1. Introduction
Prey-taxis, the movement of predators toward regions of higher prey density, plays important roles in biological control such as regulating prey (pest) population to avoid incipient outbreaks of prey or forming large-scale aggregation for survival (cf. [Reference Grünbaum13, Reference Murdoch, Chesson and Chesson32, Reference Sapoukhina, Tyutyunov and Arditi44]). This mechanism was first applied to the predator–prey systems by Kareiva and Odell [Reference Kareiva and Odell26] to interpret the heterogeneous aggregative patterns observed in a field experiment for one predator and one prey involving area-restricted search strategies. The Kareiva–Odell prey-taxis model generally reads as

where
$u(x,t)$
and
$v(x,t)$
denote predator and prey density at position
$x\in \Omega$
and time
$t$
, respectively, and
$\Omega \subset {\mathbb {R}}^n(n\geq 1)$
is a bounded domain with smooth boundary. The function
$G(v, u)$
is the functional response that describes the predator’s consumption rate of prey, and
$F(v)$
represents the per capita prey growth rate in the absence of predators.
$d_1$
and
$d_2$
are diffusion rates of the predator and the prey, respectively. The parameters
$\beta$
and
$\theta$
represent the conversion rate of captured prey into predator and the predator mortality rate, respectively. All parameters are positive unless otherwise stated.
The functional response function
$G(u,v)$
is a crucial factor shaping various dynamical behaviors in predator–prey systems [Reference Turchin53]. Over the past century, different functional responses have been identified based on various biological applications, including Holling type [Reference Holling16–Reference Holling18], Hassell-Varley type [Reference Hassell and Varley15], Beddington–DeAngelis type [Reference Beddington4, Reference Donald Lee DeAngelis and O’Neill10], ratio-dependent type [Reference Arditi and Ginzburg3] and Crowley–Martin type [Reference Crowley and Martin9], among others [Reference Turchin53]. The prey growth function
$F(v)$
typically takes the form of a logistic type

with the prey intrinsic growth rate
$\sigma$
and the environmental carrying capacity
$K$
for the prey. Apart from the logistic type,
$F(v)$
could be bistable (or Allee effect) type [Reference Wang, Shi and Wei55] or fear effect type [Reference Wang, Zanette and Zou56], and so on. In the sequel, we shall assume
$F(v)$
is of logistic type (1.2) unless otherwise stated.
This paper will be concerned with the functional response function employing the hunting cooperation strategy, which has attracted extensive attention recently. Cooperative hunting is a prominent behaviour among large social carnivores, which enhances their ability to capture prey in their natural habitats [Reference Norris and Schilt34, Reference Wilson58]. This behaviour enables predators to subdue large prey and improve their hunting success. For instance, hyenas and wolves usually hunt alone when pursuing small-size prey such as gazelles and sheep. In contrast, they prefer to hunt in packs when hunting large-size prey such as zebras and deer [Reference Kruuk27, Reference Murie33, Reference Schmidt and Mech46]. This communal hunting phenomenon, leading to increased foraging efficiency, has been observed in higher predator densities of terrestrial carnivores, including lions [Reference Scheel and Packer45], wolves [Reference Schmidt and Mech46] and African wild dogs [Reference Creel and Creel8]. To model this phenomenon of hunting cooperation, several functional responses that increase with respect to the predator density, also known as hunting cooperation functional responses, have been proposed, including

where
$\lambda \gt 0$
represents the predation rate on prey and
$\alpha \geq 0$
characterizes the level of predator cooperation during hunting,
$h$
represents the handling time per prey item,
$e_0$
is the encounter rate per predator per prey unit time, and
$c$
is a fraction of a prey item killed per predator per encounter. When
$\alpha =0$
, the Type I, II and III hunting cooperation response functions reduce to the well-known Holling I, II and III functional response functions, respectively.
Among other things, this paper is focused on the Type I hunting cooperation:

which was first proposed in [Reference Alves and Hilker52] and the corresponding temporal system (namely system (1.1) with (1.4) and
$d_1=d_2=\chi =0$
) was numerically studied in [Reference Alves and Hilker52]. It was found that hunting cooperation can benefit predator populations by increasing attack rates, and large values of
$\alpha$
can induce Hopf bifurcations.
The system (1.1) with
$\chi =0$
is referred to as the diffusive predator–prey system. It was shown that (1.1) with (1.4) will not have Turing instability without hunting cooperation (i.e.
$\alpha =0$
) (cf. [Reference Capone, Maria Francesca Carfora and Torcicollo6, Reference Wu and Zhao60]), while it will do with hunting cooperation (i.e.
$\alpha \gt 0$
) only if the predator spreads slower than the prey (i.e.
$d_1\gt d_2$
) (cf. [Reference Capone, Maria Francesca Carfora and Torcicollo6, Reference Singh, Dubey and Mishra47, Reference Wu and Zhao60]). Later, the Hopf bifurcation was investigated in [Reference Miao and He29] by the centre manifold and the normal form theory. If the Neumann boundary condition was replaced by the homogeneous Dirichlet boundary condition
$u|_{\partial \Omega }=v|_{\partial \Omega }=0$
and
$n\lt 6$
, the stationary solution of the system (1.1) with (1.4) was studied in [Reference Ryu and Ko40] showing that sufficiently large
$\alpha$
leads to the extinction of the predator species. For more related works on the predator–prey models with hunting cooperation, we refer readers to [Reference Han, Dey and Banerjee14, Reference Jang, Zhang and Larriva20, Reference Liu, Zhang and Li28, Reference Song, Song and Li50, Reference Vishwakarma and Sen54] for Allee effects in prey, [Reference Pal, Pal, Samanta and Chattopadhyay35] for fear effects in prey, [Reference Du, Niu and Wei12] for group defense in prey, [Reference Sk, Mondal, Sarkar, Santra, Baleanu and Altanji48] for three-species food chain, [Reference Dey, Banerjee and Ghorai11, Reference Mukherjee and Banerjee31, Reference Ryu and Ko41, Reference Takyi, Ohanian, Cathcart and Kumar51, Reference Vishwakarma and Sen54] for hunting cooperation functional response functions other than Type I, and references therein.
Though a considerable body of literature has studied the dynamics of predator–prey systems with hunting cooperation in the absence of prey-taxis (i.e.
$\chi =0)$
as mentioned above, only a few results are available to the predator–prey systems with prey-taxis and hunting cooperation (cf. [Reference Pierre38, Reference Ko and Ryu42, Reference Ko and Ryu43, Reference Zhang, Fu and Huang62]). When the hunting cooperation functional response function
$G(u,v)$
is Type II as given in (1.3), the existence of non-constant positive steady states of prey-taxis system (1.1) was obtained by the bifurcation theory in one dimension in [Reference Peng, Yang and Zhang37] where it was also shown that small prey-tactic sensitivity
$\chi \gt 0$
can induce the Turing instability. Recently the work [Reference Zhang, Fu and Huang62] established the existence of globally bounded classical solutions of (1.1) with Type II hunting cooperation in any dimension, and showed that negative prey-tactic sensitivity
$\chi \lt 0$
(i.e. repulsive prey-taxis) can induce the Turing instability. When the hunting cooperation functional response function
$G(u,v)$
is uniformly bounded for all
$u,v\geq 0$
, the global boundedness of solutions was established [Reference Ko and Ryu42, Reference Ko and Ryu43] where the global stability of constant positive steady states and existence/nonexistence of non-constant positive solutions were further obtained if
$G(u,v)$
is Type II. We remak the assumption in [Reference Ko and Ryu42, Reference Ko and Ryu43] rules out the Type I hunting cooperation functional response function (1.4) since it is obviously not uniformly bounded for
$u,v\geq 0$
.
It is seen from the abovementioned existing results that the prey-taxis system (1.1) with Type I hunting cooperation functional response function
$G(u,v)$
has not been studied, which is the most difficult case to study from a mathematical point of view among three types given in (1.3) since
$G(u,v)$
is not uniformly bounded for
$u,v\geq 0$
if it is of Type I. When
$G(u,v)$
is uniformly bounded for all
$u,v\geq 0$
like Type II or Type III, the regularity of the Neumann heat semigroup (cf. [Reference Pazy36]) can be directly applied to establish global boundedness of solutions, while Type I forfeits this advantage. Apart from this, it is also unclear whether the Type I hunting cooperation may induce the spatiotemporal patterns. This paper will address these questions and we therefore consider the following prey-taxis system (1.1) with Type I hunting cooperation

where the parameters
$d_1,d_2,\beta ,\lambda ,\alpha ,\theta ,\sigma ,K\gt 0$
and
$\chi \geq 0$
have the same biological interpretations as mentioned above. To reduce the number of parameters, we introduce the following rescalings

and

Substituting the above rescalings into (1.5) and dropping the tildes for brevity, we obtain the following rescaled system

where the parameters
$d_1,d_2,\alpha ,K,\sigma$
are positive and
$\chi \gt 0$
. Throughout the paper, we shall often use the following notations

for brevity.
The main analytical result of this paper is the following.
Theorem 1.1.
Let
$\Omega \subset \mathbb {R}^{n}$
(
$n\geq 2$
) be a bounded domain with smooth boundary, and let
$(u_{0}, v_{0}) \in [W^{1, q}(\Omega )]^2$
with some
$q\gt n$
and
$u_{0}(x), v_{0}(x) \geq 0(\!\not \equiv 0)$
. Then there exists
$\chi _*\in (0,+\infty ]$
such that for all
$\chi \in {(}0,\chi _*)$
, the system
(1.6)
admits a unique classical solution
$(u,v)\in [C^0(\overline {\Omega } \times [0, \infty )) \cap C^{2,1}(\overline {\Omega } \times (0, \infty ))]^2$
satisfying
$u,v\gt 0$
for all
$t\gt 0$
. Moreover, there exists a constant
$C\gt 0$
independent of
$t$
such that

In particular,
$\chi _*=+\infty$
if
$n=2$
.
Before ending this section, we outline the main difficulties and proof strategies.
1.1 Sketch of proof strategies
Without prey-taxis (i.e.
$\chi =0$
), problem (1.6) can be regarded as a special one considered in [Reference Pierre38]. Then the global boundedness of solutions to (1.6) with
$\chi =0$
in any dimension (
$n\geq 1$
) is a consequence of [Reference Pierre38, Theorem 3.1] (see also [Reference Selwyn, Robert and Michel19]) based on the
$L^p$
-duality method. Without hunting cooperation (i.e.
$\alpha =0$
), the global boundedness of solutions to (1.6) has been established in [Reference Jin and Wang23, Reference Wu, Shi and Wu61]. Now with
$\alpha \gt 0$
, the source term contains a cubic polynomial
$\alpha u^2 v$
and many arguments and estimates in [Reference Jin and Wang23, Reference Wu, Shi and Wu61] for the quadratic polynomial are no longer applicable. Hence, new technical ingredients are needed to deal with the higher-order nonlinearity. Below we briefly describe our strategies used to obtain the global boundedness of solutions for
$n=2$
and
$n\geq 3$
.
-
(i)
$n=2$ . In this case, by fully exploiting the model structural feature, we use cancellation ideas to handle the troubling prey-taxis term while simultaneously controlling the cubic nonlinear source term
$\alpha u^2v$ (see the proof of Lemma 3.1), and finally obtain the crucial uniform-in-time bound of
$\|u\|_{L^{2}(\Omega )}$ with sophisticated coupling estimates by establishing a Grownwall type inequality for the linear combination of following four terms (see (3.19) and (3.27))
\begin{align*} \frac d{dt}\int _\Omega u^2,\quad \frac d{dt}\int _\Omega \frac {|\nabla v|^2}{v},\quad \frac d{dt}\int _\Omega u\ln u,\quad \frac d{dt}\int _\Omega uv. \end{align*}
$L^p$ estimates to obtain the uniform-in-time bound of
$\|u\|_{L^{p}(\Omega )}$ for
$p\gt 2$ , which yields the global boundedness of solutions by the boundedness criterion in Lemma 2.6 and the extension criterion in Lemma 2.1. We stress that here we obtain the
$L^2$ -estimates directly with the sophisticated coupling estimates by fully exploiting the advantage of cubic decay term
$-\alpha u^2v$ . This is different from the estimates in the existing literature for the prey-taxis model without hunting cooperation such as [Reference Jin and Wang23, Reference Wu, Shi and Wu61] where the
$L^2$ -estimate of
$u$ is established based on the estimate of
$\|u\ln u\|_{L^1}$ and
$\|\nabla v\|_{L^2}$ which are first obtained separately.
-
(ii)
$n\geq 3$ . In this case, we first establish a uniform-in-time bound of the weighted
$L^p$ -norm
$\int _\Omega u^p\varphi (v)$ (
$p\gt 1$ ) by constructing an appropriate weight function
$\varphi (v)$ (see Lemma 4.1 and Lemma 4.2), and then obtain a bound of
$\|u\|_{L^{p}(\Omega )}$ under a smallness condition on
$\chi \gt 0$ .
The rest of the paper is organized as follows. In Sect. 2, we establish the local existence of solutions to the system (1.6) and derive some preliminary results. We prove Theorem 1.1 for
$n=2$
in Sect. 3 and for
$n\geq 3$
in Sect. 4. Finally, in Sect. 5, we conduct linear stability analysis to show that both Turing bifurcations and Turing–Hopf bifurcations may arise from the system (1.6), and use numerical simulations to demonstrate that (1.6) may generate various complex spatiotemporal patterns such as spatially homogeneous time-periodic patterns, stationary patterns, spatiotemporal periodic patterns and chaos.
2. Local existence and preliminaries
In this section, we establish the local existence of solutions to the system (1.6) and provide some preliminary results. Hereafter, we use
$C$
and
$C_i$
(
$i=1,2,3,\cdots$
) to denote generic positive constants that may vary from line to line in the context. We begin with the local existence of solutions.
Lemma 2.1.
Suppose that the assumptions in Theorem
1.1
hold. Then there exists
$T_{\max } \in (0, +\infty ]$
such that the system
(1.6)
has a unique classical solution

satisfying

Moreover,

Proof. Denote
$\omega =(u, v)$
. Then the system (1.6) can be written as

where
$\mathbb {A}(\omega )=\left [\begin{array}{cc} d_1 & -\chi u \\ 0 & d_2 \end{array}\right ]$
and
$ \Phi (\omega )= \left ( \begin{array}{c} f(u,v) \\ g(u,v) \end{array} \right )$
with
$f(u,v)$
and
$g(u,v)$
given by (1.7). The upper triangular matrix
$\mathbb {A}(\omega )$
is positively definite. Hence, the system (1.6) is normally parabolic. Then the local existence and uniqueness of classical solutions follow from Amann’s theorem [Reference Amann1, Theorem 7.3 and Corollary 9.3] and the blow-up criteria (2.2) follows from [Reference Amann2, Theorem 15.5]. Moreover,
$u,v\gt 0$
for
$(x, t) \in \Omega \times \left (0, T_{\max }\right )$
can be established by the strong maximum principle along with
$u_0,v_0\geq 0(\not \equiv 0)$
. These arguments are standard and we refer readers to [Reference Wang and Hillen57, Lemma2.6] and [Reference Jin and Wang24, Lemma2.1] for details. Finally, an application of [Reference Jin and Wang23, Lemma2.2] proves
$v\leq M_0$
for
$(x, t) \in \Omega \times \left (0, T_{\max }\right )$
.
The following result can be easily obtained.
Lemma 2.2.
Suppose that the assumptions in Theorem
1.1
hold and
$(u, v)$
is the solution of the system
(1.6)
. Then

Proof. Adding the first two equations of (1.6), integrating the resulting equation by parts and using Young’s inequality
$(1+\sigma )v\leq \frac \sigma K v^2+\frac {K(1+\sigma )^2}{4\sigma }$
, we have

which alongside
$u,v\geq 0$
implies

The proof is completed.
We shall recall some inequalities that will be used later.
Lemma 2.3 ([Reference Jin22, Lemma 2.3]). Let
$\alpha , \beta , T\gt 0$
,
$\tau \in (0, T)$
, and suppose that
${\phi }:[0, T) \rightarrow$
$[0, \infty )$
is absolutely continuous satisfying

where
$\sigma \gt 0$
is a constant,
${\varphi }(t), h(t) \geq 0$
with
${\varphi }(t), h(t) \in L_{l o c}^1([0, T))$
and

Then for any
$t\gt t_0$
, we have

and

where

Lemma 2.4 ([Reference Winkler59, Lemma 3.3]). Suppose that
$H \in C^1((0, \infty ),{\mathbb {R}}_+)$
and
$\Theta (s)\,:\!=\, \int _1^s \frac {d \sigma }{H(\sigma )}$
for
$s\gt 0$
. Then for all
$\varphi \in C^2(\overline {\Omega })$
fulfilling
$\frac {\partial \varphi }{\partial v}=0$
on
$\partial \Omega$
, it holds that

Lemma 2.5 ([Reference Mizoguchi and Souplet30, Lemma 4.2]). Assume that
$\Omega$
is a bounded domain, and let
$w \in C^2(\overline {\Omega })$
satisfy
$\frac {\partial w}{\partial \nu }=0$
on
$\partial \Omega$
. Then we have

where
$\kappa =\kappa (\Omega )$
is an upper bound of the curvatures of
$\partial \Omega$
.
Now we establish a boundedness criterion.
Lemma 2.6.
Suppose that the assumptions in Theorem
1.1
hold and
$(u, v)$
is the solution of the system
(1.6)
. If there exists
$p \gt \frac {3n}{2}$
(
$n\geq 2$
) such that

for a positive constant
$K_1$
, there exists a positive constant
$K_2$
independent of
$t$
such that

Proof. Assume that (2.7) holds for some
$p \gt \frac {3n}{2}$
(
$n\geq 2$
). Then there exists a constant
$C_1\gt 0$
such that

Since
$\frac {p }2\gt \frac {3n}4$
, one can use a standard argument based on the smooth property of the Neumann heat semigroup (cf. [Reference Pazy36]) to find two constants
$r_1\gt 3n$
and
$C_2\gt 0$
such that

Given
$t\in (0,T_{\max })$
, we let
$t_0\,:\!=\, (t-1)_+$
. By Duhamel’s principle,
$u$
can be represented as

By (2.3), the maximum principle and the smooth property of the Neumann heat semigroup again, for all
$t\in (0, T_{\max })$
, we can find two positive constants
$C_3$
and
$C_4$
such that

Let
$r_2\,:\!=\, \frac { {p }r_1}{ {p }+r_1}$
. Then
$r_2\gt n$
due to
$\frac 1{r_2}=\frac 1{p }+\frac 1{r_1}\lt \frac 1n$
. By (2.8) and Hölder’s inequality, for all
$t\in (0,T_{\max })$
, we have

which alongside the smooth property of the Neumann heat semigroup gives two positive constants
$C_5$
and
$C_6$
such that

for all
$t\in (0,T_{\max })$
, where we have used the fact
$\frac 12+\frac {n}{2r_2}\lt 1$
, and
$\lambda _1\gt 0$
denotes the first nonzero eigenvalue of
$-\Delta$
in
$\Omega$
under the homogeneous Neumann boundary condition.
It follows from (1.7), (2.1), (2.7), Young’s inequality and Hölder’s inequality that there exist two constants
$C_7,C_8\gt 0$
such that

Let
$\overline f(t)\,:\!=\, \frac 1{|\Omega |}\int _\Omega f(u(\cdot ,t),v(\cdot ,t))$
for all
$t\in (0,T_{\max })$
. Notice that
$\frac {3n}4\gt 1$
for
$n\geq 2$
. Then (2.12) and Hölder’s inequality imply

Using (2.12), (2.13),
$t-t_0\leq 1$
, and the
$L^p$
-
$L^q$
estimates of the Neumann heat semigroup, we can find two positive constants
$C_9$
and
$C_{10}$
satisfying

The combination of (2.9), (2.10), (2.11) and (2.14) yields that

with a constant
$C_{11}\gt 0$
. The proof is completed.
3. Proof of Theorem1.1 for
$n=2$
This section is devoted to proving Theorem1.1 for
$n=2$
. To this end, we construct an appropriate functional in the form of a linear combination of the four terms

to derive some a priori estimates including the time-independent boundedness of
$\|u\|_{L^2(\Omega )}$
. This idea was first used in [Reference Winkler59] for a chemotaxis-fluid model, and then developed for predator–prey models with prey-taxis [Reference Jin and Wang23, Reference Jin, Wang and Wu25].
3.1
$L^2$
-estimate via sophisticated coupling estimates
Lemma 3.1
Suppose that the assumptions in Theorem
1.1
hold with
$n=2$
and
$(u, v)$
is the solution of the system
(1.6)
. Then for
$\tau \in \left (0,T_{\max }\right )$
, we have

and

for all
$t\in (0,T_{\max }-\tau )$
, where
$D^2 v$
denotes the Hessian matrix of
$v$
.
Proof. We split the proof into several steps.
Step 1. An inequality for
$\frac d{dt}\int _\Omega \frac {|\nabla v|^2}{v}$
. For all
$t\in (0,T_{\max })$
, it holds that

We have from (1.7) and (2.1) that

for all
$t\in (0,T_{\max })$
. For the term
$I_4$
, we claim that there exists a positive constant
$C_1$
such that

where
$A_1=\frac {d_2}{3(2+\sqrt {2})^2+2}$
. Then the combination of (3.3)-(3.5) indicates that

Using (2.1) and Young’s inequality, we obtain

for all
$t\in (0,T_{\max })$
, where
$C_2\,:\!=\, \frac {M_0|\Omega |}{A_1}\left (\frac {1+\sigma }2+C_1\right )^2$
. By (1.7), we have

where
$I_5\,:\!=\, \int _\Omega \left (1+2\alpha u\right )\nabla u\cdot \nabla v$
. Substituting (3.7) and (3.8) into (3.6), we have

for all
$t\in (0,T_{\max })$
.
We next prove (3.5) by similar arguments to that of [Reference Jin and Wang23, 3.2 and Lemma 3.3] (see also the proof of [Reference Jin, Wang and Wu25, 3.2 and Lemma 3.3]). For completeness, we sketch the proof here. Applying [Reference Jin and Wang23, Equs. (3.19) and (3.27)] with
$F(v)=v$
therein, we have

and

Using Lemma2.4 with
$H(v)=v$
yields

To proceed, we recall the trace inequality [Reference Quittner and Souplet39, Remark 52.9]: for any
$\varepsilon \gt 0$
, there exists a constant
$C(\varepsilon )\gt 0$
such that

Denote
$\varphi _0(v)=\frac {|\nabla v|}{\sqrt v}$
. Then for all
$t\in (0,T_{\max })$
, it follows from Young’s inequality that

This alongside Lemma 2.5, (3.13) with
$\varepsilon =\sqrt {\frac {A_1}{10\kappa d_2}}$
, and the fact that
$(a+b)^2\leq 2(a^2+b^2)$
for
$a,b\in {\mathbb {R}}$
gives

where
$C_1\gt 0$
is a constant. Now the combination of (3.10)-(3.12) and (3.14) indicates

which gives (3.5) by recalling
$A_1=\frac {d_2}{3(2+\sqrt {2})^2+2}$
. Therefore, the claim (3.5) is proved, and hence (3.9) is obtained.
Step 2. Cancellation of the nonlinear term
$\int _\Omega (1+2\alpha u)\nabla u\cdot \nabla v$
. We now deal with the nonlinear term
$I_5=\int _\Omega \left (1+2\alpha u\right )\nabla u\cdot \nabla v$
appearing in (3.9). For all
$t\in (0,T_{\max })$
, using (1.6) and integration by parts, we have



Let
$A_2\,:\!=\, \frac {2(d_1+d_2)}\chi +\frac 1{2\alpha }$
. Then
$\chi A_2+\chi u-2(d_1+d_2)=\frac \chi {2\alpha }(1+2\alpha u)$
, which alongside (3.15)-(3.17) gives

for all
$t\in (0,T_{\max })$
. If we multiply (3.18) by
$\frac {2\alpha }\chi$
and add the result to (3.9), then the nonlinear term
$I_5$
can be canceled.
Step 3. A Grönwall-type inequality. Define the function

Then for all
$t\in (0,T_{\max })$
, the combination of (3.9) and (3.18) multiplied by
$\frac {2\alpha }\chi$
indicates that

We next estimate the term
$I_7$
. Indeed, Young’s inequality and (2.1) yield

which implies

It remains to estimate the term
$I_8$
. Using (1.7), (2.1), (2.3), Young’s inequality and the fact that
$-s\ln s\leq \frac 1e$
and
$\ln s\lt s$
for
$s\gt 0$
, we have

For the term
$I_6$
included in
$I_8$
, it holds that

Moreover, for all
$t\in (0,T_{\max })$
, using (2.1), (2.3) and the fact that
$s^2\geq s\ln s$
for
$s\geq 0$
, we obtain

Using (2.3), the Gagliardo–Nirenberg inequality and Young’s inequality, for all
$t\in (0,T_{\max })$
, we can find two positive constants
$C_3$
and
$C_4$
such that

The combination of (3.22)-(3.24) shows that

where
$C_5\,:\!=\, C_4+\frac {2\alpha }\chi \left [2 (1+\sigma )M_0M_1+\frac {A_2}e|\Omega |\right ]$
. Define the function

Then
$\varphi '(s)=\frac {A_2}s-1$
and hence

Therefore, by (2.1), (2.3), (3.25) and the same argument as in deriving (3.24), we know that there exists a constant
$C_7\gt 0$
such that

Substituting (3.21) and (3.26) into (3.20) yields

Finally, an application of Grönwall’s inequality along with the facts
$u,v\geq 0$
and
$u\ln u\geq -\frac 1e$
yields (3.1). Furthermore, the integration of (3.27) with respect to
$t$
over
$[t,t+\tau ]$
gives (3.2).
3.2 The uniform-in-time estimate of
$\|u(\cdot ,t)\|_{L^{p}(\Omega )}$
for
$p\geq 2$
Lemma 3.2.
Suppose that the assumptions in Theorem
1.1
hold with
$n=2$
, and
$(u, v)$
is the solution of the system
(1.6)
. Then for any
$p\geq 2$
, there exists a constant
$C(p)\gt 0$
independent of
$t$
such that

Proof. Using the first equation of (1.6) and integration by parts, for all
$t\in (0,T_{\max })$
, we obtain

For all
$t\in (0,T_{\max })$
, it follows from Young’s inequality that

For the last term in the right-hand side of the above inequality, we use Hölder’s inequality
$\|u^p|\nabla v|^2\|_{L^{1}(\Omega )}\leq \|u^p\|_{L^{2}(\Omega )}\||\nabla v|^2\|_{L^{2}(\Omega )}$
, the Gagliardo–Nirenberg inequality and Young’s inequality to find a constant
$C_1\gt 0$
such that

for all
$t\in (0,T_{\max })$
, where

For the last term in the right-hand side of (3.29), we have from (1.7), (3.1) and Young’s inequality that

for all
$t\in (0,T_{\max })$
. Let
${\phi }(t)\,:\!=\, \frac 1p\|u(\cdot ,t)\|_{L^{p}(\Omega )}^p$
for all
$t\in (0,T_{\max })$
. Then Hölder’s inequality implies

For all
$t\in (0,T_{\max })$
, the combination of (3.29)-(3.32) implies that

where
$C_4\,:\!=\, {C_3+(\alpha +1)M_0}+\left (\frac 1p\right )^{\frac {p+1}p}|\Omega |^{\frac 1p}.$
Again applying the Gagliardo–Nirenberg inequality and Young’s inequality, and using (3.1), one can find two positive constants
$C_5$
and
$C_6$
such that

where

Substituting (3.34) into (3.33), for all
$t\in (0,T_{\max })$
, we arrive at

Let
$\tau =\min \left \{1,\frac {T_{\max }}2\right \}\leq 1$
. Then it follows from (2.1) and (3.2) that there exists a constant
$C_8\gt 0$
such that

for all
$t\in (0,T_{\max }-\tau )$
.
We are now in a position to prove (3.28). We shall discuss two cases:
$T_{\max }\lt 2$
and
$T_{\max }\geq 2$
. If
$T_{\max }\lt 2$
, then
$\tau \lt 1$
, and (2.4) implies

for all
$t\in (0,T_{\max })$
. By an argument similar to that used to derive (3.36), we have

This alongside (3.37) gives

which proves (3.28) in the case of
$T_{\max }\lt 2$
. If
$T_{\max }\geq 2$
, then
$\tau =1$
. By (2.5) and (2.6), we get

where
$A=(1+2C_8)^{\frac p{1+p}}e^{4C_8}$
and

are independent of
$T_{\max }$
. Therefore, (3.38) yields (3.28) in the case of
$T_{\max }\geq 2$
. The proof is completed.
4. Proof of Theorem1.1 for
$n\geq 3$
This section is devoted to proving Theorem1.1 for
$n\geq 3$
by the weighted
$L^p$
-estimates (
$p\gt 1$
). For
$M_0$
given by (2.1) and
$p\gt 1$
, we define the following positive constants

We then construct the following function to be used later.
Lemma 4.1.
Let
$p\gt 1$
,
$\Gamma _1, \Gamma _2, \Gamma _3$
,
$\chi _p$
be given by
(4.1)
and
$\chi \in (0,\chi _p)$
. Then for all
$s\in [0,M_0]$
, the function

satisfies



Proof. Clearly, (4.1) and
$\chi \in (0,\chi _p)$
imply

Hence (4.1) and (4.2) indicate that
$\varphi (s)$
increases in
$s\in [0,M_0]$
and (4.3) holds. By a simple calculation, we have

and then (4.4) is obvious. We next prove (4.5). By tedious calculations, we arrive at

where

Clearly, it follows from (4.1) that
$B_2=B_3=0$
and

This along with (4.3), (4.6) and
$p\gt 1$
proves (4.5). The proof is completed.
Now we are in a position to use the above auxiliary function as a weight function to derive the uniform bound of
$\|u(\cdot ,t)\|_{L^{p}(\Omega )}$
for all
$t\in (0, T_{\max })$
.
Lemma 4.2.
Suppose that the assumptions in Theorem
1.1
hold and
$(u, v)$
is the solution of the system
(1.6)
. Let
$p\gt 1$
,
$\Gamma _1, \Gamma _2, \Gamma _3$
,
$\chi _p$
be given by
(4.1)
,
$\chi \in (0,\chi _p)$
and
$k_{\chi ,p}$
be given by
(4.4)
. Then there exists a constant
$C(p)\gt 0$
independent of
$t$
such that

Proof. Let
$\varphi (s)$
be defined by (4.2) for
$s\in [0,M_0]$
. Then (2.1) and (4.3) show that

With integration by parts, one has

Using Young’s inequality, for all
$t\in (0,T_{\max })$
, we obtain

For the term
$I_{10}$
, it follows from (1.7) and (4.4) that

For the term
$I_{11}$
, (2.1) and (4.7) imply that

and

which along with (4.10) indicates that

The combination of (4.5), (4.8), (4.9) and (4.11) yields

for all
$t\in (0,T_{\max })$
, where
$C_2\,:\!=\, \frac {1+\sigma k_{\chi ,p} M_0}p$
. For the last term in the right-hand side of the above inequality, it follows from (4.7) and the Gagliardo–Nirenberg inequality that there exists a constant
${C_{GN}}\gt 0$
such that

where

Since
$0\lt 2\theta \lt 2$
, by Young’s inequality, (2.3) and (4.7), we obtain from (4.13) that

where

Substituting (4.14) into (4.12), one has

Solving the above inequality, using (4.7),
$u_0(x)\in W^{1,q}(\Omega )$
(recall
$q\gt n$
) and the Sobolev embedding
$W^{1,q}(\Omega )\hookrightarrow L^p(\Omega )$
, we can find two positive constants
$C_4$
and
$C_5$
satisfying

for all
$t\in (0,T_{\max })$
. This completes the proof.
5. Linear stability analysis and spatiotemporal patterns
Spatiotemporal patterns are important to understand the population distribution of biological systems. Predator–prey systems with prey-taxis can produce spatial patterns, as observed in experiments [Reference Kareiva and Odell26]. For the corresponding temporal predator–prey system of (1.1) with (1.2), hunting cooperation (1.4) can induce the Hopf bifurcations [Reference Song, Li and Song49, Reference Alves and Hilker52, Reference Wu and Zhao60]. By incorporating diffusions for both predator and prey species, the system has Turing instability only if there is hunting cooperation and the prey species spreads faster than the predator species (
$d_2\gt d_1$
). Moreover, the prey-taxis system (1.5) has no Turing patterns without hunting cooperation (i.e.,
$\alpha =0$
) [Reference Jin and Wang23]. We expect that prey-taxis will stabilize the system (1.5), similar to that observed in [Reference Peng, Yang and Zhang37] and [Reference Zhang, Fu and Huang62]. This section is devoted to investigating the effects of the interaction of prey-taxis and hunting cooperation (1.4) on the spatiotemporal distribution of population dynamics described by (1.6). We conduct linear stability analysis and perform numerical simulations to illustrate possible spatiotemporal patterns.
Without spatial structures, (1.6) becomes the following ordinary differential system

which has a trivial equilibrium
$E_0=(0,0)$
, a prey-only equilibrium
$E_1=(0,K)$
, and possible positive equilibria
$E_*=(u_*, v_*)$
solving

where
$u_*$
is the positive root of the equation

The number of positive equilibria and the linear stability of equilibria of the system (5.1) are well studied in [Reference Song, Li and Song49, Reference Wu and Zhao60]. We reorganize these results below. Define the positive constant

and the sets

Then the number of positive equilibria of the system (5.1), denoted by
$N_0$
, is

To be precise, if
$(\alpha \sigma ,K)\in S_2$
, then we denote the two positive equilibria by

It is easy to show that
$E_0=(0,0)$
is a saddle,
$E_1=({0, K})$
is linearly stable for
$0\lt K\lt 1$
and linearly unstable for
$K\gt 1$
(see also [Reference Song, Li and Song49, Theorem 2.1]). The following results on the linear stability of positive equilibria hold.
Lemma 5.1 ([Reference Song, Li and Song49, Theorem 2.2]). Let
$K_*$
be given by
(5.3)
and

-
(a) If
$(\alpha \sigma ,K)\in S_1$ , then the unique positive equilibrium
$(u_*, v_*)$ is linearly stable for
$0\lt \alpha \lt \widetilde {\alpha }_1(K)$ and linearly unstable for
$\alpha \gt \widetilde {\alpha }_1(K)$ , and the Hopf bifurcation arise from
$(u_*, v_*)$ at
$\alpha =\widetilde {\alpha }_1(K)$ .
-
(b) If
$(\alpha \sigma ,K)\in S_2$ , then
$\left (u_{2 *}, v_{2 *}\right )$ is linearly unstable, and for
$\left (u_{1 *}, v_{1 *}\right )$ , we have the following results:
-
(i) when
$\sigma \geq \frac {3}{2},\left (v_{1 *}, u_{1 *}\right )$ is linearly stable for
$\alpha \lt \widetilde {\alpha }_1(K)$ and linearly unstable for
$\alpha \gt \widetilde {\alpha }_1(K)$ , and the Hopf bifurcation arise from
$(u_*, v_*)$ at
$\alpha =\widetilde {\alpha }_1(K)$ ;
-
(ii) when
$0\lt \sigma \lt \frac {3}{2}$ and
$\widetilde {K}^*\lt K\lt 1$ ,
$\left (v_{1 *}, u_{1 *}\right )$ is linearly stable for
$\alpha \lt \widetilde {\alpha }_1(K)$ and linearly unstable for
$\alpha \gt \widetilde {\alpha }_1(K)$ , and the Hopf bifurcation arise from
$(u_*, v_*)$ at
$\alpha =\widetilde {\alpha }_1(K)$ ;
-
(iii) when
$0\lt \sigma \lt \frac {3}{2}$ and
$K_*\lt K\leq \widetilde {K}^*\lt 1$ ,
$\left (v_{1 *}, u_{1 *}\right )$ is linearly unstable.
-
5.1 Linear stability of (1.6)
Let
$\Omega \subset \mathbb {R}^{n}$
(
$n\geq 1$
) be a bounded domain with smooth boundary. We now consider the stability of the constant steady states
$E_1=(0, K)$
and
$E_*=(u_*,v_*)$
in the presence of spatial structure. The linearized system of (1.6) at a constant steady state
$E_s=(u_s,v_s)$
is

where
$\mathcal {T}$
represents the transpose,

and
$\mathcal {J}$
is the corresponding Jacobian matrix of (5.1)

By the method of separation of variables, the linear system (5.4) has solutions in the form of

where
$\psi _k(x)$
is the eigenfunction of the Neumann eigenvalue problems

with the wave number
$k$
, the coefficients
$U_k$
and
$V_k$
are given by
$(U_k,V_k)^{\mathcal {T}}=\int _\Omega \Phi (x, 0) \psi _k(x)$
, and
$\rho$
is the temporal eigenvalue satisfying

Using the above equation and the fact that the sequence
$\left \{\psi _k\right \}_{k\geq 0}$
forms an orthonormal basis of
$L^2(\Omega )$
, we know that the two eigenvalues of the matrix
$\mathcal M_k\,:\!=\, -k^2\mathcal A+\mathcal J$
are the roots of the equation

where

and

The two roots of (5.6), denoted by
$\rho _\pm$
, are given by

Lemma 5.2.
Let
$E_s=(u_s,v_s)$
be a constant steady state of the system
(1.6)
. Then the following stability results hold for
$E_s=(u_s,v_s)$
.
-
(i)
$E_s$ is linearly stable if and only if
$\min \limits _{k^2\geq 0}\left \{P_k,Q_k\right \}\gt 0$ , and
$E_s$ is linearly unstable if and only if
$\min \limits _{k^2\geq 0}\left \{P_k,Q_k\right \}\lt 0$ .
-
(ii) Turing instability arises if and only if
\begin{align*} \beta _1\lt 0,\ \beta _2\gt 0,\ \beta _3\gt 0 \quad \text {and}\quad \min \limits _{k^2\gt 0} Q_k\lt 0. \end{align*}
Proof. The first conclusion is obvious. Moreover, Turing instability arises if
$E_s=(u_s,v_s)$
is linearly stable in the ODE system (5.1), while it is unstable in the PDE system (1.6). Therefore, Turing instability occurs if and only if

Given (5.7),
$d_1,d_2\gt 0$
and
$k^2\geq 0$
, the second conclusion of Lemma 5.2 follows immediately and the proof is completed.
At
$E_1=(0, K)$
,
$J_1=K-1$
,
$J_2=0$
,
$J_3=-K\lt 0$
,
$J_4=-\sigma \lt 0$
, which imply

This indicates
$\beta _2\lt 0$
if
$\beta _3\gt 0$
. Therefore, Lemma 5.2(ii) implies that Turing instability can never arise from
$E_1=(0, K)$
. We next investigate whether Turing instability can arise from the positive constant steady state
$E_*=(u_*, v_*)$
. Let
$E_s=E_*$
. Then (5.5) implies

Clearly, (5.2) implies
$J_3=v_*-2\lt -1$
. Hence (5.8) implies

This alongside Lemma 5.2(ii) indicates that Turing instability cannot arise from
$E_*=(u_*,v_*)$
for sufficiently large
$\chi \gt 0$
.
5.2 Spatiotemporal patterns
In this subsection, we present a specific example to illustrate the above analysis. For definiteness, we let

Then the system (1.6) with (5.10) admits a unique positive constant steady state
$E_*=(u_*,v_*)=\left (\frac {\sqrt {\alpha }-1}{\alpha },\frac {1}{\sqrt {\alpha }}\right )$
if and only if
$\alpha \gt 1$
. Hence, we assume
$\alpha \gt 1$
below. We have

where

Therefore, steady-state bifurcations occur if

where

Lemma 5.3.
Let
$d_2\gt 0$
,
$\alpha \gt 1$
,
$\chi \geq 0$
,
(5.12)
hold, and the function
$\varphi _Q(s)$
be given by
(5.14)
. Then
$\beta _2\gt 0$
and
$\varphi _Q\left (\frac {\beta _2}{2d_2}\right )\lt 0$
if and only if

where

with

Moreover, it holds that

and for any
$\chi \geq 0$
, we have

Proof. Let
$d_2\gt 0$
,
$\alpha \gt 1$
and
$\chi \geq 0$
. First, (5.12) implies that
$\beta _2\gt 0$
is equivalent to

Moreover, we have from (5.12), (5.14) and (5.17) that

It holds that
$D_1^2-4D_2D_0=32 \left (\sqrt {\alpha }-1\right )^3 \left (2 \sqrt {\alpha }-1\right ) \alpha ^3 \left ((\sqrt {\alpha }-1) \chi +\alpha \right )\gt 0$
, which along with
$D_2,D_0\lt 0$
and
$D_1\gt 0$
implies that
$\varphi _*(d_2)$
has two positive roots

Clearly,
$0\lt d^*_-(\alpha ,\chi )\lt d^*_+(\alpha ,\chi )$
. We next show that

Indeed, (5.17) and (5.22) imply

hence

This along with (5.17) indicates
$d^*_{\alpha ,\chi }\lt d^*_+(\alpha ,\chi )$
. Moreover, it follows from (5.17) and (5.22) that

which proves
$d^*_-(\alpha ,\chi )\lt d^*_{\alpha ,\chi }$
. Therefore, (5.23) holds. Then the combination of (5.20)-(5.23) proves that
$\beta _2\gt 0$
and
$\varphi _Q\left (\frac {\beta _2}{2d_2}\right )\lt 0$
if and only if (5.15) holds. We next prove (5.18). Since
$D_2\lt 0$
, we have
$d^*_+(\alpha ,\chi )=-\frac {D_1}{2D_2}+\frac 12\sqrt {\frac {D_1^2-4D_2D_0}{D_2^2}}$
. Elementary calculations (omitted for brevity) show that

which along with
$D_1^2-4 D_2 D_0\gt 0$
proves (5.18). Finally, we have

and it is elementary to show that
$\lim \limits _{\alpha \rightarrow 1}d^*_+(\alpha ,\chi )=+\infty$
. Therefore (5.19) is obtained and the proof is completed.
Clearly, (5.11) implies that Hopf bifurcations may occur if
$\alpha \geq 4$
and will never occur if
$\alpha \in (1,4)$
. Lemma 5.3 alongside (5.13) indicates that steady-state bifurcations may occur if
$d_2\gt d^*_+(\alpha ,\chi )$
. Moreover, steady-state bifurcations never occur if
$0\lt d_2\lt d^*_+(\alpha ,\chi )$
. Indeed, the proof of Lemma 5.3 shows that
$\beta _2\leq 0$
if
$0\lt d_2\leq d^*_{\alpha ,\chi }$
and
$\varphi _Q\left (\frac {\beta _2}{2d_2}\right )\gt 0$
if
$d^*_{\alpha ,\chi }\lt d_2\lt d^*_+(\alpha ,\chi )$
, this alongside
$d_2,\beta _3\gt 0$
and (5.11) indicates that
$Q_k\gt 0$
for all
$k$
if
$0\lt d_2\lt d^*_+(\alpha ,\chi )$
, which means that a steady-state bifurcation is impossible. In particular, a Turing–Hopf bifurcation occurs (cf. [Reference Jiang, An and Shi21, Definition 2.1 and Remark 2.2]) if
$(\alpha ,d_2)=(4,d_\chi ^*)$
, where

The stability of
$E_*$
can be fully classified in the
$\alpha$
-
$d_2$
plane, as the following.

Figure 1. (a) Plots of
$\textrm{Re}(\rho _+)$
and
$\textrm { Im}(\rho _+)$
in terms of
$k^2\geq 0$
at
$(\alpha ,d_2)=(4,d_1^*)$
, where
$(d_1^*,k_1^*)\approx (11.2272,0.2110)$
is given by (5.24) and (5.25). (b) Turing-Hopf bifurcation diagram in the
$\alpha$
-
$d_2$
plane, where the state-steady bifurcation curve
$d_2=d^*_+(\alpha ,1)$
given by (5.16) and the Hopf bifurcation curve
$\alpha =4$
divide the region
$\{(\alpha ,d_2):\ \alpha \gt 1, d_2\gt 0\}$
into four parts: I (stable), II (Hopf), III (Turing–Hopf) and IV (Turing). Other parameters are given by (5.10) with
$\chi =1$
.
Lemma 5.4.
Let
(5.10)
hold with
$\alpha \gt 1$
and
$d_\chi ^*$
be given by
(5.24)
. Then the system
(1.6)
has a unique positive constant steady state
$E_*=(\frac {\sqrt {\alpha }-1}{\alpha },\frac {1}{\sqrt {\alpha }})$
. Moreover, the following conclusions hold.
-
(i) The ODE system (5.1) undergoes a Hopf bifurcation at
$E_*=(\frac 14,\frac 12)$ when
$\alpha =4$ .
-
(ii) The system (1.6) undergoes a Turing–Hopf bifurcation at
$E_*=(\frac 14,\frac 12)$ when
$(\alpha ,d_2)=(4,d_\chi ^*)$ . At
$(\alpha ,d_2)=(4,d_\chi ^*)$ ,
$\mathcal {M}_k$ has the eigenvalues
(5.25)\begin{align} \begin{cases} \rho _\pm =\pm \frac {i}{\sqrt {2}},\quad & \text {if }k^2=0,\\ \rho _-=-\frac {(8+3\chi ) \sqrt {6(\chi +4)}+12 \chi }{4 (3 \chi +4)}\lt 0,\ \rho _+=0,\quad & \text {if }k^2=k_\chi ^*\,:\!=\, \frac {2}{ \sqrt {6(\chi +4)}+4},\\ \textrm{Re}(\rho _\pm )\lt 0,\quad & \text {if }k^2\neq 0,k_\chi ^*. \end{cases} \end{align}
Proof. Let
$k^2=0$
in (5.6). Then
$\rho _\pm =\pm \sqrt {Q_0}=\pm \sqrt {\beta _3}=\pm \frac {i}{\sqrt {2}}$
. The first conclusion is obtained. We next prove (ii). When
$(\alpha ,d_2)=(4,d_\chi ^*)$
, we have from the proof of Lemma 5.3 that
$Q_k\geq 0$
, where “=” holds if and only if
$k^2=\frac {\beta _2}{2d_2}=\frac {2}{ \sqrt {6(\chi +4)}+4}=k_\chi ^*$
. If
$k^2=k_\chi ^*$
, then
$P_k=(d_2+1) k^2=(d_\chi ^*+1) k_\chi ^*\gt 0$
and
$Q_k=0$
, which implies
$\rho _-=-P_k=-\frac {(8+3\chi ) \sqrt {6(\chi +4)}+12 \chi }{4 (3 \chi +4)}\lt 0$
and
$\rho _+=0$
. If
$k^2\neq 0,k_\chi ^*$
, then
$P_k,Q_k\gt 0$
, and hence
$\textrm{Re}(\rho _\pm )\lt 0$
.

Figure 3. Plots of
$\textrm{Re}(\rho _+)$
and
$\textrm { Im}(\rho _+)$
for
$k=\frac m{20}$
with
$m=0,1,2,\cdots$
under the parameter setting (5.10) with
$\chi =1$
,
$d_2=20$
and different values of
$\alpha$
: (a)
$\alpha =3$
; (b)
$\alpha =6$
; (c)
$\alpha =30$
.

Figure 4. Numerical simulations generated by the system (1.6) in the interval
$\Omega =(0,20\pi )$
with (5.10),
$\chi =1$
,
$d_2=20$
, and different values of
$\alpha$
shown in the columns: (a)
$\alpha =3$
; (b)
$\alpha =6$
; (c)
$\alpha =30$
. The initial data
$(u_0, v_0)$
are set as a small random perturbation of the positive constant steady state
$(u_*,v_*)=(\frac {\sqrt {\alpha }-1}{\alpha },\frac {1}{\sqrt {\alpha }})$
.
For clarity, we shall first discuss a special case
$\chi =1$
and then turn to the general case
$\chi \geq 0$
.
Remark 5.1.
Fig.
1
gives an illustration for Lemma 5.4 with
$\chi =1$
. Since
(5.9)
implies
$\textrm{Re}(\rho _-)\leq \textrm{Re}(\rho _+)$
, we only show the real and imaginary parts of
$\rho _+$
in Fig.
1
(a). Moreover, in the
$\alpha$
-
$d_2$
plane, the Hopf bifurcation curve
$\alpha =4$
and the steady state bifurcation curve
$d_2=d^*_+(\alpha ,1)$
given by Lemma 5.3 divide the region
$\left \{(\alpha ,d_2):\ \alpha \gt 1, d_2\gt 0\right \}$
into four parts: I (stable), II (Hopf), III (Turing–Hopf) and IV (Turing).

Figure 5. Turing–Hopf bifurcation diagram within the region
$\{(\alpha ,d_2):\ \alpha \gt 1, d_2\gt 0\}$
in the
$\alpha$
-
$d_2$
plane for the system (1.6) with (5.10) and
$\chi \in \{0,1,5,10\}$
. When
$(\alpha , d_2)$
is above the steady state bifurcation curve
$d_2=d^*_+(\alpha ,\chi )$
, which given by (5.16) is higher as
$\chi \gt 0$
is larger, the Turing instability (resp. Hopf–Turing instability) will occur if
$(\alpha , d_2)$
is left (resp. right) to the vertical Hopf bifurcation line
$\alpha =4$
.
For numerical simulations, we let

We begin with the subcritical case
$d_2\lt 8$
, for which the steady-state bifurcation will never occur (see Figure 1(b) where the horizontal asymptote
$d_2=8$
is below the steady state bifurcation curve
$d_2=d^*_+(\alpha ,1)$
). Without loss of generality, we take
$d_2=5$
. Then for
$\alpha \in (0,4)$
,
$(\alpha ,5)$
belongs to the stable region I. In this case,
$(u_*,v_*)$
is linearly stable and no patterns will arise. For the Hopf region II, we take
$\alpha =d_2=5$
, and then the system (1.6) can generate spatially homogeneous time-periodic patterns, as shown in Figure 2. We next consider the supercritical case
$d_2\gt 8$
. Without loss of generality, we take
$d_2=20$
and
$\alpha =3,6,30$
. This gives

For these three values of
$(\alpha ,d_2)$
, the eigenvalues
$\rho _+$
of
$\mathcal {M}_k$
with
$k=\frac {m\pi }L=\frac m{20}$
,
$m=0,1,2,\cdots$
, are shown in Figure 3, and the corresponding numerical simulations are shown in Figure 4. Clearly, for
$(\alpha ,d_2)=(3,20)$
in the Turing instability region IV, Figure 3(a) shows that the eigenvalues of
$\mathcal M_k$
with
$m=0,1,2,3$
are a pair of complex conjugate numbers with negative real parts, and all other eigenvalues of
$\mathcal M_k$
with
$m=4,5,6,\cdots$
are real, and
$\rho _+$
changes from negative to positive at
$m=5$
. This indicates that there is a steady-state bifurcation but no Hopf bifurcation. The numerical simulations in Figure 4(a) show that non-constant stationary patterns arise, which is aligned with our analysis. For
$(\alpha ,d_2)$
in the Turing–Hopf instability region III, the system (1.6) is unstable under temporal perturbation due to Hopf bifurcation and complex eigenvalues of
$\mathcal M_0$
have positive real parts (see Figure 3(b) and Figure 3(c) at
$m=0$
), and the system (1.6) also undergoes Turing instability with real parts of an eigenvalue changing from negative to positive for some
$k\neq 0$
(see Figure 3(b) with
$m=6$
and Figure 3(c) with
$m=7$
for instance). The interaction of Hopf and state-steady bifurcations will result in various complex patterns in the Turing–Hopf instability region III. For
$(\alpha ,d_2)=(6,20)\in \textrm{III}$
, spatiotemporal periodic patterns are observed, as shown in Figure 4(b). However, if we keep the diffusion rate
$d_2=20$
and increase the strength of hunting cooperation to
$\alpha =30$
, then chaotic oscillatory patterns appear as shown in Figure 4(c).
The above analysis is performed for
$\chi =1$
. We next consider
$\chi \geq 0$
and explain how prey-taxis stabilizes the positive constant steady state. Clearly, (5.18) and (5.19) indicate that
$d^*_+(\alpha ,\chi )$
strictly increases with respect to
$\chi \in [0,+\infty )$
, with two asymptotes:
$\alpha =1$
and
$d_2=8$
in the
$\alpha$
-
$d_2$
plane. Figure 5 gives an illustration for
$\chi =0,1,5,10$
, where the solid blue curve
$d_2={d^*_+(\alpha ,1)}$
and the red vertical line
$\alpha =4$
have been shown in Figure 1(b). The vertical coordinate of the intersection of
$d_2={d^*_+(\alpha ,\chi )}$
and
$\alpha =4$
is
$d_\chi ^*$
given by (5.24). The steady state bifurcation curve
$d^*_+(\alpha ,\chi )$
strictly increases in
$\chi \in [0,+\infty )$
for
$\alpha \gt 1$
(see (5.18)), while the area of stable region increases with respect to
$\chi \in [0,+\infty )$
, see Figure 5 for
$\chi \in \{0,1,5,10\}$
for instance. This indicates that prey-taxis plays a role in stabilizing the positive constant steady states.
As demonstrated above, the system (1.6) with
$\chi \geq 0$
and
$\alpha \gt 0$
may generate various spatiotemporal patterns, including spatially homogeneous time-periodic patterns, non-constant stationary patterns, spatially inhomogeneous time-periodic patterns and chaos. The former two types of patterns are also found in [Reference Capone, Maria Francesca Carfora and Torcicollo6, Reference Singh, Dubey and Mishra47, Reference Wu and Zhao60], where the latter two types of patterns result from the interaction of Hopf and state-steady bifurcations in the Turing–Hopf region. Moreover, we find that prey-taxis plays a stabilizing role in terms of pattern formation, which is similar to the case that the hunting cooperation functional response function adopts the Type II form [Reference Peng, Yang and Zhang37, Reference Zhang, Fu and Huang62].
Acknowledgements
The authors are grateful to the anonymous referees for their careful reading of this manuscript and valuable comments, which helped improve the precision and exposition of our results.
Financial support
The research of W. Tao was partially supported by the National Natural Science Foundation of China (No. 12201082), Start-up Research Fund of Southeast University (No. RF1028624193), PolyU Postdoc Matching Fund Scheme Project ID P0030816/B-Q75G, 1-W15F and 1-YXBT. The research of Z.-A. Wang was partially supported by the NSFC/RGC Joint Research Scheme sponsored by the Research Grants Council of Hong Kong and the National Natural Science Foundation of China (Project No.
$\mathrm {N}_{-}$
PolyU509/22) and an internal grant (no. 1-WZ03) from the Hong Kong Polytechnic University.
Competing interests
The authors declare that they have no competing interests.