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Prediction of conotoxin type based on long short-term memory network


  • Aiming at the problems of the wet experiment method in identifying the types of conotoxins, such as the complexity, low efficiency and high cost, this study proposes a method that uses the sequence information of the conotoxin peptides combined with long short term memory networks (LSTM) models to predict the Methods of spirotoxin category. This method only needs to take the conotoxin peptide sequence as input, and adopts the character embedding method in text processing to automatically map the sequence to the feature vector representation, and the model extracts features for training and prediction. Experimental results show that the correct index of this method on the test set reaches 0.80, and the AUC value reaches 0.817. For the same test set, the AUC value of the KNN algorithm is 0.641, and the AUC value of the method proposed in this paper is 0.817, indicating that this method can effectively assist in identifying the type of conotoxin.

    Citation: Feng Wang, Shan Chang, Dashun Wei. Prediction of conotoxin type based on long short-term memory network[J]. Mathematical Biosciences and Engineering, 2021, 18(5): 6700-6708. doi: 10.3934/mbe.2021332

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  • Aiming at the problems of the wet experiment method in identifying the types of conotoxins, such as the complexity, low efficiency and high cost, this study proposes a method that uses the sequence information of the conotoxin peptides combined with long short term memory networks (LSTM) models to predict the Methods of spirotoxin category. This method only needs to take the conotoxin peptide sequence as input, and adopts the character embedding method in text processing to automatically map the sequence to the feature vector representation, and the model extracts features for training and prediction. Experimental results show that the correct index of this method on the test set reaches 0.80, and the AUC value reaches 0.817. For the same test set, the AUC value of the KNN algorithm is 0.641, and the AUC value of the method proposed in this paper is 0.817, indicating that this method can effectively assist in identifying the type of conotoxin.



    Neural network dynamics have attracted much attention owing to the wide applications in associative memory [1], signal processing [2], intelligent control [3], and so on. The mainly dynamical behaviours in neural network systems include stability [4,5,6,7,8,9,10], synchronization [11,12], bifurcation [13], chaos [14] and reaction-diffusion[15], which reflect the characteristics of network systems. Fractional calculus has good free space and infinite storage space in many fields, such as artificial neural networks [16], genetic algorithm [17] and image enhancement [18].

    Time delay is an interesting phenomenon in network systems, resulting from differences in the efficiency of signal transmission from the point of generation to the point of reception during network transmission, as well as interference from other external factors. Recently, the results with regard to time delay phenomena are extensively reported including leakage time delay[19], discrete time delay[20], distributed time delay[21] and so on. In actual industrial operation, uncertainties in the parameters associated with the model coefficients can arise due to operational errors, incomplete considerations and model construction. Therefore, the models with uncertain parameters will further improve the robustness of systems in [22,23,24].

    Synchronization, as one of the typical dynamical behaviours, such as collective recitations, military parades and resonance phenomena, and has become a hot topic [15,22,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43] including Fin-TS [22,26,27,28,29], Fix-TS [22,25,26,30], exponential synchronization[31,32,33,34,35], Mittag-Leffler synchronization[36,37,38], projective synchronization[36,39], quasi-synchronization[40,41], global synchronization[42]. Lin et al. [15] explored the synchronization of directly coupled QDNNs based on pinning control. Li et al. [22] investigated Fin-TS and Fix-TS of Caputo QVNNs by employing feedback and adaptive controllers. Wei et al. [25] studied Fix-TS of QNNs by a pure power-law control design. Kashkynbayev et al. [26] discussed Fin-TS and Fix-TS of DNNs by designing proper control functions. Hu et al.[43] used an adaptive distributed approach at the edge to study the synchronization of spatio-temporal networks. In fact, Fin-TS and Fix-TS are more relevant to realistic control requirements. However, very few research results on Fin-TS and Fix-TS for fractional order NNs are reported except [44,45], where the controller designs for Fix-TS are denoted in fractional order form, then this will undoubtedly increase the difficulty to explore the dynamics of systems.

    Inspired by these works, this paper focuses on Fin-TS and Fix-TS issues on Caputo QDNNs with uncertainty. Different from the decomposition method [23,25,35,46], Laplace transform [40,47,52], comparison principle [23,48,49] and linear matrix inequality (LMI) [30,41,50], we apply the quaternion direct method, the Lyapunov stability method and the quaternion inequality method to establish the synchronization criterion for Caputo QDNNs. It is worth noting that a new Caputo differential inequality is constructed, then the fixed time of the positive definite function is estimated. The propoesd method can greatly simplify the complexity of the calculation and solve the complexity of controller design caused by the immaturity of the fractional fixed time stability theory, which is very convenient to derive Fix-TS condition to Caputo QDNNs.

    The main innovations and highlights of this paper are presented below.

    The model includes the discrete and distributed delays, uncertain term and Caputo derivative operator.

    A new Caputo differential inequality is constructed, then the fixed time of the positive definite function is estimated.

    Applying quaternion direct method rather than the decomposition method, the algebraic discriminant conditions to achieve Fin-TS and Fix-TS on Caputo QDNNs are proposed.

    The control strategies to design the appropriate self feedback and adaptive controllers can effectively reduce the consumption of control costs caused by the time delay term.

    In this section, the basic definitions, related lemmas and model introduction are described.

    Definition 2.1. Fractional integral of the order μ of k(t) is defined as [51]

    t0Dμtk(t)=1Γ(μ)tt0(tl)μ1k(l)dl.

    Definition 2.2. The Caputo-type fractional-order derivative of the function k(t) is defined as [51]

    Ct0Dμtk(t)=1Γ(nμ)tt0(tl)nμ1k(n)(l)dl,

    where t>t0, n=[μ]+1.

    Lemma 2.1. If 0<μ<1, αR, then [49]

    Ct0Dμtkα(t)=Γ(1+α)Γ(1+αμ)kαμ(t)Ct0Dμtk(t).

    Lemma 2.2. Let k(t) be a differentiable function over the quaternion field Q, then [22]

    Ct0Dμt[¯k(t)k(t)]¯k(t)Ct0Dμtk(t)+[Ct0Dμt¯k(t)]k(t), 0<μ<1.

    Lemma 2.3. Let χ and φ be any constant in the quaternion field Q, for any positive number θ in the real number field R, then [44]

    ¯χφ+¯φχθ¯χχ+θ1¯φφ.

    Lemma 2.4. If ξi0, 0<θ1, γ>1, for i=1,2,,s, then [25]

    si=1ξθi(si=1ξ)θ,  si=1ξγis1γ(si=1ξi)γ.

    Lemma 2.5. Suppose the positive definite function V(t) is a continuously differentiable function on [0,+), if there are positive numbers 0<μ<1, λ>0, v1, γ>0, such that [22]

    Ct0DμtV(t)λVv(t)γ,

    then when t¯T, limt¯TV(t)=0, and for any t¯T, V(t)=0 holds, where

    ¯T=t0+{Γ(1+μ)λ(1+v)[(V(t0)+(λγ)1v)1+v(λγ)1+vv]}1μ.

    Lemma 2.6. Suppose k(t) is a continuously differentiable function on [t0,ξ), for any constant ζ on interval [t0,ξ), then [22]

    Ct0Dμt[k(t)ζ]22[k(t)ζ]Ct0Dμtk(t), 0<μ<1.

    In this paper, a class of Caputo QDNNs with delays and uncertain coefficients is considered as the drive system

    Ct0Dμtkp(t)=apkp(t)+nw=1(bpw+Δbpw(t))gw(kw(t))+nw=1(cpw+Δcpw(t))gw(kw(tτ1(t)))+nw=1(dpw+Δdpw(t))ttτ2(t)gw(kw(s))ds+Ip(t), (2.1)

    where 0<μ<1, kp(t) is the state vector representing the p-th neuron, ap is the self feedback regulation coefficient, gw() is the activation function, bpw+Δbpw(t), cpw+Δcpw(t) and dpw+Δdpw(t) are connection weights, Δbpw(t), Δcpw(t), Δdpw(t) are the uncertain coefficients, Ip(t) is an external input, τ1(t), τ2(t) are time-varying delays, apR, the other coefficients belong to quaternion field Q.

    The response system associated with System (2.1) is

    Ct0Dμtop(t)=apop(t)+nw=1(bpw+Δbpw(t))gw(ow(t))+nw=1(cpw+Δcpw(t))gw(ow(tτ1(t)))+nw=1(dpw+Δdpw(t))ttτ2(t)gw(oq(s))ds+Ip(t)+Up(t), (2.2)

    where Up(t)Q stands for controller, kp(t0)Q and ow(t0)Q are the initial conditions of derive-response Systems (2.1) and (2.2).

    Let ~p(t)=op(t)kp(t), then error system of derive-response Systems (2.1) and (2.2) is:

    Ct0Dμt~p(t)=ap~p(t)+nw=1(bpw+Δbpw(t))(gw(ow(t))gw(kw(t)))+nw=1(cpw+Δcpw(t))(gw(ow(tτ1(t)))gw(kw(tτ1(t))))+nw=1(dpw+Δdpw(t))ttτ2(t)(gw(ow(s))gw(kw(s)))ds+Up(t), (2.3)

    then the initial condition to System (2.3) is ~p(t0)=op(t0)kp(t0).

    Throughout this paper, the following assumptions and synchronization definitions are given:

    Assumption 2.1. For any ki,oi, there exists a positive number li, such that

    |gi(ki)gi(oi)|li|kioi|, i=1,2,...,n,

    where g()=(g1(),g2(),...,gn())TQn is the activation function in System (2.1).

    Assumption 2.2. For uncertain coefficients Δ(t), Δcpw(t), Δdpw(t), there exist constants ^bpw, ^cpw, ^dpw, such thatΔbpw(t)=ˆbpwαpw(t), Δcpw(t)=ˆcpwβpw(t),Δdpw(t)=ˆdpwωpw(t), where αpw(t),βpw(t), ωpw(t) are uncertain quantities under ¯αpw(t)αpw(t)1, ¯βpw(t)βpw(t)1, ¯ωpw(t)ωpw(t)1.

    Definition 2.3. For Systems (2.1) and (2.2), if there exists a positive constant ¯T related to the initial condition, such that limt¯T||~p(t)||=0, ||~p(t)||=0 holds for any t¯T, then Systems (2.1) and (2.2) are said to reach Fin-TS [22].

    Definition 2.4. For Systems (2.1) and (2.2), if there exists a positive constant T independent of the initial condition, such that limtT||~p(t)||=0, for any tT, ||~p(t)||=0 holds, then Systems (2.1) and (2.2) are said to reach Fix-TS [44].

    Remark 2.1. The models with uncertain parameters can further improve the robustness of systems in [22,23,24]. In this paper, the model (2.1) includes the discrete and distributed delays, uncertain term and Caputo derivative operator. Different from the constant time delays in [23,34,47], the time delays in model (2.1) are variable, which can enhance the applicability of the model and enrich the results of Fin-TS and Fix-TS.

    In this section, we mainly establish Fin-TS and Fix-TS criteria between Systems (2.1) and (2.2).

    Firstly, we construct a Caputo derivative differential inequality to estimate Fix-TS time for the positive definite function V(t).

    Theorem 3.1. Let V(t)V(t,φ(t)) be a continuously positive definite and radially unbounded function, and V(t,φ(t))=0 if and only if φ(t)=0. If

    Ct0DαtV(t)ξVδ(t)ηVε(t), (3.1)

    where 0<ε<α<1, 1<δ<1+α, ξ>0, η>0, then for any tT=t0+T1+T2, the equality V(t)=0 holds, where

    T1=[Γ(1δ)Γ(1+α)ξΓ(1+αδ)]1α ,  T2=[Γ(1ε)Γ(1+α)ηΓ(1+αε)]1α. (3.2)

    Proof. We first prove that when tt0, there exists a t, such that V(t)1. Otherwise, for any tt0, V(t)>1. From inequality (3.1), we can get that the following two differential inequalities are simultaneously true

    Ct0DαtV(t)ξVδ(t),  Ct0DαtV(t)ηVε(t). (3.3)

    Taking the Caputo derivative of order α on t0t for Vαδ(t), from Lemma 2.1, then we get

    Ct0DαtVαδ(t)=Γ(1+αδ)Γ(1δ)Vδ(t)Ct0DαtV(t)Γ(1+αδ)Γ(1δ)Vδ(t)(ξVδ(t))=ξΓ(1+αδ)Γ(1δ). (3.4)

    For both sides of inequality (3.4), we take α-order fractional integral on t0t below

    t0DαtCt0DαtVαδ(t)t0Iαt(ξΓ(1+αδ)Γ(1δ)). (3.5)

    Then, we have

    Vαδ(t)Vαδ(t0)ξΓ(1+αδ)Γ(1δ)1Γ(α+1)(tt0)α, (3.6)
    (1V(t))δαVαδ(t0)+ξΓ(1+αδ)Γ(1δ)Γ(1+α)(tt0)α, (3.7)
    V(t)[1Vαδ(t0)+ξΓ(1+αδ)Γ(1δ)Γ(1+α)(tt0)α]1δα. (3.8)

    From inequality (3.8), we know that V(t) is monotonically decreasing. Take

    t=t0+[Vδα(t0)1ξΓ(1+αδ)Γ(1δ)Γ(1+α)Vδα(t0)]1α,

    then the inequality V(t)1 holds. Let

    T1=t0+[Γ(1δ)Γ(1+α)ξΓ(1+αδ)]1α,

    thus we have T1>t. Similarly, we can also get

    Ct0DαtVαε(t)=Γ(1+αε)Γ(1ε)Vε(t)Ct0DαtV(t)ηΓ(1+αε)Γ(1ε), (3.9)
    V(t)[Vαε(t)ηΓ(1+αε)Γ(1ε)Γ(1+α)(tt)α]1αε[1ηΓ(1+αε)Γ(1ε)Γ(1+α)(tt)α]1αε. (3.10)

    Let

    T2=[Γ(1ε)Γ(1+α)ηΓ(1+αε)]1α,

    when t=t+T2, then the right hand side of inequality (3.10) is equal to 0. Furthermore, we can get that V(t)0 when t=t+T2. Since V(t) is a positive definite function, when t=t+T2, V(t)0. Let t=t0+T1+T2, then we can get V(t)=0 holds. When tt0+T1+T2, we have φ(t)=0, and the settling time is estimated as T.

    Remark 3.1. Recently, many synchronization results have been reported in [15,22,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43] including Fin-TS [22,26], Fix-TS [22,25,26], exponential synchronization[31,32,33,34,35], Mittag-Leffler synchronization[36,37,38], projective synchronization[36,39] and quasi-synchronization[40,41]. In Theorem 3.1, a new Caputo differential inequality is constructed, then the fixed time of the positive definite function is estimated, which is very convenient to derive Fix-TS conditions between Systems (2.1) and (2.2).

    To achieve Fin-TS between Systems (2.1) and (2.2), the self feedback controller is designed

    {Up(t)=ψp(t)+ϕp(t),ψp(t)=αp~p(t),ϕp(t)=δ~p(t)|~p(t)|2σ~p(t)|~p(t)|2ε, (3.11)

    where ε2,αp,δ and σ are positive constants.

    Theorem 3.2. Under Assumptions 2.1, 2.2 and controller (3.11), if there exist positive constants h>1 and r>1, such that

    2nlp2+nw=1(Ω+Π+Ψ)2ap2αp+2nlp2h+2nlp2r0, (3.12)

    then Systems (2.1) and (2.2) can achieve Fin-TS, and the settling time of Systems (2.1) and (2.2) is

    ¯T=t0+{Γ(1+μ)2σnεε[(V(t0)+n(σδ)1ε1)εnε(σδ)εε1]}1μ, (3.13)

    whereΩ=|bpw|2+^|bpw|2, Π=|cpw|2+^|cpw|2, Ψ=|dpw|2+^|dpw|2, lp,lp and lp are Lipschitz coefficients.

    Proof. Choosing the following Lyapunov function

    V1(t)=np=1¯~p(t)~p(t). (3.14)

    From Lemma 2.2, we have

    Ct0DμtV1(t)np=1[¯~p(t)Ct0Dμt~p(t)+(Ct0Dμt¯~p(t))~p(t)]=np=1¯~p(t)[ap~p(t)+nw=1(bpw+Δbpw(t))(gw(ow(t))gw(kw(t)))]+np=1¯~p(t)[nw=1(cpw+Δcpw(t))(gw(ow(tτ1(t)))gw(kw(tτ1(t))))]+np=1¯~p(t)[nw=1(dpw+Δdpw(t))ttτ2(t)(gw(ow(s))gw(kw(s)))ds+Up(t)]+np=1[ap¯~p(t)+nw=1¯(gw(ow(t))gw(kw(t)))(¯bpw+¯Δbpw(t))]~p(t)+np=1[nw=1¯(gw(ow(tτ1(t)))gw(kw(tτ1(t))))(¯cpw+¯Δcpw(t))]~p(t)+np=1[nw=1ttτ2(t)¯(gw(ow(s))gw(kw(s)))ds(¯dpw+¯Δdpw(t))+¯Up(t)]~p(t). (3.15)

    By computation, we further get

    Ct0DμtV1(t)np=1[2ap¯~p(t)~p(t)+¯~p(t)Up(t)+¯Up(t)~p(t)]+np=1nw=1¯~p(t)bpw(gw(ow(t))gw(kw(t)))+np=1nw=1¯(gw(ow(t))gw(kw(t)))¯bpw~p(t)+np=1nw=1¯~p(t)Δbpw(t)(gw(ow(t))gw(kw(t)))+np=1nw=1¯(gw(ow(t))gw(kw(t)))¯Δbpw(t)~p(t)+np=1nw=1¯~p(t)cpw(gw(ow(tτ1(t)))gw(kw(tτ1(t))))+np=1nw=1¯(gw(ow(tτ1(t)))gw(kw(tτ1(t))))¯cpw~p(t)+np=1nw=1¯~p(t)Δcpw(t)(gw(ow(tτ1(t)))gw(kw(tτ1(t))))+np=1nw=1¯(gw(ow(tτ1(t)))gw(kw(tτ1(t))))¯Δcpw(t)~p(t)+np=1nw=1¯~p(t)dpwttτ2(t)(gw(ow(s))gw(kw(s)))ds+np=1nw=1ttτ2(t)¯(gw(ow(s))gw(kq(s)))ds¯dpw~p(t)+np=1nw=1¯~p(t)Δdpw(t)ttτ2(t)(gw(ow(s))gw(kw(s)))ds+np=1nw=1ttτ2(t)¯(gw(ow(s))gw(kw(s)))ds¯Δdpw(t)~p(t). (3.16)

    According to controller (3.11), we have

    np=1[¯~p(t)Up(t)+¯Up(t)~p(t)]=np=1¯~p(t)[αp~p(t)δ~p(t)|~p(t)|2σ~p(t)|~p(t)|2ε]+np=1[αp¯~p(t)δ¯~p(t)|~p(t)|2σ¯~p(t)|~p(t)|2ε]~p(t)np=1[2αp¯~p(t)~p(t)2σ(¯~p(t)~p(t))1ε2δ]. (3.17)

    In terms of Lemma 2.3, Assumptions 2.1 and 2.2, we have

    np=1nw=1¯~p(t)bpw(gw(ow(t))gw(kw(t)))+np=1nw=1¯(gw(ow(t))gw(kw(t)))¯bpw~p(t)np=1nw=1|bpw|2¯~p(t)~p(t)+np=1nw=1l2w¯~p(t)~p(t)np=1nw=1|bpw|2¯~p(t)~p(t)+nnp=1l2w¯~p(t)~p(t). (3.18)

    Similarly, we can get

    np=1nw=1¯~p(t)Δbpw(t)(gw(ow(t))gw(kw(t)))+np=1nw=1¯(gw(ow(t))gw(kw(t)))¯Δbpw(t)~p(t)+np=1nw=1¯~p(t)cpw(gw(ow(tτ1(t)))gw(kw(tτ1(t))))+np=1nw=1¯(gw(ow(tτ1(t)))gw(kw(tτ1(t))))¯cpw~p(t)+np=1nw=1¯~p(t)Δcpw(t)(gw(ow(tτ1(t)))gw(kw(tτ1(t))))+np=1nw=1¯(gw(ow(tτ1(t)))gw(kw(tτ1(t))))¯Δcpw(t)~p(t)+np=1nw=1¯~p(t)dpwttτ2(t)(gw(ow(s))gw(kw(s)))ds+np=1nw=1ttτ2(t)¯(gw(ow(s))gw(kw(s)))ds¯dpw~p(t)+np=1nw=1¯~p(t)Δdpw(t)ttτ2(t)(gw(ow(s))gw(kw(s)))ds+np=1nw=1ttτ2(t)¯(gw(ow(s))gw(ow(s)))ds¯Δdpw(t)~p(t)np=1[nl2p+nw=1^|bpw|2+nw=1(|cpw|2+^|cpw|2)+nw=1(|dpw|2+^|dpw|2)]¯~p(t)~p(t)+2nnp=1lp2¯~p(tτ1(t))~p(tτ1(t))+2nτ22(t)np=1lp2suptτ2(t)lt|~p(l)|2. (3.19)

    Substituting (3.17)(3.19) to (3.16), we can get

    Ct0DμtV1(t)np=1[2nl2p+nw=1(Ω+Π+Ψ)2ap2αp]¯~p(t)~p(t)+np=12nlp2¯~p(tτ1(t))~p(tτ1(t))+np=12nlp2τ22(t)suptτ2(t)lt|~p(l)|22σnp=1(¯~p(t)~p(t))1ε2δn, (3.20)

    where Ω=|bpw|2+^|bpw|2, Π=|cpw|2+^|cpw|2, Ψ=|dpw|2+^|dpw|2. From (3.12), Lemma 2.4, fractional-order Razumikhin theorem and Jensen Inequality, there exist h>1 and r>1, such that

    Ct0DμtV1(t)np=1[2nl2p+nw=1(Ω+Π+Ψ)2ap2αp]¯~p(t)~p(t)+np=12nlp2h¯~p(t)~p(t)+np=12nlp2r¯~p(t)~p(t)2σnp=1(¯~p(t)~p(t))1ε2δnnp=1[2nl2p+nw=1(Ω+Π+Ψ)2ap2αp+2nlp2h+2nlp2r]¯~p(t)~p(t)2σnε(np=1¯~p(t)~p(t))1ε2δn2σnεV(ε1)1(t)2δn. (3.21)

    According to Lemma 2.5, Systems (2.1) and (2.2) can realize Fin-TS under controller (3.11), and the settling time of Systems (2.1) and (2.2) is estimated as

    ¯T=t0+{Γ(1+μ)2σnεε[(V(t0)+n(σδ)1ε1)εnε(σδ)εε1]}1μ. (3.22)

    Therefore, when t¯T, we have ||~p(t)||=0, then Systems (2.1) and (2.2) can realize Fin-TS under controller (3.11).

    In order to realize Fix-TS of Systems (2.1) and (2.2), the following adaptive controller is designed

    {Up(t)=Ξp(t)+Hp(t),Ξp(t)=σp(t)~p(t),Hp(t)=k1p~p(t)(¯~p(t)~p(t))δk2p~p(t)(¯~p(t)~p(t))ε, (3.23)

    where μ<δ<0, 1μ<ε<1,k1p>0,k2p>0, and σp(t) is the adaptive control gain satisfying

    Ct0Dμtσp(t)=¯~p(t)~p(t)Sp[sign(σp(t)σp)]|σp(t)σp|12δRp[sign(σp(t)σp)]|σp(t)σp|12ε. (3.24)

    Theorem 3.3. Under Assumptions 2.1, 2.2 and controller (3.23), if there exist positive constants h>1 and r>1, such that

    nlp2+12nw=1(Ω+Π+Ψ)ap+nlp2h+nlp2rσp, (3.25)

    then Systems (2.1) and (2.2) can realize Fix-TS, and the settling time of Systems (2.1) and (2.2) is

    T=t0+[Γ(δ)Γ(1+μ)(2n)δH1Γ(μ+δ)]1μ+[Γ(ε)Γ(1+μ)H2Γ(μ+ε)]1μ, (3.26)

    where lp,lp and lp are Lipschitz coefficients.

    Proof. Take into account the following Lyapunov function

    V2(t)=np=1λp¯~p(t)~p(t)+np=1λp[σp(t)σp]2. (3.27)

    Similar to the proof Theorem 3.2, by Lemma 2.6 we have

    Ct0DμtV2(t)np=1λp[2nl2p+nw=1(Ω+Π+Ψ)2ap2σp(t)]¯~p(t)~p(t)+np=12nλplp2¯~p(tτ1(t))~p(tτ1(t))+np=12nλplp2τ2(t)suptτ2(t)lt|~p(l)|22k1pnp=1λp(¯~p(t)~p(t))1δ2k2pnp=1λp(¯~p(t)~p(t))1ε+np=1λp2(σp(t)σp)Ct0Dμtσp(t). (3.28)

    Under adaptive controller (3.23), we have

    Ct0DμtV2(t)np=1λp[2nl2p+nw=1(Ω+Π+Ψ)2ap2σp]¯~p(t)~p(t)+np=12nλplp2¯~p(tτ1(t))~p(tτ1(t))+np=12nλplp2τ2(t)suptτ2(t)lt|~p(l)|22k1pnp=1λp(¯~p(t)~p(t))1δnp=12λpSp((σp(t)σp)2)1δ2k2pnp=1λp(¯~p(t)~p(t))1εnp=12λpRp((σp(t)σp)2)1ε. (3.29)

    By fractional-order Razumikhin theorem, there are h>1,r>1, The following formula holds:

    Ct0DμtV2(t)np=1λp[2nl2p+nw=1(Ω+Π+Ψ)2ap2σp+2nlp2h+2nlp2r]¯~p(t)~p(t)2k1pnp=1λp(¯~p(t)~p(t))1δnp=12λpSp((σp(t)σp)2)1δ2k2pnp=1λp(¯~p(t)~p(t))1εnp=12λpRp((σp(t)σp)2)1ε. (3.30)

    An application of Lemma 2.4 yields that

    np=12k1pλp(¯~p(t)~p(t))1δ+np=12Spλp((σp(t)σp)2)1δ=np=12k1pλδp(λp¯~p(t)~p(t))1δ+np=12Spλδp(λp(σp(t)σp)2)1δH1[np=1(λp¯~p(t)~p(t))1δ+np=1(λp(σp(t)σp)2)1δ]2δH1[np=1[λp¯~p(t)~p(t)+λp(σp(t)σp)2]1δ](2n)δH1[np=1[λp¯~p(t)~p(t)+λp(σp(t)σp)2]]1δ=(2n)δH1V1δ2(t). (3.31)

    Similarly, one can get

    np=12k2pλp(¯~p(t)~p(t))1ε+np=12Rpλp((σp(t)σp)2)1εH2[np=1(λp¯~p(t)~p(t))1ε+np=1(λp(σp(t)σp)2)]H2np=1[λp¯~p(t)~p(t)+λp(σp(t)σp)2]1εH2[np=1[λp¯~p(t)~p(t)+λp(σp(t)σp)2]]1ε=H2V1ε2(t), (3.32)

    where H1=min1pn{2k1pλδp,2Spλδp},H2=min1pn{2k2pλεp,2Rpλεp}. Substituting (3.31) and (3.32) to (3.30), from (3.25), we have

    Ct0DμtV2(t)(2n)δH1V1δ2(t)H2V1ε2(t). (3.33)

    According to Theorem 3.1, Systems (2.1) and (2.2) can achieve Fix-TS under controller (3.23), and the settling time is estimated as

    T=t0+[Γ(δ)Γ(1+μ)(2n)δH1Γ(μ+δ)]1μ+[Γ(ε)Γ(1+μ)H2Γ(μ+ε)]1μ. (3.34)

    Therefore, when tT, we have limtT||~p(t)||=0. Thus, Systems (2.1) and (2.2) can realize Fix-TS under controller (3.23).

    Remark 3.2. Different from other synchronization controller designs such as exponential synchronization [31,32,33,34,35], quasi-synchronization [40,41] and global synchronization [42], the Fin-TS and Fix-TS controllers (3.11) and (3.23) are designed in two steps including the synchronization control term and stability control term, which can greatly improve the performance of the controller, enhance the operability and system stability, and also allow the synchronization term gain and stability term gain to be adjusted.

    Remark 3.3. In contrast to the decomposition method [46], Laplace transform [47], comparison principle [48,49] and linear matrix inequality (LMI) [50], the algebraic condition (3.12) in Theorem 3.2 is proposed to realize Fin-TS based on the quaternion direct method, Lyapunov stability theory, extended Cauchy Schwartz inequality and Jensen inequality.

    In this section, two numerical examples are given to verify the correctness and validity of Theorems 3.1–3.3 under the different derivative orders.

    Consider the following Caputo QDNN model:

    Ct0Dμtkp(t)=apkp(t)+2w=1(bpw+Δbpw(t))gw(kw(t))+2w=1(cpw+Δcpw(t))gw(kw(tτ1(t)))+2w=1(dpw+Δdpw(t))ttτ2(t)gw(kw(s))ds+Ip(t), p=1,2, (4.1)

    where

    μ=0.73, τ1(t)=0.5+0.5|sin(t)|, τ2(t)=0.5+0.5|cos(t)|, I1(t)=I2(t)=0,
    gw(kw(t))=tanh(kRw(t))+itanh(kIw(t))+jtanh(kJw(t))+ktanh(kKw(t)),
    kp(t)=kRp(t)+ikIp(t)+jkJp(t)+kkKp(t)Q,
    A=(1001), B=(0.1+0.5i+0.8j+0.1k0.20.2i+0.2j0.2k0.1+0.1i0.1j+0.1k0.1+0.3i0.1j+0.2k)+(0.4(sint+isintjsintksint)0.4(cost+icost+jcost+kcost)0.4(cost+icost+jcost+ksint)0.4(sint+isint+jsint+ksint)),C=(0.3+0.3i+0.2j+0.2k0.10.2i+0.1j+0.2k0.1+0.1i+0.1k0.6+0.6j+0.2k)+(0.4(cost+icostjsintksint)0.4(sint+icost+jcostksint)0.4(cost+isint+jsint+ksint)0.4(costicostjcost+ksint)),D=(0.1+0.1i+0.1j+0.1k0.3+0.1i+0.2j+0.2k0.1+0.1i+0.1j+0.1k0.3+0.1i+0.3j0.2k)+(0.4(sint+isint+jsint+ksint)0.4(cost+icost+jcost+kcost)0.4(sint+icost+jsint+kcost)0.4(costisintjsint+kcost)).

    The response system is

    Ct0Dμtop(t)=apop(t)+2w=1(bpw+Δbpw(t))gw(ow(t))+2w=1(cpw+Δcpw(t))gw(ow(tτ1(t)))+2w=1(dpw+Δdpw(t))ttτ2(t)gw(ow(s))ds+Ip(t)+Up(t), p=1,2, (4.2)

    where op(t)=oRp(t)+IoIp(t)+JoJp(t)+KoKp(t)Q. The initial conditions of Systems (4.1) and (4.2) are chosen as

    k1(0)=0.1+0.4i+0.3j+0.6k, k2(0)=0.10.1i0.4j+0.2k,w1(0)=0.10.4i0.3j0.6k, w2(0)=0.1+0.1i+0.4j0.2k.

    Example 4.1. To realize Fin-TS of Systems (4.1) and (4.2), for the self feedback controller (3.11), the following control gains are taken as δ=0.9, σ=0.1, ε=2.1, h=r=1.5, lp=lp=lp=1. By calculation, we can get

    9.8=α12l21+0.5(|b11|2+|^b11|2+|b12|2+|^b12|2+|c11|2+|^c11|2+|c12|2+|^c12|2+|d11|2+|^d11|2+|d12|2+|^d12|2)a1+2l12h+2l12r=9.7450,
    9.6=α22l22+0.5(|b21|2+|^b21|2+|b22|2+|^b22|2+|c21|2+|^c21|2+|c22|2+|^c22|2+|d21|2+|^d21|2+|d22|2+|^d22|2)a2+2l22h+2l22r=9.5500.

    From Theorem 3.2, the settling time can be estimated as ¯T4.5123. Figure 1 shows the state trajectories of derive-response Systems (4.1) and (4.2) without controller. Figures 2 and 3 describe Fin-TS trajectories and error norm of Systems (4.1) and (4.2) under controller (3.11) when the order is 0.73. Figures 4 and 5 depict Fin-TS trajectories and error norm of Systems (4.1) and (4.2) under controller (3.11) when the derivative order is 0.53. Figures 25 reveal that the numerical simulations are consistent with Theorem 3.2.

    Figure 1.  (a) kR1,oR1,kI1,oI1,kJ1,oJ1,kK1,oK1 without controller; (b) kR2,oR2,kI2,oI2,kJ2,oJ2,kK2,oK2 without controller.
    Figure 2.  Fin-TS errors of systems (4.1) and (4.2) under controller (3.11) when μ=0.73.
    Figure 3.  Error norm ||~(t)|| of Systems (4.1) and (4.2) under controller (3.11) when μ=0.73.
    Figure 4.  Fin-TS errors of Systems (4.1) and (4.2) under controller (3.11) when μ=0.53.
    Figure 5.  Error norm ||~(t)|| of Systems (4.1) and (4.2) under controller (3.11) when μ=0.53.

    Example 4.2. To realize Fix-TS between Systems (4.1) and (4.2), an adaptive controller (3.20) is designed based on Theorem 3.1. Taking

    k11=k12=0.1, k21=k22=0.3, δ=0.31, r=h=1.5,ε=0.9, λp=Rp=Sp=1, σ1=σ2=10.0, H1=0.2,H2=0.6,

    the other model parameters are consistent with Example 4.1. By computation, the conditions of Theorem 3.3 are satisfied. The settling time can be estimated as T5.2198. Figures 6 and 7 show Fix-TS trajectories and error norm of Systems (4.1) and (4.2) under controller (3.23) when the order is 0.73. Figures 8 and 9 characterize Fix-TS trajectories and error norm of Systems (4.1) and (4.2) under controller (3.23) when the derivative order is 0.53. Figures 69 verify that the numerical simulations are coincident with Theorems 3.1 and 3.3.

    Figure 6.  Fix-TS errors of Systems (4.1) and (4.2) under controller (3.23) when μ=0.73.
    Figure 7.  Error norm ||~(t)|| of Systems (4.1) and (4.2) under controller (3.23) when μ=0.73.
    Figure 8.  Fix-TS errors of Systems (4.1) and (4.2) under controller (3.23) when μ=0.53.
    Figure 9.  Error norm ||~(t)|| of Systems (4.1) and (4.2) under controller (3.23) when μ=0.53.

    Remark 4.1. Figures 10 and 11 depict the relationship between the settling time ¯T of Fin-TS with the order μ and the parameters σ, δ and ε. Figures 12 and 13 illustrate the relationship between the settling time T of Fix-TS with the order μ and the parameters δ, ε. For Fin-TS, it can be observed from Figures 10 and 11 that the settling time is positively correlated with σ, ε and negatively correlated with δ, μ. For Fix-TS the settling time is positively correlated with δ and negatively correlated with ε, μ. Therefore, the settling time of synchronisation is closely related to the order of the equation, regardless of whether it is Fin-TS or Fix-TS.

    Figure 10.  Relationship between settling time ¯T and μ, σ.
    Figure 11.  Relationship between settling time ¯T and δ, ε.
    Figure 12.  Relationship between settling time T and μ, δ.
    Figure 13.  Relationship between settling time T and δ, ε.

    This paper has investigated Fin-TS and Fix-TS issues for derive-response Systems (2.1) and (2.2). Firstly, a new Caputo fractional differential inequality (3.1) is constructed, then Fix-TS settling time of the positive definite function V(t) is estimated, which is very convenient to derive Fix-TS condition to Systems (2.1) and (2.2). By designing the appropriate self feedback controller (3.11) and adaptive controller (3.23), the algebraic discriminant conditions (3.12) and (3.25) to achieve Fin-TS and Fix-TS on Systems (2.1) and (2.2) are established in terms of quaternion direct method, Lyapunov stability theory, extended Cauchy Schwartz inequality, Jensen inequality. Finally, the correctness and validity of Theorems 3.1–3.3 under the orders μ=0.53 and μ=0.73 are verified by two numerical examples. The dynamics of QDNNs models including impulsive effect and multiple time delays will be our next research issue.

    This work was supported by the Natural Science Foundation of Anhui Province of China (No. 1908085MA01) and Research on green prevention and control of tea diseases and insect pests and automatic processing technology based on 5G network (No. 200118).

    The authors declare that they have no conflict of interest.



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