
Ready-mixed-concrete (RMC) is an important green and clean building material which is widely used in modern civil engineering. For the large-scale planar foundations of urban public buildings, huge amounts of RMC need to be continuously delivered to the construction site according to strict time windows, which brings the problem of multi-plants collaborative supply. In this paper, considering transportation capacity, initial setting time, and interrupt pumping time, a collaborative scheduling model for production and transportation of RMC with the objective of minimizing the penalty cost of interruption pumping and vehicle waiting time and fuel consumption cost was established. According to the characteristics of the problem, a double chromosome synchronous evolution genetic algorithm was designed. Finally, the model and algorithm proposed in the paper were verified by data experiments. The computing results showed that in two cases of different scenarios, such as ordinary constructions and emergency constructions, the proposed scheduling model can save 18.6 and 24.8% cost respectively. The scheduling model and algorithm proposed in the paper can be applied directly to improve the operational efficiency of RMC supply chain.
Citation: Jing Yin, Ran Huang, Hao Sun, Taosheng Lin. A collaborative scheduling model for production and transportation of ready-mixed concrete[J]. Mathematical Biosciences and Engineering, 2023, 20(4): 7387-7406. doi: 10.3934/mbe.2023320
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Ready-mixed-concrete (RMC) is an important green and clean building material which is widely used in modern civil engineering. For the large-scale planar foundations of urban public buildings, huge amounts of RMC need to be continuously delivered to the construction site according to strict time windows, which brings the problem of multi-plants collaborative supply. In this paper, considering transportation capacity, initial setting time, and interrupt pumping time, a collaborative scheduling model for production and transportation of RMC with the objective of minimizing the penalty cost of interruption pumping and vehicle waiting time and fuel consumption cost was established. According to the characteristics of the problem, a double chromosome synchronous evolution genetic algorithm was designed. Finally, the model and algorithm proposed in the paper were verified by data experiments. The computing results showed that in two cases of different scenarios, such as ordinary constructions and emergency constructions, the proposed scheduling model can save 18.6 and 24.8% cost respectively. The scheduling model and algorithm proposed in the paper can be applied directly to improve the operational efficiency of RMC supply chain.
In this paper, our main purpose is to estimate an approximate solution γ∗ of the equation
P(s)=0, | (1.1) |
where P:Ω⊆T1→T2 is a scalar function in an open convex interval Ω.
Solving problems of nonlinear equations is widely used in many fields, such as physics, chemistry, and biology [1]. Usually, the analytical solution of nonlinear equations is difficult to obtain in general cases. Therefore, in most situations, iterative methods are applied to find approximate solutions [2]. The most famous and fundamental iterative method is Newton's method [3]. Currently, many methods are constructed on the basis of Newton's method, and they are called Newton-type methods [4,5]. Convergence analysis is an important part of the research of the iterative method [6]. The issue of local convergence is, based on the information surrounding a solution, to find estimates of the radii of the convergence balls [7]. At present, many scholars study the local convergence analysis of iterative methods, such as Argyros et al. studied the local convergence of a third-order iterative method [8] and Chebyshev-type method [9]. In addition, some iterative methods and their local convergence are used in the study of diffusion equations [10,11,12,13]. The domain of convergence is an important problem in the study of iterative process; see [14]. Generally, the domain of convergence is small, which limits the choice of initial points. Thus, it is crucial that the domain of convergence is expanded without additional conditions. This paper will study the local convergence of a Chebyshev-type method without the second derivative in order to broaden its applied range.
The classical Chebyshev-Halley type methods of third-order convergence [15], which improves Newton's methods are defined by
sn+1=sn−(1+12(1−λKF(sn))−1KF(sn)P′(sn)−1P(sn), | (1.2) |
where
KF(sn)=P′(sn)−1P″(sn)P′(sn)−1P(sn), |
This method includes Halley's method [16] for λ=12, Chebyshev's method [17] for λ=0, and the super-Halley method for λ=1. Since these methods need to calculate the second derivative, they have an expensive computational cost. To avoid the second derivative, some scholars have proposed some variants of Chebyshev-Halley type methods free from the second derivative [18,19]. Cordero et al. [20] proposed a high-order three-step form of the modified Chebyshev–Halley type method:
tn=sn−P′(sn)−1P(sn),zn=sn−(1+P(tn)(P(sn)−2βP(tn))−1)P′(sn)−1P(sn),sn+1=zn−([zn,tn;P]+2(zn−tn)[zn,tn,sn;P]−(zn−tn)[tn,sn,sn;P])−1P(zn), | (1.3) |
where β∈R denotes a parameter, and s0∈Ω denotes an initial point. [.,.;P] and [.,.,.;P] denote divided difference of order one and two, in particular, the second-order divided difference cannot be generalized to Banach spaces. So, we study the local convergence of method (1.3) in real spaces. The order of convergence of the above method is at least six, and if β=1, it is optimal order eight.
However, earlier proofs of the analysis of convergence required third or higher derivatives. This limits the applicability of the above method. For example, define P(s) on Ω=[0,1] by
P(s)={s3lns2−s5+s4,s≠0;0,s=0. | (1.4) |
Then, P‴(s)=6lns2−60s2+24s+22 is unbounded on Ω. So when using the iterative method to solve the equation (1.4), the convergence order of the iterative method cannot be guaranteed. In this paper, the analysis of local convergence for method (1.3) only uses the first-order derivative.In particular, using Lipschitz continuity conditions based on the first derivative, the applicability of method (1.3) is extended.
The rest part of this paper is laid out as follows: Section 2 is devoted to the study of local convergence for method (1.3) by using assumptions based on the first derivative. Also, the uniqueness of the solution and the radii of convergence balls are analyzed. In Section 3, according to the different parameter values, the fractal graphs of the family are drawn. The convergence and stability of the iterative method are analyzed by drawing the attractive basins. In Section 4, the convergence criteria are verified by some numerical examples. Finally, conclusions appear in Section 5.
In this Section, we study the local convergence analysis of method (1.3) under Lipschitz continuity conditions. There are some parameters and scalar functions to be used to prove local convergence of method (1.3). β∈R and θ≥0 are parameters. Suppose the continuous function υ0:[0,+∞)→R is nondecreasing, υ0(0)=0, and
υ0(ξ)−1=0 | (2.1) |
has a smallest solution γ0∈[0,+∞)−{0}.
Let the continuous function υ:[0,γ0)→R be nondecreasing and υ(0)=0. Functions h1 and g1 on the interval [0,γ0) are defined by
h1(ξ)=∫10υ(|θ−1|ξ)dθ1−υ0(ξ) |
and
g1(ξ)=h1(ξ)−1. |
Then we obtain
g1(0)=h1(0)−1<0 |
and g1(ξ)→∞ as ξ→γ−0. According to the intermediate value theorem, the equation g1(ξ)=0 has roots in (0,γ0). Let r1 be the smallest root. Suppose continuous function ω1:[0,γ0)→R is nondecreasing and ω1(0)=0. Functions h2 and g2 on the interval [0,γ0) are defined by
h2(ξ)=∫10υ0(|θ|ξ)dθ+2|β|h1(ξ)∫10ω1(ξ|θ|h1(ξ))dθ |
and
g2(ξ)=h2(ξ)−1. |
Then we have
g2(0)=h2(0)−1<0 |
and g2(ξ)→∞ as ξ→γ−0. Similarly, the equation g2(ξ)=0 has roots in (0,γ0). Let r2 be smallest root. Functions h3 and g3 on the interval [0,r2) are defined by
h3(ξ)=h1(ξ)[1+∫10ω1(ξ|θ|h2(ξ))ω1(|θ|ξ)dθ(1−υ0(ξ))(1−h2(ξ))] |
and
g3(ξ)=h3(ξ)−1. |
Then we have
g3(0)=h3(0)−1<0 |
and g3(ξ)→∞ as ξ→r−2. Similarly, the equation g3(ξ)=0 has roots in (0,r2). Let r3 be the smallest root. Suppose continuous functions ω0,ω2:[0,γ0)2→R and ω3:[0,γ0)3→R are nondecreasing with ω0(0,0)=0, ω2(0,0)=0, and ω3(0,0,0)=0. Functions h4 and g4 on the interval [0,γ0) are defined by
h4(ξ)=ω0(h3(ξ)ξ,h1(ξ)ξ)+ξ(h1(ξ)+h3(ξ))(ω2(ξ(h3(ξ)+h1(ξ)),ξ(h1(ξ)+1))+ω3(h3(ξ)ξ,h1(ξ)ξ,ξ)) |
and
g4(ξ)=h4(ξ)−1. |
Then we have
g4(0)=h4(0)−1<0 |
and g4(ξ)→∞ as ξ→r−3. Similarly, the equation g4(ξ)=0 has roots in (0,r3). Let r4 be the smallest root. Functions h5 and g5 on the interval [0,r4) are defined by
h5=[1−∫10ω1(ξ|θ|h3(ξ))dθ1−h4(ξ)]h3(ξ) |
and
g5(ξ)=h5(ξ)−1. |
We have
g5(0)=h5(0)−1<0 |
and g5(ξ)→∞ as ξ→r−4. Similarly, the equation g5(ξ)=0 has roots in (0,r4). Let r5 be the smallest root.
Set
r=min{r1,r3,r5}. | (2.2) |
Then, for each ξ∈[0,r), we have that
0≤h1(ξ)<1, | (2.3) |
0≤h2(ξ)<1, | (2.4) |
0≤h3(ξ)<1, | (2.5) |
0≤h4(ξ)<1, | (2.6) |
0≤h5(ξ)<1. | (2.7) |
Applying the above conclusions, the analysis of local convergence for method (1.3) can be proved.
Theorem 2.1. Suppose P:Ω⊂T1→T2 is a scalar function. [.,.;P]:Ω2→L(T1,T2) and [.,.,.;P]:Ω3→L(T1,T2) are divided differences of one and two. Let γ∗∈Ω and continuous function υ0:[0,+∞)→R be nondecreasing with υ0(0)=0 such that each x∈Ω
P(γ∗)=0,P′(γ∗)−1∈L(T1,T2), | (2.8) |
‖P′(γ∗)−1(P′(s)−P′(γ∗))‖≤υ0(‖s−γ∗‖). | (2.9) |
Let Ω0=Ω∩B(γ∗,γ0). There exist β∈R, M≥0, continuous functions υ,ω1:[0,γ0)→R, ω0,ω2:[0,γ0)2→R, ω3:[0,γ0)3→R be nondecreasing such that for each x,y,z∈Ω0
‖P′(γ∗)−1(P′(s)−P′(t))‖≤υ(‖s−t‖) | (2.10) |
‖P′(γ∗)−1([s,t;P]−P′(γ∗))‖≤ω0(‖s−γ∗‖,‖t−γ∗‖) | (2.11) |
‖P′(γ∗)−1P′(s)‖≤ω1(‖s−γ∗‖) | (2.12) |
‖P′(γ∗)−1([z,t,s;P]−[t,s,s;P])‖≤ω2(‖z−t‖,‖t−s‖) | (2.13) |
‖P′(γ∗)−1[z,t,s;P]‖≤ω3(‖z−γ∗‖,‖t−γ∗‖,‖s−γ∗‖) | (2.14) |
and
ˉU(γ∗,r)⊆Ω. | (2.15) |
Then the sequence {sn} produced for s0∈U(γ∗,r)−{γ∗} by method (1.3) converges to γ∗ and remains in U(γ∗,r) for each n=0,1,2…. Furthermore, the following estimates hold:
‖tn−γ∗‖≤h1(‖sn−γ∗‖)‖sn−γ∗‖≤‖sn−γ∗‖<r, | (2.16) |
‖zn−γ∗‖≤h3(‖sn−γ∗‖)‖sn−γ∗‖≤‖sn−γ∗‖, | (2.17) |
and
‖sn+1−γ∗‖≤h5(‖sn−γ∗‖)‖sn−γ∗‖≤‖sn−γ∗‖, | (2.18) |
where functions hi(i=1,3,5) have been defined. Moreover, for R≥r, if there exists that
∫10υ0(|θ−1|R)dθ<1, | (2.19) |
then, the solution γ∗∈ˉU(γ∗,R)⊆Ω of equation P(s)=0 is unique.
Proof Using s0∈U(γ∗,r), (2.8), and the definition of r, we obtain
‖P′(γ∗)−1(P′(s0)−P′(γ∗))‖≤υ0(‖s0−γ∗‖)<υ0(r)<1. | (2.20) |
According to the Banach lemma [2], we obtain P′(s0) is invertible and
‖P′(s0)−1P′(γ∗)‖≤11−υ0(‖s0−γ∗‖)<11−υ0(r). | (2.21) |
Then, t0 is well defined. Therefore, we can write that
t0−γ∗=s0−γ∗−P′(s0)−1P(s0)=−P′(s0)−1P′(γ∗)∫10P′(γ∗)−1[P′(γ∗+θ(s0−γ∗))−P′(s0)](s0−γ∗)dθ. | (2.22) |
Using (2.2), (2.3), (2.10), (2.20), and (2.21), we obtain in turn that
‖t0−γ∗‖≤‖P′(s0)−1P′(γ∗)‖‖∫10P′(γ∗)−1[P′(γ∗+θ(‖s0−γ∗‖))−P′(s0)]‖dθ‖s0−γ∗‖≤∫10υ(‖γ∗+θ(‖s0−γ∗‖)−s0‖)dθ1−υ0(‖s0−γ∗‖)‖s0−γ∗‖=∫10υ(‖(θ−1)(s0−γ∗)‖)dθ1−υ0(‖s0−γ∗‖)‖s0−γ∗‖=h1(‖s0−γ∗‖)‖s0−γ∗‖<‖s0−γ∗‖<r, | (2.23) |
which shows the estimate (2.16) for n=0 and t0∈U(γ∗,r).
Using (2.2), (2.4), (2.10), (2.12), (2.16), and (2.23), we obtain
‖(P′(γ∗)(s0−γ∗))−1[P(s0)−P(γ∗)−2βP(t0)−P′(γ∗)(s0−γ∗)]‖≤1‖s0−γ∗‖‖∫10P′(γ∗)−1(P′(γ∗+θ(s0−γ∗))−P′(γ∗))(s0−γ∗)dθ‖+1‖s0−γ∗‖⋅2|β|‖∫10P′(γ∗)−1P′(γ∗+θ(t0−γ∗))dθ‖‖t0−γ∗‖≤1‖s0−γ∗‖‖∫10P′(γ∗)−1(P′(γ∗+θ(s0−γ∗))−P′(γ∗))(s0−γ∗)dθ‖+1‖s0−γ∗‖⋅2|β|∫10ω1(‖θ(t0−γ∗)‖)dθ‖t0−γ∗‖≤∫10υ0(‖θ(s0−γ∗)‖)dθ+2|β|h1(‖s0−γ∗‖)∫10ω1(θ(h1(‖s0−γ∗‖)‖s0−γ∗‖)r)dθ=h2(‖s0−γ∗‖)<h2(r)<1, | (2.24) |
where
P′(γ∗)−1P(t0)=P′(γ∗)−1(P(t0)−P(γ∗))=∫10P′(γ∗)−1P′(γ∗+θ(t0−γ∗))(t0−γ∗)dθ, | (2.25) |
so
‖P′(γ∗)−1P(t0)‖≤∫10ω1(‖θ(t0−γ∗)‖)‖t0−γ∗‖dθ≤h1(‖s0−γ∗‖)‖s0−γ∗‖∫10ω1(‖θ(t0−γ∗)‖)dθ | (2.26) |
and
‖γ∗+θ(t0−γ∗)−γ∗‖=θ‖t0−γ∗‖≤‖t0−γ∗‖≤r. |
Thus, (P(s0)−2βP(t0))−1∈L(T1,T2) and
‖(P(s0)−2βP(t0))−1P′(γ∗)‖≤1(1−h2(‖s0−γ∗‖))‖s0−γ∗‖. | (2.27) |
So, z0 is well defined.
Using (2.2), (2.5), (2.12), (2.16), (2.21), (2.24), and (2.27), we have that
‖z0−γ∗‖≤‖s0−γ∗−P′(s0)−1P(s0)‖+‖P′(γ∗)−1P(t0)‖‖P′(γ∗)−1P(s0)‖‖P′(s0)−1P′(γ∗)‖‖(P(s0)−2βP(t0))−1P′(γ∗)‖≤h1(‖s0−γ∗‖)‖s0−γ∗‖+∫10ω1(‖θ(t0−γ∗)‖)ω1(‖θ(s0−γ∗)‖)dθ‖t0−γ∗‖(1−υ0(‖s0−γ∗‖))(1−h2(‖s0−γ∗‖))≤h1(‖s0−γ∗‖)‖s0−γ∗‖[1+∫10ω1(‖θ(t0−γ∗)‖)ω1(‖θ(s0−γ∗)‖)dθ(1−υ0(‖s0−γ∗‖))(1−h2(‖s0−γ∗‖))]=h3(‖s0−γ∗‖)‖s0−γ∗‖<‖s0−γ∗‖<r, | (2.28) |
which shows the estimate (2.17) for n=0 and z0∈U(γ∗,r).
Next, we shall show that
([z0,t0;P]+2(z0−t0)[z0,t0,s0;P]−(z0−t0)[t0,s0,s0;P])−1∈L(T1,T2). | (2.29) |
Using (2.2), (2.6), (2.11), (2.13), and (2.14), we have that
‖P′(γ∗)−1([z0,t0;P]+2(z0−t0)[z0,t0,s0;P]−(z0−t0)[t0,s0,s0;P]−P′(γ∗))‖≤‖P′(γ∗)−1([z0,t0;P]−P′(γ∗))‖+‖z0−t0‖‖P′(γ∗)−1([z0,t0,s0;P]−[t0,s0,s0;P])‖+‖z0−t0‖‖P′(γ∗)−1[z0,t0,s0;P]‖≤ω0(‖z0−γ∗‖,‖t0−γ∗‖)+(‖z0−γ∗‖+‖t0−γ∗‖)(ω2(‖z0−t0‖,‖t0−s0‖)+ω3(‖z0−γ∗‖,‖t0−γ∗‖,‖s0−γ∗‖))=ω0(h3(‖s0−γ∗‖)‖s0−γ∗‖,h1(‖s0−γ∗‖)‖s0−γ∗‖)+(h3(‖s0−γ∗‖)‖s0−γ∗‖+h1(‖s0−γ∗‖)‖s0−γ∗‖)(ω2(h3(‖s0−γ∗‖)‖s0−γ∗‖+h1(‖s0−γ∗‖)‖s0−γ∗‖,(h1(‖s0−γ∗‖)+1)‖s0−γ∗‖)+ω3(h3(‖s0−γ∗‖)‖s0−γ∗‖,h1(‖s0−γ∗‖)‖s0−γ∗‖,‖s0−γ∗‖))=h4(‖s0−γ∗‖)<1. | (2.30) |
By the Banach lemma, we have that ([z0,t0;P]+2(z0−t0)[z0,t0,s0;P]−(z0−t0)[t0,s0,s0;P]) is invertible and
‖([z0,t0;P]+2(z0−t0)[z0,t0,s0;P]−(z0−t0)[t0,s0,s0;P])−1P′(γ∗)‖≤11−h4(‖s0−γ∗‖). | (2.31) |
Denote △=[z0,t0;P]+2(z0−t0)[z0,t0,s0;P]−(z0−t0)[t0,s0,s0;P]. Thus, x1 is well defined.
Using x1∈U(γ∗,r), (2.2), (2.8), (2.12), (2.28), and (2.31), we have that
‖s1−γ∗‖≤‖z0−γ∗‖−‖△−1P′(γ∗)P′(γ∗)−1P(z0)‖≤‖z0−γ∗‖−∫10ω1(θ‖z0−γ∗‖)dθ1−h4(‖s0−γ∗‖)‖z0−γ∗‖≤[1−∫10ω1(θ‖z0−γ∗‖)dθ1−h4(‖s0−γ∗‖)]‖z0−γ∗‖≤[1−∫10ω1(θ‖z0−γ∗‖)dθ1−h4(‖s0−γ∗‖)]h3(‖s0−γ∗‖)‖s0−γ∗‖=h5(‖s0−γ∗‖)‖s0−γ∗‖<‖s0−γ∗‖<r, | (2.32) |
which shows the estimate (2.18) for n=0 and s1∈U(γ∗,r). By substituting s0,t0,z0,s1 in the previous estimates with sk,tk,zk,sk+1, we get (2.16)–(2.18). Using the estimates
‖sk+1−γ∗‖<‖sk−γ∗‖<r, |
we derive that sk+1∈U(γ∗,r) and limk→∞sk=γ∗.
Finally, in order to prove the uniqueness of the solution γ∗, suppose there exists a second solution y∗∈ˉB(γ∗,R), then P(y∗)=0. Denote T=∫10P′(y∗+θ(γ∗−y∗))dθ. Since T(y∗−γ∗)=P(y∗)−P(γ∗)=0, if T is invertible then y∗=γ∗. In fact, by (2.19), we obtain
‖P′(γ∗)−1(T−P′(γ∗))‖≤∫10υ0(‖y∗+θ(γ∗−y∗)−γ∗‖)dθ≤∫10υ0(‖(θ−1)(γ∗−y∗)‖)dθ<∫10υ0(|θ−1|R)dθ<1. | (2.33) |
Thus, according to the Banach lemma, T is invertible. Since 0=P(y∗)−P(γ∗)=T(y∗−γ∗), we conclude that γ∗=y∗. The proof is over.
In this section, we study some dynamical properties of the family of the iterative methods (1.3), which are based on their attractive basins on the complex polynomial f(z). The convergence and stability of the iterative methods are compared by studying the structure of attractive basins.
There are some dynamical concepts and basic results to be used later. Let f:ˆC→ˆC be a rational function on the Riemann sphere ˆC. The orbit of a point z0∈ˆC is defined as
{z0,f(z0),f2(z0),⋯,fn(z0),⋯}. |
In addition, if f(z0)=z0, z0 is a fixed point. There are the following four cases:
● If |f′(z0)|<1, z0 is an attractive point;
● If |f′(z0)|=1, z0 is a neutral point;
● If |f′(z0)|>1, z0 is a repulsive point;
● If |f′(z0)|=0, z0 is an super-attractive point.
The basin of attraction of an attractor z∗ is defined by
A(z∗)={z0∈ˆC:fn(z0)→z∗,n→∞}. |
Consider the following four members of the family (1.3): M1(β=0), M2(β=0.5), M3(β=1), M4(β=2). In this study, the complex plane is Ω=[−5,5]×[−5,5] with 500×500 points. If the sequence converges to roots, it is represented in pink, yellow, and blue. Otherwise, black represents other cases, including non-convergence. When the family (1.3) is applied to the complex polynomials f(z)=z2−1 and f(z)=z3−1, their attractive basins are shown in Figures 1 and 2.
In Figures 1 and 2, the fractal graphs of the methods M1 and M4 have some black zones. The black zones indicates non-convergence, and the initial value of the black area causes the iteration to fail; relatively speaking, the method without a black region is better. However, the fractal graphs of the methods M2 and M3 have a black zone. As a result, the convergence of the methods M2 and M3 is better than that of the methods M1 and M4. In addition, the method M3 has the largest basins of attraction compared to the other three methods. Thus, the stable parameters are β=0.5,1.
In this section, we apply the following two numerical examples to compute the above results of convergence for method (1.3).
Example 4.1. Let Ω=(0,2); define the function P:Ω→R by
P(x)=x3−1. | (4.1) |
Thus, a root of P(x)=0 is γ∗=1. Then,
P′(x)=3x2 |
and
[x,y;P]=x2+xy+y2. |
Notice that using conditions (2.9)–(2.15), β=0, we obtain
υ0(ξ)=3t,υ(t)=83t, |
γ0=13,Ω0=(23,43), |
ω0(t,s)=109t+119s,ω1(t)=163t, |
and
ω2(t,s)=13t+13s,ω3(t,s,u)=13t+13s+13u+1. |
Then, according to the above definition of functions hi(i=1,2,3,4,5), one have that
r1≈0.230769,r3≈0.221531,r5≈0.130342=r. |
Example 4.2. Let Ω=(−1,1), define the function P:Ω→R by
P(x)=ex−1. | (4.2) |
Thus, a root of P(x)=0 is γ∗=0. Then,
P′(x)=ex |
and
[x,y;P]=1y−x(ey−ex). |
Notice that using conditions (2.9)–(2.15), β=1, we obtain
υ0(t)=et−1,υ(t)=et−1, |
γ0=ln2,Ω0=(−ln2,ln2), |
ω0(t,s)=1t+s(et−es)−1,ω1(t)=et, |
ω2(t+s,s+u)=(1(s+u)(u+t)+1(s+u)2)(eu−es)−1(s+t)(u+t)(es−et), |
and
ω3(t,s,u)=1(t+u)(s+u)(eu−et)−1(t+s)(s+u)(et−es). |
Then, according to the above definition of functions hi(i=1,2,3,4,5), one obtains
r1≈0.511083,r3≈0.270027,r5≈0.210013=r. |
In this section, the iterative method (1.3) is applied to the following six practical models. For the nonlinear equations obtained from the six models, we can find the solutions of the equations and the data results, such as iterative errors. Therefore, our research is valuable for practical models in various fields.
Example 4.3. Vertical stresses [21]: At uniform pressure t, the Boussinesq's formula is used to calculate the vertical stress y caused by a specific point within the elastic material under the edge of the rectangular strip footing. The following formula is obtained:
σy=tπx+cos(x)sin(x). | (4.3) |
If the value of y is determined, we can find the value of x where the vertical stress y equals 25 percent of the applied footing stress t. When x=0.4, the following nonlinear equation is obtained:
P1(s)=sπ+1πcos(s)sin(s)−14. | (4.4) |
Example 4.4. Civil Engineering Problem [22]: Some horizontal construction projects, such as the topmost portion of civil engineering beams, are used in the mathematical modeling of the beams. In order to describe the exact position of the beam in this particular case, some mathematical models based on nonlinear equations have been established. The following model is given in [22]:
P2(s)=s4+4s3−24s2+16s+16. | (4.5) |
Example 4.5. The trajectory of an electron moving between two parallel plates is defined by
y(l)=s0+(ν0+eE0mωsin(ωl0+α))+eE0mω2(cos(ωl+α)+sin(ω+α)), | (4.6) |
where m and e denote the mass and the charge of the electron at rest, ν0 and s0 denote the velocity and position of the electron at time l0, and E0sin(ωl0+α) denotes the RF electric field between the plates. By selecting specific values, one obtains
P3(s)=π4+s−12cos(s). | (4.7) |
Example 4.6. Blood rheology model [23]: Medical research that concerns the physical and flow characteristics of blood is called blood rheology. Since blood is a non-Newtonian fluid, it is often referred to as a Caisson fluid. Based on the caisson flow characteristics, when the basic fluid, such as water or blood, passes through the tube, it usually maintains its primary structure. When we observe the plug flow of Caisson fluid flow, the following nonlinear equation is considered:
P4(s)=s8441−8s563+16s29−0.05714285714s4−3.624489796s+0.36, | (4.8) |
where s is the plug flow of Caisson fluid flow.
Example 4.7. Law of population growth [24]: Population dynamics are tested by first-order linear ordinary differential equations in the following way:
P′(u)=sP(u)+c, | (4.9) |
where s denotes the population's constant birth rate and c denotes its constant immigration rate. P(u) stands for the population at time u. Then, according to solve the above linear differential equation (4.9), the following equation is obtained:
P(u)=(P0+cs)esu−cs, | (4.10) |
where P0 represents the initial population. According to the different values of the parameter and the initial conditions in [25], a nonlinear equation for calculating the birth rate is obtained:
P5(s)=−es(435s+1000)+435s+1564. | (4.11) |
Example 4.8. The non-smooth function (1.4) is defined on Ω=[0,1] by
P6(s)={s3lns2−s5+s4,s≠0;0,s=0. | (4.12) |
The parameter β=1 is selected, and the iterative method (1.3) is applied to the above six practical application examples. Table 1 gives the specific results. k denotes the number of iterations. Fun denotes the function Pi(1=1,2,3,4,5). |P(sn)−P(sn−1)| denotes the error values. |P(sn)| denotes function values at the last step. Approximated computation order of convergence denotes ACOC. γ∗ denotes the root of equation Pi(s)=0(i=1,2,3,4,5). The stopping criteria is that if the significant digits of the error precision exceed 5, the output will be made. Approximated computation order of convergence (ACOC) is defined by [26]
ACOC≈ln(|xn+1−xn|/|xn−xn−1|)ln(|xn−xn−1|/|xn−1−xn−2|). | (4.13) |
Fun | k | s0 | |P(sn)−P(sn−1)| | |P(sn)| | ACOC | γ∗ |
P1 | 5 | 2.5 | 2.21248e-101 | 1.17865e-101 | 8.0 | 0.415856 |
P2 | 5 | 2.5 | 0.0000158022 | 7.82769e-9 | 8.0 | 2.000018 |
P3 | 5 | 4.5 | 1.07326e-2387 | 9.10019e-2388 | 8.0 | -0.309093 |
P4 | 5 | 4.5 | 3.56215e-517 | 1.9089e-516 | 8.0 | 1.570111 |
P5 | 5 | 4.5 | 3.87571e-1076 | 5.18954e-1073 | 8.0 | 0.100998 |
P6 | 5 | 0.8 | 6.64779e-258 | 6.64779e-258 | 8.0 | 1.000000 |
In Table 1, for six models, the error accuracy is from 10−10 to 10−2387, and the computational order of convergence is the optimal order 8. When the initial point is 2.5, the error and precision of function P1 are higher than those of function P2. When the initial point is 4.5, the error and precision of function P3 are higher than those of functions P4 and P5. At the same time, solutions to six decimal places are obtained to improve the accuracy of solutions.
In this paper, local convergence analysis of a high-order Chebyshev-type method free from second derivatives is studied under ω-continuity assumptions. In contrast to the conditions used in previous studies, the new conditions of convergence are weaker. This study extends the applicability of method (1.3). Also, the radii of convergence balls and uniqueness of the solution are also discussed. By drawing the basins of attraction, four methods with different parameter values are compared with each other. Thus, we can find that when the parameter β=1 of method (1.3), the method M3 is relatively more stable. Then, two numerical examples are used to prove the criteria of convergence. Finally, we apply the method (1.3) to six concrete models. In Table 1, the numerical results such as iterative errors, ACOC, and so on are obtained. Therefore, our research is valuable for practical models in various fields.
The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this article.
This research was supported by the National Natural Science Foundation of China (No. 61976027), the Open Project of Key Laboratory of Mathematical College of Chongqing Normal University (No.CSSXKFKTM202005), the Natural Science Foundation of Liaoning Province (Nos. 2022-MS-371, 2023-MS-296), the Educational Commission Foundation of Liaoning Province of China (Nos. LJKMZ20221492, LJKMZ20221498, LJ212410167008), and the Key Project of Bohai University (No. 0522xn078), the Innovation Fund Project for Master's Degree Students of Bohai University (YJC2024-023).
The authors declare there are no conflicts of interest.
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Fun | k | s0 | |P(sn)−P(sn−1)| | |P(sn)| | ACOC | γ∗ |
P1 | 5 | 2.5 | 2.21248e-101 | 1.17865e-101 | 8.0 | 0.415856 |
P2 | 5 | 2.5 | 0.0000158022 | 7.82769e-9 | 8.0 | 2.000018 |
P3 | 5 | 4.5 | 1.07326e-2387 | 9.10019e-2388 | 8.0 | -0.309093 |
P4 | 5 | 4.5 | 3.56215e-517 | 1.9089e-516 | 8.0 | 1.570111 |
P5 | 5 | 4.5 | 3.87571e-1076 | 5.18954e-1073 | 8.0 | 0.100998 |
P6 | 5 | 0.8 | 6.64779e-258 | 6.64779e-258 | 8.0 | 1.000000 |
Fun | k | s0 | |P(sn)−P(sn−1)| | |P(sn)| | ACOC | γ∗ |
P1 | 5 | 2.5 | 2.21248e-101 | 1.17865e-101 | 8.0 | 0.415856 |
P2 | 5 | 2.5 | 0.0000158022 | 7.82769e-9 | 8.0 | 2.000018 |
P3 | 5 | 4.5 | 1.07326e-2387 | 9.10019e-2388 | 8.0 | -0.309093 |
P4 | 5 | 4.5 | 3.56215e-517 | 1.9089e-516 | 8.0 | 1.570111 |
P5 | 5 | 4.5 | 3.87571e-1076 | 5.18954e-1073 | 8.0 | 0.100998 |
P6 | 5 | 0.8 | 6.64779e-258 | 6.64779e-258 | 8.0 | 1.000000 |