2. Steady state bifurcation analysis

In this section, we perform a bifurcation analysis to demonstrate the existence of non-constant steady-state solutions, thereby showing that the system can generate stable spatial patterns under suitable conditions. The main idea is to translate the problem into an equivalent linear algebra setting and carry out the analysis there. In [Reference Crandall and Rabinowitz10], this approach is applied to a two–component system, where the corresponding algebra is simpler; for instance, the determinant of a $2 \times 2$ matrix has a closed-form expression, unlike the $3 \times 3$ case considered here. Following the framework of [Reference Crandall and Rabinowitz10], we emphasize the additional steps needed to address these higher–dimensional algebraic challenges.

For the sake of simplicity, we shift the scalar fields in system (E) using the steady state (SS) by setting

\begin{equation*} \tilde A(\textbf {x}, t)\;:\!=\;A(\textbf {x}, t)-\bar A, \quad \tilde \rho (\textbf {x}, t)\;:\!=\;\rho -\bar \rho , \quad \tilde u(\textbf {x}, t)\;:\!=\;u(\textbf {x}, t)-\bar u. \end{equation*}

and collect the following the equivalent system for $(\bar {A}, \bar {\rho }, \bar {u})$

(ME) \begin{align} \left \{ \begin{aligned} \frac {\partial \tilde {A}}{\partial t}=&\,D_A\Delta \tilde {A} - \tilde {A}+\tilde {A}\tilde {\rho } +\bar {\rho }\tilde {A}+ \bar {A}\tilde {\rho }+\bar {A}\bar {\rho }+\alpha , &&\text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial \tilde {\rho }}{\partial t}=&\,\nabla \cdot (D_\rho \nabla \tilde {\rho } - \frac {2(\tilde {\rho }+\bar {\rho })}{\tilde {A}+\bar {A}}\nabla \tilde {A})&&\\[5pt] &- \tilde {A} \tilde {\rho }-\bar {A} \tilde {\rho }-\bar {\rho }\tilde {A}-\tilde {\rho }\tilde {u}-{\bar {u}}\tilde {\rho }-\bar {\rho }\tilde {u}+\beta -\bar {\rho }({\bar {u}}+\bar {A}), &&\text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial \tilde {u}}{\partial t}=&\,\nabla \cdot \left(D_u \nabla \tilde {u} - \frac {\chi (\tilde {u}+{\bar {u}})}{\tilde {A}+\bar {A}}\nabla \tilde {A}\right), &&\text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial \tilde A}{\partial \textbf {n}}=&\, \frac {\partial \tilde \rho }{\partial \textbf {n}}= \frac {\partial \tilde u}{\partial \textbf {n}}=0, &&\text{ on }\partial \Omega . \end{aligned} \right . \end{align}

This new system (ME) has a shifted equilibrium $\mathbf{0}\;:\!=\;(0, 0, 0)$ , and dropping tildes we obtain

(MP) \begin{equation} \left \{ \begin{aligned} \frac {\partial A}{\partial t}=&\,D_A\Delta A - A +A\rho +\left (1-\frac {\alpha }{\lambda }\right )A+\lambda \rho , &&\quad \text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial \rho }{\partial t}=&\,\nabla \cdot \Big (D_\rho \nabla \rho - \frac {2\left (\rho +\left (1-\frac {\alpha }{\lambda }\right )\right )}{A+\lambda }\nabla A\Big )- A \rho -\lambda \rho &&\\[5pt] &-\left (1-\frac {\alpha }{\lambda }\right )A-\rho u-\rho \lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )-u\left (1-\frac {\alpha }{\lambda }\right ), &&\quad \text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial u}{\partial t}=&\,\nabla \cdot \Big (D_u \nabla u - \frac {\chi \left (u+\lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )\right )}{A+\lambda }\nabla A\Big ), &&\quad \text{ in }\Omega \times (0, T], \\[5pt] \frac {\partial A}{\partial \textbf {n}}=&\, \frac {\partial \rho }{\partial \textbf {n}}= \frac {\partial u}{\partial \textbf {n}}=0, &&\quad \text{ on }\partial \Omega . \end{aligned} \right . \end{equation}

We now aim to study the steady-state solutions of system (MP), and to this end, we introduce the operator $\mathcal F$ as follows

(2.0.1) \begin{equation} \begin{split} &\mathcal F(\chi , A, \rho , u)\\[5pt] \;:\!=\;&\begin{bmatrix} D_A\Delta A+A\rho -\frac {\alpha }{\lambda }A+\lambda \rho \\[5pt] \nabla \cdot \left [D_\rho \nabla \rho - \frac {2\left (\rho +\left (1-\frac {\alpha }{\lambda }\right )\right )}{A+\lambda }\nabla A\right ]- A \rho -\lambda \rho -\left (1-\frac {\alpha }{\lambda }\right )A-\rho u-\rho \lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )-u\left (1-\frac {\alpha }{\lambda }\right )\\[5pt] \nabla \cdot \left [D_u \nabla u - \frac {\chi \left (u+\lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )\right )}{A+\lambda }\nabla A\right ] \end{bmatrix}. \end{split} \end{equation}

Then, $\mathcal F(\chi , \mathbf{0})=0$ for any $\chi \in \mathbb{R}$ , and we are motivated to find nontrivial equilibria of (MP) that bifurcate from the trivial one. It is equivalent to solving the following problem

(EP) \begin{equation} \mathcal F(\chi , A, \rho , u)=0, \quad \chi \in \mathbb R,\quad (A, \rho , u)\in \mathcal Y, \end{equation}

where

\begin{equation*} \mathcal Y=\left \{(A, \rho , u)\in [H^2(\Omega )]^3\Big |\;\frac {\partial A}{\partial \textbf {n}}=\frac {\partial \rho }{\partial \textbf {n}}=\frac {\partial u}{\partial \textbf {n}}=0\text{ on }\partial \Omega , \, \int _\Omega u d\textbf {x}=0\right \}. \end{equation*}

Indeed, any root of $\mathcal{F} = 0$ is known to be a weak solution of (2.0.1), and standard elliptic regularity theory then ensures that this weak solution is, in fact, classical and smooth.

We now state the main bifurcation theorem used in this section. The original local result is due to Crandall and Rabinowitz [Reference Crandall and Rabinowitz10, Theorem 1.7], and it was later extended to a global bifurcation result in [Reference Shi and Wang45, Theorem 4.3]. Part (e), while not stated explicitly in either theorem, concerns the global continuation and the Fredholm property of the linearized operator. For full details, we refer the reader to these references. Here, we present a version adapted to our setting; see also [Reference Cantrell, Cosner and Manásevich8].

We will show that the conditions of Theorem2.1 are satisfied for $\mathcal{F}=F$ in (EP), $\mathcal{Y}=Y$ , $\mathcal{Z}=Z$ and $\mathcal{V}=V$ defined as follows

\begin{equation*} V=\left \{(\chi , A, \rho , u)\in \mathbb{R}\times \mathcal Y|\; A\gt -\lambda , \, \rho \gt \frac {\alpha }{\lambda }-1, \, u\gt \lambda \left (1-\frac {\beta }{\lambda -\alpha }\right )\right \}, \end{equation*}

and $Z\;:\!=\;[L^2(\Omega )]^3$ .

Now that $\mathcal F(\chi , \textbf {0})=0$ holds for all $\chi \in \mathbb R$ , to look for nonconstant solutions, one first needs the implicit function theorem to fail at this trivial location. For this purpose, we consider the following eigenvalue problem

(LN) \begin{equation} \Delta \phi +\mu \phi =0 \text{ in }\Omega , \text{ with } \partial _{\textbf {n}} \phi =0 \text{ on }\partial \Omega \quad \text{ and } \Vert \phi \Vert _{L^2(\Omega )}=1. \end{equation}

It is well known that its eigen pairs $\lt \mu _j, \phi _j\gt$ consist of a sequence of real, non-negative and diverging eigenvalues:

\begin{equation*}0 = \mu _0 \lt \mu _1 \leq \mu _2 \leq \ldots \to \infty , \end{equation*}

and the eigenfunction set $ \{\phi _j\}_{j=0}^\infty \subset H^1(\Omega )$ form a complete orthonormal basis of $ L^2(\Omega )$ . To apply the bifurcation from simple eigenfunctions, we assume that $\mu$ has algebraic multiplicity one. Then, $y_0$ in Theorem2.1 is relabelled as $\textbf {P}(\textbf {x})$ and defined as follows

(2.0.2) \begin{equation} \begin{split} \textbf {P}(\textbf {x}) =\left (1, \frac {1}{\lambda }\left ( D_A\mu +\frac {\alpha }{\lambda }\right ), \frac {(2\mu -\lambda )(\lambda -\alpha )^2-(D_A\lambda \mu +\alpha )(D_\rho \mu (\lambda -\alpha )+\beta \lambda )}{\lambda (\lambda -\alpha )^2}\right )\phi (\textbf {x}). \end{split} \end{equation}

The associated linear functional on $Y$ is then

\begin{equation*} \ell \varphi =\int _\Omega \varphi \cdot \textbf {P}(\textbf {x}), \end{equation*}

which allows us to define the closed complement $\mathcal{W}=W$

\begin{equation*} W=\{\varphi \in Y|\ell \varphi =0\}. \end{equation*}

Using the definitions above and Theorem 1.7 in [Reference Crandall and Rabinowitz10], we extend Theorems2.2 and 2.6 in [Reference Cantrell, Cosner and Manásevich8] as follows.

Theorem 2.2. Let $\mu \gt 0$ be a generic and simple eigenvalue of ( LN ). Denote

(2.0.3) \begin{equation} \chi = \overbrace { -\frac {D_u}{(\beta +\alpha -\lambda )}\left [\left (\lambda -\alpha +\frac {\alpha \beta }{\lambda -\alpha }\right )+\mu \left ({-}2\left (1-\frac {\alpha }{\lambda }\right )+\frac {D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right )+\mu ^2D_AD_\rho \right ]}^{\triangleq \chi _0} \end{equation}

and assume that

\begin{align*} \frac {(D_u-\chi _0)(\alpha ^2+\alpha (\beta -2\lambda )+\lambda ^2)-\beta \lambda \chi _0}{\mu (\lambda -\alpha )}\ \end{align*}

is not eigenvalue of ( LN ). Then, a branch of spatially nonconstant solutions of $\mathcal F$ bifurcates from the equilibrium $(\bar {A}, \bar {\rho }, \bar {u})$ at $\chi =\chi _0$ . In a neighbourhood of the bifurcation point, the bifurcating branch can be parametrized as $(A, \rho , u)(\textbf {x};\,s)=(\bar {A}, \bar {\rho }, \bar {u})+s\textbf {P}(\textbf {x})+s^2\textbf {Q}(\textbf {x};\,s)$ with $\textbf {P}$ given by ( 2.0.2 ) and $\textbf {Q}(\textbf {x};\,s)\in W$ for any $s\in ({-}\epsilon , \epsilon )$ , and $\chi (0)=\chi _0$ . Furthermore, the bifurcation branch is part of a connected component $\mathcal{C}$ of the set $\bar {\mathcal{S}}$ , where $\mathcal{S}=\{(\chi , A, \rho , u)\,:\,(\chi , A-\bar {A}, \rho -\bar {\rho }, u-\bar {u})\in V\, |\, \mathcal F(\chi , A-\bar {A}, \rho -\bar {\rho }, u-\bar {u})=0,$ $(A, \rho , u)\not =(\bar {A}, \bar {\rho }, \bar {u})\}$ , and $\mathcal{C}$ either is not compact or contains point $(\chi ^*, \bar {A}, \bar {\rho }, \bar {u})$ with $\chi ^*\not =\chi _0$ .

Mathematically, the value $\chi _0$ marks the point at which the homogeneous steady state loses stability and new nontrivial steady states emerge through bifurcation. From a criminological perspective, this corresponds to a tipping point in policing intensity: below $\chi _0\gt 0$ , police and offenders distribute uniformly in space; however, once $\chi _0$ is exceeded, stable, spatially inhomogeneous patterns arise, which may manifest as persistent crime hotspots despite ongoing policing efforts. This seems counterintuitive. However, one could explain this by noting that high concentrations of $u$ may lead to a local decrease in $\rho$ and $A$ , thereby displacing these scalar fields elsewhere. Then, $u$ would follow the gradient, displacing hotspots again. In this way, one can obtain temporally varying solutions as well. At the same time, such a paradox may highlight the modelling limitations of the system and call for further refinement. There is also another explanation, as we unravel the expression for $\chi _0$ . For a fixed $\mu$ , which essentially represents geometry, the positivity of $\chi _0$ is dependent on the coefficient in front of $\mu$ in (2.0.3). $\chi _0$ is proportional to $D_u$ . Hence, more police “spread” requires more “concentrated movement” to generate a pattern and vice versa. Thus, to eliminate any clusters, the police agents need to increase their diffusion or lower their concentration intensity. The relationship between $\chi _0$ and other parameters is more convoluted, but one could observe that higher values of $D_A$ and $D_\rho$ would lead to the fact that there is no $\mu \gt 0$ for which $\chi _0\gt 0$ . Thus, again, patterns cannot be formed at least from the initial constant steady state. The relationship will be more illustrative in the later chapter, where we perform numerical simulations and parameter explorations.

2.1. Identification of bifurcation points

To apply the Crandall–Rabinowitz bifurcation theory [Reference Crandall and Rabinowitz10, Reference Shi and Wang45], we first note that $\mathcal F$ is Fréchet differentiable and its functional derivative at $(A, \rho , u)$ with $\textbf {v}\;:\!=\;(v_1, v_2, v_3)$ is given by

(2.1.1) \begin{equation} \begin{split} &D\mathcal F_{(A, \rho , u)}(\chi , A, \rho , u)[\textbf {v}]\\[5pt] =&\, \begin{bmatrix} D_A \Delta v_1 + \Bigl (\rho - \frac {\alpha }{\lambda }\Bigr )v_1 + (A+\lambda )\, v_2 \\[1em] \nabla \cdot \Biggl [ D_\rho \nabla v_2 - \frac {2v_2}{A+\lambda }\,\nabla A - 2\Bigl (\rho +1-\frac {\alpha }{\lambda }\Bigr ) \left ( \frac {\nabla v_1}{A+\lambda } - \frac {v_1 \nabla A}{(A+\lambda )^2} \right ) \Biggr ] \\[1em] \quad -\Bigl (\rho +1-\frac {\alpha }{\lambda }\Bigr )\, v_1 - \left (A+u+\frac {\lambda \beta }{\lambda -\beta }\right ) v_2 - \Bigl (\rho +1-\frac {\alpha }{\lambda }\Bigr ) v_3 \\[1em] \nabla \cdot \Biggl [ D_u \nabla v_3 - \frac {\chi v_3}{A+\lambda }\,\nabla A - \chi \left ( u + \lambda \Bigl (\frac {\beta }{\lambda -\alpha }-1\Bigr ) \right ) \left ( \frac {\nabla v_1}{A+\lambda } - \frac {v_1 \nabla A}{(A+\lambda )^2} \right ) \Biggr ] \end{bmatrix}. \end{split} \end{equation}

One can continue to show that $\frac {d}{d\chi }D\mathcal F_{(A, \rho , u)}(\chi , A, \rho , u)[\textbf {v}]$ exists and is continuous. To fail the implicit function theorem at $(\chi , \mathbf{0})$ , we evaluate (2.1.1) the following way

(2.1.2) \begin{equation} \begin{split} &D\mathcal F_{(A, \rho , u)}(\chi , \textbf {0})[\textbf {v}]\\[5pt] =&\, \begin{bmatrix} D_A\Delta v_1-\frac {\alpha }{\lambda }v_1+\lambda v_2\\[0.5em] D_\rho \Delta v_2-\frac {2}{\lambda }\left (1-\frac {\alpha }{\lambda }\right )\Delta v_1-\left (1-\frac {\alpha }{\lambda }\right )v_1-\frac {\lambda \beta }{\lambda -\alpha }v_2-\left (1-\frac {\alpha }{\lambda }\right )v_3\\[0.5em] D_u\Delta v_3-\chi \left (\frac {\beta }{\lambda -\alpha }-1\right )\Delta v_1 \end{bmatrix}. \end{split} \end{equation}

Then we are to look for nontrivial solutions of the following equation

(LE) \begin{align} \left \{ \begin{aligned} &D_A\Delta v_1-\frac {\alpha }{\lambda }v_1+\lambda v_2=0, &&\quad \text{ in }\Omega , \\[5pt] &D_\rho \Delta v_2-\frac {2}{\lambda }\left (1-\frac {\alpha }{\lambda }\right )\Delta v_1-\left (1-\frac {\alpha }{\lambda }\right )v_1-\frac {\lambda \beta }{\lambda -\alpha }v_2-\left (1-\frac {\alpha }{\lambda }\right )v_3=0, &&\quad \text{ in }\Omega , \\[5pt] &D_u\Delta v_3-\chi \left (\frac {\beta }{\lambda -\alpha }-1\right )\Delta v_1=0, &&\quad \text{ in }\Omega , \\[5pt] &\frac {\partial v_1}{\partial \textbf {n}}= \frac {\partial v_2}{\partial \textbf {n}}= \frac {\partial v_3}{\partial \textbf {n}}=0, &&\quad \text{ on }\partial \Omega . \end{aligned} \right . \end{align}

We test each equation with $\phi$ and then apply integration by parts to obtain

(2.1.3) \begin{equation} \overbrace { \begin{bmatrix} -D_A\mu -\frac {\alpha }{\lambda }&\lambda &0\\[0.5em] \left (\frac {2\mu }{\lambda }-1\right )\left (1-\frac {\alpha }{\lambda }\right )&-D_\rho \mu -\frac {\beta \lambda }{\lambda -\alpha }&-\left (1-\frac {\alpha }{\lambda }\right )\\[0.5em] \mu \chi \left (\frac {\beta }{\lambda -\alpha }-1\right )&0&-D_u\mu \end{bmatrix} }^{\triangleq H} \begin{bmatrix} \int _\Omega v_1\phi \\[5pt] \int _\Omega v_2\phi \\[5pt] \int _\Omega v_3\phi \end{bmatrix} = \begin{bmatrix} 0 \\[5pt] 0 \\[5pt] 0 \end{bmatrix} . \end{equation}

Then the existence of nontrivial solutions of (LE) will in turn give us nontrivial solutions for (2.1.3), where $H$ is such that $\int _\Omega D\mathcal F_{(A, \rho , u)}(\chi , \textbf {0})[\phi \textbf {v}]=H \int _\Omega \phi \textbf {v}$ . That said, matrix $H$ must be non-invertible such that

\begin{equation*}-D_u\mu \left (D_A\mu +\frac {\alpha }{\lambda }\right )\left (D_\rho \mu +\frac {\beta \lambda }{\lambda -\alpha }\right )+ D_u\lambda \mu \left (\frac {2\mu }{\lambda }-1\right )\left (1-\frac {\alpha }{\lambda }\right ) -\lambda \mu \chi \left (1-\frac {\alpha }{\lambda }\right )\left (\frac {\beta }{\lambda -\alpha }-1\right )=0\end{equation*}

or equivalently when $\chi$ is given by (2.0.3).

This analysis identifies the critical bifurcation values of $\chi$ , representing the policing intensity, that mark the transition from homogeneous to patterned states, as determined by the linear stability analysis of the constant solution (SS). Moreover, when $\chi = \chi _0$ , it follows directly from (2.1.3) that the kernel of $D\mathcal{F}(\chi _0, \mathbf{0})$ is one-dimensional and is spanned by $\mathbf{P}$ defined in (2.0.2).

To proceed further, we verify Agmon’s condition following [Reference Cantrell, Cosner and Manásevich8, Reference Shi and Wang45]. Define the principal part of the elliptic operator $F(\chi , A, \rho , u)$ and $D\mathcal F_{(A, \rho , u)}(\chi , A, \rho , u)$

\begin{align*} A_1(\chi , A, \rho , u)=\begin{bmatrix} D_A&0&0\\[0.5em] -2\frac {\rho +\left (1-\frac {\alpha }{\lambda }\right )}{A+\lambda }&D_\rho &0\\[0.5em] -\chi \frac {u+\lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )}{A+\lambda }&0&D_\rho \end{bmatrix}. \end{align*}

More importantly, we need to look at the determinant $A_1(\chi , A, \rho , u)+\sigma I$ , $\sigma \in \mathbb{C}$

\begin{align*} \begin{vmatrix} D_A+\sigma &0&0\\[0.5em] -2\frac {\rho +\left (1-\frac {\alpha }{\lambda }\right )}{A+\lambda }&D_\rho +\sigma &0\\[0.5em] {-\chi \frac {u+\lambda \left (\frac {\beta }{\lambda -\alpha }-1\right )}{A+\lambda }}&0&D_u+\sigma \end{vmatrix}=(D_A+\sigma )(D_\rho +\sigma )(D_u+\sigma ). \end{align*}

The later is nonzero when $\sigma =0$ or $\arg \sigma \in [-\pi /2, \pi /2]$ . This, in turn, implies that the operator $D\mathcal F_{(A, \rho , u)}(\chi , A, \rho , u)$ is a Fredholm operator with index 0 and $\textrm {ran}(D\mathcal F_{(A, \rho , u)}(\chi _0, \mathbf{0}))$ has a codimension of 1.

2.2. Transversality and steady-state bifurcation

We now verify that bifurcation does occur at $\chi _0$ given by (2.0.3) by proving the following transversality condition

$$\begin{equation*}\frac {d}{d\chi}D\mathcal F_{(A, \rho , u)}(\chi _0, \mathbf{0})[\textbf {P}(\textbf {x}) ]\not \in {ran}(D\mathcal F_{(A, \rho , u)}(\chi _0, \mathbf{0})).\end{equation*}$$

We argue by contradiction and assume that there exists nonzero $\hat{\mathbf{v}}\;:\!=\;(\hat v_1, \hat v_2, \hat v_3)$ such that

\begin{equation*}D\mathcal F_{(A, \rho , u)} (\chi , \mathbf{0})[\hat{\mathbf v}]=\frac {d}{d\chi }D\mathcal F_{(A, \rho , u)}(\chi , \mathbf{0})[\textbf {P}(\textbf {x}) ].\end{equation*}

Since

\begin{align*} \frac {d}{d\chi }D\mathcal F_{(A, \rho , u)}(\chi _0, \mathbf{0})[\textbf {P}(\textbf {x}) ]=\begin{bmatrix} 0\\[5pt] 0\\[5pt] \mu \left (\frac {\beta }{\lambda -\alpha }-1\right )\phi \end{bmatrix}, \end{align*}

we collect the following system

(S₁) \begin{equation} \left \{ \begin{aligned} &D_A\Delta \hat v_1-\frac {\alpha }{\lambda }\hat v_1+\lambda \hat v_2=0, &&\text{in }\Omega , \\[5pt] &D_\rho \Delta \hat v_2-\frac {2}{\lambda }\left (1-\frac {\alpha }{\lambda }\right )\Delta \hat v_1-\left (1-\frac {\alpha }{\lambda }\right )\hat v_1-\frac {\lambda \beta }{\lambda -\alpha }\hat v_2-\left (1-\frac {\alpha }{\lambda }\right )\hat v_3 =0, &&\text{in }\Omega , \\[5pt] &D_u\Delta \hat v_3-\chi _0 \left (\frac {\beta }{\lambda -\alpha }-1\right )\Delta \hat v_1=\mu \left (\frac {\beta }{\lambda -\alpha }-1\right )\phi , &&\text{in }\Omega , \\[5pt] &\frac {\partial \hat v_1}{\partial \textbf {n}}=\frac {\partial \hat v_2}{\partial \textbf {n}}=\frac {\partial \hat v_3}{\partial \textbf {n}}=0, &&\text{on }\partial \Omega . \end{aligned} \right . \end{equation}

We test (S₁ ) by $\phi$ and then collect the following identity using the fact that $\Vert \phi \Vert _{L^2}=1$

\begin{align*} \begin{bmatrix} -D_A\mu -\frac {\alpha }{\lambda }&\lambda &0\\[0.5em] \left (\frac {2\mu }{\lambda }-1\right )\left (1-\frac {\alpha }{\lambda }\right )&-D_\rho \mu -\frac {\beta \lambda }{\lambda -\alpha }&-\left (1-\frac {\alpha }{\lambda }\right )\\[0.5em] \mu \chi _0\left (\frac {\beta }{\lambda -\alpha }-1\right )&0&-D_u\mu \end{bmatrix} \begin{bmatrix} \int _\Omega \hat v_1\phi \\[5pt] \int _\Omega \hat v_2\phi \\[5pt] \int _\Omega \hat v_3\phi \end{bmatrix} = \begin{bmatrix} 0 \\[5pt] 0 \\[5pt] \mu \left (\frac {\beta }{\lambda -\alpha }-1\right ) \end{bmatrix} . \end{align*}

However, this reaches a contradiction to (2.1.3) since $H$ therein is non-invertible with $\chi =\chi _0$ . This verifies the transversality condition, and Theorem2.2 follows from those in [Reference Crandall and Rabinowitz10].

3. Stability analysis of the bifurcating steady states

In this section, we establish conditions for the stability of spatially heterogeneous patterns. Unlike previous analyses, our approach explicitly incorporates the geometry of the domain. Nevertheless, the results remain applicable to a broad class of domains, including discs. Compared to [Reference Cantrell, Cosner and Manásevich8], the algebra in our setting is more involved because it includes cubic polynomials. We carefully work through these terms to obtain a general result. To this end, we introduce the following cubic equation in $\sigma$ , which is a characteristic equation of matrix $H$ in (2.1.3) The characteristic equation is given as:

(3.0.1) \begin{equation} \sigma ^3+a_2(\mu )\sigma ^2+a_1(\mu )\sigma ^1+a_0(\mu ,\chi )=0, \end{equation}

where

(3.0.2) \begin{equation} \begin{split} a_2(\mu )\;:\!=\;&\frac {\alpha }{\lambda }+\frac {\beta \lambda }{\lambda -\alpha }+\mu \left (D_A+D_\rho +D_u\right ), \\[5pt] a_1(\mu )\;:\!=\;&\left (\lambda -\alpha \right )+\frac {\alpha \beta }{\lambda -\alpha }+\mu \left [-2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }+D_u\left (\frac {\beta \lambda }{\lambda -\alpha }+\frac {\alpha }{\lambda }\right )\right ]\\[5pt] &\quad +\mu ^2\left (D_AD_\rho +D_AD_u+D_\rho D_u\right ), \\[5pt] a_0(\mu ,\chi )\;:\!=\;&D_u\mu \biggl \{-\left [\mu _*\left ({-}2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right )+\mu _*^2D_AD_\rho \right ]\\[5pt] &\quad +\mu \left [-2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right ] +\mu ^2D_AD_\rho \biggr \}. \end{split} \end{equation}

We are going to explore when the eigenvalues of $H$ have positive real parts. We will apply Routh–Hurwitz criterion, where we need to look at the polynomial equation $a_2(\mu )a_1(\mu )-a_0(\mu ,\chi )=0$

(3.0.3) \begin{equation} \begin{split} 0=&\,\mu ^0\biggl \{\left (\frac {\alpha }{\lambda }+\frac {\beta \lambda }{\lambda -\alpha }\right )\left [\left (\lambda -\alpha \right )+\frac {\alpha \beta }{\lambda -\alpha }\right ]\biggr \} +\mu ^1\biggl \{\left (D_A+D_\rho +D_u\right )\left (\left (\lambda -\alpha \right )+\frac {\alpha \beta }{\lambda -\alpha }\right )\\[5pt] &+\left (\frac {\alpha }{\lambda }+\frac {\beta \lambda }{\lambda -\alpha }\right )\left [-2\left (1-\frac {\alpha }{\lambda }\right )+\frac {D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }+D_u\left (\frac {\beta \lambda }{\lambda -\alpha }+\frac {\alpha }{\lambda }\right )\right ]\\[5pt] &+\mu _*\left [\left ({-}2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right )+\mu _* D_AD_\rho \right ]\biggr \}\\[5pt] &+\mu ^2\biggl \{\left (D_A+D_\rho \right )\left [-2\left (1-\frac {\alpha }{\lambda }\right )+\frac {D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right ]+\left [\left (D_A+D_\rho +D_u\right )\left (\frac {\beta \lambda }{\lambda -\alpha }+\frac {\alpha }{\lambda }\right )\right ]\\[5pt] &+\left (\frac {\alpha }{\lambda }+\frac {\beta \lambda }{\lambda -\alpha }\right )\left (D_AD_\rho +D_AD_u+D_\rho D_u\right )\biggr \}\\[5pt] &+\mu ^3\biggl \{\left (D_A+D_\rho \right )\left (D_A+D_u\right )\left (D_\rho +D_u\right )\biggr \}\\[5pt] & = C\left (\mu -\mu _1\right )\left (\mu -\mu _2\right )\left (\mu -\mu _3\right ), \end{split} \end{equation}

where $\mu _i$ denote the roots of (3.0.3). At least one of these roots must be negative; without loss of generality, we denote this root by $\mu _3$ . With this set-up, we are ready to state the next result.

Theorem 3.1. Suppose that $\mu$ is the eigenvalue of $-\Delta$ appearing in Theorem 2.2 with normalized eigenfunction $\phi$ . Suppose that the hypotheses of Theorem 2.2 are satisfied. Assume that $\int _\Omega \phi ^3\not =0$ and $\beta \not =-C_2/C_1$ , where

\begin{align*} \begin{split} C_1=- \lambda \left (\chi _0-D_u\right ) \left ({-}\alpha \chi _0+2 D_A D_u\lambda \mu +2D_u \alpha +\lambda \chi _0\right ), \end{split} \end{align*}

\begin{align*} \begin{split} C_2=&\,-(\lambda -\alpha ) \big\{\lambda \big [-2 D_u^2 \mu \big(D_A (\mu D_{\rho }-\lambda +\mu )-1\big)+D_u\lambda \chi _0 (1-2 \mu D_A)-\lambda \chi _0^2\big ]\\[5pt] &+\alpha \big[2 D_u^2 \big(\lambda -\mu (D_{\rho }+2)\big)-3D_u \lambda \chi _0 +\lambda \chi _0^2\big]\big\}. \end{split} \end{align*}

Suppose that there are no eigenvalue of $-\Delta$ , $\nu$ , such that $(\!\max \{0, \theta -\mu \}\lt \nu \lt \max \{\mu , \theta -\mu \})$ , where

\begin{equation*} \theta =\frac {2\lambda (\lambda -\alpha )-\alpha (\lambda -\alpha )(2+D_\rho )-D_A\beta \lambda ^2}{D_AD_\rho \lambda (\lambda -\alpha )}. \end{equation*}

If $\mu _1$ and $\mu _2$ are both positive roots of ( 3.0.3 ), further suppose that, $\mu$ (and $\theta -\mu$ in case it is an eigenvalue of $-\Delta$ ) are outside of the interval $(\!\min \{\mu _1, \mu _2\}, \max \{\mu _1, \mu _2\})$ . Then the branch $(\chi (s), A(s), \rho (s), u(s))$ of solution of ( EQ ) bifurcating from $(\chi _0, \bar {A}, \bar {\rho }, {\bar {u}})$ is stable for sufficiently small and non-zero $|s|$ .

Proof. We proceed by following the approach outlined in [Reference Cantrell, Cosner and Manásevich8], where the authors apply the bifurcation theory developed in [Reference Crandall and Rabinowitz11]. The stability of the bifurcation branch $(\chi (s), A(s), \rho (s), u(s))$ of (EP) (or equivalently (EQ), by translation) is determined by the eigenvalues of $D\mathcal{F}{(A,\rho ,u)}(\chi (s), A(s), \rho (s), u(s))$ . In particular, the branch is stable if all eigenvalues have negative real parts. Theorem2.2 implies that $D\mathcal{F}{(A,\rho ,u)}(\chi _0, \mathbf{0})$ has $0$ as an $i$ -simple eigenvalue, where $i$ is an injection. Moreover, Corollary 1.13 in [Reference Crandall and Rabinowitz11] ensures the existence of intervals $I$ and $J$ with $\chi _0 \in I$ and $0 \in J$ , together with continuously differentiable functions $\gamma \,:\, I \to \mathbb{R}, \quad \sigma \,:\, J \to \mathbb{R}, \quad [\mathbf{v}] \,:\, I^3 \to Y$ and $ (w_1, w_2, w_3)\,:\, J^3 \to Y$ such that

\begin{equation*} D\mathcal F_{(A, \rho , u)}(\chi , \mathbf{0})[\textbf {v}]^T=\gamma (\chi )[\textbf {v}]^T, \end{equation*}

\begin{equation*} D\mathcal F_{(A, \rho , u)}(\chi (s), A(s), \rho (s), u(s))(w_1, w_2, w_3)^T=\sigma (s)(w_1, w_2, w_3)^T, \end{equation*}

such that

\begin{equation*} \chi (0)=\chi _0, \quad \gamma (\chi _0)=\sigma (0)=0, \quad (v_1(\chi _0), v_2(\chi _0), v_3(\chi _0))=(w_1(0), w_2(0), w_3(0))=\textbf {P}(\textbf {x}), \end{equation*}

\begin{equation*} (v_1(\chi ), v_2(\chi ), v_3(\chi ))-\textbf {P}(\textbf {x}) \in W, \quad (w_1(s), w_2(s), v_3(s))-\textbf {P}(\textbf {x}) \in W. \end{equation*}

Theorem 1.16 in [Reference Crandall and Rabinowitz11] states that under the assumptions and definitions of Corollary 1.13, $\sigma (s)$ has only zero at $s=0$ and the same sign as $s$ for $|s|\gt 0$ for sufficiently small $|s|$ and whenever $\chi '(0)\not =0$ . It follows that if $\gamma (\chi _0)=\sigma (0)$ is the eigenvalue of (2.0.1) with the largest real part at $(\chi _0, \mathbf{0})$ , then again for sufficiently small nonzero $s$ , $\sigma (s)$ is eigenvalue of the linearization of (2.0.1) at $(\chi (s), A(s), \rho (s), u(s))$ with the largest real part. In particular, if $\mathcal{R}e(\sigma (0))\lt 0$ , then $\mathcal{R}e(\sigma (s))\lt 0$ .

Hence, it remains to show that, under assumptions of Theorem3.1, (a) $\chi '(0) \neq 0$ , and (b) $\sigma (0) = 0$ is the largest eigenvalue of the linearized operator $D\mathcal{F}_{(A,\rho ,u)}(\chi ,A,\rho ,u)$ at $(\chi _0,\mathbf{0})$ .

To this end, we write system (EP) with the bifurcating solution as

\begin{equation*}\mathcal{F}(\chi (s), A(s), \rho (s), u(s)) = 0,\end{equation*}

with $\mathbf{x}$ omitted for notational simplicity. We then differentiate twice with respect to $s$ at $s = 0$ to obtain.

\begin{align*} \begin{split} D_A\Delta A''(0)+2A'(0)\rho '(0)-\frac {\alpha }{\lambda }A''(0)+\lambda \rho ''(0)=0, \end{split} \end{align*}

\begin{align*} \begin{split} &D_\rho \Delta \rho ''\left (0\right )-\frac {2}{\lambda }\left (1-\frac {\alpha }{\lambda }\right )\Delta A''\left (0\right )-\nabla \cdot \left [\frac {4}{\lambda }\rho '\left (0\right )\nabla A'\left (0\right )\right ]\\[5pt] &\quad +\nabla \cdot \left [\frac {4}{\lambda ^2}\left (1-\frac {\alpha }{\lambda }\right )A'\left (0\right )\nabla A'\left (0\right )\right ]-2A'\left (0\right )\rho '\left (0\right )-\left (1-\frac {\alpha }{\lambda }\right )A''\left (0\right )\\[5pt] &\quad -2\rho '\left (0\right )u'\left (0\right )-\frac {\lambda \beta }{\lambda -\beta }\rho ''\left (0\right )-\left (1-\frac {\alpha }{\lambda }\right )u''\left (0\right )=0, \end{split} \end{align*}

and

\begin{align*} \begin{split} &D_u\Delta u''\left (0\right )-\chi _0\left (\frac {\beta }{\lambda -\alpha }-1\right )\Delta A''\left (0\right )-\nabla \cdot \left [2\chi '\left (0\right )\left (\frac {\beta }{\lambda -\alpha }-1\right )\nabla A'\left (0\right )\right ]\\[5pt] &\quad -\nabla \cdot \left [2\chi _0\frac {1}{\lambda }u'\left (0\right )\nabla A'\left (0\right )\right ]+\nabla \cdot \left [2\chi _0\frac {1}{\lambda }\left (\frac {\beta }{\lambda -\alpha }-1\right )A'\left (0\right )\nabla A'\left (0\right )\right ]=0. \end{split} \end{align*}

Multiply the above three equations by $\phi$ and integrate, and we should get the following

(3.0.4) \begin{equation} H\left (\int _\Omega \phi A''(0), \int _\Omega \phi \rho ''(0), \int _\Omega \phi u''(0)\right )^T+\widehat {h}=0, \end{equation}

where $\widehat {h}$ is the vector containing the lower derivative terms

\begin{align*} \widehat {h}=\begin{bmatrix} \int _\Omega 2A'\left (0\right )\rho '\left (0\right )\phi \\[1em] \big\{\int _\Omega \big ({-}\nabla \cdot \big[\frac {4}{\lambda }\rho '\left (0\right )\nabla A'\left (0\right )\big] +\nabla \cdot \left [\frac {4}{\lambda ^2}\left (1-\frac {\alpha }{\lambda }\right )A'\left (0\right )\nabla A'\left (0\right )\right ]\\[5pt] \quad -2A'\left (0\right )\rho '\left (0\right )-2\rho '\left (0\right )u'\left (0\right )\big)\phi \big\}\\[1em] \big\{\int _\Omega \big({-}\nabla \cdot \left [2\chi '\left (0\right )\left (\frac {\beta }{\lambda -\alpha }-1\right )\nabla A'\left (0\right )\right ] -\nabla \cdot \left [2\chi _0\frac {1}{\lambda }u'\left (0\right )\nabla A'\left (0\right )\right ]\\[9pt] \quad +\nabla \cdot \left [2\chi _0\frac {1}{\lambda }\left (\frac {\beta }{\lambda -\alpha }-1\right )A'\left (0\right )\nabla A'\left (0\right )\right ]\big)\phi \big\} \end{bmatrix}. \end{align*}

We know that $\chi _0$ makes $H$ singular. The left eigenvector of $H$ corresponding to 0 is

\begin{equation*} \widehat {\textbf {P}(\textbf {x}) }=\left ({-}\frac {D_u\mu (\beta \lambda + D_\rho \mu (\lambda -\alpha ))}{(\lambda -\alpha )^2}, -\frac {D_u\lambda \mu }{\lambda -\alpha }, 1\right )^T. \end{equation*}

We multiply (3.0.4) by $\widehat {\textbf {P}(\textbf {x}) }$ from the left

\begin{align*} \widehat {\textbf {P}(\textbf {x}) }^TH\left (\int _\Omega \phi A''(0), \int _\Omega \phi \rho ''(0), \int _\Omega \phi u''(0)\right )^T+\widehat {\textbf {P}(\textbf {x}) }^T\widehat {h}=\widehat {\textbf {P}(\textbf {x}) }^T0\implies \widehat {\textbf {P}(\textbf {x}) }^T\widehat {h}=0. \end{align*}

We expand $\widehat {\textbf {P}(\textbf {x})}^T\widehat {h}$ and use fact that $(A'(0), \rho '(0), u'(0))=\textbf {P}(\textbf {x})$ . In addition, integration by parts and Green’s first identity let us deal with gradients in the following way

\begin{equation*} \int _\Omega \phi (\nabla \phi \cdot \nabla \phi )=\frac {1}{2}\int _\Omega \nabla \phi \cdot \nabla (\phi ^2)=-\frac {1}{2}\int _\Omega \phi ^2\Delta \phi =\frac {\mu }{2}\int _\Omega \phi ^3. \end{equation*}

We collect terms containing $\chi '(0)$ on the left-hand side (where we also use $\int _\Omega \phi ^2=1$ ) and those containing $\int _\Omega \phi ^3$ on the right-hand side

\begin{equation*} 2D_u\lambda ^2(\lambda -\alpha )(\alpha +\beta -\lambda )\chi '(0)=(C_1\beta +C_2)\int _\Omega \phi ^3, \end{equation*}

where

(3.0.5) \begin{equation} \begin{split} C_1\;:\!=\;- \lambda \left (\chi _0-D_u\right ) \left ({-}\alpha \chi _0+2 D_A D_u\lambda \mu +2D_u \alpha +\lambda \chi _0\right ), \end{split} \end{equation}

and

(3.0.6) \begin{align} C_2&=-(\lambda -\alpha ) \big\{\lambda \bigl [-2 D_u^2 \mu \bigl (D_A (\mu D_{\rho }-\lambda +\mu )-1\bigr )+D_u\lambda \chi _0 (1-2 \mu D_A)-\lambda \chi _0^2\bigr ]\nonumber\\[5pt] &+\alpha \big[2 D_u^2 \bigl (\lambda -\mu (D_{\rho }+2)\bigr )-3D_u \lambda \chi _0 +\lambda \chi _0^2\big]\big\}. \end{align}

The coefficients on the left-hand side are non-zero by assumption on the parameters. Hence, $\chi '(0)\not =0$ if $\beta \not =-C_2/C_1$ and $\int _\Omega \phi ^3\not =0$ . This completes part (a).

Remark 3.1. Note that $\chi _0$ depends on $\beta$ through its definition. Thus, determining $\beta ^*$ such that $C_2 \beta ^* + C_1 \neq 0$ and ensuring that $\beta$ is independent of $\chi _0$ reduces to solving a quadratic equation. The explicit expression for $\beta ^*$ can be obtained from the discriminant; however, it is algebraically cumbersome and therefore omitted here. Moreover, since $\beta \gt \lambda - \alpha \gt 0$ , one can derive sufficient conditions to guarantee either $-C_2/C_1 \lt \lambda - \alpha$ or $-C_2/C_1 \lt 0$ .

Remark 3.2. As noted in [Reference Cantrell, Cosner and Manásevich8], on a disc domain, a transcritical bifurcation arises because the eigenfunctions of the Laplace operator involve Bessel functions, which lack the symmetry required to ensure $\int _\Omega \phi ^3 = 0$ . Consequently, the analysis developed here remains valid in this setting. In contrast, for rectangular domains, the solutions of the Helmholtz equation are products of cosine functions, which satisfy $\int _\Omega \phi ^3 = 0$ (for example, $\int _{[0,\pi ]\times [0,\pi ]} \cos ^3(nx)\cos ^3(my) dxdy = 0$ ). Therefore, the same bifurcation scenario does not directly apply in rectangular domains. This observation is consistent with previous studies by [Reference Short, Bertozzi and Brantingham46, Reference Yerlanov, Wang and Rodríguez62], which demonstrate that pitchfork bifurcations are expected in rectangles, where $\chi '(0) = 0$ . To analyse the stability of these bifurcating branches, one must therefore examine higher-order terms, in particular $\chi ''(0)$ .

We follow [Reference Cantrell, Cosner and Manásevich8] to verify part (b): we show that $\sigma (0)=0$ is the eigenvalue of $D\mathcal F_{(A, \rho , u)}(\chi , A, \rho , u)$ at $(\chi _0, \mathbf{0})$ with the largest real part. The corresponding eigenvalue problem is

\begin{align*} \left \{ \begin{aligned} &D_A\Delta v_1-\frac {\alpha }{\lambda }v_1+\lambda v_2=\sigma v_1, &&\quad \text{ in }\Omega , \\[5pt] &D_\rho \Delta v_2-\frac {2}{\lambda }\left (1-\frac {\alpha }{\lambda }\right )\Delta v_1-\left (1-\frac {\alpha }{\lambda }\right )v_1-\frac {\lambda \beta }{\lambda -\alpha }v_2-\left (1-\frac {\alpha }{\lambda }\right )v_3=\sigma v_2, &&\quad \text{ in }\Omega , \\[5pt] &D_u\Delta v_3-\chi \left (\frac {\beta }{\lambda -\alpha }-1\right )\Delta v_1=\sigma v_3, &&\quad \text{ in }\Omega , \\[5pt] &\frac {\partial v_1}{\partial \textbf {n}}= \frac {\partial v_2}{\partial \textbf {n}}= \frac {\partial v_3}{\partial \textbf {n}}=0, &&\quad \text{ on }\partial \Omega , \end{aligned} \right . \end{align*}

which can be rewritten as follows for $3\times 3$ matrices $P, \, Q$

(3.0.7) \begin{equation} P\Delta \vec {v}+Q\vec {v}=\sigma \vec {v}. \end{equation}

By spectral theorem, $\vec {v}=\sum _{i=1}^\infty \vec {v}_i \phi _i$ , where $\phi _i$ is orthonormal eigenfunction of $-\Delta$ with homogeneous Neumann boundary conditions. If $\sigma$ is an eigenvalue, then for some $i$ , $\vec {v}_i\not =0$ . Integrate (3.0.7) by $\phi _i$ , then we should get

\begin{equation*} -P\mu _i\vec {v}_i+Q\vec {v}_i=\sigma v_i. \end{equation*}

Hence, $\sigma$ can be represented as an eigenvalue of $-P\mu _i +Q$ for some eigenvalue $\mu _i$ of $-\Delta$ . On the other hand, any $\mu _i$ leads to 3 eigenvalues of (3.0.7) corresponding to the eigenvalues of $-P\mu _i+Q$ . To avoid confusion, we denote the eigenvalue of $-\Delta$ that appears in Theorems2.2, 3.1 as $\mu _*$ . We drop the $i$ subscript, then at the bifurcation point, $-P\mu +Q=H$ with $\chi =\chi _0$ . We analyse the eigenvalues from the following equation

\begin{equation*} H\left (\int _\Omega v_1\phi , \int _\Omega v_2\phi , \int _\Omega v_3\phi \right )^T=\sigma \left (\int _\Omega v_1\phi , \int _\Omega v_2\phi , \int _\Omega v_3\phi \right )^T. \end{equation*}

According to Routh–Hurwitz stability criterion, (3.0.1) has roots with non-positive real parts if $a_2 \geq 0$ , $a_0 \geq 0$ and $a_2 a_1 \geq a_0$ . Our goal is to determine conditions that ensure none of the eigenvalues of $-\Delta$ violate these inequalities. Each coefficient $a_i$ is treated as a polynomial in $\mu$ , and the corresponding equalities must be analysed carefully. Note that $a_2 \geq 0$ for all non-negative values of $\mu$ .

We focus on $a_0=0$ , which is a critical point for the condition $a_0\geq 0$ . We already know that, when condition $a_0(\mu ,\chi )=0$ holds first at $\mu =\mu _1^{\text{Neumann}}$ , the first Neumann mode bifurcates; when it hits at $\mu _k^{\text{Neumann}}$ , mode $k$ bifurcates, leading to $k$ -peak steady state patterns. At the bifurcation point $(\chi _0, \mathbf{0})$ with $\mu =\mu _*$ , one of the roots of (3.0.1) is $\sigma =0$ , $a_0$ must be $0$ , thus considering $a_0\gt 0$ is not needed. We get that the other two roots (besides $\mu _*$ ) are

\begin{equation*} \mu _\circ =0, \quad \mu _\dagger =\frac {1}{D_A D_\rho }\left [2\left (1-\frac {\alpha }{\lambda }\right )-\frac {\alpha D_\rho }{\lambda }-\frac {D_A\beta \lambda }{\lambda -\alpha }\right ]-\mu _*, \end{equation*}

where the second one is obtained via Vieta’s formula. We need to assume that there are no other eigenvalues of $-\Delta$ in the interval $[\max \{\mu _\circ , \mu _\dagger \}, \max \{\mu _*, \mu _\dagger \}]$ besides $\mu _\circ$ , $\mu _*$ and $\mu _\dagger$ .

We need to guarantee that for $\mu _*$ , $\mu _\circ$ and $\mu _\dagger$ (in the case it is non-negative and an eigenvalue of $-\Delta$ ), the other two roots of (3.0.1) have a negative real part. We do so by looking at $a_2a_1-a_0$ , whose equation is given by (3.0.3). The coefficients in front of $\mu ^0$ and $\mu ^3$ are positive, hence by Descartes’ rule of signs, we expect at least one negative solution, let it be $\mu _3$ . The other two roots can be both positive, negative or complex conjugates. If they are negative or complex, then for any $\mu \geq 0$ , the above polynomial will be positive. If the roots are positive, say $\mu _1\lt \mu _2$ , we need to put extra conditions that there are no eigenvalues of $-\Delta$ in $(\mu _1, \mu _2)$ . This guarantees that there is no $\mu$ for which an associated $\sigma$ has a positive real part, including $\mu _\circ$ , $\mu _*$ and $\mu _\dagger$ . This concludes part (b).

Corollary 3.1. Suppose that $\mu$ is the eigenvalue of $-\Delta$ appearing in Theorem 2.2 with normalized eigenfunction $\phi$ . Suppose that the hypotheses of Theorem 2.2 are satisfied. Assume that $\int _\Omega \phi ^3\not =0$ and $\beta \not =-C_2/C_1$ , where $C_1$ and $C_2$ are given by ( 3.0.5 ) and ( 3.0.6 )

Further suppose that

\begin{equation*} -2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\gt 0. \end{equation*}

If $\mu$ is the first positive eigenvalue of $-\Delta$ , then the branch $(\chi (s), A(s), \rho (s), u(s))$ of solution of ( EQ ) bifurcating from $(\chi _0, \bar {A}, \bar {\rho }, {\bar {u}})$ is stable for sufficiently small and non-zero $|s|$ .

Proof. With the same notation as in the proof of Theorem3.1, suppose that

\begin{equation*} -2\left (1-\frac {\alpha }{\lambda }\right ) +\frac {D_\rho \alpha }{\lambda } +\frac {D_A \beta \lambda }{\lambda -\alpha } \geq 0. \end{equation*}

In this case, the coefficients of $\mu ^1$ and $\mu ^2$ in (3.0.3) are positive, which implies that no positive roots exist. However, this condition also forces $\mu _\dagger$ to be negative. Consequently, stability requires $\mu _*$ to be the first eigenvalue of $-\Delta$ , since we must ensure that no eigenvalues lie in the interval $(0,\mu _*)$ .

With Corollary3.1, we arrive at a dichotomy. If

(3.0.8) \begin{equation} -2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\gt 0, \end{equation}

then stability is guaranteed only when $\mu$ corresponds to the first positive eigenvalue. On the other hand, if

(3.0.9) \begin{equation} -2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\lt -\mu D_AD_\rho \lt 0, \end{equation}

then $\mu _\dagger \gt 0$ , and stability requires that no eigenvalues of $\Delta$ fall within the interval $(\!\min \{\mu _, \mu _\dagger \}, \max \{\mu _, \mu _\dagger \})$ (recall, $\mu =\mu ^*$ ). This condition is less restrictive on $\mu _*$ , since it does not force it to be the first eigenvalue. However, in this case, one must further ensure that no eigenvalues are present between $r_1$ and $r_2$ , the positive solutions of (3.0.3), if such exist.

These inequalities, and the resulting stability regions, depend sensitively on parameter choices. For instance, if $D_\rho \gt 2\frac {\lambda -\alpha }{\alpha }$ , then (3.0.8) holds, while if $D_\rho \lt 2\frac {\lambda -\alpha }{\alpha }$ and $D_A\lt \frac {({-}D_\rho \alpha +2(\lambda -\alpha ))(\lambda -\alpha )}{\lambda (\beta +D_\rho \mu (\lambda -\alpha ))}$ , then (3.0.9) applies. Mathematically, this shows that smaller diffusion rates broaden the range of eigenvalues that can support stable non-constant branches, i.e. patterned steady states.

The stability of the uniform steady state depends very sensitively on the diffusion parameters of the model. Mathematically, the key inequalities show that when offender diffusion ( $D_\rho$ ) and attractiveness diffusion ( $D_A$ ) are relatively large, the system tends to remain close to uniform, and only the simplest spatial modes can be stable. By contrast, when both diffusion rates are small, the conditions for stability relax, and more spatial modes are permitted. In this regime, the uniform steady state can lose stability, and the system may bifurcate to non-uniform solutions – steady patterns that represent spatial clustering.

From a criminological perspective, these bifurcation points can be interpreted as thresholds in offender and guardian mobility. When offenders move broadly and randomly across space and when the attractiveness of a crime event spreads widely, local concentrations of crime are smoothed out. However, if offender movement is limited and the attractiveness effect remains strongly localized, the system can cross a threshold where uniform crime distributions are no longer sustainable. Instead, stable heterogeneous patterns emerge, corresponding to persistent hotspots. Social science research suggests that such mechanisms may underlie the persistence of crime in certain neighbourhoods. Limited offender mobility, coupled with strong near-repeat effects, reinforces clustering and creates conditions where particular areas remain chronically affected. In this sense, the mathematics formalizes a well-known observation in criminology: that reduced movement and strong local feedback can lock specific places into cycles of concentrated criminal activity. While empirical confirmation in the exact setting of this model is still lacking, the analysis provides a plausible theoretical explanation for the formation and persistence of crime hotspots.

4. Hopf bifurcations and time-periodic dynamics

In this section, we investigate Hopf bifurcations, which correspond to the emergence of periodic solutions. Following a similar approach as in the previous section, we demonstrate that, under appropriate conditions, these cycles exist. We further validate the theoretical findings through numerical simulations of the original system. Here, we follow the framework developed in [Reference Rodríguez, Wang and Zhang39], which studies a one-dimensional version of (E). We extend their analysis by treating eigenvalues on general domains, without relying on explicit wavemode vectors.

Note that following Theorem4.1 is stated for the shift problem (EP), but it holds for the original system (E).

Theorem 4.1. Let $\mu$ be a positive eigenvalue of $-\Delta$ with homogeneous Neumann boundary condition such that $a_1(\mu )\gt 0$ in ( 3.0.1 ), and $\mu$ be larger than local maximizer of $\chi _*$ , defined as follows

(4.0.1) \begin{equation} \chi _*\;:\!=\;\frac {1}{\beta +\alpha -\lambda }\left \{\frac {a_1a_2}{D_u\mu }-\left (\lambda -\alpha \right )-\frac {\alpha \beta }{\lambda -\alpha }-\mu \left [-2\left (1-\frac {\alpha }{\lambda }\right )+\frac { D_\rho \alpha }{\lambda }+\frac {D_A\beta \lambda }{\lambda -\alpha }\right ] -\mu ^2D_AD_\rho \right \}. \end{equation}

Then system ( EP ) has in a neighbourhood of $(\chi _*, \mathbf{0})\in V$ a unique one-parameter family $\gamma (s);\;0\lt s\lt \varepsilon$ of noncritical periodic orbits. More precisely: there exists $\varepsilon \gt 0$ and

\begin{align*} (\chi ({\cdot}), A({\cdot}), \rho ({\cdot}), u({\cdot}), T({\cdot}))\in C^\infty (({-}\varepsilon , \varepsilon ), V\times \mathbb{R}^+) \end{align*}

with

\begin{align*} (\chi (0), A(0), \rho (0), u(0), T(0))=\left (\chi _*, \bar {A}, \bar {\rho }, {\bar {u}}, \frac {2\pi }{\sqrt {a_1(\mu )}}\right ) \end{align*}

such that

\begin{align*} \gamma (s)\;:\!=\;\gamma (A(s), \rho (s), u(s)), \quad 0\lt s\lt |\varepsilon | \end{align*}

is a noncritical periodic orbit of ( EP ) with $\chi =\chi (s)$ of period $T(s)$ passing through $A(s), \rho (s), u(s)\in Y$ . Moreover, the family $\{\gamma (s);\, 0\lt s\lt \varepsilon \}$ contains every noncritical periodic orbit of ( EP ) lying in a suitable neighbourhood of $(\chi _*, \mathbf{0}, T(0))\in V\times \mathbb{R}^+$ , and $\gamma (s_1)\not =\gamma (s_2)$ for $s_1\neq s_2$ .

Proof. We verify that the conditions of Theorem 1 in [Reference Amann, Busenberg and Martelli1] are satisfied. In addition, we follow the proof strategies developed in [Reference Rodríguez, Wang and Zhang39, Reference Wang, Yang and Zhang56]. Specifically, we analyse the eigenvalues of (2.1.2), the linearization of $\mathcal{F}$ at $\mathbf{0}$ . The procedure mirrors our earlier approach: multiply by $\phi$ and integrate over the domain. This again reduces the problem to studying the characteristic equation of $H$ , defined in (3.0.1) and (3.0.2), and determining the conditions under which purely imaginary roots arise.

Let $\sigma _2$ and $\sigma _3$ be purely imaginary roots of the form $\pm i \omega _0$ with $\omega _0 \gt 0$ , and let $\sigma _1$ denote the remaining real root. Then, (3.0.1) can be rewritten as

\begin{equation*}(\sigma - \sigma _1)(\sigma ^2 + \omega _0^2) = \sigma ^3 - \sigma _1 \sigma ^2 + \omega _0^2 \sigma - \sigma _1 \omega _0^2.\end{equation*}

It follows that $\sigma _1 = -a_2(\mu ) \lt 0$ and $\sigma _{2,3} = \pm i \sqrt {a_1(\mu )}$ . To guarantee that the roots are purely imaginary, we require $a_1(\mu ) \gt 0$ , which holds whenever $\mu$ is chosen outside the real roots of $a_1(\mu )$ . The critical bifurcation value $\chi _*(\mu )$ is then defined by the condition $a_2(\mu ) a_1(\mu ) = a_0(\mu )$ . In general, the rational function of $\mu$ given in (4.0.1) is continuous but not necessarily injective. Let $\mu _M$ denote a real local maximizer of this function. Then, for any $\chi _*(\mu ) \gt \chi _*(\mu _M)$ , the corresponding value of $\mu$ is uniquely determined.

Finally, we need to check the transversality condition. Let $\sigma _1(\chi )$ and $\sigma _{2, 3}(\chi )=p(\chi )+iq(\chi )$ be solutions to (3.0.1) in the neighbourhood of $\chi =\chi _*$ . Then, upon substitution and equating the coefficient in front of the power of $\sigma$ , we get

\begin{align*} \left \{ \begin{aligned} -a_2&=2p(\chi )+\sigma _1(\chi ), \\[5pt] a_1&=p^2(\chi )+q^2(\chi )+2p(\chi )\sigma _1(\chi ), \\[5pt] -a_0&=(p^2(\chi )+q^2(\chi ))\sigma _1(\chi ). \end{aligned} \right . \end{align*}

Differentiating with respect to $\chi$ , we get that $a_0(\mu )'=D_u\mu (\lambda -\alpha )\left (\frac {\beta }{\lambda -\alpha }-1\right )\gt 0$ .

\begin{align*} \left \{ \begin{aligned} 0&=2p'(\chi )+\sigma _1'(\chi ), \\[5pt] 0&=2p(\chi )p'(\chi )+2q(\chi )q'(\chi )+2p'(\chi )\sigma _1(\chi )+2p(\chi )\sigma _1'(\chi ), \\[5pt] a_0'&=2(p(\chi )p'(\chi )+q(\chi )q'(\chi ))\sigma _1(\chi )+(p^2(\chi )+q^2(\chi ))\sigma _1'(\chi ). \end{aligned} \right . \end{align*}

We evaluate at $\chi = \chi _*$ , where $p(\chi _*) = 0$ , $q(\chi _*) = \sqrt {a_1(\mu )}$ and $\sigma _1(\chi _*) = -a_2(\mu )$ . Thus,

\begin{align*} \left \{ \begin{aligned} 0 &= 2p'(\chi _*) + \sigma _1'(\chi _*), \\[5pt] 0 &= 2\sqrt {a_1}\, q'(\chi _*) - 2p'(\chi _*)a_2, \\[5pt] a_0' &= -2\sqrt {a_1}\, q'(\chi _*)a_2 + a_1\sigma _1'(\chi _*). \end{aligned} \right . \end{align*}

Solving this system for $(p'(\chi _*),\, q'(\chi _*),\, \sigma _1'(\chi _*))^T$ , we obtain

\begin{equation*} p'(\chi _*) = -\frac {2a_0'}{a_1(\mu ) + a_2^2(\mu )} \lt 0, \end{equation*}

where the inequality follows from the assumption that $\mu$ lies outside the interval where $a_1(\mu ) \lt 0$ .

The bifurcation value $\chi _*$ determines the onset of Hopf instabilities, where the spatially homogeneous steady states lose stability and give rise to oscillatory behaviour. These periodic solutions exhibit spatio-temporal behaviour in that they repeat not only in time but also exhibit structured, recurring patterns in space. This behaviour will be observed in the numerical simulations illustrated in Figure 2c, for example. In social-science terms, this suggests that when policing intensity crosses these thresholds, crime dynamics may enter into recurring cycles – periods of high and low crime concentrated in particular neighbourhoods – rather than settling into a stable equilibrium. Such cyclical hotspot activity has been observed empirically and reflects the limitations of static policing strategies.

5. Numerical simulations and pattern formation

In this section, we numerically investigate heterogeneous steady states in two dimensions, a natural setting for studying urban crime since it reflects how hotspots emerge and persist across neighborhoods. Previous studies [Reference Rodríguez, Wang and Zhang39, Reference Yerlanov, Wang and Rodríguez62] employed linear stability analysis to identify key thresholds, denoted by $\chi ^-$ and $\chi ^+$ (see [Reference Yerlanov, Wang and Rodríguez62] for precise definitions). The constant steady state is linearly stable whenever $\chi ^- \lt \chi \lt \chi ^+$ . Crossing these thresholds corresponds to intensities at which uniform crime–guardian equilibria destabilize, producing either stationary clustering (steady-state bifurcation) or cycling hotspots (Hopf). From a social perspective, these bifurcation values mark thresholds of police responsiveness: when policing intensity remains between $\chi ^-$ and $\chi ^+$ , uniform safety can be maintained, but crossing either boundary destabilizes the system, potentially leading to persistent or oscillatory crime concentrations.

Here, we focus on cases in which at most one of these inequalities is violated. For reproducibility and further exploration, the simulation codes are publicly available: parameter exploration can be carried out with https://github.com/MaYeatCo/urban_bifurcation, while individual one- and two-dimensional simulations can be found in https://github.com/MaYeatCo/urban_suppression.

Since the number of parameters is large, we fix most of them and focus on how the diffusion rates affect the solutions. Specifically, we consider the case of hotspot policing, where police movement mimics that of crime agents, i.e., $\chi = 2$ and $D_u = D_\rho$ , (in later subsections, we will consider the case of various $D_\rho$ vs $D_u$ and $D_u$ vs $\chi$ , so these assumptions are not true throughout the whole numerical simulations). Our simulations are conducted in two dimensions on a square domain with side length $L$ . We perform a parameter sweep over a fixed range of $D_A$ and $D_\rho$ and compute the orderings of $\chi$ , $\chi ^-$ , and $\chi ^+$ . The results are summarized in Figure 1. To create this figure, we apply the linear stability results from [Reference Rodríguez, Wang and Zhang39, Reference Yerlanov, Wang and Rodríguez62] using wave numbers/vectors $k$ . We then verify that the stability conditions hold across a wide range of $|k|$ . All possible orderings are represented by regions I–VI, and these regions correspond to different policing thresholds, where small changes in deployment intensity can qualitatively alter crime distributions. For instance, the border between regions I and III occurs precisely when $a_2(\mu )a_1(\mu ) = a_0(\mu )$ in Theorem4.1 (or equivalently $a_2(k)a_1(k)=a_0(k)$ in Proposition 2.1 in [Reference Rodríguez, Wang and Zhang39]). Our objective is to determine whether periodic or near-periodic solutions emerge, thereby confirming the theoretical predictions. After identifying the stability regions, we carry out numerical simulations.

We select three parameter combinations within the interior of the regions (labelled A–C), as well as three parameter combinations located around the borders between region I and the others (labelled D–F). Here, we did not conduct simulations for regions IV–VI in Figure 1. These regions lie farther from region I and correspond to cases where multiple Routh–Hurwitz conditions are violated, making the system’s behaviour less predictable. As shown in [Reference Rodríguez, Wang and Zhang39], solutions in these regimes can exhibit chaotic dynamics. Examples of such less predictable behaviour (in the theoretical sense) will be presented in the following subsections.

Figure 1. Illustration of the effect of diffusion rates on the ordering of $\chi$ , $\chi ^-$ and $\chi ^+$ obtained from linear stability analysis. Roman numerals indicate the corresponding inequality regimes, while letters denote parameter combinations selected for further simulations. Region I corresponds to the linearly stable regime. The remaining parameters are fixed at $\alpha = 1.0, \beta = 1.0, \lambda = 1.5, \chi = 2, L = \pi$ . Each region represents a distinct ordering of $\chi , \chi ^-$ and $\chi ^+$ . Note that this figure illustrates only the predictions from linear stability analysis. Non-linear effects may significantly influence the solution behaviour, particularly near the boundaries between regions.

We use the PDE toolbox in MATLAB [51, 52] to perform numerical simulations. As simulations are done in two dimensions, it is not straightforward to depict the evolution of the solution. Thus, we choose to track changes in overall amplitude via a root mean square function. All solutions are initiated at the steady-state constant plus a small perturbation ( $0.01$ ) using a cosine function. The time evolutions are shown in Figure 2. We use the root mean square metric, defined as $\text{RMS}[f(x, t)]=\sqrt {|\Omega |^{-1}\int _\Omega f(\mathbf{x}, t)^2d\mathbf{x}}$ . In addition, we plot the final frames of the simulation to show the patterns they exhibit, see Figure 3.

We now turn to Figures 2 and 3 for a more detailed examination of the dynamics. At point A, corresponding to region I, perturbations decay monotonically, and the solution converges to the spatially uniform steady state, in full agreement with the linear stability predictions. At points B, D, and E, the solution amplitude increases and then saturates at a nonzero level, yielding spatially heterogeneous but temporally stationary states. These patterns may appear as hotspots, symmetric arrangements or related structures. At point C, located in region III, the long-time dynamics approach a time-periodic orbit. Near regime boundaries, as exemplified by point F, the system exhibits more intricate dynamics, with oscillations of varying amplitude that indicate the onset of mixed-type or higher-order bifurcations. Such transitional regimes call for more refined analysis, either through extended simulations or by applying weakly non-linear techniques. In summary, the numerical results confirm the existence of periodic solutions, consistent with the statement of Theorem4.1.

Figure 2. Examples of amplitude evolutions from Figure 1, computed using $A_{amp}=\mathrm{RMS}[A(\mathbf{x},t)-\lambda ]$ , illustrate how diffusion rates shape system dynamics. In (a), amplitudes decay monotonically, confirming the stability of the uniform steady state. In (b), they saturate at a non-zero level, producing stationary hotspots. In (c), periodic oscillations arise through a Hopf bifurcation, resembling recurrent “crime waves.” in (d), irregular oscillations signal mixed or higher-order bifurcations and parameter sensitivity. Near regime borders, as in (e) and (f), small perturbations can trigger clustering or quasi-periodic oscillations with irregular amplitudes, marking transitions to more complex or weakly chaotic behaviour. Together, these results show how the system shifts from uniform stability to persistent hotspots, oscillatory patterns and chaotic regimes as diffusion rates vary.

Figure 3. Examples of patterns corresponding to the points in Figure 1. The diffusion rates are (a) region I, $D_A=0.12, D_\rho =0.06$ ; (b) region II, $D_A=0.025, D_\rho =0.18$ ; (c) region III, $D_A=0.09, D_\rho =0.04$ ; (d) Intersection of all regions, $D_A=0.047, D_\rho =0.071$ ; (e) near the border between regions I and II, $D_A=0.042, D_\rho =0.107$ ; (f) near the border between regions I and III, $D_A=0.111, D_\rho =0.04$ . The remaining parameters are fixed at $\alpha =0.5, \beta =1.0, \lambda =0.75, \chi =2, L=\pi$ . The snapshots reveal distinct regimes: uniform states (a), stationary hotspots (b), periodic oscillations (c), irregular mixed patterns at parameter intersections (d) and near-threshold behaviour with localized clustering or quasi-periodic fluctuations (e), (f). Together, they illustrate how tuning diffusion rates drives transitions from uniform stability to heterogeneous clustering, oscillations and complex dynamics.

5.1. Time-periodic patterns

In two-dimensional simulations, the solution may require a considerable time to converge, as can be observed in Figure 2f. To investigate periodic behaviour more efficiently, we therefore turn to a one-dimensional setting, where simulations are computationally less demanding. This reduction not only decreases the run-time but also allows the use of a smaller time step $\Delta t$ , improving the numerical accuracy. While simplified, the one-dimensional results remain informative, as they capture the essential dynamics and can be extended qualitatively to the two-dimensional case, particularly concerning the existence of distinct classes of solution behaviour.

To demonstrate the comparison between the two domains, we simulate system (E) over the interval under the same combination as in Figure 2c. The results are illustrated in Figure 4. Figure 4a is the one-dimensional counterpart of Figure 2c. Although there are differences, the overall qualitative behaviour is the same between the two. Moreover, the simulations over an interval take a shorter time to stabilize (200 in 1-D versus 500 in 2-D), and we see a clearer periodic solution, i.e. we are more confident in characterizing this behaviour as periodic. This trend is further supported in Figure 4b, where we observe a limit cycle. The period seems to be $\approx 240$ time units. Further time-series analysis can be performed, which can be helpful when examining multiple simulations, such as a parameter sweep setting in Figure 1, but this is beyond the scope of this paper. Instead, in the following section, we utilize the speed and reliability of one-dimensional simulations to shed light on another type of solution: chaos.

Figure 4. Representation of a one-dimensional simulation of (E) with the same parameters as in 2c. (a) Emergence and stabilization of periodic behaviour in the amplitude of the $A$ component, $A_{amp}=\mathrm{RMS}[A(x,t)-\lambda ]$ . Data are sampled every 3 time units to provide a clearer visualization of the oscillations. The figure shows that, after an initial transient, the solution does not converge to a steady state but instead settles into sustained periodic dynamics, reflecting the onset of a Hopf bifurcation. (b) Limit cycle in the $\rho _{amp}$ versus $u_{amp}$ = ( $\mathrm{RMS}[\rho (x,t)-\bar {\rho }]$ versus $\mathrm{RMS}[u(x,t)-{\bar {u}}]$ ) phase portrait for $t \in [300,600]$ , with trajectories represented in colour. The closed orbit indicates that the dynamics of the offender density ( $\rho$ ) and the guardian density ( $u$ ) are locked into a recurring cycle rather than stabilizing to an equilibrium. These results highlight the transition from stationary to oscillatory crime–policing patterns. In dynamical systems terms, the system crosses a bifurcation threshold where uniform hotspots lose stability and periodic oscillations emerge. From a criminological perspective, this suggests that crime and enforcement densities may fluctuate in sustained cycles – so hotspots not only persist but also oscillate in intensity and location over time, echoing empirical observations of recurring “crime waves.”.

5.2. Exploring chaos

A natural question is what occurs in regions IV–VI of Figure 1. As shown in [Reference Rodríguez, Wang and Zhang39], under certain parameter regimes – for instance, when diffusion rates are sufficiently small – the system can exhibit chaotic behaviour. To provide further evidence of this phenomenon, we present the bifurcation diagram in Figure 5. The diagram reveals that as diffusion decreases, new dynamical behaviours emerge. The first periodic solution appears around $D_\rho = 0.06$ . At $D_\rho = 0.03$ , successive period-doublings occur, eventually leading to the onset of chaos. We explore these regimes through representative solutions in Figures 6 and 7. In Figure 6a, the time series of $A_m(t)$ displays unpredictable fluctuations, and the system quickly settles into this chaotic regime. By contrast, Figure 7a shows a clear periodic orbit, though it takes longer for the dynamics to stabilize, and the oscillation frequency is relatively high ( $\gg 1$ ).

The corresponding phase portraits for $\rho$ and $u$ further illustrate the difference: in the chaotic case (Figure 6b), trajectories approach a strange attractor, whereas in the periodic case (Figure 7b), a well-defined closed orbit is observed. Chaotic solutions also exhibit larger deviations from the steady state. For example, although ${\bar {u}} = 1$ in both cases, in the periodic regime $u$ oscillates between approximately $0.65$ and $1.2$ , while in the chaotic regime it can range from near zero to as high as nine. Many additional phenomena could be uncovered with a more detailed analysis. However, it is worth noting that the theory of chaos in infinite-dimensional PDE systems is less developed than in finite dimensions, making rigorous characterization challenging. Nevertheless, the present model appears to provide a promising and mathematically rich setting for future research on spatiotemporal chaos in criminology-inspired systems.

Figure 5. Bifurcation diagram of the midpoint value $A(\pi /2,t^*)$ in the one-dimensional simulation of (E) in $(0,\pi )$ with initial perturbation of the form $0.05\cos (x)$ . The $y$ -axis records all extreme values of $A(\pi /2,t)$ with $t \in [800,1000]$ , after transients have decayed. $t^*$ denotes a maximizer or a minimizer. Simulations are run up to $T_{\max }=1000$ , treating $t \in [0,800]$ as transient. Parameters are fixed at $D_A=0.1$ , $\alpha =\beta =1$ , $\lambda =(1+\sqrt {5})/2$ and $\chi =2$ , with varying $D_\rho$ to reveal the bifurcation structure. The diagram illustrates how decreasing $D_\rho$ drives qualitative changes in the long-term behaviour of the system. For relatively large diffusion rates, solutions converge to spatially uniform steady states, consistent with linear stability predictions. As $D_\rho$ decreases, periodic solutions emerge, followed by successive period-doublings, and eventually chaotic dynamics. This transition reflects the loss of stability of homogeneous states and the onset of complex spatio-temporal behaviour. In particular, the appearance of chaos indicates that small diffusion rates can amplify non-linear feedback, leading to unpredictable but persistent fluctuations in the crime–policing system.

Figure 6. Representations of the chaotic solution to (E) with the same parameters as in Figure 5, except that $D_\rho = D_u = 0.01$ . As before, we investigate dynamics at the spatial midpoint, $x = \pi /2$ . (a) Time evolution of $A(\pi /2,t)$ . Instead of converging to a steady state or periodic orbit, the trajectory exhibits irregular oscillations with no discernible repeating pattern, characteristic of chaos. (b) Phase portrait of the non-transient trajectories of $\rho (\pi /2,t)$ and $u(\pi /2,t)$ for $t \in [800,1000]$ , with colours indicating temporal progression (dark blue at $t = 800$ , yellow at $t = 1000$ ). The trajectory does not close into a limit cycle but instead wanders in a complex set consistent with a strange attractor. Together, these figures again illustrate that very small diffusion rates destabilize uniform or periodic states and produce chaotic dynamics. From a criminological perspective, this corresponds to volatile crime–policing interactions, where hotspots neither stabilize nor repeat regularly but instead fluctuate unpredictably over time.

Figure 7. Representations of a periodic solution to (E). The parameters are the same as in Figure 5, but additionally $D_\rho =D_u=0.05$ . (a) The full time of evolution of $A(\pi /2,t)$ is given. (b) The non-transient $\rho (\pi /2,t)$ and $u(\pi /2,t)$ are plotted against each other. The colours represent the time: dark blue – $t=800$ and yellow – $t=1000$ . When compared to Figure 6, we only slightly increased diffusion rates, yet now the trajectory is an orbit after passing the aperiodic transient state. Similarly to Figure 4, we observe ”crime waves”. Moreover, the overall amplitudes are smaller. This figure, along with 6, demonstrates how changes in the agents’ movement affect the solution.

5.3. Further exploration of parameter space

In this section, we complement our theoretical findings by examining how parameter choices affect the behaviour of solutions. Specifically, we focus on the movement dynamics of real agents – namely, how variations in the diffusion and advection rates of $\rho$ and $u$ influence the system. All other parameters are held fixed. In this way, our analysis can be interpreted as studying the outcomes of strategic decisions from one side: given the random movement of criminal agents, what spatial patterns or effects might arise under different police deployment strategies? To address this, we use an interval domain for phase-plane simulations, which enables us to employ sufficiently small time steps to capture the dynamics at lower diffusion values. Recall that large diffusion rates lead to a linearly stable regime, a case that has already been analysed.

Similar to Figure 1, we examine the influence of diffusion rates, but with $D_A$ held fixed. In particular, we explore combinations of relatively small values of $D_\rho$ and $D_u$ , with the results shown in Figure 8. As expected, smaller diffusion rates lead to chaotic behaviour. As diffusion rates increase, solutions tend to become spatially heterogeneous or exhibit periodic patterns. Only when both diffusion rates are sufficiently large ( $D_\rho \gt 0.1$ and $D_u \gt 0.05$ ) does the system converge to constant solutions. This relationship can be interpreted as crime-stabilizing strategies: police agents may increase their diffusion to drive the system towards a constant-in-time state. Moreover, we observe that temporally varying solutions typically attain significantly higher and lower amplitudes compared to the constant steady-state values, with smaller diffusion rates producing larger deviations. This observation suggests a potential crime-suppression strategy: wait until the density of criminal agents reaches a low point and then intervene to stabilize the system at that level (see [Reference Yerlanov, Wang and Rodríguez62] for additional suppression strategies).

Figure 8. Solutions to (E) for various $D_\rho$ (columns) and $D_u$ (rows). The non-transient $\rho (\pi /2,t)$ and $u(\pi /2,t)$ are plotted against each other. The remaining parameters are $D_A=0.1$ , $\alpha =\beta =1$ , $\lambda =(1+\sqrt {5})/2$ , $\chi =2$ . The colours represent the time: dark blue – $t=800$ and yellow – $t=1000$ . The star represents the constant-in-time solutions. Whenever $\rho (\pi /2,t)=0.382$ and $u(\pi /2,t)=1$ , this indicates constant-in-space solutions as well. We observe that the reduction in the diffusion, which is a proxy for random movement here, leads to less predictable behaviour, destabilizing the crime landscape.

Next, we consider a scenario in which the diffusion rate of crime agents is fixed while the police advection rate is varied. This provides an alternative perspective for exploring potential strategies and policy outcomes. The corresponding results are shown in Figure 9. Recall that $\chi =2$ represents hotspot policing, where the police advection rate matches that of crime agents (second row). Increasing $\chi$ concentrates police more strongly around hotspots (first row), whereas flipping the sign corresponds to off-hotspot policing, where police avoid areas of high attractiveness (last row). We also examine the case with no advection (third row). We observe that increasing $\chi$ while keeping $D_u$ small results in chaotic or periodic behaviour, which can be attributed to the fact that $\chi \gt \chi ^+$ . By contrast, increasing $D_u$ appears to stabilize the system, at least in a temporal sense.

Figure 9. Solutions to (E) for various $D_u$ (columns) and $\chi$ (rows). The non-transient $\rho (\pi /2, t)$ and $u(\pi /2,t)$ are plotted against each other. The remaining parameters are $D_A=0.1$ , $D_\rho =0.01$ , $\alpha =\beta =1$ , $\lambda =(1+\sqrt {5})/2$ . We represent two snapshots using dark blue ( $t=800$ ) and yellow ( $t=1000$ ). The star represents the constant-in-time solutions. Here, we note that not only diffusion rates, but other parameters as well, may affect the crime landscape. We observe that the magnitude and sign of $\chi$ can significantly impact the local density of both agents, leading to values far from the constant steady state.

However, as shown by the linear stability analysis in [Reference Yerlanov, Wang and Rodríguez62], no value of $D_u$ with fixed $\chi = 4$ can shift the system into the linearly stable regime; in other words, there does not exist $D_u \gt 0$ such that $\chi ^- \lt \chi \lt \chi ^+$ for the parameters given in the caption of Figure 9. In this setting, high police concentration in highly attractive regions prevents the system from reaching spatial uniformity, regardless of adjustments to patrolling (i.e., random movement). In particular, when police movement has no advection component, the system decouples: $u$ converges to a constant steady state, while the remaining scalar fields develop spatially heterogeneous solutions. In this case, the model effectively reduces to a two-component system, which has already been extensively studied in the works referenced in the introduction.

In our simulations, off-hotspot policing is associated with higher crime density and lower police presence, whereas the opposite trend is observed under hotspot policing. For example, in the bottom-left corner of Figure 9, the crime density reaches $\approx 28.3$ , about 73 times higher than the constant steady-state value. While such disparities may resemble the heterogeneous distribution of crime in urban areas (cf, [Reference Thacher50]), we emphasize that these findings are model-based and hypothetical. Further empirical validation would be required before drawing any policy implications.