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Research article

Conversion of crude palm oil to biofuels via catalytic hydrocracking over NiN-supported natural bentonite

  • Received: 21 September 2022 Revised: 17 February 2023 Accepted: 01 March 2023 Published: 06 March 2023
  • Nickel nitride supported on natural bentonite was prepared and tested for hydrocracking Crude Palm Oil (CPO). The catalyst was prepared using the wet impregnation method and various nickel nitride loading. Subsequently, the nickel nitrate-bentonite was calcined and nitrided under H2 steam. The surface acidity of as-synthesized NiN-bentonite was evaluated using the gravimetric pyridine gas. Meanwhile, the physiochemical features of the catalyst were assessed using XRD, FT-IR and SEM-EDX. The results showed that the NiN species was finely dispersed without affecting the bentonite's structure. Furthermore, the co-existence of Ni and N species on EDX analysis suggested the NiN was successfully supported onto the bentonite, while the surface acidity features of raw bentonite were increased to 1.713 mmol pyridine/g at 8 mEq/g of nickel nitride loading. The catalytic activity towards the CPO hydrocracking demonstrated that the surface acidity features affect the CPO conversion, with the highest conversion achieved (84.21%) using NiN-bentonite 8 mEq/g loading. At all nickel nitride loading, the NiN-bentonite could generate up to 81.98–83.47% of bio-kerosene fraction, followed by the bio-gasoline ranging from 13.12–13.9%, and fuel oil ranging from 2.89–4.57%.

    Citation: Hasanudin Hasanudin, Wan Ryan Asri, Utari Permatahati, Widia Purwaningrum, Fitri Hadiah, Roni Maryana, Muhammad Al Muttaqii, Muhammad Hendri. Conversion of crude palm oil to biofuels via catalytic hydrocracking over NiN-supported natural bentonite[J]. AIMS Energy, 2023, 11(2): 197-212. doi: 10.3934/energy.2023011

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  • Nickel nitride supported on natural bentonite was prepared and tested for hydrocracking Crude Palm Oil (CPO). The catalyst was prepared using the wet impregnation method and various nickel nitride loading. Subsequently, the nickel nitrate-bentonite was calcined and nitrided under H2 steam. The surface acidity of as-synthesized NiN-bentonite was evaluated using the gravimetric pyridine gas. Meanwhile, the physiochemical features of the catalyst were assessed using XRD, FT-IR and SEM-EDX. The results showed that the NiN species was finely dispersed without affecting the bentonite's structure. Furthermore, the co-existence of Ni and N species on EDX analysis suggested the NiN was successfully supported onto the bentonite, while the surface acidity features of raw bentonite were increased to 1.713 mmol pyridine/g at 8 mEq/g of nickel nitride loading. The catalytic activity towards the CPO hydrocracking demonstrated that the surface acidity features affect the CPO conversion, with the highest conversion achieved (84.21%) using NiN-bentonite 8 mEq/g loading. At all nickel nitride loading, the NiN-bentonite could generate up to 81.98–83.47% of bio-kerosene fraction, followed by the bio-gasoline ranging from 13.12–13.9%, and fuel oil ranging from 2.89–4.57%.



    Assuming that the underlying asset process follows a geometric Brownian motion, the Black-Scholes model was firstly proposed in 1973, where the option value satisfies a partial difference equation and depends only on the risk-free interest rate and the volatility of asset price [1]. In order to fit the empirical facts of practical financial markets, more extended models were introduced and studied, including jump-diffusion models [2,3], stochastic volatility models [4], fractional differential models [5,6,7] and regime-switching models [8].

    The idea of switching regimes is prevalently applied in order to allow Lévy processes to switch in a finite state space by a Markov chain. In option pricing models, the parameters, such as interest rate, drift and volatility, are allowed to take diverse values in a finite number of regimes [9]. For instance, the option models based on exponential Lévy processes under switching regimes were proposed and widely discussed to capture the sudden state movement from the bull market to bear market, and deal with the non-stationary behavior [10,11,12]. Since the partial integro-differential equation (PIDE) derived from the regime-switching exponential Lévy processes is difficult to be solved in closed form, it is essential to develop effective numerical methods.

    Recently, numerical solution of fractional option models under switching regimes attract much attention from the community of financial engineering. Cartea and del-Castillo-Negrete [13] proposed a first-order shifted Grünwald difference formula for the option pricing models, including the finite moment log stable (FMLS) model [6], CGMY model [7] and KoBoL model [5]. A first-order penalty method for fractional regime-switching American option pricing models, was constructed in [14]. Further, an implicit-explicit preconditioned direct method was developed in [12] for fractional regime-switching models which was of first order in spatial approximation.

    In this paper, we consider a second-order numerical scheme for fractional regime-switching option pricing models, based on the weighted and shifted Grünwald difference (WSGD) formula and Crank-Nicolson scheme. Theoretical analysis on the stability and second-order convergence of the numerical scheme is studied in detail. A second-order ADI method is proposed to accelerate the computation with a preconditioned direct solver for the discrete linear system. Numerical experiments on both fractional PDE and multi-regime FMLS and CGMY models are presented to show the convergence and efficiency of the proposed approach.

    The structure of this paper is organized as follows: A second-order numerical scheme for fractional regime-switching option pricing models is presented in Section 2. Numerical analysis of stability and the second-order convergence are shown in Section 3. In Section 4, we introduce the ADI method with preconditioned direct solver for the discrete linear system. Numerical experiments in Section 5 demonstrated the convergence and efficiency of the proposed method. Finally, conclusions are drawn in Section 6.

    Under the risk-neutral measure, assume that the stock price St follows a geometric Lévy process

    d(lnSt)=(rν)dt+dLt,

    where r is the risk-free rate, ν is a convexity adjustment and dLt is the increment of a Lévy process under the equivalent martingale measure [15]. Below, we discuss the general fractional regime-switching option model derivated by three particular Lévy processes: LS, CGMY and KoBoL, see [13] for more details.

    Let Vs(x,t) be the value of an European option in state s, the fractional regime-switching option model is defined by

    Vs(x,t)t+cs,1Vs(x,t)x+cs,2Dξs,αs+Vs(x,t)+cs,3Dλs,αsVs(x,t)dsVs(x,t)+ˉSj=1qs,jVj(x,t)=0, (2.1)

    where x=lnSt, 1<αs<2,s=1,2,,ˉS. The other parameters in Eq (2.1) depend on a certain state of a Markov process in the finite set {1,2,,ˉS}. The constants qs,j represent the elements of the state transition matrix of the Markov process, which satisfy the conditions ˉSj=1qs,j=0 and qs,j0,js.

    The left and right Riemann-Liouville tempered fractional derivatives Dξs,αs+ and Dλs,αs are defined by

    Dξs,αs+Vs(x,t)=eξsxΓ(2αs)2x2xeξsζVs(ζ,t)(ζx)αs1dζ,Dλs,αsVs(x,t)=eλsxΓ(2αs)2x2xeλsζVs(ζ,t)(xζ)αs1dζ, (2.2)

    where Γ() is the Gamma function.

    In the CGMY model, the parameters in the model (2.1) are given by

    cs,1=rCΓ(αs)[(ξs1)αsξαss+(λs+1)αsλαss],cs,2=cs,3=CΓ(αs),ds=r+CΓ(αs)(ξαss+λαss),C>0,λs0,ξs0. (2.3)

    The model (2.1) also covers FMLS and KoBoL models by different choices, and we refer the readers to [16] for more details.

    The terminal and boundary conditions for call options are given by

    Vs(x,T)=max{exK,0},xlxxr,Vs(xl,t)=0,0t<T,Vs(xr,t)=exrKer(Tt),0t<T, (2.4)

    where K is the strike price.

    Let N and M be the number of the uniform discrete points in the space and time direction, respectively, and let h=(xrxl)/(N+1) and τ=T/M be the corresponding step length. Define tm=mτ(m=0,1,2,,M),xn=xl+nh(n=0,1,2,,N+1).

    Assume that the function Vs(x,t) is continuously differentiable and 2Vs(x,t)/x2 is integrable in the interval [0,T)×[xl,xr], then for every α(0<α<2), the Riemann-Liouville derivative of Vs(x,t) exists and coincides with the Grünwald-Letnikov type [17]. Hence, we can use the Grünwald difference approaches to approximate the tempered fractional derivatives in Eq (2.2) to avoid the strong singularity when ζ=x.

    The first-order shifted Grünwald difference scheme [18] was first proposed to approximate the fractional derivatives and used to solve the fractional option pricing models [12,14]. Now we consider the second-order weighted and shifted Grünwald difference scheme [19] in the discrete process of Eq (2.1).

    Based on the weighted and shifted Grünwald difference scheme, the fractional derivative can be approximated by

    Dξs,αs+Vs(xn,tm)=1hαsNn+2k=0ωαskeξs(k1)hVs(xn+k1,tm)+O(h2),Dλs,αsVs(xn,tm)=1hαsn+1k=0ωαskeλs(k1)hVs(xnk+1,tm)+O(h2), (2.5)

    where

    {ωαs0=αs2gαs0,ωαsk=αs2gαsk+2αs2gαsk1,gαs0=1,gαsk=(1αs+1k)gαsk1,k=1,2,,k=0gαsk=0,gαs1=αs<0gαs2>gαs3>>0,ωαs0=αs2,ωαs1=2αsα2s2<0,ωαs2=αs(α2s+αs4)4. (2.6)

    Denote Vms,n be the numerical solution at the discrete point (xn,tm) of regime s. Discretising the convection term and the time term in Eq (2.1) by central differences, and the Crank-Nicolson scheme respectively, and introducing the time-reverse transformation t=Tt, dropping for simplicity, the following fully discrete scheme is derived:

    Vm+1s,nVms,nτ=12[cs,1Vm+1s,n+1Vm+1s,n12h+cs,2hαsNn+2k=0ωαskeξs(k1)hVm+1s,n+k1+cs,3hαsn+1k=0ωαskeλs(k1)hVm+1s,nk+1dsVm+1s,n+ˉSj=1qs,jVm+1j,n+cs,1Vms,n+1Vms,n12h+cs,2hαsNn+2k=0ωαskeξs(k1)hVms,n+k1+cs,3hαsn+1k=0ωαskeλs(k1)hVms,nk+1dsVms,n+ˉSj=1qs,jVmj,n],n=1,2,,N,m=0,1,2,,M1. (2.7)

    Denote Vm=(Vm1,1,Vm1,2,,Vm1,N,Vm2,1,,Vm2,N,,VmˉS,N)T, Q=[qs,j]ˉSs,j=1 and pm+12=12τ(pm+1+pm), where

    pm=(pm1,pm2,,pmˉS)T,pms=cs,12hpms,1+cs,2hαspms,2+cs,3hαspms,3,pms,1=(Vms,0,0,,0,Vms,N+1)T,pms,2=(ωαs0eξshVms,0+ωαsN+1eξsNhVms,N+1,,ωαs2eξshVms,N+1)T,pms,2=(ωαs2eλshVms,0,,ωαsN+1eλsNhVms,0+ωαs0eλshVms,N+1)T.

    The matrix form of the numerical scheme (2.7) can be written as:

    (IˉSN12τ(MB+QIN))Vm+1=(IˉSN+12τ(MB+QIN))Vm+pm+12, (2.8)

    where

    MB=diag(T1,T2,,TˉS),Ts=cs,12hJ+cs,2hαsWs+cs,3hαsGsdsIN, (2.9)

    with

    J=tridiag(1,0,1),Ws=(ωαs1ωαs2eξshωαsN1eξs(N2)hωαsNeξs(N1)hωαs0eξshωαs1ωαs2eξshωαsN1eξs(N2)h0ωαs0eξshωαs1ωαs2eξsh00ωαs0eξshωαs1),Gs=(ωαs1ωαs0eλsh00ωαs2eλshωαs1ωαs0eλsh0ωαsN1eλs(N2)hωαs2eλshωαs1ωαs0eλshωαsNeλs(N1)hωαsN1eλs(N2)hωαs2eλshωαs1).

    In this section, the stability and convergence of the numerical scheme (2.8) are established.

    A matrix is called positive definite if, and only, if its symmetric part is positive definite, that is, all the eigenvalues are positive.

    Lemma 3.1. (Gerschgorin Disk Theorem) Suppose A=[aij]Cn×n, let

    Gi(A)={zC:|zaii|ji|aij|},i=1,,n,

    then

    λ(A)G1(A)G2(A)Gn(A).

    Theorem 3.1. (Stability) Assume that 1<αs<2 and set

    ηs(x):=(αsehx+2αs)(1ehx)αs. (3.1)

    If

    cs,22hαsηs(ξs)+cs,32hαsηs(λs)ds12(qs,s+ˉSk=1,ksqk,s), (3.2)

    for all s=1,2,,ˉS, then the discretisation scheme (2.8) is stable.

    Proof. Denote B=MBQIN and consider the matrix

    Z=(I+12τB)1(I12τB).

    In order to show the stability of the scheme (2.8), it suffices to prove that the eigenvalues λZ of the matrix Z satisfy the estimate |λZ|<1. Or equivalently, that the eigenvalues λB of matrix B satisfy the estimate

    |11/2τλB1+1/2τλB|<1. (3.3)

    The inequality (3.3) means that any λB has a positive real part (λB). Therefore, the numerical scheme (2.8) is stable if the matrix B is positive definite, i.e., its symmetric part B is positive definite.

    Consider the symmetric Toeplitz matrix

    Ts=cs,22hαs(Ws+WTs)cs,32hαs(Gs+GTs)+dsIN,

    and block diagonal Toeplitz matrix

    T=diag(T1,T2,,TˉS),

    thus,

    B=TQ+QT2IN.

    Note that cs,2,cs,3 and ds are nonnegative, we have

    [B]l,l=(cs,2+cs,3)ωαs1hαs+dsqs,s>0,

    where 1+(s1)NlsN, s=1,2,,ˉS.

    Therefore, if the matrix B is strictly row diagonally dominant, then it is positive definite by Lemma 3.1, which means B satisfies the condition

    [B]l,l>ˉSNk=1,kl|[B]l,k| (3.4)

    for 1+(s1)NlsN where s=1,2,,ˉS.

    It is clear that the lth and the (1+(2s1)Nl)th rows are the same. Without loss of generality, we choose 1+(s1)Nl(s1)N+N2, then

    ˉSNk=1,kl|[B]l,k|=cs,22hαs(2(ωαs0eξsh+ωαs2eξsh++ωαseξs(1)h)+ωαs+1eξsh++ωαsNeξs(N1)h)+cs,32hαs(2(ωαs0eλsh+ωαs2eλsh++ωαseλs(1)h)+ωαs+1eλsh++ωαsNeλs(N1)h)+ˉSk=1,ksqs,k+qk,s2,

    where =l(s1)N. By rearranging the sequence {gαsk} from {ωαsk} and according to the properties in Eq (2.6), we have

    2(ωαs0eξsh+ωαs2eξsh++ωαseξs(1)h)+ωαs+1eξsh++ωαsNeξs(N1)h=2k=0ωαskeξs(1k)h+Nk=+1ωαskeξs(1k)h2ωαs1<(αseξsh+2αs)(1eξsh)αs2ωαs1,

    and

    2(ωαs0eλsh+ωαs2eλsh++ωαseλs(1)h)+ωαs+1eλsh++ωαsNeλs(N1)h<(αseλsh+2αs)(1eλsh)αs2ωαs1.

    Thus, the condition (3.4) becomes

    (cs,2+cs,3)ωαs1hαs+dsqs,scs,22hαs(αseξsh+2αs)(1eξsh)αscs,2hαsωαs1+cs,32hαs(αseλsh+2αs)(1eλsh)αscs,3hαsωαs1qs,s2+12ˉSk=1,ksqk,s,

    which can be written as

    cs,22hαsηs(ξs)+cs,32hαsηs(λs)ds12(qs,s+ˉSk=1,ksqk,s),

    where ηs(x) is defined in Eq (3.1).

    It is similar that the stability condition in Theorem 3.1 from [16] is given by

    cs,2ηs(ξs)hαs(1+eαs(λsξs)h)+cs,3ηs(λs)hαs(1+eαs(ξsλs)h)ds12(qs,s+ˉSk=1,ksqk,s). (3.5)

    Consider the specific parameters of the CGMY model from Eq (2.3), the stability condition (3.2) can be rewritten as

    CΓ(αs)(ηs(ξs)+ηs(λs)2hαsξαssλαss)r12(qs,s+ˉSk=1,ksqk,s),

    while condition (3.5) turns to

    CΓ(αs)(ηs(ξs)hαs(1+eαs(λsξs)h)+ηs(λs)hαs(1+eαs(ξsλs)h)ξαssλαss)r12(qs,s+ˉSk=1,ksqk,s).

    It is can be seen that the condition (3.2) allows a wider range of the parameters in Eq (2.1), which can describe more state movement as the financial markets change.

    Consider now the convergence of the scheme (2.8). Due to the non-smoothness of the initial and boundary conditions in Eq (2.4), Eq (2.1) does not have a solution in the classical form. As a result, we consider the generalized solution, which satisfies the fractional PDE almost everywhere in (0,T)×(xl,xr). We define the viscosity solution of Eq (2.1) similar as Definition 2.4 in [20].

    Theorem 3.2. (Convergence) Let Vm be the viscosity solution of Eq (2.1). The scheme (2.8) is of second order convergence, i.e.,

    VmVmC0(h2+τ2) (3.6)

    if the matrix B=MBQIN is positive definite, i.e.,

    cs,22hαsηs(ξs)+cs,32hαsηs(λs)ds12(qs,s+ˉSk=1,ksqk,s),

    where the norm v=hˉSNi=0v2i and C0 is a positive constant.

    Proof. The proof is similar as Theorem 3.2 in [16], and we omit the specific process here.

    In this section, the ADI method will be used to solve scheme (2.7). The ADI method proposed by Peaceman and Rachford [21] in 1955 was widely used to solve two dimensional problems due to its computational effectiveness. Recently, the ADI method was also applied to solve two-asset option pricing problems under fractional models [22,23].

    Denote

    ΔsVms,n=ˉSj=1qs,jVmj,n

    and

    ΔsxVms,n=cs,1Vms,n+1Vms,n12h+cs,2hαsNn+2k=0ωαskeξs(k1)hVms,n+k1+cs,3hαsn+1k=0ωαskeλs(k1)hVms,nk+1dsVms,n,

    From Eq (2.7), it is easy to show

    (1τ2Δsx)(1τ2Δs)Vm+1s,n=(1+τ2Δsx)(1+τ2Δs)Vms,n+R, (4.1)

    where

    R=τ24ΔsxΔs(Vm+1s,nVms,n). (4.2)

    When the time step τ>0 is sufficiently small, we omit the term R and define the following ADI scheme similar to that of the Peaceman–Rachford type [21]:

    (1τ2Δsx)ˆVs,n=(1+τ2Δs)Vms,n, (4.3)
    (1τ2Δs)Vm+1s,n=(1+τ2Δsx)ˆVs,n. (4.4)

    The following theorem illustrates the convergence order of the ADI scheme (4.3) and (4.4).

    Theorem 4.1. Assume that the exact solution of the fractional PDE in Eq (2.1) is unique, and its partial derivatives are in L1(R) and vanish outside [0,T)×[xl,xr]. The ADI discretization for Eq (2.1) defined in Eqs (4.3) and (4.4) is also of second order convergence O(h2+τ2).

    Proof. From Theorem 3.2, we have proved that the Crank–Nicolson method has convergence of order O(h2+τ2). In the ADI scheme, compared to the Crank–Nicolson scheme (2.7), the scheme (4.3) and (4.4) incurs an additional perturbation error R defined in Eq (4.2).

    Since

    R=τ24ΔsxΔs(Vm+1s,nVms,n)=τ34ΔsxΔs(Vst|(xn,tm)+O(τ))=τ34Δs(LsVst|(xn,tm)+O(h2+τ)),

    where

    LsVs=cs,1Vsx+cs,2Dξs,αs+Vs+cs,3Dλs,αsVsdsVs.

    When τ is sufficiently small, the perturbation error R is a higher-order term than the other terms in Eq (4.1). Therefore, the convergence order of the ADI scheme (4.3) and (4.4) is O(h2+τ2).

    In order to solve the ADI scheme (4.3)-(4.4), we need to define boundary conditions for ˆVs,n, which is accomplished by subtracting Eq (4.4) from Eq (4.3)

    2ˆVs,n=(1+τ2Δs)Vms,n+(1τ2Δs)Vm+1s,n. (4.5)

    The corresponding algorithm is implemented as follows:

    Algorithm 1 ADI method for scheme (4.3), (4.4)
    1: Initialize V0s,n for s=1,2,,ˉS and n=1,2,,N using the payoff function.
    2: for m=0,1,2,,M1, do
    3:    For s=1,2,,ˉS, solve the following system for ˆVs,=(ˆVs,1,ˆVs,2,,ˆVs,N)T.
         (INτ2Ts)ˆVs,=Vms,+τ2ˉSj=1qs,jVmj,+τ2ˆps,(4.6)
       where Ts is defined in Eq (2.9) , Vns,=(Vms,1,Vms,2,,Vms,N)T,ˆps=cs,12hˆps,1+cs,2hαsˆps,2+cs,3hαsˆps,3, with
         ˆps,1=(ˆVs,0,0,,0,ˆVs,N+1)T,ˆps,2=(ωαs0eξshˆVms,0+ωαsN+1eξsNhˆVms,N+1,,ωαs2eξshˆVs,N+1)T,ˆps,2=(ωαs2eλshˆVs,0,,ωαsN+1eλsNhˆVs,0+ωαs0eλshˆVs,N+1)T.
    4:   For n=1,2,,N, solve the following system for Vm+1,n=(Vm+11,n,Vm+12,n,,Vm+1ˉS,n)T.
         (IˉSτ2Q)Vm+1,n=(1+τ2Δsx)ˆV,n,(4.7)
       where Vm+1,n=(Vm+1,n,Vm+1,n,,Vm+1,n)T.
    5: end for

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    In Algorithm 1, denote ˜Ts=INτ2Ts to be the coefficient matrix of the linear system (4.6), which has Toeplitz structure. Using the preconditioned direct method proposed in [12,24], the computation process of solving the linear equations with coefficient matrix ˜Ts can be accelerated by fast Fourier transformations (FFT). The total computation cost to solve Eq (4.6) for each s=1,2,,ˉS is O(NlogN).

    Since the order of the matrix Q represents the number of the regime-switching states, which is far less than N, the linear system (4.7) can be quickly solved.

    For more modern ADI approaches, we refer the readers to [25,26], which will be our future work to study them under fractional option pricing problems.

    In this section, numerical experiments on the fractional PDE, with known exact solution and European call options under multi-regime FMLS and CGMY models, are presented to show the convergence and efficiency of the proposed ADI approach.

    Compared with the ADI method, GMRES and BiCGSTAB are used to solve the linear equation on every temporal layer, where the vector Vm1 is taken as a initial guess and the iteration is terminated when the residual r(k) satisfies r(k)2/r(0)2107. All numerical experiments are carried out by Matlab R2020a.

    Example 5.1. Consider the following FPDE problem with source term:

    {Vs(x,t)tVs(x,t)xDλs,αsVs(x,t)ˉSj=1qs,jVj(x,t)=fs(x,t),Vs(0,t)=0,0<t1,Vs(1,t)=etλs,0<t1,Vs(x,0)=eλsxx2+αs,0x1, (5.1)

    with

    fs(x,t)=etλsx(Γ(3+αs)Γ(3)x2+(1λs)x2+αs+(2+αs)x1+αs)ˉSj=1qs,jVj(x,t),

    where the exact solution is Vs(x,t)=etλsxx2+αs.

    The following two cases are considered as the settings in [12]:

    (a) ˉS=2, α=(1.9,1.6), λ=(0.92,1.20), Q=(6688).

    (b) ˉS=8,α=(1.6,1.1,1.9,1.8,1.8,1.3,1.6,1.1),λ=(2.04,4.1,3.6,4.85,2.66,1.63,0.53,3.06),

    Q=(2511052223438101024536239410557528322102374373826972566393103567974585410774643).

    In Figures 1, 2, the surfaces of the numerical solution and error |VMVM| of case (a) are presented respectively, for s=1,2, when M=N=1024.

    Figure 1.  The numerical solution and error of case (a) in Example 5.1 when s=1.
    Figure 2.  The numerical solution and error of case (a) in Example 5.1 when s=2.

    Define the convergence order of the numerical scheme as

    Orderm=log2Vm1Vm1VmVm,

    where Vm is the exact solution on tm and -norm is defined in Theorem 3.2.

    In Tables 1, 2, the error and convergence order of Crank-Nicolson scheme and ADI scheme are listed for case (a) and case (b), respectively. We use "D-ADI" to represent the ADI Algorithm 1 with preconditioned direct method.

    Table 1.  Error and convergence order of three numerical schemes for case (a) in Example 5.1.
    GMRES BiCGSTAB D-ADI
    Regime N=M VmVm Order VmVm Order VmVm Order
    24 2.3967E-04 2.3967E-04 1.9205E-04
    25 6.3382E-05 1.9189 6.3380E-05 1.9189 5.1484E-05 1.8993
    26 1.6324E-05 1.9571 1.6322E-05 1.9572 1.3344E-05 1.9479
    s=1 27 4.1466E-06 1.9770 4.1434E-06 1.9779 3.3981E-06 1.9735
    28 1.0494E-06 1.9824 1.0450E-06 1.9873 8.5744E-07 1.9866
    29 2.6886E-07 1.9646 2.6360E-07 1.9871 2.1536E-07 1.9933
    210 7.4745E-08 1.8468 6.7470E-08 1.9660 5.3965E-08 1.9967
    24 2.6564E-04 2.6563E-04 3.2512E-04
    25 6.9890E-05 1.9263 6.9886E-05 1.9264 8.4830E-05 1.9383
    26 1.7969E-05 1.9596 1.7965E-05 1.9598 2.1702E-05 1.9667
    s=2 27 4.5625E-06 1.9776 4.5583E-06 1.9786 5.4916E-06 1.9826
    28 1.1551E-06 1.9817 1.1500E-06 1.9869 1.3814E-06 1.9910
    29 2.9661E-07 1.9614 2.9041E-07 1.9854 3.4645E-07 1.9955
    210 8.3315E-08 1.8319 7.4617E-08 1.9605 8.6747E-08 1.9977

     | Show Table
    DownLoad: CSV
    Table 2.  Error and convergence order of three numerical schemes for case (b) in Example 5.1.
    GMRES BiCGSTAB D-ADI
    Regime N=M VmVm Order VmVm Order VmVm Order
    27 2.3244E-06 2.3236E-06 2.7531E-05
    s=1 28 5.8678E-07 1.9860 5.8543E-07 1.9888 6.8850E-06 1.9995
    29 1.4837E-07 1.9836 1.4697E-07 1.9939 1.7221E-06 1.9993
    27 2.6927E-06 2.6917E-06 3.7611E-05
    s=2 28 6.7564E-07 1.9947 6.7401E-07 1.9977 9.3779E-06 2.0038
    29 1.7016E-07 1.9893 1.6848E-07 2.0002 2.3407E-06 2.0023
    27 2.0421E-06 2.0412E-06 3.2462E-05
    s=3 28 5.1579E-07 1.9852 5.1445E-07 1.9883 8.1187E-06 1.9994
    29 1.3055E-07 1.9822 1.2917E-07 1.9937 2.0306E-06 1.9993
    27 2.2554E-06 2.2544E-06 4.1254E-05
    s=4 28 5.6974E-07 1.9850 5.6817E-07 1.9883 1.0316E-05 1.9996
    29 1.4428E-07 1.9815 1.4266E-07 1.9937 2.5801E-06 1.9994
    27 2.1676E-06 2.1668E-06 2.8966E-05
    s=5 28 5.4738E-07 1.9855 5.4605E-07 1.9885 7.2445E-06 1.9994
    29 1.3848E-07 1.9829 1.3710E-07 1.9938 1.8120E-06 1.9993
    27 2.6192E-06 2.6183E-06 3.0412E-05
    s=6 28 6.5989E-07 1.9888 6.5841E-07 1.9916 7.5967E-06 2.0012
    29 1.6671E-07 1.9849 1.6517E-07 1.9951 1.8992E-06 2.0000
    27 2.7223E-06 2.7214E-06 2.5136E-05
    s=7 28 6.8708E-07 1.9862 6.8567E-07 1.9888 6.2867E-06 1.9994
    29 1.7361E-07 1.9846 1.7213E-07 1.9940 1.5725E-06 1.9992
    27 2.6352E-06 2.6343E-06 3.4432E-05
    s=8 28 6.6171E-07 1.9937 6.6016E-07 1.9965 8.5878E-06 2.0034
    29 1.6671E-07 1.9889 1.6510E-07 1.9995 2.1439E-06 2.0021

     | Show Table
    DownLoad: CSV

    From Tables 1, 2, it is seen that both the Crank-Nicolson and ADI schemes have second-order convergence. It is also observed that the convergence of the ADI scheme is more stable. Since the order from Tables 1, 2 represents the convergence on each regime, it can further verify the theoretical analysis in Theorem 3.2.

    In Tables 3, 4, the average of the iteration number (denoted by "IT") and the total CPU time (in seconds, denoted by "CPU") of GMRES, BiCGSTAB and ADI methods are compared when the number of discrete points N increases from 24 to 29 respectively.

    Table 3.  Iteration numbers and CPU time of different solvers for case (a) in Example 5.1.
    GMRES BiCGSTAB D-ADI
    N=M IT CPU IT CPU CPU
    24 47 0.0345 22.94 0.0059 0.0242
    25 77 0.0539 40.47 0.0063 0.0368
    26 119 0.1674 62.45 0.0321 0.1222
    27 182 0.7743 84.90 0.2811 0.4580
    28 307 5.2065 112.75 2.4813 2.0023
    29 520 56.9593 156.25 28.1146 10.3205
    210 886 922.9244 218.91 390.7879 57.3228

     | Show Table
    DownLoad: CSV
    Table 4.  Iteration numbers and CPU time of different solvers for case (b) in Example 5.1.
    GMRES BiCGSTAB D-ADI
    N=M IT CPU IT CPU CPU
    24 57 0.0410 27.63 0.0079 0.0329
    25 91 0.0820 45.16 0.0173 0.0792
    26 145 0.3451 72.38 0.1356 0.3364
    27 218 2.1381 107.41 1.3419 1.2518
    28 340 22.8717 151.21 15.3208 5.8594
    29 591 345.5954 232.94 237.7708 32.4836

     | Show Table
    DownLoad: CSV

    From Tables 3, 4, it is observed that both GMRES and BiCGSTAB require more iteration step than ADI method, and so does the CPU time. By comparing the CPU time of the three methods, it is obvious that the preconditioned direct ADI method is fast, and can significantly reduce the computation time.

    Then, the proposed preconditioned direct ADI method is applied to deal with the multi-regime European option pricing model in Example 5.3. The parameters in this example change in different regimes, by which the sudden state movement and the non-stationary behavior of the market is described.

    In order to verify the convergence order for non-smooth payoff function as initial conditions in Eq (2.4), we demonstrate the results of an option pricing problem in Example 5.2.

    Example 5.2. Consider the multi-regime FMLS model for pricing European call option, where xl=ln(0.1),xr=ln(100),K=50,r=0.05,T=1. The regime-switching parameters are set as

    ˉS=2,α=(1.9,1.6),σ=(0.25,0.5),Q=(6688).

    In Table 5, we list the error and convergence order of ADI scheme. The viscosity solution is approximated by the numerical solution using a dense mesh with N=M=213.

    Table 5.  Error and convergence order of the ADI scheme in Example 5.2.
    Regime N=M VmVm Order VmVm Order
    27 1.1242E-02 1.3525E-02
    28 2.1656E-03 2.3760 2.4681E-03 2.4542
    s=1 29 5.2820E-04 2.0356 6.6201E-04 1.8985
    210 1.4432E-04 1.8719 1.5758E-04 2.0708
    211 3.0417E-05 2.2463 4.2304E-05 1.8972
    27 1.1462E-02 1.3801E-02
    28 2.2038E-03 2.3788 2.4871E-03 2.4722
    s=2 29 5.3432E-04 2.0442 6.5044E-04 1.9350
    210 1.4726E-04 1.8593 1.7085E-04 1.9287
    211 3.0424E-05 2.2751 4.1473E-05 2.0425

     | Show Table
    DownLoad: CSV

    From Table 5, it is observed that the ADI scheme can keep the second-order convergence under the non-smooth initial conditions. The convergence orders are not as steady as those in Example 5.1 perhaps because of the discontinuity at the strike price K, which can be improved by the Padé schemes proposed in [27].

    Example 5.3. Consider the multi-regime CGMY model for pricing European call option where xl=ln(0.1),xr=ln(200),K=60,r=0.05,T=1,C=0.1.

    Consider the following two cases:

    (a) ˉS=4,α=(1.5,1.7,1.3,1.8),σ=(0.25,0.5,0.75,0.5),ξ=(2,1,5,1),λ=(1,3,2,4),

    Q=(122468201025410124814).

    (b) ˉS=6, α=(1.5,1.2,1.7,1.3,1.6,1.8), σ=(0.25,0.5,0.3,0.75,0.5,0.2), ξ=(1,2,1,2,3,3), λ=(3,4,3,1,2,2),

    Q=(13241243208342211024124216171131714411212).

    The option values of four regimes and six regimes are depicted, respectively, in Figure 3 when M=N=512, where the blue dashed line represents the payoff of the European call option and the other colored lines represent the option prices with different regimes at the value date.

    Figure 3.  The value of European call option under the multi-regime CGMY model and payoff function in Example 5.3.

    In this paper, a second-order finite difference method is proposed to discretise a class of fractional regime-switching option pricing models. In addition, the sufficient conditions of stability and convergence of the numerical scheme are studied in detail. The ADI scheme with preconditioned direct method is considered to deal with the multi-regime structure to accelerate the computation. Numerical experiments verify the theoretical convergence order and show the efficacy of the proposed method.

    The authors are very grateful to the referees for their constructive comments and valuable suggestions, which greatly improved the original manuscript of the paper. This work is supported by the National Natural Science Foundation of China (No. 11971354 and No. 12171366).

    The authors declare there is no conflicts of interest.



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