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Research article Special Issues

Optimal treatment strategy of cancers with intratumor heterogeneity


  • Intratumor heterogeneity hinders the success of anti-cancer treatment due to the interaction between different types of cells. To recapitulate the communication of different types of cells, we developed a mathematical model to study the dynamic interaction between normal, drug-sensitive and drug-resistant cells in response to cancer treatment. Based on the proposed model, we first study the analytical conclusions, namely the nonnegativity and boundedness of solutions, and the existence and stability of steady states. Furthermore, to investigate the optimal treatment that minimizes both the cancer cells count and the total dose of drugs, we apply the Pontryagin's maximum(or minimum) principle (PMP) to explore the combination therapy strategy with either quadratic control or linear control functionals. We establish the existence and uniqueness of the quadratic control problem, and apply the forward-backward sweep method (FBSM) to solve the optimal control problems and obtain the optimal therapy scheme.

    Citation: Haifeng Zhang, Jinzhi Lei. Optimal treatment strategy of cancers with intratumor heterogeneity[J]. Mathematical Biosciences and Engineering, 2022, 19(12): 13337-13373. doi: 10.3934/mbe.2022625

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  • Intratumor heterogeneity hinders the success of anti-cancer treatment due to the interaction between different types of cells. To recapitulate the communication of different types of cells, we developed a mathematical model to study the dynamic interaction between normal, drug-sensitive and drug-resistant cells in response to cancer treatment. Based on the proposed model, we first study the analytical conclusions, namely the nonnegativity and boundedness of solutions, and the existence and stability of steady states. Furthermore, to investigate the optimal treatment that minimizes both the cancer cells count and the total dose of drugs, we apply the Pontryagin's maximum(or minimum) principle (PMP) to explore the combination therapy strategy with either quadratic control or linear control functionals. We establish the existence and uniqueness of the quadratic control problem, and apply the forward-backward sweep method (FBSM) to solve the optimal control problems and obtain the optimal therapy scheme.



    Intratumor heterogeneity contributes to the emergence of therapy resistance, which plays a vital role in cancer relapse. Biologically, heterogeneity may originate from cellular genetic and epigenetic modifications as well as the environmental changes [1,2]. Clinically, adaptive responses to targeted therapies can facilitate both the expansion of pre-existing drug-resistant subpopulations and the acquisition of new mutations, which yields heterogeneity [2,3,4]. However, the dynamics of how intratumor heterogeneity may affect tumor evolution is not well understood, and is important for us to understand the mechanisms of drug resistance in cancer therapy.

    There are mounting evidences that mutation can create favorable conditions for heterogeneity and result in cancer therapy resistance. A critical question arises that whether mutation is prior to or after the onset of therapy. Experiments have showed that mutations in KRAS, TP53, ABL or MET can pre-exist before the initiation of therapy, and contribute to the development of drug resistance [5,6,7,8,9,10]. In addition, it is shown that mutations can also emerge in response to treatment stress and promote drug resistance [11,12,13,14,15,16]. The two mechanisms may imply different dynamics of cancer relapse, and quantitative studies are necessary to uncover the process of how mutation may affect treatment resistance over time.

    Many mathematical models have been developed to study the complex dynamics of cancer resistance/recurrence [17,18,19,20,21,22,23,24]. For example, various ordinary differential equations models were developed to describe how the interaction between drug-sensitive and drug-resistant cancer cells may shape the progression of drug resistance [17,18,19,20]. Moreover, the interaction between cancer cells and stroma [21] or immune cells [22,23,24] are considered in different types of models. In addition to the tumor cells, the competition between normal cells and tumor cells can be important for tumor progression [25,26]. Most existing models consider the tumor progression dynamics with pre-existing resistant cells, which interact with sensitive tumor cells through the competition in resources. Nevertheless, resistance cells can also be induced by the treatment behavior, by which sensitive cells can transit to resistant cells due to treatment stress. The mechanism of cell plasticity induced drug resistance is important clinically, however, to our knowledge, is not well studied quantitatively.

    In recent years, the idea of adaptive therapy has attracted the attention of many researchers, and the mathematical tool of optimal control theory was applied to obtain the optimal therapy schemes in adaptive therapy. For example, from the standpoint of optimal control, minimization of the total drug count was analyzed in order to control IgG multiple myeloma [27]. The optimal control method was utilized in treatments of various types of cancers, including metastatic prostate cancer [17], immunotherapeutic treatment [28,29], chemotherapy [30], combination of chemotherapy and stem cell transplants for acute myeloid leukemia [31], combination therapy of chronic myeloid leukemia [32], combination chemotherapy of antiangiogenic treatment [33], and bone metastasis treatment [34]. In these studies, the effects of cell plasticity induced drug resistance and the competition between tumor cells and normal cells are not included. Here, we ask how optimal control theory can help us to determine the optimal therapy strategy when both effects of the cell plasticity and competitions are considered.

    In this study, to have a better understanding of tumor progression in the base of competitions between normal cells and various types of cancer cells, we develop a mathematical model that includes normal cells, drug-sensitive tumor cells and drug-resistant tumor cells, and apply the model to study the dynamics of tumor progression and treatment responses. First, mathematically, we consider the nonnegativity and boundedness of the model solutions, and the existence and stability of steady states. Next, applying the Pontryagin's maximum(or minimum) principle (PMP) [35], we derive the optimal treatment schedule that can minimize the tumor burden during the treatment and the total drug dose of combination therapy. Two types of optimal control problems are considered with different designations of cost functionals, including the quadratic and linear drug control, respectively.

    To model the interaction between normal and tumor cells, we consider a mathematical model of tumor progression dynamics that includes normal cells, drug-sensitive and drug-resistant tumor cells (Figure 1). In the model, each type of cells proliferate with different rates that are dependent on the cell numbers and the microenvironmental cytokines regulating the cell proliferation pathway, and are removed due to cell death. All cells can secrete cytokines to regulate the proliferation of all cells, which form the competition between different types of cells. To consider the occurrence of mutation induced by treatment stress, we assume a possible transition from drug-sensitive to drug-resistant cells.

    Figure 1.  Schematic of the proposed model. There are three types of cells, including normal cells (x1(t)), drug-sensitive (x2(t)) and drug-resistant (x3(t)) tumor cells, all cells undergo proliferation and cell death, and can secrete cytokines to regulate the proliferation of all cells. Drug-sensitive tumor cells can transit to drug-resistant tumor cells due to random gene mutations.

    To formulate the model, we consider the numbers of normal, drug-sensitive and drug-resistant cells, which are represented by x1(t), x2(t) and x3(t), respectively. Dynamically, these three types of cells different from each other in their associated proliferation rates and removal rates.

    Biologically, the self-renewal ability of a cell is determined by both microenvironmental conditions, e.g., growth factor receptors and cell cycle checkpoints, such as fibroblast growth factors (FGFs) and the transforming growth factor beta (TGF-β) family [36,37,38]. The exact activation pathways that regulate the self-renewal of cells are poorly understood. However, a Hill type proliferation function can be derived based on simple but general assumptions on either positive or negative regulation growth factors [39,40]. Let

    ci=3j=1aijxj,i=1,2,3, (2.1)

    represent the overall effects of how cytokines secreted from all types of cells may regulate the self-renewal of type i cells, the competitions from cell type j to cell type i are given by the coefficients aij (i,j=1,2,3). Thus, according to the Hill type function proposed in [39,40], the proliferation rate for normal cells can be formulated as

    β1θ1θ1+c1,

    where β1 represents the maximum proliferation rate of normal cells, and θ1 is the 50% effective coefficient (EC50) that is associated with the effective concentration of cytokines. Here, we take the Hill coefficient to be 1 for simplicity. The proliferation rates of tumor cells are given similarly. However, tumor cells can escape the antigrowth signals due to the capability of self-sufficiency to growth signals and insensitivity to anti-growth signals [41], we thus introduce an additional nonzero constant βi0 (i=2,3) for the effects of self-sustained growth signals of tumor cells. Hence, the proliferation rates of drug-sensitive and drug-resistance cells are formulated as

    β2θ2θ2+c2+β20,β3θ3θ3+c3+β30,

    respectively.

    The three types of cells undergo cell death with rates μi, respectively. Moreover, we assume that drug-sensitive cells can transit to drug-resistant cells with a rate η. These arguments give rise to the following model

    {dx1dt=β1θ1θ1+c1x1μ1x1,dx2dt=(β2θ2θ2+c2+β20)x2μ2x2ηx2,dx3dt=(β3θ3θ3+c3+β30)x3μ3x3+ηx2. (2.2)

    Biologically, all parameters are non-negative, i.e.

    βi, β20, β30, η, aij (ij)0, θi, μi, aii>0,i,j=1,2,3. (2.3)

    Without loss of generality, we let

    aii=1 (i=1,2,3).

    In the model (2.2), we apply Hill type functions to describe the proliferation rates of cells, which are derived based on the assumption of cell proliferation regulated by cytokines. Nevertheless, we note that in many studies, logistic growth or Gompertizian growth are often applied to model the dynamics of tumor growth [17,18,19,22,23,24,30]. These growth rate functions are consistent in describing the same property that cell growth rates decrease with the cell number, however are originated from difference biological assumptions. Biologically, Hill type growth rate is more proper to model tumor growth, by which the effects of cytokines are described explicitly.

    In the current study, we would be always interested at the situation with positive cell numbers prior treatment. Thus, we have the following assumptions:

    (H1) The maximal proliferation rate β1 is greater than the death rate μ1 of normal cells, i.e.,

    ξ1β1μ11>0. (2.4)

    (H2) The maximal proliferation rate of drug-sensitive cells (β2+β20) is larger than the total removal rate due to either cell death or transition (μ2+η), and the residual proliferation rate β20 should be smaller than the total removal rate to avoid infinity cell numbers (uncontrolled cell growth). These assumptions give

    ξ2β2μ2+ηβ201>0. (2.5)

    (H3) The maximal proliferation rate of drug-resistance cells (β3+β30) is larger than the cell death rate (μ3), and the residual proliferation rate β30 should be smaller than the death rate to avoid infinity cell numbers (uncontrolled cell growth). These assumptions give

    ξ3β3μ3β301>0. (2.6)

    The assumptions (H1)–(H3) give biologically natural restrictions to the proliferation and death rates for the three types of cells.

    In this section, we first study the mathematical properties of the model (2.2), next consider the optimal strategy using PMP.

    Theorem 1. Assume the conditions (2.3)(2.6), let

    Ω={(x1,x2,x3)R30x1ξ1θ1,0x2ξ2θ2,0x3β3θ3+ηξ2θ2μ3β30}, (3.1)

    then Ω is an invariant set of the model (2.2), i.e., any solution of (2.2) with initial condition (x10,x20,x30)Ω satisfies

    (x1(t),x2(t),x3(t))Ω,t0.

    Proof. Let (x1(t),x2(t),x3(t)) be the solution of the model (2.2) with initial condition (x10,x20,x30)Ω.

    Firstly, it is easy to have

    and

    From the third equation of (2.2), we have

    dx3dt(β3θ3θ3+a31x1(t)+a32x2(t)+x3(t)+β30)x3μ3x3. (3.2)

    Multiplying both sides of (3.2) by , we have

    which gives

    (3.3)

    Integrating (3.3) over (0,t) with x3(0)=x30, we have

    x3(t)et0(β3θ3θ3+a31x1(s)+a32x2(s)+x3(s)+β30μ3)dsx300,

    which gives

    x3(t)x30et0(β3θ3θ3+a31x1(τ)+a32x2(τ)+x3(τ)+β30μ3)dτ0.

    Thus, any solution of (2.2) with nonnegative initial condition remains nonnegative over t>0.

    Next, we show that any nonnegative solution of (2.2) has finite upper bound. From the initial condition x1(0)=x10ξ1θ1 and

    dx1(t)dt|{x1=ξ1θ1,x2,x30}=β1θ1θ1+ξ1θ1+a12x2+a13x3ξ1θ1μ1ξ1θ1β1θ1θ1+ξ1θ1ξ1θ1μ1ξ1θ1=β1μ1β1ξ1θ1μ1ξ1θ1=0,

    we have x1(t)ξ1θ1,t0.

    Similar calculations yield x2(t)ξ2θ2 and x3(t)β3θ3+ηξ2θ2μ3β30,t0. This completes the proof.

    Now, we consider the steady state solutions of the model (2.2). Let (x1,x2,x3) be the nonnegative steady state, we have

    {β1θ1θ1+c1x1μ1x1=0,(β2θ2θ2+c2+β20)x2μ2x2ηx2=0,(β3θ3θ3+c3+β30)x3μ3x3+ηx2=0, (3.4)

    where

    c1=x1+a12x2+a13x3,c2=a21x1+x2+a23x3,c3=a31x1+a32x2+x3.

    We are only interested at the steady states that the cell numbers are nonnegative, which can be divided into one of the 8 possible types (+/0,+/0,+/0), here '+' means a positive number, and '0' means zero. It is easy to see that, there always exists a zero steady sate E0=(0,0,0), however this state represents the state of death and is biologically not interested. Since η>0, x3=0 always implies x2=0, there is no steady state of form (0,+,0) or (+,+,0). Thus, there are 6 possible steady states (here xi>0)

    E0=(0,0,0), E1=(x1,0,0), E3=(0,0,x3),E13=(x1,0,x3), E23=(0,x2,x3), E123=(x1,x2,x3). (3.5)

    The theorem below gives the existence of nonnegative steady states.

    Theorem 2. Consider the model (2.2), and assume that all parameters satisfy (2.3).

    (1) There always exists the zero steady state E0=(0,0,0).

    (2) If (2.4) holds, (2.2) has tumor-free equilibrium E1=(ξ1θ1,0,0).

    (3) If (2.6) holds, (2.2) has normal-free equilibrium E3=(0,0,ξ3θ3).

    (4) If both (2.4) and (2.6) hold, let

    s2=1a13a31, ξ4=ξ1θ1a13ξ3θ3, ξ5=ξ3θ3a31ξ1θ1, (3.6)

    (2.2) has one steady state of form E13=(ξ4s2,0,ξ5s2) only when s2, ξ4 and ξ5 are non-zero and have the same sign.

    (5) If both (2.5) and (2.6) hold, then

    (i) if a23>ξ2θ2ξ3θ3, let

    p1=a32+θ3ξ2θ2,q1=1+a32β30μ3η+θ3ξ2θ2(a23+β3+β30μ3η),r1=a23θ3ξ2θ2β3+β30μ3ημ3β30η, (3.7)

    if

    0<q12p1<μ3β30η,q214p1r1>0 (or =0), (3.8)

    (2.2) has two (or one) steady state of E23-type; otherwise, (2.2) has no steady state of E23-type.

    (ii) if a23<ξ2θ2ξ3θ3, (2.2) has one and only one steady state of E23-type.

    (6) If (2.4)(2.6) hold, (2.2) has at most two steady states of form E123=(x1,x2,x3). Moreover, let

    p2=(s3+a31(a12a23a13)+a32(a13a21a23))(s3(μ3β30)η(a13a21a23)),q2=s23θ3(β3+β30μ3)+s3(ηθ3(a13a21a23)+ξ1θ1((a21a32a31)(μ3β30)ηa21)+ξ2θ2((a12a31a32)(μ3β30)+η))ηξ1θ1((a21a32a31)(2a13a21a23)+a23a21(a12a31a32))ηξ2θ2((a12a31a32)(a13a212a23)a13(a21a32a31)),r2=η(ξ1θ1a21ξ2θ2)(s3θ3ξ1θ1(a21a32a31)ξ2θ2(a12a31a32)), (3.9)

    where s3=1a21a120, the E123-type steady states are determined by the solutions x3=x3 of the equation

    p2x32+q2x3+r2=0, (3.10)

    and the solution x3 satisfy: if s3>0,

    1a21(ξ2θ2a23x3)>(ξ1θ1a13x3)>a12(ξ2θ2a23x3), (3.11)

    and if s3<0,

    a12(ξ2θ2a23x3)>(ξ1θ1a13x3)>1a21(ξ2θ2a23x3)>0. (3.12)

    In this case, x1 and x2 are given by

    x1=1s3((ξ1θ1a13x3)a12(ξ2θ2a23x3)), (3.13)
    x2=1s3((ξ2θ2a23x3)a21(ξ1θ1a13x3)). (3.14)

    Proof. (1). It is trivial to see that model (2.2) always has the zero steady state E0.

    (2). Let x2=x3=0 and x10, from the first equation of (2.2), x1 satisfies

    β1θ1θ1+x1x1μ1x1=0, (3.15)

    which gives

    β1θ1θ1+x1μ1=0. (3.16)

    Hence, condition (2.4) implies

    x1=(β1μ11)θ1=ξ1θ1>0.

    (3). Let x1=x2=0 and x30. From the third equation of (3.4), we have

    (β3θ3θ3+x3+β30)x3μ3x3=0, (3.17)

    which gives

    β3θ3θ3+x3+β30μ3=0. (3.18)

    Thus, condition (2.6) implies

    x3=(β3μ3β301)θ3=ξ3θ3>0.

    (4) Let x2=0, the first and the third equation of (3.4) become

    {β1θ1θ1+x1+a13x3x1μ1x1=0,(β3θ3θ3+a31x1+x3+β30)x3μ3x3=0. (3.19)

    Given x1,x30, (3.19) can be rewritten as

    {β1θ1θ1+x1+a13x3μ1=0,β3θ3θ3+a31x1+x3+β30μ3=0, (3.20)

    which yields

    {x1+a13x3=ξ1θ1,a31x1+x3=ξ3θ3. (3.21)

    From (3.21), we obtain

    x1=ξ4s2,x3=ξ5s2

    when s2,ξ4 and ξ5 are given by (3.6). Thus, (2.2) has a steady state of form E13 only when s2,ξ4 and ξ5 are non-zero and have the same sign.

    (5). To consider the steady state of form E23, let x1=0 in (3.4), we obtain

    {(β2θ2θ2+x2+a23x3+β20)x2μ2x2ηx2=0,(β3θ3θ3+a32x2+x3+β30)x3μ3x3+ηx2=0. (3.22)

    When x2,x30, (3.22) can be rewritten as

    {β2θ2θ2+x2+a23x3=μ2+ηβ20,β3θ3θ3+a32x2+x3=μ3ηx2x3β30. (3.23)

    Thus, we have

    {x2+a23x3=ξ2θ2,a32x2+x3=(β3μ3ηx2/x3β301)θ3. (3.24)

    Dividing both sides of (3.24) by x3, we have

    {x2/x3+a23=ξ2θ2/x3,a32x2/x3+1=(β3μ3ηx2/x3β301)θ3/x3. (3.25)

    Denote y=x2x3 and z=1x3, then

    0<y<μ3β30η,z>0,

    and (3.25) becomes

    {y+a23=ξ2θ2z,a32y+1=(β3μ3ηyβ301)θ3z. (3.26)

    The first equation of (3.26) implies

    z=y+a23ξ2θ2. (3.27)

    The second equation of (3.26) implies

    z=(a32y+1)(μ3ηyβ30)θ3(β3μ3+ηy+β30). (3.28)

    Hence, (3.27) and (3.28) together give the equation for y=y,

    y+a23ξ2θ2=(a32y+1)(μ3ηyβ30)θ3(β3μ3+ηy+β30),

    which implies

    f(y)p1y2+q1y+r1=0, (3.29)

    where p1,q1,r1 are given by (3.7). Thus, to get the positive solution of (3.26), we only need to solve the equation (3.29) for the solution 0<y<μ3β30η.

    When (3.29) has a solution y(0,μ3β30η), we have z>0 from (3.27), and the nonnegative steady state E23=(0,x2,x3) is given by x2=yz and x3=1z. Now, we identify the conditions to have such a solution based on the competition coefficient a23.

    (i) If a23>ξ2θ2ξ3θ3, we have p1>0, and

    f(0)=a23θ3ξ2θ2β3+β30μ3ημ3β30η>1ξ3β3+β30μ3ημ3β30η=1ξ3β3η(1ξ3+1)μ3β30η=1ξ3β3η1ξ3β3μ3β30μ3β30η=0. (3.30)

    Moreover,

    f(μ3β30η)=β3θ3ηξ2θ2(a23+μ3β30η)>0.

    Hence, if

    0<q12p1<μ3β30η,q214p1r1>0 (or=0),

    (3.29) has two (or one) positive solutions in the interval (0,μ3β30η), i.e., (2.2) has two (or one) steady states of E23-type; otherwise, (2.2) has no steady state of E23-type.

    (ii) If a23<ξ2θ2ξ3θ3, similar to the above argument of (3.30), we have

    f(0)<1ξ3β3+β30μ3ημ3β30η=0.

    Thus, since,

    f(μ3β30η)>0,

    the quadratic function f(y) has one and only one root in (0,μ3β30η), i.e., (2.2) has one and only one steady state of E23-type.

    (6). To consider the positive steady sate of form E123=(x1,x2,x3), we need to find the positive solution of

    {β1θ1θ1+x1+a12x2+a13x3μ1=0,β2θ2θ2+a21x1+x2+a23x3+β20μ2η=0,(β3θ3θ3+a31x1+a32x2+x3+β30)x3μ3x3+ηx2=0. (3.31)

    From the first and the second equations of (3.31), we have

    {x1+a12x2=ξ1θ1a13x3,a21x1+x2=ξ2θ2a23x3, (3.32)

    which gives

    {x1=1s3((ξ1θ1a13x3)a12(ξ2θ2a23x3)),x2=1s3((ξ2θ2a23x3)a21(ξ1θ1a13x3)), (3.33)

    where s3=1a21a120.

    Substituting (3.33) into the third equation of (3.31), x3 satisfies the quadratic equation

    p2x32+q2x3+r2=0, (3.34)

    where p2, q2 and r2 are given by (3.9). Moreover, from (3.32) and (3.33), if s3>0, x3 should satisfy

    1a21(ξ2θ2a23x3)>(ξ1θ1a13x3)>a12(ξ2θ2a23x3)>0; (3.35)

    and if s3<0, x3 satisfies

    a12(ξ2θ2a23x3)>(ξ1θ1a13x3)>1a21(ξ2θ2a23x3)>0. (3.36)

    Thus, (2.2) has at most two steady states of form E123, which are determined by the solutions of (3.34) and (3.33) with x3 satisfies (3.35) when s3>0, or (3.36) when s3<0.

    Theorem 2 establishes the conditions for the existence of nonnegative steady states of different types. Biologically, the conditions (2.4)–(2.6) are satisfied by most tissue cells, and hence the steady states of types E0,E1 and E3 always exist. Moreover, under the extreme condition when the competition coefficients aij=0 for any ij, it is easy to have the existence of the steady states of types E13 and E23 from (4) and (5), and from (6),

    p2=(μ3β30)<0, r2=ηθ2θ3ξ2>0,s3=1>0,

    which yield the existence of a steady state of type E123. Thus, from the continuous dependence, the proposed model (2.2) have steady states of all types in (3.5) when the competition coefficients aij>0 (ij) are small enough.

    Now, we study the stability of the steady state E=(x1,x2,x3). Let x=x1x1, y=x2x2 and z=x3x3, and linearize the model (2.2) at E, we have the linearization equation

    {dxdt=A1x+A2y+A3z,dydt=B1x+B2y+B3z,dzdt=C1x+C2y+C3z, (3.37)

    where

    A1=θ1β1θ1+c1μ1α1, A2=a12α1, A3=a13α1,
    B1=a21α2, B2=θ2β2θ2+c2+β20μ2ηα2, B3=a23α2,
    C1=a31α3, C2=a32α3+η, C3=θ3β3θ3+c3α3μ3+β30,
    α1=β1θ1x1(θ1+c1)2, α2=β2θ2x2(θ2+c2)2, α3=β3θ3x3(θ3+c3)2.

    The characteristic equation of (3.37) is written as

    λ3+aλ2+bλ+c=0. (3.38)

    where

    a=(A1+B2+C3), b=B2C3+A1B2+A1C3B3C2A2B1A3C1,c=A1B2C3+A1B3C2+A2B1C3A3B1C2A2B3C1+A3B2C1. (3.39)

    Based on the characteristic Eq (3.39), the condition for asymptotical stability of steady states are given by the Theorem below.

    Theorem 3. Consider the model(2.2), and assume that all parameters satisfy (2.3) and the conditions for the existence of steady states listed in Theorem 2, we have the following results.

    (1) The zero steady state E0=(0,0,0) is asymptotically stable if and only if none of the conditions (2.4)(2.6) holds, i.e.,

    β1μ1<0,β2+β20μ2<η,β3+β30μ3<0. (3.40)

    Furthermore, if

    β1μ1<0,β2+β20μ2<0,β3+β30μ3<0, (3.41)

    E0 is globally stable for any solutions in Ω.

    (2) If (2.4) holds, the steady state E1=(x1,0,0) is asymptotically stable if and only if

    ξ2θ2ξ1θ1<a21,ξ3θ3ξ1θ1<a31. (3.42)

    (3) If (2.6) holds, the steady state E3=(0,0,x3) is asymptotically stable if and only if

    ξ1θ1ξ3θ3<a13,ξ2θ2ξ3θ3<a23. (3.43)

    (4) If (2.4) and (2.6) hold, the steady state E13=(x1,0,x3) is asymptotically stable if and only if

    1a13a31>0,andξ2θ2<a21x1+a23x3. (3.44)

    (5) If (2.5) and (2.6) hold, the steady state E23=(0,x2,x3) is asymptotically stable if and only if

    ξ1θ1<a12x2+a13x3,(1a23a32)+ηβ3θ3x3(x2x3+a23)(θ3+a32x2+x3)2>0. (3.45)

    (6) If (2.4)(2.6) hold, the steady state E123=(x1,x2,x3) is asymptotically stable if and only if

    a>0,abc>0,c>0, (3.46)

    where a,b,c are defined by (3.39). Particularly, if the following conditions are satisfied

    ξ1,ξ2,ξ3>0,1a23a32a12a21a13a31+a13a21a32+a12a23a31>0,2a13a21a32a12a23a310,1a23a320, 1a12a21>0, 1a13a310, a23a13a210, (3.47)

    E123 is asymptotically stable.

    Proof. (1) For the steady state E0, the coefficient matrix of the linearized Eq (3.37) is

    JE0=(β1μ1000β2+β20μ2η00ηβ3+β30μ3). (3.48)

    It is straight forward to obtain the corresponding eigenvalues

    λ1=β1μ1, λ2=β2+β20μ2η, λ3=β3+β30μ3.

    Thus, E0 is asymptotically stable if and only if λ1,λ2,λ3<0, i.e., none of the conditions (2.4)–(2.6) holds.

    Next, to show the global stability of E0, we construct a Lyapunov function V(x1,x2,x3) as

    V(x1,x2,x3)=12(x21+(x2+x3)2). (3.49)

    It is easy to see that V(x1,x2,x3) is positive definite, and the derivative of V(x1(t),x2(t),x3(t)) along any solution of (2.2) is given by

    dV(x1(t),x2(t),x3(t))dt|(2.2)=(x1˙x1+(x2+x3)(˙x2+˙x3))|(2.2)=(β1θ1θ1+c1μ1)x21+(x2+x3)((β2θ2θ2+c2+β20μ2)x2+(β3θ3θ3+c3+β30μ3)x3). (3.50)

    From Theorem 1 and the proof therein, any solution of (2.2) with initial condition (x10,x20,x30)Ω remains in Ω for all t>0, i.e., x1(t),x2(t),x3(t)0. Hence, when (3.41) is satisfied, the derivative (3.50) along any solution in Ω is negative definite. According to Theorem 1.1 in chapter X.1 of [36], E0 is globally stable for any solutions in Ω.

    (2) For the steady state E1=(x1,0,0), the coefficient matrix of Eq (3.37) is

    JE1=(μ1(β1μ1)β1a12β1θ1x1(θ1+x1)2a13β1θ1x1(θ1+x1)20β2θ2θ2+a21ξ1θ1+β20μ2η00ηβ3θ3θ3+a31ξ1θ1+β30μ3). (3.51)

    It is easy to have the eigenvalues

    λ1=μ1(β1μ1)β1λ2=β2θ2θ2+a21ξ1θ1+β20μ2η,λ3=β3θ3θ3+a31ξ1θ1+β30μ3.

    When (2.4) holds, we have ξ1>0, and λ1<0. Moreover, we have

    λ2<0β2θ2θ2+a21ξ1θ1+β20μ2η<0β2θ2<(μ2+ηβ20)(θ2+a21ξ1θ1) and (μ2+ηβ20)>0β2θ2μ2+ηβ20<θ2+a21ξ1θ1ξ2θ2ξ1θ1<a21.

    and

    λ3<0β3θ3θ3+a31ξ1θ1+β30μ3<0β3θ3<(μ3β30)(θ3+a31ξ1θ1) and (μ3β30)>0β3θ3μ3β30<θ3+a31ξ1θ1ξ3θ3ξ1θ1<a31.

    Thus, E1 is asymptotically stable if and only if λ2<0 and λ3<0, i.e., ξ2θ2ξ1θ1<a21 and ξ3θ3ξ1θ1<a31.

    (3) For the steady state E3=(0,0,x3), the coefficient matrix of (3.37) is given by

    JE1=(β1θ1θ1+a13x3μ1000β2θ2θ2+a23x3+β20μ2η0a31β3θ3x3(θ3+x3)2a32β3θ3x3(θ3+x3)2+η(μ3β30)(β3+β30μ3)β3). (3.52)

    This, it is straight forward to have the eigenvalues λ1, λ2, and λ3 as:

    λ1=β1θ1θ1+a13x3μ1,λ2=β2θ2θ2+a23x3+β20μ2η,λ3=(μ3β30)(β3+β30μ3)β3.

    From the condition (2.6), we have ξ3>0, and hence λ3<0. Moreover, note x3=ξ3θ3, similar to the argument in (2), we have

    λ1=β1θ1θ1+a13ξ3θ3μ1<0β1θ1μ1<θ1+a13ξ3θ3ξ1θ1ξ3θ3<a13,

    and

    λ2=β2θ2θ2+a23ξ3θ3+β20μ2η<0β2θ2μ2+ηβ20<θ2+a23ξ3θ3ξ2θ2ξ3θ3<a23.

    Hence, E3 is asymptotically stable if and only if λ1<0 and λ2<0, i.e., ξ1θ1ξ3θ3<a13 and ξ2θ2ξ3θ3<a23.

    (4) For the steady state E13=(x1,0,x3), the coefficient matrix of (3.37) is given by

    JE13=(α4a12α4a13α40β2θ2θ2+a21x1+a23x3+β20μ2η0a31α5ηa32α5α5), (3.53)

    where

    α4=β1θ1x1(θ1+x1+a13x3)2, α5=β3θ3x3(θ1+a31x1+x3)2.

    The eigenvalues λ1, λ2 and λ3 of JE13 satisfy

    λ1+λ3=(α4+α5), λ1λ3=(1a13a31)α4α5

    and

    λ2=β2θ2θ2+a21x1+a23x3+β20μ2η.

    Since α4>0,α5>0, we have λ1<0,λ3<0 if and only if 1a13a31>0. Moreover, similar to the previous argument,

    λ2<0β2θ2<(μ2+ηβ30)(θ2+a21x1+a23x3)ξ2θ2<a21x1+a23x3.

    Thus, E13 is asymptotically stable if and only if (3.44) is satisfied.

    (5) For the steady state E23=(0,x2,x3), the coefficient matrix of (3.37) is given by

    JE23=(β1θ1θ1+a12x2+a13x3μ100a21α6α6a23α6a31α7ηa32α7ηx2x3α7), (3.54)

    where

    α6=β2θ2x2(θ2+x2+a23x3)2, α7=β3θ3x3(θ3+a32x2+x3)2.

    The eigenvalues λ1, λ2 and λ3 of JE23 satisfy

    λ1=β1θ1θ1+a12x2+a13x3μ1,

    and

    λ2+λ3=(α6+ηx2x3+α7),andλ2λ3=α6((1a23a32)α7+η(x2x3+a23)).

    Similar to the previous argument,

    λ1<0β1θ1θ1+a12x2+a13x3<μ1ξ1θ1<a12x2+a13x3.

    Moreover, since α6>0 and α7>0, we have

    λ2<0, λ3<0(1a23a32)α7+η(x2x3+a23)>0(1a23a32)+ηβ3θ3x3(x2x3+a23)(θ3+a32x2+x3)2>0.

    Thus, E23 is asymptotically stable if and only if (3.45) is satisfied.

    (6) For the steady state E123=(x1,x2,x3), the characteristic equation for (3.37) is given by (3.38).

    From the Routh-Hurwitz stability criterion, all eigenvalues have negative real parts if and only if a>0, abc>0 and c>0. Hence, E123 is asymptotically stable if and only if (3.46) is satisfied.

    Let

    α1=β1θ1x1(θ1+c1)2, α2=β2θ2x2(θ2+c2)2, α3=β3θ3x3(θ3+c3)2,

    and applying (3.31), the coefficient matrix of (3.37) at E123 is given by

    JE13=(α1a12α1a13α1a21α2α2a23α2a31α3a32α3+ηα3ηx2x3). (3.55)

    Since α1,α2,α3,x2,x3>0, we have

    a=α1+α2+α3+ηx2x3>0.

    When the conditions in (3.47) are satisfied, we have

    1a23a32a12a21a13a31+a13a21a32+a12a23a31>0, 1a12a21>0, a23a13a210,

    and hence

    c=α1(a23α2(ηa32α3)α2(α3+ηx2x3))a12α1(a21α2(α3+ηx2x3)a23α2a31α3)a13α1[a31α2α3+a21α2(ηa32α3)]=α1(a23α2(ηa32α3)α2(α3+ηx2x3)+a12(a21α2(α3+ηx2x3)a23α2a31α3)+a13(a31α2α3+a21α2(ηa32α3)))=α1((1a23a32a12a21a13a31+a13a21a32+a12a23a31)α2α3+(a23a21a13)ηα2+(1a21a12)ηα2x2x3)>0.

    Furthermore, since

    2a13a21a32a12a23a310, 1a23a320, 1a12a21>0, 1a13a310,

    we have

    abc=α21α2+α21(α3+ηx2x3)a12a21α21α2a13a31α21α3+α22(α3+ηx2x3)+α1α22+α1α2(α3+ηx2x3)+a23α22(ηa32α3)a12a21α1α22+α2(α3+ηx2x3)2+α1α2(α3+ηx2x3)+α1(α3+ηx2x3)2+a23α2(ηa32α3)(α3+ηx2x3)a13a31α1α3(α3+ηx2x3)+a13a21α1α2(ηa32α3)a12a31a23α1α2α3=α21α2a12a21α21α2+α21(α3+ηx2x3)a13a31α21α3+α1α22a12a21α1α22+α22(α3+ηx2x3)+a23α22(ηa32α3)+α1(α3+ηx2x3)2a13a31α1α3(α3+ηx2x3)+2α1α2(α3+ηx2x3)+a13a21α1α2(ηa32α3)a12a31a23α1α2α3+α2(α3+ηx2x3)2+a23α2(ηa32α3)(α3+ηx2x3)=(1a12a21)α21α2+(1a13a31)α21α3+α21ηx2x3+(1a12a21)α1α22+(1a23a32)α22α3+ηα22x2x3+a23ηα22+(1a13a31)α1α3(α3+ηx2x3)+α1η(α3+ηx2x3)x2x3+(2a13a21a32a12a31a23)α1α2α3+(2x2x3+a13a21)ηα1α2+(1a23a32)α2α3(α3+ηx2x3)+(ηα2x2x3+a23ηα2)(α3+ηx2x3)>0.

    Hence, from the Routh-Hurwitz stability criterion, E123 is asymptotically stable.

    Theorem 3 gives the conditions for the asymptotical stability of steady states of different types. Specifically, the zero steady state E0 is asymptotically stable if none of the biological restrictions (2.4)–(2.6) holds, i.e., there is no steady state with non-zero cell numbers. When (2.4)–(2.6) are satisfied, and the competition coefficients aij=0 (ij), the steady state E123=(x1,x2,x3) exists, and is asymptotically stable, however other nonnegative steady states (E1, E3, E13 and E23) are unstable. The steady state E123 becomes unstable when the competition coefficients increase, and other corresponding nonnegative steady states become stable.

    Now, we consider the problem of optimal therapy strategy when both drug-sensitive and drug-resistant tumor cells are co-existence. To this end, we extend the model to include the effect of drug-induced tumor cell death and transition. Here, we consider the possible combination therapy with two drugs, targeted to sensitive cells and resistant cells, respectively. Thus, we introduce the parameters u and v to represent the extra removal rates of drug-sensitive and drug-resistant cells due to treatment stress, respectively. In addition, we assume that the drug targeted to sensitive cells can induce transitions from sensitive cells to resistant cells, the transition rate is represented as su. Thus, the model (2.2) is modified as

    {dx1dt=β1θ1θ1+c1x1μ1x1,dx2dt=(β2θ2θ2+c2+β20)x2μ2x2ηx2ux2,dx3dt=(β3θ3θ3+c3+β30)x3μ3x3+ηx2+sux2vx3. (3.56)

    Next we discuss the optimal therapy strategies based on (3.56) by designing the objective functionals with quadratic and linear controls, respectively.

    Firstly, we analyze the quadratic control problem, and study the existence and uniqueness of optimal solutions. In cancer therapy, we try to minimize the total quantity of drugs and the tumor burden during treatment, and hence the associated objective functional can be defined as

    J(u,v)=tf0(b(x2(t)+x3(t))+cu(t)2+dv(t)2)dt, (3.57)

    where tf denotes the duration of treatment, and b>0,c,d are constants, which represent non-negative weights of the three parts. Thus, the optimization problem is formulated as

    min(u,v)AJ(u,v)s.t.  {dx1dt=β1θ1θ1+c1x1μ1x1,dx2dt=(β2θ2θ2+c2+β20)x2μ2x2ηx2ux2,dx3dt=(β3θ3θ3+c3+β30)x3μ3x3+ηx2+sux2vx3.t0;(x1(0),x2(0),x3(0))=(x10,x20,x30)Ω,A={(u,v)L1[0,tf]|0u(t)umax,0v(t)vmax,t[0,tf]}. (3.58)

    Now, we prove the existence of the solution for the optimal control of (3.58).

    Theorem 4. There exists at least one pair of optimal control (u,v) such that

    J(u,v)=min(u,v)AJ(u,v).

    Proof. First, we show properties below for the control problem (3.57).

    (1). First, similar to the argument in Theorem 1, any solutions of (2.2) with initial condition in Ω1 is bounded with (x1(t),x2(t),x3(t))Ω1 for any t>0. From the Carathéodory Theorem (Theorem 5.1 in chapter I.5 of [42]), there exist (x10,x20,x30)Ω1 and (u,v)A so that the solution of Eq (3.56) with initial condition (x1(0),x2(0),x3(0))=(x10,x20,x30) is well defined in the interval t(0,tf).

    (2). Since the intervals [0,umax] and [0,vmax] are closed and convex, the admissible control set A is also closed and convex.

    (3). The the right hand side of (3.56) is continuous. Moreover, we can write the right hand side as

    ζ1(x1,x2,x3)+ζ2(x1,x2,x3)(uv),

    where

    ζ1(x1,x2,x3)=(β1θ1θ1+c1x1μ1x1(β2θ2θ2+c2+β20)x2μ2x2ηx2(β3θ3θ3+c3+β30)x3μ3x3+ηx2),andζ2(x1,x2,x3)=(00x20sx2x3).

    Since (x1,x2,x3)Ω1 is bounded, there exists K>0 so that

    Thus,

    \left\| \zeta_1(x_1, x_2, x_3)+ \zeta_2 (x_1, x_2, x_3) \cdot \left( \begin{array}{c} u\\ v\\ \end{array}\right)\right\| \leq K (\|x\| + \|(u, v)\|).

    (4). It is easy to verify that L = b (x_2(t) + x_3(t)) + c u(t)^2 + d v(t)^2 is convex with respect to u and v . Moreover, let c_1 = \min \{c, d \} , \beta = 2 , we have

    L \geqslant c_1 \|(u, v)\|_2^\beta.

    Finally, the existence of the optimal control (u^*, v^*) is followed from the above properties and Corollary 4.1 in [43].

    Now, we try to solve the optimal control solution (u^*, v^*) . To this end, applying the Pontryagin's maximum(or minimum) principle (PMP), the associated Hamiltonian H is defined as

    \begin{eqnarray} H(x_1, x_2, x_3, u, v, \lambda_1, \lambda_2, \lambda_3 ) & = & b (x_2 + x_3) + c u^2 + d v^2 \\ &&{} + \lambda_1 ( \beta_1 \dfrac{ \theta_1 }{ \theta_1 + c_1 } - \mu_1 ) x_1 + \lambda_2 ( \beta_2 \dfrac{ \theta_2 }{ \theta_2 + c_2 } + \beta_{20} - \mu_2 - \eta - u) x_2 \\ &&{} + \lambda_3 (\beta_3 \dfrac{ \theta_3 }{ \theta_3 + c_3 } + \beta_{30} )x_3 - \mu_3 x_3 + \eta x_2 + s u x_2 - v x_3). \end{eqnarray} (3.59)

    Therewith, the associated co-state equations are

    (3.60)

    here,

    \gamma_1 = \dfrac{ \beta_1 \theta_1 x_1}{( \theta_1 + c_1)^2},\ \gamma_2 = \dfrac{ \beta_2 \theta_2 x_2}{( \theta_2 + c_2)^2},\ \gamma_3 = \dfrac{ \beta_3 \theta_3 x_3}{( \theta_3 + c_3)^2},

    and the associated transversality conditions are

    \lambda_1(t_f) = 0, \quad \lambda_2(t_f) = 0, \quad \lambda_1(t_f) = 0.

    On the interior of the control set \mathscr{A}, the optimal controls satisfy the condition

    \dfrac{\partial H}{\partial u} = \dfrac{\partial H}{\partial v} = 0.

    Furthermore, a standard optimality technique implies the optimal controls are given by

    \begin{equation} u^*(t) = \max \Big\{0, \min\big \{ u_{\max}, \dfrac{( \lambda_2(t) - s \lambda_3(t)) x_2(t)}{2 c} \big\} \Big\} \end{equation} (3.61)

    and

    \begin{equation} v^*(t) = \max \Big\{0, \min\big \{ v_{\max}, \dfrac{ \lambda_3(t) x_3(t)}{2 d} \big\} \Big\}. \end{equation} (3.62)

    Now, analogous to the discussions in previous studies [29,30,34], we consider the uniqueness of the optimal control problem. Similar to the argument in Theorem 1, the state variables (x_1, x_2, x_3) of (3.56) are bounded, and there exists an invariant set \Omega_1 for the Eq (3.56) with

    \begin{equation} \Omega_1 = \{ (x_1, x_2, x_3) \in \mathbb{R} ^3 \mid 0 \leqslant x_1 \leqslant b_1, 0 \leqslant x_2 \leqslant b_2, 0 \leqslant x_3 \leqslant b_3 \}, \end{equation} (3.63)

    where b_1, b_2, b_3 > 0 . Moreover, the solutions of the co-state system (3.60) are bounded with t\in (0, t_f) .

    Theorem 5. There exists a sufficiently small final time t_f such that the optimal control solution is unique.

    Proof. We assume that there are two different solutions (x_1, x_2, x_3, \lambda_1, \lambda_2, \lambda_3) and (\bar{x}_1, \bar{x}_2, \bar{x}_3, \bar{\lambda}_1, \bar{\lambda}_2, \bar{\lambda}_3) that solve (3.56) and (3.60), and will come out with a contradiction.

    For a given positive parameter m > 0 (to be determined latter), set

    \begin{equation*} p_i(t) = x_i(t) e^{-mt}, \quad q_i(t) = \lambda_i(t) e^{mt}, \quad \bar{p}_i(t) = \bar{x}_i(t) e^{-mt}, \quad \bar{q}_i(t) = \bar{\lambda}_i(t) e^{mt}, \quad i = 1, 2, 3. \end{equation*}

    The optimal control solutions u(t), v(t), \bar{u}(t), \bar{v}(t) are given by p_i(t), q_i(t), \bar{p}_i(t), \bar{q}_i(t) as

    (3.64)

    Substituting x_i(t) = p_i(t) e^{mt}, \lambda_i(t) = q_i(t) e^{-mt} into Eqs (3.56) and (3.60), after a tedious calculation (see the Appendix), we obtain that there exist L_{1, i} > 0, L_{2, i} > 0 so that

    \begin{equation} m \int_{0}^{t_f} (p_i -\bar{p}_i)^2 dt \leqslant L_{1,i} (1 + e^{m t_f}) \int_{0}^{t_f} \left(\sum\limits_{j = 1}^3 (( \bar{p}_j - p_j)^2 + ( \bar{q}_j - q_j)^2)\right) dt, \end{equation} (3.65)

    and

    \begin{equation} m \int_{0}^{t_f} (q_i -\bar{q}_i)^2 dt \leqslant L_{2,i} (1 + e^{m t_f} + e^{2 m t_f} + e^{ 3 m t_f} ) \int_{0}^{t_f} \left(\sum\limits_{j = 1}^3 (( \bar{p}_j - p_j)^2 + ( \bar{q}_j - q_j)^2)\right) dt. \end{equation} (3.66)

    Thus, adding up (3.65) and (3.66) for i = 1, 2, 3 , there exists L_3 = \max_{i = 1, 2, 3}\{L_{1, i} + L_{2, i}\} so that

    \begin{equation} (m - L_3(1 + e^{ m t_f} + e^{ 2 m t_f} + e^{ 3 m t_f} ) ) \int_{0}^{t_f} \left(\sum\limits_{j = 1}^3 (( \bar{p}_j - p_j)^2 + ( \bar{q}_j - q_j)^2)\right) dt \leqslant 0, \end{equation} (3.67)

    and L_3 only depends on all equation coefficients.

    Now, while we choose m = L_3 (1 + 3 e) and t_f < \dfrac{1}{ 3 m} , then m - L(1 + e^{ m t_f} + e^{ 2 m t_f} + e^{ 3 m t_f}) > 0 , which come out with a contradiction with (3.67) if (p_j, q_j) \not = (\bar{p}_j, \bar{q}_j) . Thus, we conclude p_i = \bar{p}_i and q_i = \bar{q}_i , and hence u = \bar{u} and v = \bar{v} from (3.64).

    Now, we consider the situation of linear control problem, and seek to minimize the pay-off functional J_1 that is defined as

    \begin{equation} J_1(u,v) = \int_{0}^{t_f} [ b (x_2(t) + x_3(t) ) + c u(t) + d v(t) ]dt. \end{equation} (3.68)

    Similar to discussions in Theorem 4, we have the existence of optimal control strategy (u, v) that minimizes J_1(u, v) .

    Now, the necessary conditions of the above optimal problem can be given by the PMP [44]. According to PMP, the associated Hamiltonian H is written as

    H(x_1, x_2, x_3, u, v, \lambda_1, \lambda_2, \lambda_3 ) = b (x_2 + x_3) + c u + d v \\ {} + \lambda_1 ( \beta_1 \dfrac{ \theta_1 }{ \theta_1 + c_1 } - \mu_1 ) x_1 + \lambda_2 ( \beta_2 \dfrac{ \theta_2 }{ \theta_2 + c_2 } + \beta_{20} - \mu_2 - \eta - u) x_2 \\ {} + \lambda_3 [(\beta_3 \dfrac{ \theta_3 }{ \theta_3 + c_3 } + \beta_{30} )x_3 - \mu_3 x_3 + \eta x_2 + s u x_2 - v x_3] . (3.69)

    Thus, the associated co-state equations are

    (3.70)

    where

    \gamma_1 = \dfrac{ \beta_1 \theta_1 x_1}{( \theta_1 + c_1)^2}, \gamma_2 = \dfrac{ \beta_2 \theta_2 x_2}{( \theta_2 + c_2)^2}, \gamma_3 = \dfrac{ \beta_3 \theta_3 x_3}{( \theta_3 + c_3)^2},

    and the associated transversality conditions are

    \lambda_1(t_f) = 0, \quad \lambda_2(t_f) = 0, \quad \lambda_1(t_f) = 0.

    The optimal control solution (u, v) satisfies

    \begin{equation} \dfrac{\partial H}{\partial u} = c - \lambda_2 x_2 + s \lambda_3 x_2 ,\quad \dfrac{\partial H}{\partial v} = d - \lambda_3 x_3 . \end{equation} (3.71)

    Hence the optimal control solution is given by

    \begin{equation} u^*(t) = \left\{ \begin{array}{rcl} 0 , & c - \lambda_2 x_2 + s \lambda_3 x_2 > 0, \\ u_{\max} , & c - \lambda_2 x_2 + s \lambda_3 x_2 < 0. \\ \end{array} \right. \end{equation} (3.72)

    and

    \begin{equation} v^*(t) = \left\{ \begin{array}{rcl} 0 , & d - \lambda_3 x_3 > 0, \\ v_{\max} , & d - \lambda_3 x_3 < 0. \\ \end{array} \right. \end{equation} (3.73)

    From (3.72) and (3.73), the optimal controls for the linear problem is a bang-bang control with either zero or maximum dose drugs.

    Now, we perform numerical simulations to verify the above analytic discussions. To carry out the numerical simulation, firstly we need to specify parameter values in our model. Since our model is proposed to describe the dynamics of tumor growth with both drug-sensitive and drug-resistant cells, we assume that the proliferation rate of drug-sensitive cancer cells is larger than that of normal cells, and the self-sustained growth rates of cancer cells are nonzero. Moreover, the proliferation rate of drug-resistant cells is larger than that of sensitive cells, but sensitive cells can strongly inhibit the proliferation of drug-resistant cells. Thus, we should have

    \beta_3 > \beta_2 > \beta_1,\ \beta_{20} > 0,\ \beta_{30} > 0, \ a_{32} > 1.

    Different types of cells response differently to the cytokines, and hence we assume that \theta_i can be different for different types of cells. Default parameter values used in numerical simulation are listed in the Table 1. Figure 2(a) shows the cell number dynamics in the case without treatment, in which the system states (x_1, x_2, x_3) approaches the steady state of E_{123} -type. At this state, drug-sensitive cells are dominant in the system, and there are a small fraction of pre-existing drug-resistant cells.

    Table 1.  Default parameter values.
    Parameter Value Unit
    \beta_1 0.85 \mathrm{day}^{-1}
    \beta_2 1.1 \mathrm{day}^{-1}
    \beta_3 1.2 \mathrm{day}^{-1}
    \theta_1 45.0 \times 10^{6} \mathrm{cells}
    \theta_2 96.0 \times 10^{6} \mathrm{cells}
    \theta_3 60.0 \times 10^{6} \mathrm{cells}
    \beta_{20} 0.0002 \mathrm{day}^{-1}
    \beta_{30} 0.0002 \mathrm{day}^{-1}
    \mu_1 0.05 \mathrm{day}^{-1}
    \mu_2 0.05 \mathrm{day}^{-1}
    \mu_3 0.05 \mathrm{day}^{-1}
    \eta 0.0002 \mathrm{day}^{-1}
    a_{12} 0.16 -
    a_{13} 0.44 -
    a_{21} 0.46 -
    a_{23} 0.38 -
    a_{31} 0.57 -
    a_{32} 1.2 -
    u_{\max} 0.24 \mathrm{day}^{-1}
    v_{\max} 0.3 \mathrm{day}^{-1}
    s 0.002 -
    b 1 -
    c 70 -
    d 0.15 -

     | Show Table
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    Figure 2.  Evolution of cell counts. (a) Cell count dynamics with no treatment. (b) Cell count dynamics under sequential treatment with two drugs. Here, the u -drug and v -drug are administrated in the time interval of t \in [t_1, t_2] and t \in [t_2,700] , respectively. In all simulations, initial conditions are x_{10} = 600, x_{20} = 32, x_{30} = 2 , and parameters are taken from Table 1.

    Now, we consider the effect of sequential treatment, with only one drug at one period. To this end, we run the model Eq (3.56) with u = v = 0 to t = 200\ \mathrm{days} so that cancer cells numbers reach a high level near the steady state. Next, we set u = u_{\max} to turn on the drug targeted to sensitive cells ( u -drug for short) for 200 days. Then, we set u = 0 and v = v_{\max} to turn on the drug targeted to resistant cells ( v -drug for short). Figure 2(b) shows the cell number dynamics after sequential treatment. From Figure 2(b), after the administration of u -drug, sensitive cell numbers rapidly decreases to an extreme low level, however resistant cells number increases to a high level and becomes dominant. Next, after the administration of v -drug, resistant cells number decreases, and sensitive cells number increases again, which show the clinical symptom of tumor relapse.

    Now, we investigate the dynamics of cell number ratios under different treatment strategies with either u -drug or v -drug alone, or sequential treatment with the two drugs. Here, the drug is applied at t = 200 as in Figure 2 by which sensitive cells are dominant. After the administration of u -drug for 60 days, the ratio of sensitive cells decrease over time, however the ratio of resistant cells increase along with treatment, and the ratio of total cancer cells slowly increases following the decreasing phase in the early stage after treatment (Figure 3(a), (b)). If v -drug is applied alone, there is no obvious decreases in the cancer cells ratio after treatment (Figure 3(c), (d)). The reason is obvious, since the v -drug targeted cells contribute only a small fraction of cancer cells before treatment. Finally, in the case with sequential treatment of two drugs, the total cancer cells ratio shows continuous decrease over time, and reaches a level below 0.2 after 60 days treatment (Figure 3). These results suggest that various treatment strategies can result in different outcomes.

    Figure 3.  Dynamics of cancer cells ratio under different treatment strategies. (a) Treatment strategy with continuous u -drug. (b) Dynamics of cancer cells ratio corresponding to the strategy (a). (c) Treatment strategy with continuous v -drug. (d) Dynamics of cancer cells ratio corresponding to the strategy (c). (e) Treatment strategy with sequential treatment with u -drug and v -drug. (f) Dynamics of cancer cells ratio corresponding to the strategy (e). Parameters are taken from Table 1.

    To investigate the effect of optimal control strategy, we numerically solve the optimal control problem with the method of forward-backward sweep method (FBSM) [45]. Figure 4 shows the result corresponding to the quadratic control problem. Here, we take the weight coefficients b = 1 , c = 70 and d = 0.15 (Table 1). The optimal solution in Figure 4 suggests that we should apply the maximum dose drugs simultaneously, and continuously reduce the drug doses at the end point of treatment. In this case, the total cancer cells ratio continuously decreases toward a level ( 2.93 \% ) much lower than those in Figure 3.

    Figure 4.  Optimal solution of quadratic control problem. (a) Drug doses corresponding to the optimal solution of the quadratic control problem. (b) Cancer cells ratio corresponding to the optimal solution in (a). Parameters are taken from Table 1.

    In the Eq (3.56), we introduce a parameter s to represent the effect of transition from sensitive cells to resistant cells. Biologically, the transition can be induced by epigenetic, adaptive changes, or gene mutation due to drug stress. To investigate how the transition may affect the optimal control treatment, we vary the relative strength of the transition rate (measured by the ratio s u_{\max} / \eta ), and calculate the total drug doses

    \begin{equation} U(t) = \int_0^{t_f} u(t) d t, V(t) = \int_0^{t_f} v(t) d t, \end{equation} (3.74)

    and the ratio of cancer cells at t = 60 for each value s u_{\max} . Results show that both total doses and the ratio of cancer cells are insensitive with changes in the relative strength of the transition rate (Figure 5).

    Figure 5.  Optimal solutions of quadratic control with different values s u_{\max} /\eta . (a) Total drug doses defined by (3.74) during treatment versus s u_{max} /\eta . (b) Cancer cells ratio at t = 60 versus s u_{\max} /\eta . Here, other parameters are taken from Table 1.

    Similarly, we solve the optimal control problem with linear control pay-off functional, which yields a bang-bang control. We obtain similar optimal solutions as in the case of quadratic control, in which both drugs are administrated simultaneously with maximum doses, and stop the treatment at later stage (Figure 6). Correspondingly, the final total cancer cells ratio at t = 60 decreases to about 4.54 \% . Moreover, we vary the relative strength of the transition rate s u_{\max} / \eta to examine the dependences of the total drug doses and final cancer ratios on the relative strength of the transition rate s u_{\max} / \eta . Similar to the situation of quadratic control problem, both the total drug doses and final cancer cells ratio are nonsensitive with the transition rate s u_{\max} / \eta (Figure 7).

    Figure 6.  Optimal solution of linear control problem. (a) Drug doses corresponding to the optimal solution of the linear control problem. (b) Cancer cells ratio corresponding to the optimal solution in (a). Parameters are taken from Table 1.
    Figure 7.  Optimal solutions of linear control problem with different values s u_{\max} / \eta . (a) Total drug doses defined by (3.74) during treatment versus s u_{\max} / \eta . (b) Cancer cells ratio at t = 60 versus s u_{\max} / \eta . Here, other parameters are taken from Table 1.

    Intratumor heterogeneity is important to cell competition, and may play important roles in cancer evolution. Here, we study a mathematical model of cancer evolution that includes competition between normal cells and two types of cancer cells, as well as the transition between cancer cells. Moreover, the potential transition from drug-sensitive cancer cells to drug-resistant cancer cells is also involved in the model. Based on the model, the invariant set of the nonnegative solutions, and the existence and the stability of steady sates are discussed. We further discuss the optimal control problem that trying to find the treatment strategy to minimize the optimal functional for both tumor burden and drug doses. We prove the existence and uniqueness of the optimal control strategy for the proposed model. Finally, numerical simulations are performed to verify the optimal control solutions.

    In the present study, we study the problem of optimal treatment strategy of cancer through a simple differential equation model. This model considers the competition between different types of cells. In the realistic world, optimal treatment of cancer relies on two techniques: (1) effective method to measure the state of tumor growth; (2) reliable prediction of tumor growth. However, neither of these two techniques are available at present, and there is still a long way toward real world application of the concept of optimal control treatment. This paper is rather a conceptual study that try to explore the possible cell population dynamics when there are competitions between different types of cells, and the possible benefit of optimal treatment in comparing with traditional maximum dose treatment (MDT). The current study is based on a toy model of cell competitions in which different types of cells are assumed to be homogeneous, and the effects of microenvironment are not included in the model, the immune response are not included explicitly. To develop a more realistic and applicable model, these factors are for sure to be included, which is a big ambition in the field of computational cancer biology.

    This work was funded by National Natural Science Foundation of China (NSFC 11831015).

    The authors declare there is no conflict of interest.

    Proof of the inequalities (3.65) and (3.66)

    Substituting x_i(t) = p_i(t) e^{mt}, \lambda_i(t) = q_i(t) e^{-mt} into equations (3.56) and (3.60), we have (hereafter, \dot{} means \dfrac{d\ }{d t} )

    and

    Multiplying both sides of the first three equation by e^{-m t} , and the last three equations by e^{mt} , respectively, we obtain

    \begin{eqnarray*} \dot{p}_1 + m p_1 & = & \dfrac{ \beta_1 \theta_1 p_1 }{ \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3 } - \mu_1 p_1, \\ \dot{p}_2 + m p_2 & = & \dfrac{ \beta_2 \theta_2 p_2 }{ \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3 } + ( \beta_{20} - \mu_2 - \eta) p_2 - u p_2, \\ \dot{p}_3 + m p_3 & = &\dfrac{ \beta_3 \theta_3 p_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 } + ( \beta_{30} - \mu_3) p_3 + \eta p_2 + s u p_2 - v p_3,\\ \dot{q}_1 - m q_1 & = & - \dfrac{ \beta_1 \theta_1 q_1 }{ \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3 } + \mu_1 q_1 \\ &&{} + \dfrac{ \beta_1 \theta_1 e^{mt} p_1 q_1 }{ ( \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3)^2 } + \dfrac{ a_{21} \beta_2 \theta_2 e^{mt} p_2 q_2 }{ ( \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3)^2 } \\ &&{} + \dfrac{ a_{31} \beta_3 \theta_3 e^{mt} p_3 q_3 }{ ( \theta_3 + a_{31} e^{mt} p_1 + a_{32} e^{mt} p_2 + e^{mt} p_3)^2 }, \\ \dot{q}_2 - m q_2 & = & -b e^{mt} + \dfrac{a_{12} \beta_1 \theta_1 e^{mt} p_1 q_1 }{ ( \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3)^2 } + (\mu_2 + \eta - \beta_{20}) q_2 + u q_2 \\ &&{} - \dfrac{ \beta_2 \theta_2 q_2 }{ \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3 } + \dfrac{ \beta_2 \theta_2 e^{mt} p_2 q_2 }{ ( \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3)^2 } \\ &&{} + \dfrac{ a_{32} \beta_3 \theta_3 e^{mt} p_3 q_3 }{ ( \theta_3 + a_{31} e^{mt} p_1 + a_{32} e^{mt} p_2 + e^{mt} p_3)^2 } - \eta q_3 - s u q_3, \\ \dot{q}_3 - m q_3 & = & -b e^{mt} + \dfrac{a_{13} \beta_1 \theta_1 e^{mt} p_1 q_1 }{ ( \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3)^2 } \\ &&{} + \dfrac{ a_{23} \beta_2 \theta_2 e^{mt} p_2 q_2 }{ ( \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3)^2 } - \dfrac{ \beta_3 \theta_3 q_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32} e^{mt} p_2 + e^{mt} p_3 } \\ &&{} + (\mu_3 - \beta_{30}) q_3 + v q_3 + \dfrac{ \beta_3 \theta_3 e^{mt} p_3 q_3 }{ ( \theta_3 + a_{31} e^{mt} p_1 + a_{32} e^{mt} p_2 + e^{mt} p_3)^2 }. \end{eqnarray*}

    Similarly, we obtain the same form equations of \bar{p}_i and \bar{\lambda}_i , i = 1, 2, 3 .

    Next, subtracting the equations for p_i and \bar{p}_i , and the equations for q_i and \bar{q}_1 , we have

    \begin{eqnarray*} ( \dot{p}_1 - \dot{\bar{p}}_1) + m (p_1 -\bar{p}_1) & = & \dfrac{ \beta_1 \theta_1 p_1 }{ \theta_1 + e^{mt} p_1 + a_{12}e^{mt} p_2 + a_{13}e^{mt} p_3 } - \dfrac{ \beta_1 \theta_1 \bar{p}_1 }{ \theta_1 + e^{mt} \bar{p}_1 + a_{12}e^{mt} \bar{p}_2 + a_{13}e^{mt} \bar{p}_3 } \\ &&{} - \mu_1 (p_1 - \bar{p}_1), \\ ( \dot{p}_2 - \dot{\bar{p}}_2) + m (p_2 -\bar{p}_2) & = & \dfrac{ \beta_2 \theta_2 p_2 }{ \theta_2 + a_{21} e^{mt} p_1 + e^{mt} p_2 + a_{23}e^{mt} p_3 } - \dfrac{ \beta_2 \theta_2 \bar{p}_2 }{ \theta_2 + a_{21} e^{mt} \bar{p}_1 + e^{mt} \bar{p}_2 + a_{23}e^{mt} \bar{p}_3 } \\ && + ( \beta_{20} - \mu_2 - \eta) ( p_2 - \bar{p}_2 ) - ( u p_2 - \bar{u} \bar{p}_2 ), \\ ( \dot{p}_3 - \dot{\bar{p}}_3) + m (p_3 -\bar{p}_3) & = & \dfrac{ \beta_3 \theta_3 p_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 } - \dfrac{ \beta_3 \theta_3 \bar{p}_3 }{ \theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3 } \\ &&{} + ( \beta_{30} - \mu_3) ( p_3 - \bar{p}_3 )+ \eta (p_2 - \bar{p}_2) + s (u p_2- \bar{u} \bar{p}_2 ) - (v p_3 - \bar{v} \bar{p}_3 ), \end{eqnarray*}

    and

    Now, we consider the equations for (p_3 - \bar{p}_3) and (-q_3 + \bar{q}_3) , and other equations can be treated similarly. Multiplying the equation for (p_3 - \bar{p}_3) by (p_3 - \bar{p}_3) , and integrating the obtained equation from 0 to t_f , we have

    \begin{eqnarray} && \dfrac{1}{2} ( p_3(t) - \bar{p}_3(t) )^2 \big |_0^{t_f} + m \int_{0}^{t_f} (p_3 -\bar{p}_3)^2 dt \\ & = & \int_{0}^{t_f} \Big( \dfrac{ \beta_3 \theta_3 p_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 } - \dfrac{ \beta_3 \theta_3 \bar{p}_3 }{ \theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3 } \Big) (p_3 - \bar{p}_3) dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt. \end{eqnarray} (4.1)

    Multiplying the equation for (q_3 - \bar{q}_3) by (- q_3 + \bar{q}_3) , and integrating the obtained equation from 0 to t_f , we have

    (4.2)

    We note that p_3(0) = \bar{p}_3(0) = x_{30} , equation (4.1) implies

    \begin{eqnarray} && \dfrac{1}{2} ( p_3(t_f) - \bar{p}_3(t_f) )^2 + m \int_{0}^{t_f} (p_3 -\bar{p}_3)^2 dt \\ & = & \int_{0}^{t_f} \Big( \dfrac{ \beta_3 \theta_3 p_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 } - \dfrac{ \beta_3 \theta_3 \bar{p}_3 }{ \theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3 } \Big) (p_3 - \bar{p}_3) dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt \\ &\leqslant & \int_{0}^{t_f} \Big | \dfrac{ \beta_3 \theta_3 p_3 }{ \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 } - \dfrac{ \beta_3 \theta_3 \bar{p}_3 }{ \theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3 } \Big | |p_3 - \bar{p}_3| dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt. \end{eqnarray} (4.3)

    Since the solutions of (3.56) are nonnegative, namely p_i, \bar{p}_i \geqslant 0 , we have

    (\theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3) (\theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3) \geqslant \theta_3^2.

    Hence,

    \begin{eqnarray} && \dfrac{1}{2} ( p_3(t_f) - \bar{p}_3(t_f) )^2 + m \int_{0}^{t_f} (p_3 -\bar{p}_3)^2 dt \\ &\leqslant & \dfrac{\beta_3 }{\theta_3} \int_{0}^{t_f} \Big | p_3 (\theta_3 + a_{31} e^{mt} \bar{p}_1 + a_{32}e^{mt} \bar{p}_2 + e^{mt} \bar{p}_3 ) \\ &&{}- \bar{p}_3 ( \theta_3 + a_{31} e^{mt} p_1 + a_{32}e^{mt} p_2 + e^{mt} p_3 ) \Big | |p_3 - \bar{p}_3| dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt \\ & = & \dfrac{\beta_3 }{\theta_3} \int_{0}^{t_f} \Big | \theta_3 ( p_3 - \bar{p}_3 ) + a_{31} e^{mt} ( p_3 \bar{p}_1 - \bar{p}_3 p_1 ) + a_{32}e^{mt} ( p_3 \bar{p}_2 - \bar{p}_3 p_2 ) \Big | |p_3 - \bar{p}_3| dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt \\ &\leqslant & \dfrac{\beta_3 }{\theta_3} \int_{0}^{t_f} \Big ( \theta_3 | p_3 - \bar{p}_3 | + a_{31} e^{mt} | p_3 \bar{p}_1 - \bar{p}_3 p_1 | + a_{32}e^{mt} | p_3 \bar{p}_2 - \bar{p}_3 p_2 | \Big ) |p_3 - \bar{p}_3| dt \\ &&{} + ( \beta_{30} - \mu_3) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt \\ & = & \dfrac{\beta_3 }{\theta_3} \int_{0}^{t_f} \Big ( a_{31} e^{mt} | p_3 \bar{p}_1 - \bar{p}_3 p_1 | + a_{32}e^{mt} | p_3 \bar{p}_2 - \bar{p}_3 p_2 | \Big ) |p_3 - \bar{p}_3| dt \\ &&{} + ( \beta_{30} - \mu_3 + {\beta_3 } ) \int_{0}^{t_f} ( p_3 - \bar{p}_3 )^2 dt + \eta \int_{0}^{t_f} (p_2 - \bar{p}_2)( p_3 - \bar{p}_3 ) dt \\ &&{} + s \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt. \end{eqnarray} (4.4)

    Now, we perform estimations to some terms of (4.4), and the other terms can be obtained by similar discussions. Applying the Cauchy inequality, there exists M_1 > 0 such that

    \int_{0}^{t_f} a_{31} e^{mt} | p_3 \bar{p}_1 - \bar{p}_3 p_1 | |p_3 - \bar{p}_3| dt \leqslant a_{31} e^{m t_f} \int_{0}^{t_f} | (p_3 \bar{p}_1 - \bar{p}_3 p_1 ) (p_3 - \bar{p}_3 )| dt \\ = a_{31} e^{m t_f} \int_{0}^{t_f} | (p_3 \bar{p}_1 - p_3 p_1 + p_3 p_1 - \bar{p}_3 p_1 ) (p_3 - \bar{p}_3 )| dt \\ = a_{31} e^{m t_f} \int_{0}^{t_f} | (p_3 ( \bar{p}_1 - p_1) (p_3 - \bar{p}_3 ) + (p_3 - \bar{p}_3) p_1 ) (p_3 - \bar{p}_3 )| dt \\ \leqslant a_{31} e^{m t_f} \int_{0}^{t_f} | p_3 ( \bar{p}_1 - p_1) (p_3 - \bar{p}_3 )| + | p_1 | (p_3 - \bar{p}_3)^2 dt \\ \leqslant a_{31} e^{m t_f} M_1 \int_{0}^{t_f} ( ( \bar{p}_1 - p_1)^2 + (p_3 - \bar{p}_3)^2 ) dt. (4.5)

    Next, since p_i(t) and \bar{p}_i(t) are nonnegative functions for t\in (0, t_f) ,

    Moreover, since the function f(p_2, q_2, q_3) = \dfrac{ (q_2 - s q_3) p_2^2 }{2 c} is locally Lipschitz, there exists M_2 > 0 so that

    \begin{eqnarray*} && \int_{0}^{t_f} \Big| \dfrac{( q_2 - s q_3 ) p_2^2 }{2 c} - \dfrac{( \bar{q}_2 - s \bar{q}_3 ) \bar{p}_2^2 }{2 c} \Big | | p_3 - \bar{p}_3 | dt \\ &\leqslant & M_2 \int_{0}^{t_f} ( | p_2 - \bar{p}_2 | + | q_2 - \bar{q}_2 | +| q_3 - \bar{q}_3 | ) | p_3 - \bar{p}_3 | dt \\ &\leqslant & \dfrac{ M_2}{2} \int_{0}^{t_f} ( ( p_2 - \bar{p}_2 )^2 + ( q_2 - \bar{q}_2 )^2 + ( q_3 - \bar{q}_3 )^2 + 3 ( p_3 - \bar{p}_3 )^2 ) dt. \end{eqnarray*}

    Hence,

    \begin{equation} \int_{0}^{t_f} (u p_2- \bar{u} \bar{p}_2 )( p_3 - \bar{p}_3 ) dt \leqslant \dfrac{ M_2}{2} \int_{0}^{t_f} ( ( p_2 - \bar{p}_2 )^2 + ( q_2 - \bar{q}_2 )^2 + ( q_3 - \bar{q}_3 )^2 + 3 ( p_3 - \bar{p}_3 )^2 ) dt. \end{equation} (4.6)

    Similarly, there exists M_3 > 0 so that

    \begin{equation} - \int_{0}^{t_f} (v p_3 - \bar{v} \bar{p}_3 )( p_3 - \bar{p}_3 ) dt \leqslant \dfrac{ M_3}{2} \int_{0}^{t_f} ( ( q_3 - \bar{q}_3 )^2 + 3 ( p_3 - \bar{p}_3 )^2 ) dt . \end{equation} (4.7)

    Thus, from (4.4) and (4.5)-(4.7), and note (p_3(t_f) - \bar{p}_3(t_f))^2 \geqslant 0 , there exists L_{1, 3} > 0 so that

    m \int_{0}^{t_f} (p_3 -\bar{p}_3)^2 dt \leqslant L_{1,3} (1 + e^{m t_f}) \int_{0}^{t_f} \left(\sum\limits_{j = 1}^3 (( \bar{p}_j - p_j)^2 + ( \bar{q}_j - q_j)^2)\right) dt,

    which gives an inequality of form (3.65).

    Applying the analogous scheme, we obtain for L_{2, 3} > 0 so that

    m \int_{0}^{t_f} (q_3 -\bar{q}_3)^2 dt \leqslant L_{2,3} (1 + e^{m t_f} + e^{2 m t_f} + e^{ 3 m t_f} ) \int_{0}^{t_f} \left(\sum\limits_{j = 1}^3 (( \bar{p}_j - p_j)^2 + ( \bar{q}_j - q_j)^2)\right) dt,

    which gives an inequality of form (3.66).



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