In addition, both symmetric and non-symmetric polynomials are helpful for several Gaussian quadrature rules, such as Jacobi–Gauss and Jacobi–Lobatto, which are commonly employed for high-accuracy numerical integration; see [22]. Many contributions employ the JPs and their particular sequences to treat several DEs. For instance, the authors of [23] used the JPs for numerically solving some stochastic FDEs. In addition, the authors of [24] treated the Bloch equation based on the Jacobi operational matrix method. In [25], a review was performed regarding the employment of JPs to solve some partial DEs. Specific operational matrices of integrals of the shifted JPs were introduced and utilized in [26] to treat some fractional DEs. Some other integral equations were treated in [27] using specific operational matrices of the shifted JPs. A non-polynomial B-spline method introduced in [28] to handle the time-fractional nonlinear coupled Burgers’ equations using the shifted Jacobi spectral collocation method.
Regarding mathematical analysis and its practical applications, hypergeometric functions and their generalized versions are indispensable. One can express nearly all significant functions and celebrated polynomials in terms of them. These functions appear in many crucial problems related to special functions. For example, the explicit formulas for the integer derivatives of certain JPs were developed and used in [21].
Connection and linearization formulas are fundamental in the scope of special functions and their applications. Connection formulas allow the expression of a given family of polynomials as combinations of other polynomials. Thus, these formulas enable the transformation between different bases. On the other hand, the linearization formulas involve expanding the product of two or more special functions as a linear combination of other functions. These formulas are especially valuable in solving nonlinear problems and developing numerical schemes. There were many contributions devoted to investigating these formulas. For linearization formulas of some orthogonal polynomials, one can refer to [29,30,31]. Other contributions can be found in [32,33,34,35].
Spectral methods are numerical methods using orthogonal polynomials and special functions to treat several types of DEs. They have many advantages compared to some other numerical techniques; see, for example, [36,37,38]. Spectral methods involve three main versions that were used extensively to solve many DEs. The collocation method is the most commonly used method among these methods. It was used in many contributions. The authors of [39] proposed collocation methods to deal with some important models that appear in different scientific and engineering models. The authors of [40] followed a comprehensive survey focusing on polynomial matrix collocation methods. The Haar wavelet-based collocation method was employed in [41] to obtain accurate numerical solutions to Fisher’s reaction–diffusion equation. A collocation procedure was followed in [42] to treat multi-dimensional nonlinear time-fractional Schrödinger equations. In [43], the quintic B-spline collocation method was used to treat KdV-type equations. In [44], the authors proposed a fast spectral collocation method and utilized Legendre and Romanovski polynomials to handle some fractional DEs with Riesz derivatives. In [45], the authors showed how fractional B-spline collocation can solve fractional pantograph-type problems. The authors of [46] used a meshless collocation method to treat third-kind Volterra integro-DEs. The authors of [47] followed a collocation approach to deal with specific nonlinear parabolic PDEs. Lastly, the authors of [48] used the Bernstein polynomial-based collocation method to find numerical solutions to systems of Emden–Fowler-type equations.
The main aim of the current article is to establish some new formulas concerned with certain JPs that can be applied in numerical analysis. More precisely, we will deal with normalized JPs R k ( ρ , ν ) ( x ) that correspond to the following two choices of the parameters:
(i)
ν = ρ + 2 .
(ii)
ν = ρ + 3 .
Many new formulas for the polynomials R k ( ρ , ρ + 2 ) ( x ) will be established, while we will give an account of the derivation of formulas of the polynomials R k ( ρ , ρ + 3 ) ( x ) .
The main aims of the current paper can be summarized in the following points:
  • Introducing some new fundamental formulas of the polynomials R k ( ρ , ρ + 2 ) ( x ) that will be pivotal to developing further formulas of these polynomials.
  • Developing new derivatives of the moments of the polynomials R k ( ρ , ρ + 2 ) ( x ) .
  • Introducing some linearization formulas involving the polynomials R k ( ρ , ρ + 2 ) ( x ) .
  • Presenting a repeated integral formula for R k ( ρ , ρ + 2 ) ( x ) .
  • Introducing some other derivative expressions for different polynomials as combinations of the polynomials R k ( ρ , ρ + 2 ) ( x ) .
  • Presenting some fundamental formulas of the polynomials R k ( ρ , ρ + 3 ) ( x ) .
  • Presenting an application to solve the FitzHugh–Nagumo equation using the collocation method.
The remainder of the paper is organized as follows. The next section displays an overview of the JPs and some of their particular classes. Some new essential formulas of the polynomials R k ( ρ , ρ + 2 ) ( x ) are given in Section 3. Section 4 is devoted to developing the derivatives of the moments of these classes of polynomials and introducing some basic expressions as special cases. Some new linearization formulas are found in Section 5. A new expression for the repeated integrals is presented in Section 6. Some other derivative expressions are presented in Section 7. Some essential formulas for another class of JPs are given in Section 8. Section 9 presents an application in numerical analysis. Finally, some conclusions are reported in Section 10.

2. Fundamentals and Key Formulas

This section presents an account of the JPs and some essential formulas. It also provides an overview of Zeilberger’s algorithm.

2.1. An Overview of JPs

The set of orthogonal polynomials P ( ν , θ ) ( x ) 0 , defined on [ 1 , 1 ] , with ν > 1 and θ > 1 , (see, [49,50,51]), can be generated using the next Rodrigues formula:
P ( ν , θ ) ( x ) = ( 1 ) 2 ! ( 1 x ) ν ( 1 + x ) θ d d x ( 1 x ) ν + ( 1 + x ) θ + .
P ( ν , θ ) ( x ) may also be represented using the following hypergeometric form:
P ( ν , θ ) ( x ) = ( ν + 1 ) ! F 1 2 , + ν + θ + 1 ν + 1 1 x 2 ,
where ( z ) represents the Pochhammer symbol defined by
( z ) = Γ ( z + ) Γ ( z ) .
It is beneficial to employ the following normalized JPs that were first introduced in [52].
R ( ν , θ ) ( x ) = F 1 2 , + ν + θ + 1 ν + 1 1 x 2 .
The expression in (1) implies that
R ( ν , θ ) ( 1 ) = 1 , = 0 , 1 , 2 , .
It is straightforward to derive analogues for R ( ν , θ ) ( x ) from any relations or formulas for P ( ν , θ ) ( x ) . The orthogonality property of R ( ν , θ ) ( x ) can be written as
1 1 ( 1 x ) ν ( 1 + x ) θ R ( ν , θ ) ( x ) R k ( ν , θ ) ( x ) d x = 0 , k , h ν , θ , k = ,
where
h ν , θ = 2 ν + θ + 1 ! Γ ( + θ + 1 ) Γ ( ν + 1 ) 2 ( 2 + ν + θ + 1 ) Γ ( + ν + θ + 1 ) Γ ( + ν + 1 ) .
It is remarkable that the following six specific families of the normalized JPs R ( ν , θ ) ( x ) are presented.
T ( x ) = R ( 1 2 , 1 2 ) ( x ) , U ( x ) = ( + 1 ) R ( 1 2 , 1 2 ) ( x ) , V ( x ) = R ( 1 2 , 1 2 ) ( x ) , W ( x ) = ( 2 + 1 ) R ( 1 2 , 1 2 ) ( x ) , C ( α ) ( x ) = R ( α 1 2 , α 1 2 ) ( x ) , L ( x ) = R ( 0 , 0 ) ( x ) ,
where T ( x ) , U ( x ) , V ( x ) , and W ( x ) are the first, second, third, and fourth kinds of Chebyshev polynomials (CPs), respectively, while C ( α ) ( x ) and L ( x ) stand for the ultraspherical and Legendre polynomials, respectively.
It is to be noted here that the four kinds of CPs have a unified recurrence relation. That is, if ϕ k ( x ) is any one of the four kinds of CPs, then the following recursive formula is satisfied:
x ϕ k ( x ) = 2 x ϕ k 1 ( x ) ϕ k 2 ( x ) ,
but with different initials.
Among the important formulas regarding the normalized JPs are the analytic form of these polynomials and their inverse expression. The following two lemmas present these formulas.
Lemma 1.
For any non-negative integer m, R m ( ρ , ν ) ( x ) has the following representation [53]:
R m ( ρ , ν ) ( x ) = r = 0 m 1 2 r ( m ) r ( m + ρ + ν + 1 ) r r ! ( ρ + 1 ) r F 1 2 m + r , m + r + ρ + ν + 1 r + ρ + 1 1 2 x r .
Lemma 2.
For any non-negative integer m, the inverse expression to (4) is [53]
x m = m ! Γ ( ρ + 1 ) n = 0 m 2 n Γ ( n + ρ + 1 ) Γ ( n + ρ + ν + 1 ) ( m n ) ! n ! Γ ( 2 n + ρ + ν + 1 ) F 1 2 m + n , n + ρ + 1 2 n + ρ + ν + 2 2 R n ( ρ , ν ) ( x ) .
Remark 1.
The two terminating hypergeometric functions that appear in (4) and (5) have no closed forms in general, but for specific values of μ and ν, they can be reduced. The reductions of such formulas lead to the development of new formulas of the JPs.
Remark 2.
In [21], the authors developed new formulas for the power form representation and its inversion formula for the polynomials R k ( ρ , ρ + 1 ) ( x ) . Thus, many important formulas regarding these polynomials were developed.
Remark 3.
This paper concentrates on developing new formulas for the JPs R k ( ρ , ρ + 2 ) ( x ) . The key to such formulas is the development of the analytic formula and its inversion formula in reduced forms that do not involve any hypergeometric functions. From now on, we will denote R k ( ρ , ρ + 2 ) ( x ) by V k ( ρ ) ( x ) .

2.2. An Account on Zeilberger’s Algorithm

This part is confined to giving an account of Zeilberger’s algorithm. This algorithm is highly effective in obtaining closed forms for complicated summations; specifically, this algorithm aims to find a recurrence relation that is satisfied by the summation S n = k = 0 n F k , n . The Maple software can be used via the “sumrecursion command” for this purpose.
It is worth mentioning that after determining the recurrence relation that satisfies the sum, it can be solved exactly using a suitable symbolic algebra algorithm in some cases. The algorithm of Petkovsek [54], or the improved one of van Hoeij [55], may be used. In addition, the package in Maple software called “LREtools[hypergeomsols]” may be used for this purpose.
Remark 4.
Most essential problems in special functions, such as connection, linearization, moments formulas, derivatives, and repeated integral expressions, involve terminating hypergeometric functions of specific arguments. In many cases, these hypergeometric functions can be summed using Zeilberger’s algorithm, which is very important in special functions.

3. New Essential Formulas of the Polynomials V k ( ρ ) ( x )

This section is confined to presenting some new essential formulas of the polynomials V k ( ρ ) ( x ) that will be the fundamental basis of these polynomials. We will derive the following three important essential formulas:
  • The power form representation of these polynomials.
  • The inversion formula of these polynomials.
  • A new connection formula for the symmetric JPs with the polynomials R k ( ρ , ρ + 2 ) ( x ) .

3.1. The Analytic Form of V k ( ρ ) ( x ) and Its Inverse Formula

In this part, we will develop two new fundamental formulas of V k ( ρ ) ( x ) . More precisely, we will state and prove two lemmas regarding the series expression of the polynomials V k ( ρ ) ( x ) and their inverse formula. These two formulas will be the key to developing further important formulas for these polynomials.
Lemma 3.
Let k be a non-negative integer. The polynomials V k ( ρ ) ( x ) have the following power form representation:
V k ( ρ ) ( x ) = k ! Γ ( ρ + 1 ) π Γ ( 3 + k + 2 ρ ) × = 0 k 2 ( 1 ) 2 2 + k 2 + 2 ρ ( 1 + k 2 + ρ ) Γ 3 2 + k + ρ ! ( k 2 ) ! x k 2 + = 0 k 2 ( 1 ) + 1 2 2 + k 2 + 2 ρ Γ 3 2 + k + ρ ! ( k 2 1 ) ! x k 2 1 ,
and z represents the floor function.
Proof. 
Setting ν = ρ + 2 in Formula (4), yields
V k ( ρ ) ( x ) = Γ ( ρ + 1 ) ( ρ + 1 ) k Γ ( 1 + k + ρ ) = 0 k 2 k + ( + 1 ) k ( 3 + k + 2 ρ ) k ( k ) ! ( ρ + 1 ) k × F 1 2 , 3 + 2 k + 2 ρ 1 + k + ρ | 1 2 x k .
For summing the hypergeometric function in (7), let
G , k = F 1 2 , 3 + 2 k + 2 ρ 1 + k + ρ | 1 2 .
In virtue of Zeilberger’s algorithm (see, Koepf [54]), it can be deduced that G , k obeys the following second-order recursive formula:
( 1 ) ( 4 + 2 k + 2 ρ ) G 2 , k + 4 ( 2 + k + ρ ) G 1 , k + 4 ( 1 + k + ρ ) ( 2 + k + ρ ) G , k = 0 , G 0 , k = 1 , G 1 , k = 1 k + ρ ,
whose solution can be explicitly given as
G , k = 1 π ( 1 ) 2 Γ + 1 2 ( 2 + k + ρ ) 2 , even , 2 ( 1 ) + 1 2 Γ 2 + 1 ( 1 + k + ρ ) + 1 2 , odd ,
and, therefore, Formula (6) can be obtained. □
The following lemma presents the inversion formula for the analytic formula in (6).
Lemma 4.
For every non-negative integer k, the following inversion formula holds:
x k = 2 2 k 2 ρ π ( 2 + k + ρ ) k ! Γ ( ρ + 1 ) × = 0 k 2 3 2 + k 2 + ρ Γ ( 3 + k 2 + 2 ρ ) ( 1 + k 2 + ρ ) ( 2 + k 2 + ρ ) ! ( k 2 ) ! Γ 5 2 + k + ρ V k 2 ( ρ ) ( x ) + 2 1 k 2 ρ π k ! Γ ( ρ + 1 ) × = 0 k 1 2 1 2 + k 2 + ρ Γ ( 2 + k 2 + 2 ρ ) ( k 2 + ρ ) ( 1 + k 2 + ρ ) ! ( k 2 1 ) ! Γ 3 2 + k + ρ V k 2 1 ( ρ ) ( x ) .
Proof. 
If we set ν = ρ + 2 in (5), then we get
x k = k ! Γ ( ρ + 1 ) = 0 k 2 k Γ ( 1 + k + ρ ) Γ ( 3 + k + 2 ρ ) ( k ) ! ! Γ ( 3 + 2 k 2 + 2 ρ ) × F 1 2 , 1 + k + ρ 2 ( 2 + k + ρ ) | 2 V k ( ρ ) ( x ) .
We will simplify the last formula using symbolic algebra. To this end, set
H , k = F 1 2 , 1 + k + ρ 2 ( 2 + k + ρ ) | 2 .
Again, Zeilberger’s algorithm enables one to show that H , k obeys the following recursive formula:
( 1 ) ( 5 2 k + 2 ρ ) ( 4 k + ρ ) ( 2 k + ρ ) 2 H 2 , k ( 7 2 k + 2 2 ρ ) ( 5 2 k + 2 2 ρ ) ( 3 k + ρ ) ( 2 + k + ρ ) H 1 , k + ( 7 2 k + 2 2 ρ ) ( 5 2 k + 2 2 ρ ) ( 3 k + ρ ) 2 ( 2 k + ρ ) H , k = 0 ,
governed by the following initial values:
H 0 , k = 1 , H 1 , k = 1 k + ρ + 1 .
whose solution can be explicitly given as
H , k = 1 π ( 2 + k + ρ ) ( 2 + k + ρ ) Γ + 1 2 5 2 + k + ρ 2 , even , 2 Γ 1 + 2 5 2 + k + ρ 1 2 , odd ,
and, accordingly, relation (8) can be obtained. □

3.2. Some Connection Formulas Between Some Classes of JPs

In this part, we will develop a new connection formula between the symmetric JPs and the polynomials V k ( ρ ) ( x ) . First, we give the general connection formulas between two classes of normalized JPs.
Theorem 1
([50]). The following connection formula holds for every positive integer n:
R n ( ρ , θ ) ( x ) = n ! Γ ( ρ + 1 ) Γ ( 1 + γ ) Γ ( 1 + n + ρ + θ ) × k = 0 n Γ ( 1 k + n + γ ) Γ ( 1 k + n + γ + δ ) Γ ( 1 k + 2 n + ρ + θ ) k ! ( n k ) ! Γ ( 1 2 k + 2 n + γ + δ ) Γ ( 1 k + n + ρ ) × F 2 3 k , 1 k + n + γ , 1 k + 2 n + ρ + θ 2 2 k + 2 n + γ + δ , 1 k + n + ρ | 1 R n k ( γ , δ ) ( x ) .
Remark 5.
The F 2 3 ( 1 ) that appears in (11) may be reduced for particular parameters of the four parameters that appear ρ , θ , γ , and δ. The following corollary exhibits the connection formula between the two JPs R n ( ρ , ρ ) ( x ) and V n ( ρ ) ( x ) .
Corollary 1.
The following connection formula holds:
R n ( ρ , ρ ) ( x ) = ( 1 + n + 2 ρ ) ( 2 + n + 2 ρ ) 2 ( 1 + n + ρ ) ( 1 + 2 n + 2 ρ ) V n ( ρ ) ( x ) + n ( 1 + n + 2 ρ ) 2 ( n + ρ ) ( 1 + n + ρ ) V n 1 ( ρ ) ( x ) + ( n 1 ) n 2 ( n + ρ ) ( 1 + 2 n + 2 ρ ) V n 2 ( ρ ) ( x ) .
Proof. 
The substitution by θ = γ = ρ , and δ = ρ + 2 in (11) yields
R n ( ρ , ρ ) ( x ) = n ! Γ ( 1 + n + 2 ρ ) k = 0 n Γ ( 3 k + n + 2 ρ ) Γ ( 1 k + 2 n + 2 ρ ) k ! ( k + n ) ! Γ ( 3 2 k + 2 n + 2 ρ ) × F 2 3 k , 1 k + n + ρ , 1 k + 2 n + 2 ρ 4 2 k + 2 n + 2 ρ , 1 k + n + ρ | 1 V n k ( ρ ) ( x ) .
Based on the identity
F 2 3 k , 1 k + n + ρ , 1 k + 2 n + 2 ρ 4 2 k + 2 n + 2 ρ , 1 k + n + ρ | 1 = 1 , n = 0 , 1 1 + n + ρ , n = 1 , 1 ( n + ρ ) ( 1 + 2 n + 2 ρ ) , n = 2 ,
the following connection formula holds:
R n ( ρ , ρ ) ( x ) = ( 1 + n + 2 ρ ) ( 2 + n + 2 ρ ) 2 ( 1 + n + ρ ) ( 1 + 2 n + 2 ρ ) V n ( ρ ) ( x ) + n ( 1 + n + 2 ρ ) 2 ( n + ρ ) ( 1 + n + ρ ) V n 1 ( ρ ) ( x ) + ( n 1 ) n 2 ( n + ρ ) ( 1 + 2 n + 2 ρ ) V n 2 ( ρ ) ( x ) .
The proof is complete. □

4. Derivatives of the Moments of V k ( ρ ) ( x )

Based on the basic formula that was developed in the previous section, this section is devoted to deriving the derivatives of the moments of the JPs V n ( ρ ) ( x ) . Two essential formulas can be obtained from this formula as particular cases.
Theorem 2.
Consider the three positive integers k , n , and m with k + n m . The following formula holds:
D m x n V k ( ρ ) ( x ) = 2 1 + m n k ! Γ ( 3 + k + 2 ρ ) × r = 0 1 2 ( k + n m ) ( 3 + 2 k 2 m + 2 n 4 r + 2 ρ ) Γ ( 3 + k m + n 2 r + 2 ρ ) ( 1 + k m + n 2 r + ρ ) ( 2 + k m + n 2 r + ρ ) ( k m + n 2 r ) ! × s = 0 r ( 1 ) s ( 1 + k + n 2 s ) ! Γ 3 2 + k s + ρ ( 1 + k 2 s ) ! s ! × 4 ( 1 + r s ) ! Γ 3 2 + k m + n r s + ρ + ( k + n 2 s ) ( 1 + k 2 s + ρ ) ( 2 + k m + n 2 s + ρ ) ( k 2 s ) ( r s ) ! Γ 5 2 + k m + n r s + ρ V k + n m 2 r ( ρ ) ( x ) + 2 m n k ! Γ ( 3 + k + 2 ρ ) × r = 0 1 2 ( k + n m 1 ) ( 1 + 2 k 2 m + 2 n 4 r + 2 ρ ) Γ ( 2 + k m + n 2 r + 2 ρ ) ( k m + n 2 r + ρ ) ( 1 + k m + n 2 r + ρ ) ( 1 + k m + n 2 r ) ! × s = 0 r ( 1 ) s ( 1 + k + n 2 s ) ! ( k m + n 2 m s + n ρ ) Γ 3 2 + k s + ρ ( k 2 s ) ! ( r s ) ! s ! Γ 3 2 + k m + n r s + ρ V k + n m 2 r 1 ( ρ ) ( x ) .
Proof. 
The analytic form in (6) allows expressing D m x n V k ( ρ ) ( x ) in the following form:
D m x n V k ( ρ ) ( x ) = s = 0 k 2 A ¯ s , k , n , m x k + n 2 s m + s = 0 k 1 2 B ¯ s , k , n , m x k + n 2 s m 1 ,
where
A ¯ s , k , n , m = ( 1 ) s 2 2 + k 2 s + 2 ρ ( 1 + k 2 s + ρ ) k ! Γ ( ρ + 2 ) Γ 3 2 + k s + ρ ( 1 + k m + n 2 s ) m π ( ρ + 1 ) ( k 2 s ) ! s ! ( 2 + k + 2 ρ ) ! , B ¯ s , k , n , m = ( 1 ) s + 1 2 2 + k 2 s + 2 ρ k ! Γ ( ρ + 1 ) Γ 3 2 + k s + ρ ( k m + n 2 s ) m π ( 1 + k 2 s ) ! s ! Γ ( 3 + k + 2 ρ ) .
Formula (8) converts the preceding expression to the following one:
D m x n V k ( ρ ) ( x ) = s = 0 k 2 A ¯ s , k , n , m r = 0 1 2 ( k + n 2 s m ) F r , k + n 2 s m V k + n 2 s m 2 r ( ρ ) ( x ) + r = 0 1 2 ( k + n 2 s m 1 ) G r , k + n 2 s m V k + n 2 s m 2 r 1 ( ρ ) ( x ) + s = 0 k 1 2 B ¯ s , k , n , m r = 0 1 2 ( k + n 2 s m 1 ) F r , k + n 2 s m 1 V k + n 2 s m 2 r 1 ( ρ ) ( x ) + r = 0 1 2 ( k + n 2 s m 2 ) G r , k + n 2 s m 1 V k + n 2 s m 2 r 2 ( ρ ) ( x ) ,
where F i , k and G i , k are given, respectively, by the following forms:
F i , k = 2 4 i + k ( 2 + k + ρ ) k ! Γ ( 1 2 i + k + ρ ) Γ ( 3 2 i + k + 2 ρ ) ( 2 2 i + k + ρ ) i ! ( 2 i + k ) ! Γ ( ρ + 1 ) Γ ( 3 4 i + 2 k + 2 ρ ) 5 2 2 i + k + ρ i ,
G i , k = 2 2 k 2 ρ π ( 1 4 i + 2 k + 2 ρ ) ( k + 1 ) ! Γ ( 2 2 i + k + 2 ρ ) ( 1 + k ) ( 2 i + k + ρ ) ( 1 2 i + k + ρ ) i ! ( 2 i + k 1 ) ! Γ ( ρ + 1 ) Γ 3 2 i + k + ρ .
Some lengthy manipulation converts (18) to the more convenient one:
D m x n V k ( ρ ) ( x ) = r = 0 1 2 ( k + n m ) s = 0 r A ¯ s , k , n , m F r s , k + n 2 s m + B ¯ s , k , n , m G r s 1 , k + n 2 s m 1 V k + n m 2 r ( ρ ) ( x ) + r = 0 1 2 ( k + n m 1 ) s = 0 r A ¯ s , k , n , m G r s , k + n m 2 s + B ¯ s , k , n , m F r s , k + n 2 s m 1 V k + n 2 r m 1 ( ρ ) ( x ) ,
which can be written in the form
D m x n V k ( ρ ) ( x ) = r = 0 1 2 ( k + n m ) s = 0 r H r , s , k , n , m V k + n m 2 r ( ρ ) ( x ) + r = 0 1 2 ( k + n m 1 ) s = 0 r H ¯ r , s , k , n , m V k + n 2 r m 1 ( ρ ) ( x ) ,
where the coefficients H r , s , k , n , m and H ¯ r , s , k , n , m , are respectively given by
H r , s , k , n , m = ( 1 ) s 2 1 + m n ( 3 + 2 k 4 r 2 m + 2 n + 2 ρ ) k ! ( k 2 s + n 1 ) ! ( 1 + k 2 r m + n + ρ ) ( 2 + k 2 r m + n + ρ ) ( k 2 s 1 ) ! s ! × Γ 3 2 + k s + ρ Γ ( 3 + k 2 r m + n + 2 ρ ) ( k 2 r m + n ) ! Γ ( 3 + k + 2 ρ ) × 4 ( r s 1 ) ! Γ 3 2 + k s r m + n + ρ + ( k 2 s + n ) ( 1 + k 2 s + ρ ) ( 2 + k 2 s m + n + ρ ) ( k 2 s ) ( r s ) ! Γ 5 2 + k s r m + n + ρ ,
H ¯ r , s , k , n , m = ( 1 ) s 2 m n k ( 1 + 2 k 4 r 2 m + 2 n + 2 ρ ) ( k m 2 s m + n + n ρ ) ( k 1 ) ! ( k 2 s + n 1 ) ! ( k 2 r m + n + ρ ) ( 1 + k 2 r m + n + ρ ) ( k 2 s ) ! s ! ( r s ) ! ( k 2 r m + n 1 ) ! × Γ 3 2 + k s + ρ Γ ( 2 + k 2 r m + n + 2 ρ ) Γ 3 2 + k s r m + n + ρ Γ ( 3 + k + 2 ρ ) .
Now, Formula (22) can be expressed as in (16). This proves Theorem 2. □
Remark 6.
We comment here that two important formulas can be deduced from Formula (16) as special cases. More precisely, we can deduce the following two expressions:
  • The high-order derivatives of V k ( ρ ) ( x ) in terms of their original ones.
  • The moment formula of V k ( ρ ) ( x ) .
The following two corollaries exhibit these results.
Corollary 2.
The derivatives of V k ( ρ ) ( x ) can be expressed as
D m V k ( ρ ) ( x ) = r = 0 k m 2 R r , k , m V k m 2 r ( ρ ) ( x ) + r = 0 k m 1 2 R ¯ r , k , m V k m 2 r 1 ( ρ ) ( x ) , k m ,
where
R r , k , m = 2 m 1 ( 3 2 k + 2 m + 4 r 2 ρ ) k ! Γ 3 2 + k r + ρ Γ ( 3 + k m 2 r + 2 ρ ) ( m ) r ( 1 + k m 2 r + ρ ) ( 2 + k m 2 r + ρ ) r ! ( k m 2 r ) ! Γ 5 2 + k m r + ρ Γ ( 3 + k + 2 ρ ) × 2 k 2 + m + 3 r 2 r ( m + r ) + k ( 3 + m + 2 r 2 ρ ) 3 ρ + ( m + 2 r ) ρ ρ 2 ,
R ¯ r , k , m = 2 m m ( 1 + 2 k 2 m 4 r + 2 ρ ) k ! Γ 3 2 + k r + ρ Γ ( 2 + k m 2 r + 2 ρ ) ( m + 1 ) r ( k m 2 r + ρ ) ( 1 + k m 2 r + ρ ) r ! ( k m 2 r 1 ) ! Γ 3 2 + k m r + ρ Γ ( 3 + k + 2 ρ ) .
Proof. 
Setting n = 0 in (16) yields the follwoing formula:
D m V k ( ρ ) ( x ) = 2 m 1 k ! Γ ( 3 + k + 2 ρ ) r = 0 k m 2 ( 3 + 2 k 2 m 4 r + 2 ρ ) Γ ( 3 + k m 2 r + 2 ρ ) ( 1 + k m 2 r + ρ ) ( 2 + k m 2 r + ρ ) ( k m 2 r ) ! × s = 0 r ( 1 ) s Γ 3 2 + k s + ρ s ! × 4 ( 1 + r s ) ! Γ 3 2 + k m r s + ρ + ( 1 + k 2 s + ρ ) ( 2 + k m 2 s + ρ ) ( r s ) ! Γ 5 2 + k m r s + ρ V k m 2 r ( ρ ) ( x ) + 2 m k ! Γ ( 3 + k + 2 ρ ) r = 0 1 2 ( k m 1 ) ( 1 + 2 k 2 m 4 r + 2 ρ ) Γ ( 2 + k m 2 r + 2 ρ ) ( k m 2 r + ρ ) ( 1 + k m 2 r + ρ ) ( 1 + k m 2 r ) ! × s = 0 r ( 1 ) s m ( k 2 s ) ( 1 + k 2 s ) ! Γ 3 2 + k s + ρ ( k 2 s ) ! ( r s ) ! s ! Γ 3 2 + k m r s + ρ V k 2 r m 1 ( ρ ) ( x ) .
In order to reduce the last formula, we make use of symbolic computation, and in particular, Zeilberger’s algorithm [54]. For this purpose, set
Z r , k , m = s = 0 r ( 1 ) s m ( k 2 s ) ( 1 + k 2 s ) ! Γ 3 2 + k s + ρ ( k 2 s ) ! ( r s ) ! s ! Γ 3 2 + k m r s + ρ ,
Z ¯ r , k , m = s = 0 r ( 1 ) s Γ 3 2 + k s + ρ s ! × 4 ( 1 + r s ) ! Γ 3 2 + k m r s + ρ + ( 1 + k 2 s + ρ ) ( 2 + k m 2 s + ρ ) ( r s ) ! Γ 5 2 + k m r s + ρ .
The utilization of Zelibereger’s algorithm [54] leads to the following recursive formula for Z r , k , m :
( m + r ) ( 3 + 2 k 2 m 2 r + 2 ρ ) Z r 1 , k , m + r ( 2 k 2 r + 2 ρ + 3 ) Z r , k , m = 0 ,
with the initial condition
Z 0 , k , m = m Γ k + ρ + 3 2 Γ k m + ρ + 3 2 .
Equation (31) can be exactly solved to give
Z r , k , m = Γ 3 2 + k r + ρ ( m ) r + 1 r ! Γ 3 2 + k m r + ρ .
In addition, the following recursive formula is satisfied by Z ¯ r , k , m :
( 1 + m + r ) k 2 k m 2 k r + 2 k ρ + 2 m r m ρ + 2 r 2 2 r ρ + ρ 2 + 3 k m 3 r + 3 ρ + 2 × ( 5 + 2 k 2 m 2 r + 2 ρ ) Z ¯ r 1 , k , m + r ( 2 ρ + 3 2 r + 2 k ) × k 2 k m 2 k r + 2 k ρ + 2 m r m ρ + 2 r 2 2 r ρ + ρ 2 + 5 k 3 m 7 r + 5 ρ + 7 Z ¯ r , k , m = 0 ,
with the following initial condition:
Z ¯ 0 , k , m = ( k + ρ + 1 ) ( k m + ρ + 2 ) Γ k + ρ + 3 2 Γ k m + ρ + 5 2 .
Equation (33) can be exactly solved to give
Z ¯ r , k , m = Γ 3 2 + k r + ρ ( m ) r r ! Γ 5 2 + k m r + ρ × 2 + k 2 m 3 r + 2 r ( m + r ) k ( 3 + m + 2 r 2 ρ ) + 3 ρ ( m + 2 r ) ρ + ρ 2 ,
and therefore we can write
D m V k ( ρ ) ( x ) = r = 0 k m 2 R r , k , m V k m 2 r ( ρ ) ( x ) + r = 0 1 2 ( k m 1 ) R ¯ r , k , m V k m 2 r 1 ( ρ ) ( x ) ,
where the coefficients R r , k , m and R ¯ r , k , m are given, respectively, by (26) and (27). □
Remark 7.
We comment here that the derivatives of the non-symmetric polynomials V k ( ρ ) ( x ) = V k ( ρ , ρ + 2 ) ( x ) are expressed as a combination of two sums of their original polynomials. This is due to the non-symmetry in their parameters, while the derivative formula of the symmetric Jacobi polynomials V k ( ρ , ρ ) ( x ) is expressed only in one sum [56]. This means that the derivations of the derivative formula and other formulas are more difficult in the non-symmetric case.
Corollary 3.
For all positive integers k and n, the following moment formula holds:
x n V k ( ρ ) ( x ) = 2 1 n k ! Γ ( 3 + k + 2 ρ ) r = 0 k + n 2 ( 3 + 2 k 4 r + 2 n + 2 ρ ) Γ ( 3 + k 2 r + n + 2 ρ ) ( 1 + k 2 r + n + ρ ) ( 2 + k 2 r + n + ρ ) ( k 2 r + n ) ! × s = 0 r ( 1 ) s ( k 2 s + n 1 ) ! Γ 3 2 + k s + ρ s ! ( k 2 s 1 ) ! × 4 ( r s 1 ) ! Γ 3 2 + k s r + n + ρ + ( k 2 s + n ) ( 1 + k 2 s + ρ ) ( 2 + k 2 s + n + ρ ) ( k 2 s ) ( r s ) ! Γ 5 2 + k s r + n + ρ V k + n 2 r ( ρ ) ( x ) + 2 n n ( ρ + 1 ) k ! Γ ( 3 + k + 2 ρ ) r = 0 1 2 ( k + n 1 ) ( 1 + 2 k 4 r + 2 n + 2 ρ ) Γ ( 2 + k 2 r + n + 2 ρ ) ( k 2 r + n + ρ ) ( 1 + k 2 r + n + ρ ) ( k 2 r + n 1 ) ! × s = 0 r ( 1 ) s ( k 2 s + n 1 ) ! Γ 3 2 + k s + ρ s ! ( k 2 s ) ! ( r s ) ! Γ 3 2 + k s r + n + ρ V k + n 2 r 1 ( ρ ) ( x ) .
Proof. 
Formula (36) can be followed by a direct application of (16) by setting m = 0 . □
Some specific moment formulas can be deduced in reduced forms from (36). The following corollary gives a simplified moment formula for the polynomials R k ( 1 2 , 3 2 ) ( x ) .
Corollary 4.
The following moment formula holds:
x n R k ( 1 2 , 3 2 ) ( x ) = 2 n n ! k + 1 s = 0 k + n 2 ( 1 + k 2 s + n ) ( 3 8 s + 2 n + 4 k ( 2 + k 2 s + n ) ) s ! ( n s ) ! ( 1 + 2 k 4 s + 2 n ) ( 3 + 2 k 4 s + 2 n ) R k + n 2 s ( 1 2 , 3 2 ) ( x ) + 2 2 n n ! k + 1 s = 0 1 2 ( k + n 1 ) ( k 2 s + n ) s ! ( n s 1 ) ! ( 1 + 2 k 4 s + 2 n ) ( 1 + 2 k 4 s + 2 n ) R k + n 2 s 1 ( 1 2 , 3 2 ) ( x ) .
Proof. 
Setting ρ = 1 2 in (36) yields the following formula:
x n R k ( 1 2 , 3 2 ) ( x ) = 2 2 n k + 1 r = 0 k + n 2 ( 1 + k + n 2 r ) 2 ( 1 + 2 k + 2 n 4 r ) ( 3 + 2 k + 2 n 4 r ) s = 0 r ( 1 ) s ( 1 + k + n 2 s ) ! ( k s ) ! ( 1 + k 2 s ) ! s ! × 4 ( 1 + r s ) ! ( k + n r s ) ! + 1 2 + k 2 s ( k + n 2 s ) 3 2 + k + n 2 s ( k 2 s ) ( r s ) ! ( k + n r s + 1 ) ! R k + n 2 r ( 1 2 , 3 2 ) ( x ) + 2 n + 2 n k + 1 r = 0 1 2 ( k + n 1 ) ( k + n 2 r ) 2 ( 1 + 2 k + 2 n 4 r ) ( 1 + 2 k + 2 n 4 r ) × s = 0 r ( 1 ) s ( k + n 2 s 1 ) ! ( k s ) ! ( k 2 s ) ! ( r s ) ! s ! ( k + n r s ) ! R k + n 2 r 1 ( 1 2 , 3 2 ) ( x ) .
Zeilberger’s algorithm [54] aids in obtaining the following two reduction formulas:
s = 0 r ( 1 ) s ( k + n 2 s 1 ) ! ( k s ) ! ( k 2 s ) ! ( r s ) ! s ! ( k + n r s ) ! = ( n r ) r r ! ( 2 r + k + n ) ,
s = 0 r ( 1 ) s ( 1 + k + n 2 s ) ! ( k s ) ! ( 1 + k 2 s ) ! s ! × 4 ( 1 + r s ) ! ( k + n r s ) ! + 1 2 + k 2 s ( k + n 2 s ) 3 2 + k + n 2 s ( k 2 s ) ( r s ) ! ( k + n r s + 1 ) ! = ( n r + 1 ) r ( ( 8 r 3 ) + 2 n + 4 k ( 2 r + k + n + 2 ) ) 4 r ! ( 2 r + k + n + 1 ) .
The substitution by (39) and (40) leads to the following formula:
x n R k ( 1 2 , 3 2 ) ( x ) = 2 n n ! k + 1 s = 0 k + n 2 ( 1 + k 2 s + n ) ( 3 8 s + 2 n + 4 k ( 2 + k 2 s + n ) ) s ! ( n s ) ! ( 1 + 2 k 4 s + 2 n ) ( 3 + 2 k 4 s + 2 n ) R k + n 2 s ( 1 2 , 3 2 ) ( x ) + 2 2 n n ! k + 1 s = 0 1 2 ( k + n 1 ) ( k 2 s + n ) ϕ ( k + n 2 s 1 ) s ! ( n s 1 ) ! ( 1 + 2 k 4 s + 2 n ) ( 1 + 2 k 4 s + 2 n ) R k + n 2 s 1 ( 1 2 , 3 2 ) ( x ) .
This proves Corollary 4. □

5. Some Linearization Formulas

In this section, we give some linearization formulas involving the polynomials V k ( ρ ) ( x ) .
Theorem 3.
For any two non-negative integers r and s, the following linearization formula holds:
R r ( ρ , ρ ) ( x ) R s ( ρ , ρ ) ( x ) = L 1 , r , s V r + s 2 r 2 ( ρ ) ( x ) + m = 0 min ( r , s ) L 2 , m , r , s V r + s 2 m ( ρ ) ( x ) + m = 0 min ( r , s ) L 3 , m , r , s V r + s 2 m 1 ( ρ ) ( x ) ,
where
L 1 , r , s = 4 ρ 1 s ! Γ ( ρ + 1 ) Γ 1 2 + r + ρ Γ 1 2 r + s + ρ π ( r + s + ρ ) ( s r 2 ) ! Γ 3 2 + s + ρ Γ ( 1 + r + 2 ρ ) ,
L 2 , r , s , m = 4 ρ 1 r ! s ! Γ ( ρ + 1 ) π Γ 1 2 + ρ Γ ( 1 + r + 2 ρ ) Γ ( 1 + s + 2 ρ ) × ( 1 + r + s 2 m + 2 ρ ) ( 2 + r + s 2 m + 2 ρ ) ( 1 + r + s 2 m + ρ ) ( r m ) ! ( s m ) ! m ! Γ 3 2 + r + s m + ρ × Γ 1 2 + r m + ρ Γ 1 2 + s m + ρ Γ 1 2 + m + ρ Γ ( 1 + r + s m + 2 ρ ) + ( 1 + r + s 2 m ) ( 2 + r + s 2 m ) ( 2 + r + s 2 m + ρ ) ( r m + 1 ) ! ( s m + 1 ) ! ( m 1 ) ! Γ 5 2 + r + s m + ρ × Γ 3 2 + r m + ρ Γ 3 2 + s m + ρ Γ 1 2 + m + ρ Γ ( 2 + r + s m + 2 ρ ) ,
L 3 , r , s , m = 2 1 + 2 ρ ( r + s 2 m ) ( 1 + r + s 2 m + 2 ρ ) Γ ( ρ + 1 ) Γ 1 2 + r m + ρ Γ 1 2 + s m + ρ π ( r + s 2 m + ρ ) ( 1 + r + s 2 m + ρ ) m ! Γ 1 2 + r + s 2 m + ρ × Γ ( 1 + r + s m + 2 ρ ) ( 1 + r m ) m ( 1 + s m ) m 1 2 + ρ m Γ ( 1 + r + 2 ρ ) Γ ( 1 + s + 2 ρ ) 3 2 + r + s 2 m + ρ m .
Proof. 
We start with the following linearization formula of R j ( ρ , ρ ) ( x ) [57]:
R r ( ρ , ρ ) ( x ) R s ( ρ , ρ ) ( x ) = 4 ρ Γ ( ρ + 1 ) π Γ ( 1 + r + 2 ρ ) Γ ( 1 + s + 2 ρ ) × m = 0 min ( r , s ) Γ 1 2 + r m + ρ Γ 1 2 + s m + ρ Γ ( 1 + r + s m + 2 ρ ) 1 2 + ρ r m ! Γ 1 2 + r + s 2 m + ρ 3 2 + r + s 2 m + ρ r × ( 1 + r m ) r ( 1 + s m ) r R r + s 2 m ( ρ , ρ ) ( x ) .
Based on the connection Formula (12), Formula (45), after performing some algebraic computations, leads to the linearization Formula (41). □
Now, we recall the two generalized classes of Fibonacci and Lucas polynomials that are respectively generated by the following two recursive formulas [5]:
F j A , B ( x ) = A x F j 1 A , B ( x ) + B F j 2 A , B ( x ) , F 0 A , B ( x ) = 1 , F 1 A , B ( x ) = A x , j 2 ,
L j C , D ( x ) = C x L j 1 C , D ( x ) + D L j 2 C , D ( x ) , L 0 C , D ( x ) = 2 , L 1 C , D ( x ) = C x , j 2 .
The following two theorems present the linearization formulas of the polynomials V k ( ρ ) ( x ) with the two classes of the generalized Fibonacci and Lucas polynomials.
Theorem 4.
Consider r and s to be two non-negative integers. The following linearization formula holds:
V r ( ρ ) ( x ) F s A , B ( x ) = k = 0 r M k , r , s F r + s 2 k A , B + k = 0 r M ¯ k , r , s F r + s 2 k 1 A , B ,
where
M k , r , s = 2 1 + r + 2 ρ A r ( B ) k Γ ( ρ + 1 ) B π Γ ( 3 + r + 2 ρ ) × ( A 2 ( r 1 ) r r 2 k 1 Γ 1 2 + r + ρ F 1 2 1 k , 1 r + k 1 2 r ρ | A 2 4 B + 2 B ( 1 + r + ρ ) r k Γ 3 2 + r + ρ × F 1 2 k , r + k 1 2 r ρ | A 2 4 B ) ,
M ¯ k , r , s = 2 2 + r + 2 ρ A 1 r ( B ) k r r 1 k Γ ( ρ + 1 ) Γ 3 2 + r + ρ π Γ ( 3 + r + 2 ρ ) × F 1 2 k , 1 r + k 1 2 r ρ | A 2 4 B .
Proof. 
The power form representation in (6) leads to the following linearization formula:
V r ( ρ ) ( x ) F s A , B ( x ) = r ! Γ ( ρ + 1 ) π Γ ( 3 + r + 2 ρ ) = 0 r 2 ( 1 ) 2 2 + r 2 + 2 ρ ( 1 + r 2 + ρ ) Γ 3 2 + r + ρ ( r 2 ) ! ! x r 2 + = 0 r 1 2 ( 1 ) + 1 2 2 + r 2 + 2 ρ Γ 3 2 + r + ρ ( 1 + r 2 ) ! ! x r 2 1 F s A , B ( x ) .
Based on the moment formula of F s A , B ( x ) given by [58]
x r F s A , B ( x ) = j = 0 r r j A r ( B ) j F s + r 2 j A , B ( x ) ,
then, after some manipulations, we get the following formula:
V r ( ρ ) ( x ) F s A , B ( x ) = r ! Γ ( ρ + 1 ) π Γ ( 3 + r + 2 ρ ) × ( = 0 r 2 ( 1 ) 2 2 + r 2 + 2 ρ ( 1 + r 2 + ρ ) Γ 3 2 + r + ρ ( r 2 ) ! ! × m = 0 r 2 A r + 2 ( B ) m r 2 m F r + s 2 2 m A , B ( x ) + = 0 r 1 2 ( 1 ) + 1 2 2 + r 2 + 2 ρ Γ 3 2 + r + ρ ( 1 + r 2 ) ! ! × m = 0 r 2 A 1 r + 2 ( B ) m 1 + r 2 m F r + s 2 2 m 1 A , B ( x ) ) .
Some manipulations enable us to obtain the following linearization formula:
V r ( ρ ) ( x ) F s A , B ( x ) = k = 0 r M k , r , s F r + s 2 k A , B ( x ) + k = 0 r M ¯ k , r , s F r + s 2 k 1 A , B ( x ) ,
where M k , r , s and M ¯ k , r , s are respectively given by (49) and (50). This proves Theorem 4. □
Theorem 5.
Consider r and s to be two non-negative integers. The following linearization formula holds:
V r ( ρ ) ( x ) L s C , D ( x ) = k = 0 r T k , r , s L r + s 2 k C , D + k = 0 r T ¯ k , r , s L r + s 2 k 1 C , D ,
where
T k , r , s = 2 1 + r + 2 ρ C r ( D ) k Γ ( ρ + 1 ) D π Γ ( 3 + r + 2 ρ ) × ( C 2 ( r 1 ) r r 2 k 1 Γ 1 2 + r + ρ F 1 2 1 k , 1 r + k 1 2 r ρ | C 2 4 D + 2 D ( 1 + r + ρ ) r k Γ 3 2 + r + ρ × F 1 2 k , r + k 1 2 r ρ | C 2 4 D ) . ,
T ¯ k , r , s = 2 2 + r + 2 ρ C 1 r ( D ) k r r 1 k Γ ( ρ + 1 ) Γ 3 2 + r + ρ π Γ ( 3 + r + 2 ρ ) × F 1 2 k , 1 r + k 1 2 r ρ | C 2 4 D .
Proof. 
Similar to the proof of Theorem 4, noting that the moment formula of L k C , D ( x ) is given by
x r L s C , D ( x ) = j = 0 r r j C r ( D ) j L s + r 2 j C , D ( x ) .
Theorem 6.
Let ϕ k ( x ) be any one of the four kinds of CPs. The following linearization formula holds for all positive integers r and s:
V r ( ρ ) ( x ) ϕ s ( x ) = 2 1 + 2 ρ r ! Γ ( ρ + 1 ) π Γ 5 2 + ρ Γ ( 3 + r + 2 ρ ) × k = 0 r 4 k 2 + ( ρ + 1 ) ( 3 + 2 ρ ) + r ( 3 + 4 k + 2 ρ ) Γ 3 2 + r k + ρ Γ 3 2 + k + ρ k ! ( r k ) ! ϕ s + r 2 k ( x ) 4 k = 0 r 1 Γ 3 2 + r k + ρ Γ 5 2 + k + ρ k ! ( r k 1 ) ! ϕ s + r 2 k 1 ( x ) .
Proof. 
Similar to the proof of Theorem 4. □

6. Expression for the Repeated Integral Formula

This section is interested in deriving a formula for the repeated integrals of the polynomials V k ( ρ ) ( x ) . The following theorem exhibits this result.
Theorem 7.
Let the m-times repeated integration of V k ( ρ ) ( x ) be written as
I k ( m ) ( x ) = ( m ) V k ( ρ ) ( x ) ( d x ) m = m t i m e s V k ( ρ ) ( x ) d x d x d x m t i m e s ;
the following repeated integral formula holds:
I k ( m ) ( x ) = = 0 m ξ , k , m V k + m 2 ( ρ ) ( x ) + = 0 m η , k , m V k + m 2 1 ( ρ ) ( x ) + π m 1 ( x ) ,
where π m 1 ( x ) is a polynomial of degree at most ( m 1 ) , and the coefficients ξ , k , m and η , k , m are given by
ξ , k , m = ( 1 ) + 1 2 1 m ( 3 2 k + 4 2 m 2 ρ ) k ! ( 1 + m ) L ( 1 + k 2 + m + ρ ) ( 2 + k 2 + m + ρ ) ! ( k 2 + m ) ! × Γ 3 2 + k + ρ Γ ( 3 + k 2 + m + 2 ρ ) Γ 5 2 + k + m + ρ Γ ( 3 + k + 2 ρ ) × k 2 + 2 2 + ( ρ + 1 ) ( 2 + m + ρ ) + k ( 3 2 + m + 2 ρ ) ( 3 + 2 m + 2 ρ ) ,
η , k , m = ( 1 ) + 1 2 m ( 1 + 2 k 4 + 2 m + 2 ρ ) k ! Γ 3 2 + k + ρ Γ ( 2 + k 2 + m + 2 ρ ) ( + m ) + 1 ( k 2 + m + ρ ) ( 1 + k 2 + m + ρ ) ! Γ ( k 2 + m ) Γ 3 2 + k + m + ρ Γ ( 3 + k + 2 ρ ) .
Proof. 
Integrating the analytic formula in (6) yields
I k ( m ) ( x ) = = 0 k 2 A k , ( k 2 + 1 ) m x k 2 + m + = 0 k 1 2 B k , ( k 2 ) m x k 2 + m 1 + π m 1 ( x ) ,
where
A k , = ( 1 ) 2 2 + k 2 + 2 ρ ( 1 + k 2 + ρ ) Γ 3 2 + k + ρ k ! Γ ( ρ + 1 ) π Γ ( 3 + k + 2 ρ ) ! ( k 2 ) ! , B k , = ( 1 ) + 1 k ! Γ ( ρ + 1 ) 2 2 + k 2 + 2 ρ Γ 3 2 + k + ρ π Γ ( 3 + k + 2 ρ ) ! ( k 2 1 ) ! .
Formula (62) can be written as
I k ( m ) ( x ) = = 0 k 2 G k , , m x k 2 + m + = 0 k 1 2 H k , , m x k 2 + m 1 + π m 1 ( x ) ,
where
G k , , m = A k , ( k 2 + 1 ) m , H k , , m = B k , ( k 2 ) m .
The inversion formula (8) leads to
I k ( m ) ( x ) = = 0 k 2 G k , , m i = 0 1 2 ( k + m 2 ) D i , k 2 + m V k 2 + m 2 i ( ρ ) ( x ) + i = 0 1 2 ( k + m 2 1 ) E i , k 2 + m V k 2 + m 2 i 1 ( ρ ) ( x ) + = 0 k 1 2 H k , , m i = 0 1 2 ( k + m 2 1 ) D i , k 2 + m 1 V k 2 + m 2 i 1 ( ρ ) ( x ) + i = 0 1 2 ( k + m 2 2 ) E i , k 2 + m 1 V k 2 + m 2 i 2 ( ρ ) ( x ) + π m 1 ( x ) .
Some lengthy algebraic computations convert (64) into
I k ( m ) ( x ) = 1 + 2 + π m 1 ( x ) ,
where
1 = = 0 k 2 G k , , m i = 0 1 2 ( k + m 2 ) D i , k 2 + m V k 2 + m 2 i ( ρ ) ( x ) + = 0 k 1 2 H k , , m i = 0 1 2 ( k + m 2 2 ) E i , k 2 + m 1 V k 2 + m 2 i 1 ( ρ ) ( x ) , 2 = = 0 k 2 G k , , m i = 0 1 2 ( k + m 2 1 ) E i , k 2 + m V k 2 + m 2 i 1 ( ρ ) ( x ) + = 0 k 1 2 H k , , m i = 0 1 2 ( k + m 2 1 ) D i , k 2 + m 1 V k 2 + m 2 i 2 ( ρ ) ( x ) .
Now, we can write (65) into the form
I k ( m ) ( x ) = = 0 m ξ , k , m V k + m 2 ( ρ ) ( x ) + = 0 m η , k , m V k + m 2 1 ( ρ ) ( x ) + π m 1 ( x ) ,
where the coefficients ξ k , , m , and η k , , m are given by
ξ k , , m = 2 1 m ( 3 + 2 k 4 + 2 m + 2 ρ ) k ! Γ ( 3 + k 2 + m + 2 ρ ) ( 1 + k 2 + m + ρ ) ( 2 + k 2 + m + ρ ) ( k 2 + m ) ! Γ ( 3 + k + 2 ρ ) × r = 0 ( 1 ) r Γ 3 2 + k r + ρ r ! ( r ) ! Γ 5 2 + k + m r + ρ × 2 + k 2 + 4 2 + m + 2 m r + ( 3 + m ) ρ + ρ 2 + k ( 3 4 + m + 2 ρ ) 2 ( 3 + 2 m + 2 ρ ) , η k , , m = r = 0 ( 1 ) r + 1 2 m m ( 1 + 2 k 4 L + 2 m + 2 ρ ) k ! Γ 3 2 + k r + ρ ( k 2 L + m + ρ ) ( 1 + k 2 L + m + ρ ) ( k 2 L + m 1 ) ! r ! ( r ) ! × Γ ( 2 + k 2 L + m + 2 ρ ) Γ 3 2 + k + m r + ρ Γ ( 3 + k + 2 ρ ) .
Symbolic algebra aids in simplifying the coefficients ξ k , , m , η k , , m . Zeilberger’s algorithm leads to the two reduction formulas:
r = 0 ( 1 ) r Γ 3 2 + k r + ρ r ! ( r ) ! Γ 5 2 + k + m r + ρ × 2 + k 2 + 4 2 + m + 2 m r + ( 3 + m ) ρ + ρ 2 + k ( 3 4 + m + 2 ρ ) 2 ( 3 + 2 m + 2 ρ ) = ( 1 ) ( m + 1 ) Γ 3 2 + k + ρ ! Γ 5 2 + k + m + ρ × k 2 + 2 2 + ( ρ + 1 ) ( 2 + m + ρ ) + k ( 3 2 + m + 2 ρ ) ( 3 + 2 m + 2 ρ ) ,
r = 0 ( 1 ) r + 1 Γ 3 2 + k r + ρ r ! ( r ) ! Γ 3 2 + k + m r + ρ = ( 1 ) + 1 ( m ) Γ 3 2 + k + ρ ! Γ 3 2 + k + m + ρ .
Therefore, the coefficients ξ , k , m and η , k , m can be computed to give their forms in (60) and (61). □

7. Derivatives of Some Polynomials in Terms of V k ( ρ ) ( x )

This section derives the derivative formulas for different polynomials in terms of V k ( ρ ) ( x ) .
Theorem 8.
Let H k ( x ) be the standard Hermite polynomials. The following derivative formula for H k ( x ) is valid for k m :
D m H k ( x ) = 2 3 + m 2 ρ π ( 2 + k m + ρ ) k ! Γ ( ρ + 1 ) × s = 0 k m 2 ( 3 + 2 k 4 s 2 m + 2 ρ ) Γ ( 3 + k 2 s m + 2 ρ ) ( 1 + k 2 s m + ρ ) ( 2 + k 2 s m + ρ ) s ! ( k 2 s m ) ! Γ 5 2 + k s m + ρ × F 1 3 s , ρ 2 k 2 + m 2 , 3 2 k + s + m ρ ρ 2 k 2 + m 2 1 | 1 V k m 2 s ( ρ ) ( x ) + 2 2 + m 2 ρ π k ! Γ ( ρ + 1 ) × s = 0 1 2 ( k m 1 ) ( 1 + 2 k 4 s 2 m + 2 ρ ) Γ ( 2 + k 2 s m + 2 ρ ) s ! ( k 2 s m 1 ) ! Γ k s m + ρ + 3 2 ( k 2 s m + ρ ) ( 1 + k 2 s m + ρ ) × F 0 2 s , 1 2 k + s + m ρ | 1 V k m 2 s 1 ( ρ ) ( x ) .
Proof. 
First, using the analytic form of the Hermite polynomials [50], we get
D m H k ( x ) = r = 0 k m 2 ( 1 ) r 2 k 2 r k ! ( 1 + k m 2 r ) m ( k 2 r ) ! r ! x k 2 r m .
The inversion Formula (8) transforms Formula (70) into the following form:
D m H k ( x ) = k ! Γ ( ρ + 1 ) r = 0 k m 2 ( 1 ) r 2 k 2 r ( 1 + k m 2 r ) m ( k 2 r ) ! r ! × i = 0 k m 2 r 2 4 i + k m 2 r ( 2 + k m 2 r + ρ ) ( k m 2 r ) ! ( 2 2 i + k m 2 r + ρ ) i ! ( 2 i + k m 2 r ) ! 5 2 2 i + k m 2 r + ρ i × Γ ( 1 2 i + k m 2 r + ρ ) Γ ( 3 2 i + k m 2 r + 2 ρ ) Γ ( 3 4 i + 2 k 2 m 4 r + 2 ρ ) V k 2 r m 2 i ( ρ ) ( x ) + i = 0 k m 1 2 r 2 2 k + m + 2 r 2 ρ π ( 1 4 i + 2 k 2 m 4 r + 2 ρ ) ( 2 i + k m 2 r + ρ ) ( 1 2 i + k m 2 r + ρ ) i ! × ( k m 2 r ) ! Γ ( 2 2 i + k m 2 r + 2 ρ ) ( 2 i + k m 2 r 1 ) ! Γ 3 2 i + k m 2 r + ρ V k 2 r m 2 i 1 ( ρ ) ( x ) .
The last formula leads to Formula (69) after some algebraic computations. □
Theorem 9.
Let F k A , B ( x ) be the generalized Fibonacci polynomials that are constructed by (46). The following derivative formula for F k A , B ( x ) is valid for k m :
D m F k A , B ( x ) = A k ( 2 + k m + ρ ) k ! Γ ( ρ + 1 ) × s = 0 k m 2 2 k 4 s m Γ ( 1 + k 2 s m + ρ ) Γ 5 2 + k 2 s m + ρ Γ ( 3 + k 2 s m + 2 ρ ) ( 2 + k 2 s m + ρ ) ( k 2 s m ) ! s ! Γ 5 2 + k s m + ρ Γ ( 3 + 2 k 4 s 2 m + 2 ρ ) × F 2 3 s , 3 2 k + s + m ρ , k 2 + m 2 ρ 2 k , 1 k 2 + m 2 ρ 2 | 4 B A 2 V k m 2 s ( ρ ) ( x ) + 2 2 k + m 2 ρ A k π k ! Γ ( ρ + 1 ) × s = 0 1 2 ( k m 1 ) ( 1 + 2 k 4 s 2 m + 2 ρ ) Γ ( 2 + k 2 s m + 2 ρ ) ( k 2 s m + ρ ) ( 1 + k 2 s m + ρ ) s ! ( k 2 s m 1 ) ! Γ 3 2 + k s m + ρ × F 1 2 s , 1 2 k + s + m ρ k | 4 B A 2 V k m 2 s 1 ( ρ ) ( x ) .
Proof. 
This proof is similar to that of Theorem 8. □
Theorem 10.
The derivatives of V k ( ρ ) ( x ) can be expressed in terms of the ultraspherical polynomials C k ( λ ) ( x ) as
D m V k ( ρ ) ( x ) = 2 2 + m 2 λ + 2 ρ k ! Γ ( ρ + 1 ) Γ 1 2 + k + ρ Γ 1 2 + λ Γ ( 3 + k + 2 ρ ) s = 0 k m 2 ( k + m + 2 s λ ) Γ ( k m 2 s + 2 λ ) ( k m 2 s ) ! s ! Γ ( 1 + k m s + λ ) × 4 s ( k + s + m λ ) 1 2 s m ρ + λ s 1 1 2 k ρ s 1 ( 1 + k + ρ ) ( 1 + 2 k + 2 ρ ) 1 2 s m ρ + λ s 1 2 k ρ s C k m 2 s ( λ ) ( x ) + 2 4 + m + 2 ρ 2 λ k ! Γ ( ρ + 1 ) Γ 3 2 + k + ρ Γ ( 3 + k + 2 ρ ) Γ 1 2 + λ × s = 0 1 2 ( k m 1 ) ( 1 k + 2 s + m λ ) Γ ( 1 + k 2 s m + 2 λ ) 5 2 + m + ρ λ s s ! ( k 2 s m 1 ) ! Γ ( k s m + λ ) 3 2 + k s + ρ s C k m 2 s 1 ( λ ) ( x ) .
Proof. 
This proof is similar to that of Theorem 8. □

8. Another Class of JPs

This section explains how to derive other formulas concerned with the class of JPs R k ( ρ , ρ + 3 ) ( x ) . From the preceding sections, many formulas were developed for the class of JPs R k ( ρ , ρ + 2 ) ( x ) . The derivation of such formulas was based on developing a new analytic formula for these polynomials and their inversion formula. Some other new formulas can be developed for the JPs R k ( ρ , ρ + 3 ) ( x ) by following similar approaches in the previous sections. Here, we will present these polynomials’ power form representation and inversion formula. Here, we derive new expressions for their representations.
Lemma 5.
The polynomials R m ( ρ , ρ + 3 ) ( x ) can be represented explicitly in the following form:
R m ( ρ , ρ + 3 ) ( x ) = Γ ( 1 + ρ ) π r = 0 m 2 ( 1 ) m r 2 m + 2 r ( 1 + m 4 r + ρ ) Γ 1 2 + r ( m ) m 2 r ( m + 2 ρ + 4 ) m 2 r ( m 2 r ) ! Γ ( 2 + m r + ρ ) x m 2 r + r = 0 m 1 2 ( 1 ) m r 2 1 m + 2 r ( 3 + 3 m 4 r + 3 ρ ) Γ 3 2 + r ( m ) 1 + m 2 r ( m + 2 ρ + 4 ) 1 + m 2 r ( m 2 r 1 ) ! Γ ( 2 + m r + ρ ) x m 2 r 1 .
Proof. 
Substituting by ν = ρ + 3 in Formula (4) leads to the following formula:
R m ( ρ , ρ + 3 ) ( x ) = r = 0 m 1 2 m r ( m ) m r ( m + 2 ρ + 4 ) m r ( m r ) ! ( 1 + ρ ) m r F 1 2 r , 2 m r + 2 ρ + 4 1 + m r + ρ | 1 2 x m r .
The utilization of Zeilberger’s algorithm again enables one to sum the F 1 2 ( 1 ) that appears in (75) in the following closed form:
F 1 2 r , 2 m r + 2 ρ + 4 1 + m r + ρ | 1 2 = 1 π ( 1 ) r / 2 1 + m 2 r + ρ Γ 1 + r 2 1 + m r + ρ 1 + r 2 if r is even , ( 1 ) ( r 1 ) / 2 5 3 m + 2 r 3 ρ Γ 1 + r 2 1 + m r + ρ 3 + r 2 if r is odd .
The reduction in (76) converts Formula (75) into Formula (74). □
Lemma 6.
Let m be any non-negative integer. x m can be expanded in terms of R k ( ρ , ρ + 3 ) ( x ) as in the following form:
x m = 2 3 m 2 ρ π m ! Γ ( 1 + ρ ) × n = 0 m 2 ( 3 + m + 2 n + ρ ) Γ ( 4 + m 2 n + 2 ρ ) ( 1 + m 2 n + ρ ) ( 3 + m 2 n + ρ ) ( m 2 n ) ! n ! Γ 5 2 + m n + ρ R m 2 n ( ρ , ρ + 3 ) ( x ) + n = 0 m 1 2 ( 6 + 3 m 2 n + 3 ρ ) Γ ( 3 + m 2 n + 2 ρ ) ( m 2 n + ρ ) ( 2 + m 2 n + ρ ) ( m 2 n 1 ) ! n ! Γ 5 2 + m n + ρ R m 2 n 1 ( ρ , ρ + 3 ) ( x ) .
Proof. 
The proof is similar to the proof of Lemma 4. □
Remark 8.
Following similar approaches to those followed for deriving the formula of R k ( ρ , ρ + 2 ) ( x ) , we can develop some formulas for the polynomials R k ( ρ , ρ + 3 ) ( x ) .
Remark 9.
Table 1 lists the new formulas derived in this paper with a brief description for each one.

9. An Application of JPs in Numerical Analysis

In this section, we will solve the following FitzHugh–Nagumo equation [59]:
W t = W x x W ( μ W ) ( 1 W ) , 0 < μ 1 ,
which is constrained by the following initial and boundary conditions:
W ( x , 0 ) = ξ 0 ( x ) , 0 < x 1 , W ( 0 , t ) = ξ 1 ( t ) , W ( 1 , t ) = ξ 2 ( t ) , 0 < t 1 ,
where ξ 0 ( x ) , ξ 1 ( t ) and ξ 2 ( t ) are given functions.

9.1. The Derivation of the Proposed Numerical Method

This part analyzes how to treat the FitzHugh–Nagumo equation using the collocation method.
Define the following space:
A M ( Ω ) = span { V i ( ρ ) ( x ) V j ( ρ ) ( t ) } 0 i , j M ,
where Ω = ( 0   , 1 ] 2 . Any function W M ( x , t ) A M ( Ω ) may be expressed as
W M ( x , t ) = i = 0 M j = 0 M c i j V i ( ρ ) ( x ) V j ( ρ ) ( t ) .
The following corollary, which presents the first- and second-order derivatives of the polynomials V k ( ρ ) ( x ) , is needed for the design of our proposed collocation algorithm.
Corollary 5.
The first and second derivatives of V k ( ρ ) ( x ) may be represented in the following form:
d V k ( ρ ) ( x ) d x = r = 0 k 1 2 R r , k , 1 V k 1 2 r ( ρ ) ( x ) + r = 0 k 1 1 2 R ¯ r , k , 1 V k 1 2 r 1 ( ρ ) ( x ) ,
d 2 V k ( ρ ) ( x ) d x 2 = r = 0 k 2 2 R r , k , 2 V k 2 2 r ( ρ ) ( x ) + r = 0 k 2 1 2 R ¯ r , k , 2 V k 2 2 r 1 ( ρ ) ( x ) ,
where R r , k , m and R ¯ r , k , m are defined in (26) and (27), respectively.
Proof. 
Formulas (82) and (83) are direct special cases of Formula (25), by setting m = 1 , 2 , respectively. □
Now, by using Equation (81) and Corollary 5, the residual R ( x , t ) of Equation (78) can be expressed as
R ( x , t ) = W t M ( x , t ) W x x M ( x , t ) + μ W M ( x , t ) + ( W M ( x , t ) ) 3 ( μ + 1 ) ( W M ( x , t ) ) 2 = i = 0 M j = 0 M c i j V i ( ρ ) ( x ) r = 0 j 1 2 R r , j , 1 V j 1 2 r ( ρ ) ( t ) + r = 0 j 1 1 2 R ¯ r , j , 1 V j 1 2 r 1 ( ρ ) ( t ) i = 0 M j = 0 M c i j V j ( ρ ) ( t ) r = 0 i 2 2 R r , i , 2 V i 2 2 r ( ρ ) ( x ) + r = 0 i 2 1 2 R ¯ r , i , 2 V i 2 2 r 1 ( ρ ) ( x ) + μ i = 0 M j = 0 M c i j V i ( ρ ) ( x ) V j ( ρ ) ( t ) + i = 0 M j = 0 M c i j V i ( ρ ) ( x ) V j ( ρ ) ( t ) 3 ( μ + 1 ) i = 0 M j = 0 M c i j V i ( ρ ) ( x ) V j ( ρ ) ( t ) 2 .
By virtue of the typical collocation method and letting the residual R ( x , t ) vanish at specific nodes ( x i , t j ) , we get
R ( x r , t s ) = 0 , r = 1 , 2 , 3 , , M 1 , s = 1 , 2 , 3 , , M .
Moreover, the conditions in (79) lead to
i = 0 M j = 0 M c i j V i ( ρ ) ( x r ) V j ( ρ ) ( 0 ) = ξ 0 ( x r ) , r = 1 , 2 , 3 , , M + 1 , i = 0 M j = 0 M c i j V i ( ρ ) ( 0 ) V j ( ρ ) ( t s ) = ξ 1 ( t s ) , s = 1 , 2 , 3 , , M , i = 0 M j = 0 M c i j V i ( ρ ) ( 1 ) V j ( ρ ) ( t s ) = ξ 2 ( t s ) , s = 1 , 2 , 3 , , M ,
where { ( x r , t s ) : r , s = 1 , 2 , 3 , , M + 1 } denote the first different zeros of V M + 1 ( ρ ) ( x ) and V s ( ρ ) ( t ) , respectively. Therefore, Newton’s iterative method may be employed to solve the ( M + 1 ) 2 nonlinear system presented in (85) and (86).
Remark 10.
The first distinct real zeros of the orthogonal polynomials V M + 1 ( ρ ) ( x ) for every choice of ρ can be evaluated numerically using the Mathematica program.

9.2. Two Illustrative Examples

In this section, we present two numerical examples to validate and demonstrate the applicability and accuracy of our proposed numerical algorithm. We also present comparisons with some other methods. Now, if we consider the successive errors E M and E M + 1 , then the order of convergence for the given method can be calculated as
Order = log E M + 1 E M log M + 1 M .
Example 1.
The authors of [60] considered the following equation:
W t = W x x W ( μ W ) ( 1 W ) , 0 < μ 1 ,
governed by the following constraints:
W ( x , 0 ) = 2 e x 2 + 2 , 0 < x 1 , W ( 0 , t ) = 2 e t 2 + 2 , 0 < t 1 , W ( 1 , t ) = 2 e t 2 1 2 + 2 , 0 < t 1 .
For μ = 1 , the exact solution is
W ( x , t ) = 2 2 + e t 2 x 2 .
Table 2 compares AE at t = 0.001 between our method and the method in [60]. Table 3 presents the L errors at different values of M and ρ when μ = 1 .   Figure 1 shows the absolute errors (left) and the approximate solution (right) at ρ = 0.5 , μ = 1 , and M = 14 . Also, Figure 2 illustrates the exact and the approximate solutions at ρ = 1.5 , and M = 14 . Figure 3 illustrates the stability | W M + 1 W M | at t = 0.5 and different values of x , M when ρ = 1 . Table 4 shows the L errors and the order of convergence, which is calculated by (87) at different values of M . Finally, Table 5 shows the AE at ρ = 0.5 and M = 14 . These findings show that this method’s results are close to the exact solution.
Example 2.
The authors of [61] considered the following equation:
W t = W x x W ( μ W ) ( 1 W ) , 0 < μ 1 ,
governed by the following constraints:
W ( x , 0 ) = 1 e x 2 + 1 , 0 < x 1 , W ( 0 , t ) = 1 e t / 2 + 1 , 0 < t 1 , W ( 1 , t ) = 1 2 tanh 1 4 2 t + 1 , 0 < t 1 .
For μ = 1 , the exact solution is
W ( x , t ) = 1 2 tanh 1 4 2 x t + 1 .
Table 6 shows the AE at ρ = 2 and M = 14 . In Table 7, we compare the L errors of our technique at ρ = 3 and M = 14 with those in [61]. Figure 4 illustrates the AE at different values of ρ when M = 14 . Figure 5 illustrates the exact and the approximate solutions at ρ = 2 , and M = 14 . Figure 6 illustrates the stability | W M + 1 W M | at x = t and different values of M when ρ = 3 . These findings show that this method’s results are close to the exact solution.

10. Conclusions

The paper has presented new, explicit, and simplified expressions for certain classes of the classical Jacobi polynomials. The core of the derivation of the new formulas is based on introducing some fundamental formulas of such polynomials along with the utilization of symbolic algebra and, in particular, Zeilberger’s algorithm. Many derivative expressions are expressed in terms of their original ones. Some linearization and connection formulas were also developed. To our knowledge, most of the developed formulas in this article are new. They may be helpful, particularly in spectral methods, where orthogonal polynomials are the basis of function approximation. A suggested spectral solution of the FitzHugh–Nagumo equation was explored using a collocation scheme based on the proposed polynomials and some of their developed formulas. We expect to use the introduced polynomials and their new formulas to solve other DEs that arise in the applied sciences. In addition, our proposed algorithm may be extended to solve fractional differential equations and multidimensional problems. All codes were written and debugged by Mathematica 11 on an HP Z420 Workstation, (Hewlett-Packard, Palo Alto, CA, USA) equipped with an Intel(R) Xeon(R) CPU E5-1620 v2—3.70 GHz, 16 GB DDR3 RAM, and 512 GB storage.

Author Contributions

Conceptualization, W.M.A.-E.; Methodology, M.A.A., N.M.A.A. and A.G.A.; Software, W.M.A.-E. and A.G.A.; Validation, W.M.A.-E., N.M.A.A. and A.G.A.; Formal analysis, W.M.A.-E., N.M.A.A. and A.G.A.; Investigation, W.M.A.-E., M.A.A., N.M.A.A. and A.G.A.; Writing—original draft, W.M.A.-E. and M.A.A.; Writing—review & editing, W.M.A.-E.; Funding acquisition, M.A.A. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported and funded by the Deanship of Scientific Research at Imam Mohammad Ibn Saud Islamic University (IMSIU) (grant number IMSIU-DDRSP2502).

Data Availability Statement

Data are contained within the article.

Acknowledgments

This work was supported and funded by the Deanship of Scientific Research at Imam Mohammad Ibn Saud Islamic University (IMSIU) (grant number IMSIU-DDRSP2502).

Conflicts of Interest

The authors declare no conflicts of interest.

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Figure 1. The absolute errors (left) and the approximate solution (right) for Example 1 at ρ = 0.5 , and M = 14 .
Figure 1. The absolute errors (left) and the approximate solution (right) for Example 1 at ρ = 0.5 , and M = 14 .
Symmetry 17 01440 g001
Figure 2. The exact and the approximate solutions for Example 1 at ρ = 1.5 , and M = 14 .
Figure 2. The exact and the approximate solutions for Example 1 at ρ = 1.5 , and M = 14 .
Symmetry 17 01440 g002
Figure 3. Stability | W M + 1 W M | at t = 0.5 for Example 1.
Figure 3. Stability | W M + 1 W M | at t = 0.5 for Example 1.
Symmetry 17 01440 g003
Figure 4. The AE of Example 2 at M = 14 .
Figure 4. The AE of Example 2 at M = 14 .
Symmetry 17 01440 g004
Figure 5. The exact and the approximate solutions for Example 2 at ρ = 2 , and M = 14 .
Figure 5. The exact and the approximate solutions for Example 2 at ρ = 2 , and M = 14 .
Symmetry 17 01440 g005
Figure 6. Stability | W M + 1 W M | at x = t for Example 2.
Figure 6. Stability | W M + 1 W M | at x = t for Example 2.
Symmetry 17 01440 g006
Table 1. Reference table for the new formulas in the paper.
Table 1. Reference table for the new formulas in the paper.
ItemEquation No.Brief Description
1(6)Power-series form of V k ( ρ ) ( x ) .
2(8)Inversion formula: x k expressed as finite sum of V k ( ρ ) ( x ) .
3(12)Connection formula between R n ( ρ , ρ ) ( x ) and V n ( ρ ) ( x ) .
4(16)Derivative of the moments D m x n V k ( ρ ) ( x ) in terms of V k ( ρ ) ( x ) .
5(25)Higher-order derivative expression of V k ( ρ ) ( x ) in terms of their original ones.
6(36)General moment formula: x n V k ( ρ ) ( x ) expanded in V k ( ρ ) ( x ) .
7(37)Special moment formula for x n R k ( 1 2 , 3 2 ) ( x ) in terms of their original ones.
8(41)Linearization formula: R r ( ρ , ρ ) ( x ) R s ( ρ , ρ ) ( x ) expanded in V k ( ρ ) ( x ) .
9(48)Linearization of V r ( ρ ) ( x ) F s A , B ( x ) in the F k A , B ( x ) basis.
10(54)Linearization of V r ( ρ ) ( x ) L s C , D ( x ) in the L k C , D ( x ) basis.
11(58)Unified linearization formula with Chebyshev family polynomials.
12(59)Repeated integral formula of V k ( ρ ) ( x ) in terms of their original ones.
13(69)Derivative representation of Hermite polynomials D m H k ( x ) in terms of  V k ( ρ ) ( x ) .
14(72)Derivative representation of the generalized Fibonacci polynomials D m F k A , B ( x ) in terms of V k ( ρ ) ( x ) .
15(73)Derivative representation of V k ( ρ ) ( x ) in terms of the ultraspheical polynomials C k ( λ ) ( x ) .
16(74)Power form expression of V k ( ρ , ρ + 3 ) ( x ) .
17(77)Inversion formula of V k ( ρ , ρ + 3 ) ( x ) .
Table 2. Comparison of the AE of Example 1 at t = 0.001 .
Table 2. Comparison of the AE of Example 1 at t = 0.001 .
x Method in [60] Our Method at M = 14
ρ = 1 ρ = 1 . 5 ρ = 2
0.0000 9.2601 × 10 9 4.3299 × 10 15 3.6637 × 10 15 1.9096 × 10 14
0.0010 9.2669 × 10 9 3.8858 × 10 15 3.4417 × 10 15 1.7764 × 10 14
0.0020 9.2734 × 10 9 3.5527 × 10 15 3.2196 × 10 15 1.6764 × 10 14
0.0030 9.2798 × 10 9 3.4417 × 10 15 2.9976 × 10 15 1.5654 × 10 14
0.0040 9.2865 × 10 9 3.2196 × 10 15 2.6645 × 10 15 1.4655 × 10 14
0.0050 9.2929 × 10 9 2.9976 × 10 15 2.5535 × 10 15 1.3767 × 10 14
0.0060 9.2995 × 10 9 2.6645 × 10 15 2.3315 × 10 15 1.2657 × 10 14
Table 3. The L errors of Example 1.
Table 3. The L errors of Example 1.
M 3691214
ρ = 0.5 1.6209 × 10 4 6.1180 × 10 8 4.4869 × 10 11 1.5876 × 10 14 2.7756 × 10 16
ρ = 1.0 1.6335 × 10 4 6.0508 × 10 8 5.3315 × 10 11 2.0706 × 10 14 6.6613 × 10 16
Table 4. The L errors and order of convergence for Example 1.
Table 4. The L errors and order of convergence for Example 1.
M ErrorOrder
2 7.6096 × 10 4 0.7661
3 1.6335 × 10 4 1.0596
4 8.6370 × 10 6 0.9813
5 1.7019 × 10 6 1.1239
6 6.0508 × 10 8 1.0153
7 1.0983 × 10 8 1.0859
8 5.8034 × 10 10 1.0526
9 5.3315 × 10 11 1.0739
10 2.7471 × 10 12 1.0505
11 2.2538 × 10 13 1.0441
12 2.0706 × 10 14 1.0300
13 2.8311 × 10 15 1.0139
14 6.6613 × 10 16
Table 5. The AE of Example 1 at ρ = 0.5 and M = 14 .
Table 5. The AE of Example 1 at ρ = 0.5 and M = 14 .
x t = 0.3 t = 0.6 t = 0.9
0.10 1.1102 × 10 16 1.1102 × 10 16
0.20 5.5511 × 10 17 1.6653 × 10 16
0.3 5.5511 × 10 17 5.5511 × 10 17 1.1102 × 10 16
0.4 5.5511 × 10 17 5.5511 × 10 17 1.1102 × 10 16
0.5000
0.6 5.5511 × 10 17 00
0.7 5.5511 × 10 17 00
0.8 8.3267 × 10 17 00
0.9 2.7756 × 10 17 5.5511 × 10 17 4.4409 × 10 16
Table 6. The AE of Example 2 at ρ = 2 and M = 14 .
Table 6. The AE of Example 2 at ρ = 2 and M = 14 .
x t = 0.3 t = 0.6 t = 0.9
0.1 3.9205 × 10 16 3.8164 × 10 16 3.6082 × 10 16
0.2 9.7145 × 10 17 1.0408 × 10 16 6.9389 × 10 17
0.3 1.9949 × 10 16 2.8450 × 10 16 2.9837 × 10 16
0.4 1.8735 × 10 16 2.6888 × 10 16 2.8450 × 10 16
0.5 2.2205 × 10 16 2.5327 × 10 16 3.4348 × 10 16
0.6 2.2205 × 10 16 4.6144 × 10 16 4.4929 × 10 16
0.7 1.5266 × 10 16 4.3715 × 10 16 5.9501 × 10 16
0.8 1.1102 × 10 16 3.4695 × 10 16 4.6491 × 10 16
0.9 2.4980 × 10 16 3.8858 × 10 16 1.7347 × 10 16
Table 7. Comparison of L errors for Example 2.
Table 7. Comparison of L errors for Example 2.
tMethod in [61]Our Method at ρ = 3 and M = 14
0.2 8.712 × 10 6 4.8572 × 10 16
0.4 3.395 × 10 5 2.2205 × 10 16
0.6 6.511 × 10 5 2.5674 × 10 16
0.8 2.612 × 10 4 5.2181 × 10 15
1.0 3.064 × 10 6 2.8232 × 10 13
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Abd-Elhameed, W.M.; Abdelkawy, M.A.; Alsafri, N.M.A.; Atta, A.G. Novel Formulas of Specific Non-Symmetric Jacobi Polynomials with an Application in Numerical Analysis. Symmetry 2025, 17, 1440. https://doi.org/10.3390/sym17091440

AMA Style

Abd-Elhameed WM, Abdelkawy MA, Alsafri NMA, Atta AG. Novel Formulas of Specific Non-Symmetric Jacobi Polynomials with an Application in Numerical Analysis. Symmetry. 2025; 17(9):1440. https://doi.org/10.3390/sym17091440

Chicago/Turabian Style

Abd-Elhameed, Waleed Mohamed, Mohamed A. Abdelkawy, Naher Mohammed A. Alsafri, and Ahmed Gamal Atta. 2025. "Novel Formulas of Specific Non-Symmetric Jacobi Polynomials with an Application in Numerical Analysis" Symmetry 17, no. 9: 1440. https://doi.org/10.3390/sym17091440

APA Style

Abd-Elhameed, W. M., Abdelkawy, M. A., Alsafri, N. M. A., & Atta, A. G. (2025). Novel Formulas of Specific Non-Symmetric Jacobi Polynomials with an Application in Numerical Analysis. Symmetry, 17(9), 1440. https://doi.org/10.3390/sym17091440

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