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Article

Boundedness of Solutions for an Attraction–Repulsion Model with Indirect Signal Production

1
College of Computer Science, Chengdu University, Chengdu 610106, China
2
Visual Computing and Virtual Reality Key Laboratory of Sichuan Province, Sichuan Normal University, Chengdu 610068, China
3
Division of Mathematics, Sichuan University Jinjiang College, Meishan 620860, China
*
Author to whom correspondence should be addressed.
Mathematics 2024, 12(8), 1143; https://doi.org/10.3390/math12081143
Submission received: 13 March 2024 / Revised: 3 April 2024 / Accepted: 3 April 2024 / Published: 10 April 2024
(This article belongs to the Special Issue Applications of Partial Differential Equations, 2nd Edition)

Abstract

:
In this paper, we consider the following two-dimensional chemotaxis system of attraction–repulsion with indirect signal production
𝜕 t u = Δ u · χ 1 u v 1 + · ( χ 2 u v 2 ) , x R 2 , t > 0 , 0 = Δ v j λ j v j + w , x R 2 , t > 0 , ( j = 1 , 2 ) , 𝜕 t w + δ w = u , x R 2 , t > 0 , u ( 0 , x ) = u 0 ( x ) , w ( 0 , x ) = w 0 ( x ) , x R 2 ,
where the parameters χ i 0 ,   λ i > 0 ( i = 1 , 2 ) and non-negative initial data ( u 0 ( x ) , w 0 ( x ) ) L 1 ( R 2 ) L ( R 2 ) . We prove the global bounded solution exists when the attraction is more dominant than the repulsion in the case of χ 1 χ 2 . At the same time, we propose that when the radial solution satisfies χ 1 χ 2 2 π δ u 0 L 1 ( R 2 ) + w 0 L 1 ( R 2 ) , the global solution is bounded. During the proof process, we found that adding indirect signals can constrict the blow-up of the global solution.

1. Introduction

The chemotactic model was proposed by Keller and Segel in [1] to describe the movement mechanism of organisms, cells or bacteria under the action of chemicals. Classified based on the direction of movement, we have chemotactic attraction and chemotactic repulsion. These forces play a crucial role in many development systems. In recent years, the issue of chemotaxis has been extensively studied. For example, global solvability has been studied in [2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24], large time behavior in [6,25,26,27,28,29], finite time blow-up in [6,30,31,32,33,34,35,36], nontrivial stationary solutions in [18,37,38,39,40], nonlinear diffusion in [41,42], indirect signaling in [43,44,45,46,47], etc. These studies provide important assistance for us to gain a deeper understanding of chemotactic phenomena.
A classical chemotaxis model is described as follows:
𝜕 t u Δ u = · χ u v , x Ω , t > 0 , τ v t Δ v u + λ v = 0 , x Ω , t > 0 ,
where u = u ( x , t ) and v = v ( x , t ) denote cell density and chemical concentration, respectively. Ω R n is a domain and τ { 0 , 1 } . When Ω is bounded, we propose the homogeneous Neumann initial boundary value conditions:
𝜕 u 𝜕 ν = 𝜕 v 𝜕 ν = 0 , x 𝜕 Ω , t > 0 , u ( x , 0 ) = u 0 ( x ) , x Ω
When Ω = R n , we give the initial data
u ( x , 0 ) = u 0 ( x ) , x R n .
These equations are used to describe the phenomenon of chemotactic aggregation. However, many biological processes also involve chemotactic repulsion. In [48], Luca proposed a more general model to describe attraction and repulsion phenomena as follows:
𝜕 t u Δ u = χ 1 · u v 1 + χ 2 · u v 2 , x Ω , t > 0 , τ 𝜕 t v 1 Δ v 1 u + λ 1 v 1 = 0 , x Ω , t > 0 , τ 𝜕 t v 2 Δ v 2 u + λ 2 v 2 = 0 , x Ω , t > 0 .
If the chemicals diffuse much more rapidly than the movement of cells, the case where τ = 0 can be considered as an approximate version of the case where τ = 1 . Rigorous proof of this limiting process can be found in [49]. For τ = 1 , Jiu and Liu in [50] considered a balanced case. For τ = 0 , Shi and Wang in [6] found that the system (1) has unique non-negative solutions locally in time for initial data u 0 satisfying
u 0 0 on R 2 , u 0 0 , u 0 L 1 ( R 2 ) L ( R 2 ) .
The non-negative solutions exist globally in time and are bounded in the repulsion-dominant χ 1 < χ 2 . Nagai and Yamada investigated the case χ 1 > χ 2 in [5].
Based on the motivation of indirect signal influence, we hope to see that the addition of an indirect signal does not damage the solution of the original system. In the real world, systems can be influenced by other signals at any time. Therefore, we consider the following indirect signal model:
𝜕 t u = Δ u · χ 1 u v 1 + · ( χ 2 u v 2 ) , x R 2 , t > 0 , 0 = Δ v j λ j v j + w , x R 2 , t > 0 , ( j = 1 , 2 ) , 𝜕 t w + δ w = u , x R 2 , t > 0 , u ( 0 , x ) = u 0 ( x ) , w ( 0 , x ) = w 0 ( x ) , x R 2 .
We suppose that the initial data satisfy
( u 0 , w 0 ) 0 on R 2 , u 0 0 , ( u 0 , w 0 ) L 1 ( R 2 ) L ( R 2 ) .
Our main result is stated as follows:
Theorem 1. 
Let χ 1 χ 2 and assume that u 0 L 1 ( R 2 ) < 8 π δ 4 + ( χ 1 χ 2 ) 2 . Then, we have
u L p ( R 2 ) + i = 1 2 v i W 2 , p ( R 2 ) + w L p ( R 2 ) C , i = 1 , 2
for all 1 p .
Theorem 2. 
Let M 0 : = 1 δ u 0 L 1 ( R 2 ) + w 0 L 1 ( R 2 ) and assume that non-negative initial data u 0 , w 0 are radial and ( χ 1 χ 2 ) M 0 2 π . Then, we have
u L p ( R 2 ) + i = 1 2 v i W 2 , p ( R 2 ) + w L p ( R 2 ) C , i = 1 , 2
for all 1 p .
Remark 1. 
Because 4 + ( χ 1 χ 2 ) 2 4 ( χ 1 χ 2 ) , we have
8 π δ 4 + ( χ 1 χ 2 ) 2 2 π χ 1 χ 2 .
Thus, the constriction of initial data for u 0 L 1 ( R 2 ) becomes weaker.
Remark 2. 
Using the Duhamel’s principle in (2), we denote the solution as
u ( x , t ) = G ( · , t ) u 0 + 0 t G ( t τ , · ) ( u V ) ( τ ) d τ ,
where G ( x , t ) = ( 4 π t ) 1 e | x | 2 4 t is the heat kernel, and
V = χ 1 v 1 χ 2 v 2 = χ 1 ( λ 1 Δ ) 1 χ 2 ( λ 2 Δ ) 1 u .
Here, ( λ i Δ ) 1 ( i = 1 , 2 ) denotes the inverse pseudo-differential operator of λ i Δ , and we represent it using Fourier and inverse Fourier transformations. That is,
( λ Δ ) 1 u : = F 1 ( λ | 1 ξ | 2 ) 1 F [ u ] ( ξ ) = F 1 ( λ + | ξ | 2 ) 1 u = K λ u ,
where K λ ( x ) = 0 e λ t G ( x , t ) d t is the Bessel kernel. We also denote the fractional-order differential operator Λ k = ( Δ ) k 2 ( k > 0 ) by
Λ k u = F 1 | ξ | k F [ u ] ( ξ ) .
For more detailed related information, please refer to [51,52].
Applying the following Young’s inequality of convolution
( λ Δ ) 1 f L p ( R 2 ) = K λ f L p ( R 2 )   K λ L r ( R 2 ) f L q ( R 2 ) for all 1 + 1 p = 1 q + 1 r
and the estimates
K λ L p ( R 2 ) < , 1 p < and 𝜕 x K λ L p ( R 2 ) < , 1 p < 2 ,
we can obtain the Lemma 2 below.

2. Preliminaries

Before giving an energy estimate, we need to utilize the following important mass conservation properties.
Lemma 1. 
Let ( u , v i , w ) ( i = 1 , 2 ) be the non-negative solution to the Cauchy problem (2) with non-negative initial data u 0 , w 0 satisfying (3). Then, we have
u L 1 ( R 2 ) = u 0 L 1 ( R 2 )
and
w L 1 ( R 2 )   w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 )
as well as
w L 1 ( R 2 ) = λ i v i L 1 ( R 2 ) , i = 1 , 2 .
Proof. 
We integrate the first equation of (2) to obtain (4). Integrating the third equation of (2) and using (4), we see that
d d t R 2 w d x + δ R 2 w d x = R 2 u 0 d x .
For t > 0 , we solve the above ODE to obtain
w L 1 ( R 2 ) = w 0 L 1 ( R 2 ) e δ t + u 0 L 1 ( R 2 ) δ ( 1 e δ t )   w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 ) .
Integrating the second equation of (2), we complete the proof. □
Lemma 2. 
For λ > 0 , we have
v j ( t ) L p ( R 2 ) C ( p , q ) w ( t ) L q ( R 2 ) , 1 q p < ,
v j ( t ) L ( R 2 ) C ( q ) w ( t ) L q ( R 2 ) , 1 < q ,
v j ( t ) L ( R 2 ) C ( q ) w ( t ) L q ( R 2 ) , 2 < q .
In particular, the following holds
v j ( t ) L p ( R 2 ) C ( p ) w ( t ) L 1 ( R 2 ) , 1 p < .
According to Lemma 2.3 in [5], we have
Lemma 3. 
If the non-negative function g L 1 ( R 2 ) W 1 , 2 ( R 2 ) , it holds that
R 2 g 2 d x 1 + ε 4 π R 2 g d x R 2 | g | 2 1 + g d x + 2 ε R 2 g d x for all ε > 0 .
According to Lemma 2.1 of [53], we have the following lemma.
Lemma 4. 
If the non-negative function g L 1 ( R 2 ) W 1 , 2 ( R 2 ) , it holds that
R 2 g 3 d x ε R 2 ( 1 + g ) log ( 1 + g ) d x R 2 | g | 2 d x + C ( ε ) R 2 g d x ,
where ε is any positive number and C ( ε ) tends to infinity as ε 0 .

3. A Prior Estimate

Lemma 5. 
Let χ 1 χ 2 and assume that u 0 L 1 ( R 2 ) < 8 π δ 4 + ( χ 1 χ 2 ) 2 . Then,
K : = sup 0 < t < T 1 + u ( t ) log 1 + u ( t ) 1 < for all T > 0 .
Proof. 
Multiplying the first equation of (2) with log ( 1 + u ) and noting R 2 𝜕 t u = 0 , log ( 1 + u ) u , we have
d d t R 2 ( 1 + u ) log ( 1 + u ) d x = R 2 log ( 1 + u ) 𝜕 t u d x = R 2 Δ u log ( 1 + u ) d x R 2 · u χ 1 v 1 χ 2 v 2 log ( 1 + u ) d x = R 2 | u | 2 1 + u d x + R 2 u 1 + u u · χ 1 v 1 χ 2 v 2 d x = R 2 | u | 2 1 + u d x + R 2 u · χ 1 v 1 χ 2 v 2 d x R 2 1 1 + u u · χ 1 v 1 χ 2 v 2 = R 2 | u | 2 1 + u d x R 2 u χ 1 Δ v 1 χ 2 Δ v 2 d x + R 2 log ( 1 + u ) χ 1 Δ v 1 χ 2 Δ v 2 d x = R 2 | u | 2 1 + u d x + ( χ 1 χ 2 ) R 2 u w d x R 2 u ( χ 1 λ 1 v 1 χ 2 λ 2 v 2 ) d x ( χ 1 χ 2 ) R 2 w log ( 1 + u ) d x + R ( χ 1 λ 1 v 1 χ 2 λ 2 v 2 ) log ( 1 + u ) d x R 2 | u | 2 1 + u d x + ( χ 1 χ 2 ) R 2 u w d x + ε 1 R 2 u 2 d x + 2 C ( ε 1 ) i = 1 2 R 2 χ i 2 λ i 2 v i 2 d x R 2 | u | 2 1 + u d x + δ 2 R 2 w 2 d x + ( χ 1 χ 2 ) 2 2 δ + ε 1 R 2 u 2 d x + 2 C ( ε 1 ) i = 1 2 R 2 χ i 2 λ i 2 v i 2 d x ,
where 0 < ε 1 < 1 is small enough to be determined.
On the other hand, we multiply the third equation of (2) with 2 w and use the Young’s inequality to obtain
d d t R 2 w 2 d x + 2 δ R 2 w 2 d x = 2 R 2 u w d x δ 2 R 2 w 2 d x + 2 δ R 2 u 2 d x .
Adding the Equations (11) and (12), we have
d d t R 2 ( 1 + u ) log ( 1 + u ) d x + R 2 w 2 d x + R 2 | u | 2 1 + u d x + δ R 2 w 2 d x ( χ 1 χ 2 ) 2 + 4 2 δ + ε 1 R 2 u 2 d x + 2 C ( ε 1 ) i = 1 2 R 2 χ i 2 λ i 2 v i 2 d x .
Let δ : = min ε 1 , δ . Thus, we add the two sides of the Equation (13) with δ · R 2 ( 1 + u ) log ( 1 + u ) d x and apply the inequality ( 1 + u ) log ( 1 + u ) u + u 2 to obtain
d d t R 2 ( 1 + u ) log ( 1 + u ) d x + R 2 w 2 d x + R 2 | u | 2 1 + u d x + δ · R 2 w 2 d x + R 2 ( 1 + u ) log ( 1 + u ) d x ( χ 1 χ 2 ) 2 + 4 2 δ + 2 ε 1 R 2 u 2 d x + 2 C ( ε 1 ) i = 1 2 R 2 χ i 2 λ i 2 v i 2 d x + ε 1 u 0 L 1 ( R 2 ) .
Applying Lemmas 2 and 3 as g = u ( t ) to (14) yields the following:
d d t R 2 ( 1 + u ) log ( 1 + u ) d x + R 2 w 2 d x + 1 ( χ 1 χ 2 ) 2 + 4 2 δ + 2 ε 1 · 1 + ε 1 4 π u 0 L 1 ( R 2 ) R 2 | u | 2 1 + u d x + δ · R 2 w 2 d x + R 2 ( 1 + u ) log ( 1 + u ) d x 2 C ( ε 1 ) i = 1 2 R 2 χ i 2 λ i 2 v i 2 d x + ( χ 1 χ 2 ) 2 + 4 δ ε 1 + 4 u 0 L 1 ( R 2 ) C ( u 0 L 1 ( R 2 ) , ε 1 , χ i , λ i , δ ) .
Thanks to u 0 L 1 ( R 2 ) < 8 π δ 4 + ( χ 1 χ 2 ) 2 , we can take a small enough value of ε 1 such that
1 ( χ 1 χ 2 ) 2 + 4 2 δ + 2 ε 1 · 1 + ε 1 4 π u 0 L 1 ( R 2 ) 0 .
Using Gronwall’s inequality, we have
1 + u ( t ) log 1 + u ( t ) 1 1 + u 0 log 1 + u 0 1 + w 0 L 2 ( R 2 ) 2 e δ t + C ( u 0 L 1 ( R 2 ) , χ i , λ i , δ ) , i = 1 , 2 .
Therefore, we complete the proof of Lemma 5. □
Next, we will give the gradient estimates of v i .
Lemma 6. 
Let 0 < T and assume χ 1 χ 2 holds. We have the following estimate
M : = i = 1 2 sup 0 < t < T v j ( t ) L ( R 2 ) + sup 0 < t < T v j ( t ) L ( R 2 ) < .
Proof. 
Multiplying the first equation of (2) with u p 1 ( p > 1 ) and integrating by parts, we can deduce that
1 p d d t u L p ( R 2 ) p + 4 ( p 1 ) p 2 u p 2 2 2 = χ 2 R 2 u p 1 ( u · v 2 + u Δ v 2 ) χ 1 R 2 u p 1 ( u · v 1 + u Δ v 1 ) = 1 1 p R u p ( χ 2 Δ v 2 χ 1 Δ v 1 ) d x = 1 1 p R u p χ 2 λ 2 v 2 χ 1 λ 1 v 1 + ( χ 1 χ 2 ) w d x 1 1 p χ 2 λ 2 R 2 u p v 2 + 1 1 p ( χ 1 χ 2 ) R 2 u p w d x δ 4 R 2 w p + 1 d x + 4 p ( p 1 ) p ( χ 1 χ 2 ) p p p δ p + p p + 1 R 2 u p + 1 d x + 1 p + 1 R 2 v 2 p + 1 d x .
We multiply the third equation of (2) by w p and apply the Young’s inequality yielding
1 p + 1 d d t R 2 w p + 1 d x + δ R 2 w p + 1 d x = R 2 u w p d x δ 4 R 2 w p + 1 d x + 4 p δ p R 2 u p + 1 d x .
Combining (16) and (17), we have
d d t 1 p u L p ( R 2 ) p + 1 p + 1 w L p + 1 ( R 2 ) p + 1 + 4 ( p 1 ) p 2 u p 2 L 2 ( R 2 ) 2 + δ 2 w L p + 1 ( R 2 ) p + 1 4 p ( p 1 ) p ( χ 1 χ 2 ) p + 4 p p p p p δ p + p p + 1 u L p + 1 ( R 2 ) p + 1 + 1 p + 1 v 2 L p + 1 ( R 2 ) p + 1 .
Next, we take p = 2 in (18) to obtain
d d t 1 2 u L 2 ( R 2 ) 2 + 1 3 w L 3 ( R 2 ) 3 + u L 2 ( R 2 ) 2 + δ 2 w L 3 ( R 2 ) 3 4 ( χ 1 χ 2 ) 2 + 16 δ 2 + 2 3 u L 3 ( R 2 ) 3 + 1 3 v 2 L 3 ( R 2 ) 3 .
Applying the estimate (10), we have
v 2 L 3 ( R 2 ) C 1 3 w ( t ) L 1 ( R 2 ) C 1 3 w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 ) ,
where C 1 is a positive constant.
For the term u L 3 ( R 2 ) , we use the Lemma 4 to obtain
u L 3 ( R 2 ) 3 ε 2 ( 1 + u ) log ( 1 + u ) L 1 ( R 2 ) u L 2 ( R 2 ) 2 + C ( ε 2 ) u L 1 ( R 2 ) ε 2 K u L 2 ( R 2 ) 2 + C ( ε 2 ) u 0 L 1 ( R 2 ) for all 0 < ε 2 < 1 .
Thus, substituting (20) and (21) into (19) yields
d d t 3 u L 2 ( R 2 ) 2 + 2 w L 3 ( R 2 ) 3 + 6 ε 2 K 4 + 24 ( χ 1 χ 2 ) 2 + 96 δ 2 u L 2 ( R 2 ) 2 + 3 δ w L 3 ( R 2 ) 3 4 + 24 ( χ 1 χ 2 ) 2 + 96 δ 2 C ( ε 2 ) u 0 L 1 ( R 2 ) + C 1 u 0 L 1 ( R 2 ) 3 + 1 δ 3 u 0 L 1 ( R 2 ) 3 .
We can use the Gagliardo–Nirenberg inequality and Young’s inequality to obtain
u L 2 ( R 2 ) 2 C G N u L 2 ( R 2 ) u 0 L 1 ( R 2 ) u L 2 ( R 2 ) 2 + C G N 2 4 u 0 L 1 ( R 2 ) 2 .
Taking a suitable value of ε 2 such that 6 ε 2 K 4 + 24 ( χ 1 χ 2 ) 2 + 96 δ 2 = min 9 2 δ , 6 ε 2 * > 0 , then substituting (23) into (22), we have
d d t 3 u L 2 ( R 2 ) 2 + 2 w L 3 ( R 2 ) 3 + min 3 2 δ , 2 ε 2 * 3 3 u L 2 ( R 2 ) 2 + 2 w L 3 ( R 2 ) 3 C ( ε 2 , δ , χ 1 , χ 2 , C G N , u 0 L 1 ( R 2 ) , w 0 L 1 ( R 2 ) )
for all 3 < ε 2 * < 6 .
Applying Gronwall’s inequality in (24), we show that
u L 2 ( R 2 ) + w L 3 ( R 2 ) C ,
where C > 0 is a constant depending on ε 2 , δ , χ 1 , χ 2 , C G N , u 0 L 1 ( R 2 ) L 2 ( R 2 ) , w 0 L 1 ( R 2 ) L 3 ( R 2 ) .
Taking p = 4 in (18), we can obtain
d d t 1 4 u L 4 ( R 2 ) 4 + 1 5 w L 5 ( R 2 ) 5 + 3 4 u 2 L 2 ( R 2 ) 2 + δ 2 w L 5 ( R 2 ) 5 81 ( χ 1 χ 2 ) 4 + 256 δ 4 + 4 5 u L 5 ( R 2 ) 5 + 1 5 v 2 L 5 ( R 2 ) 5 .
To control u L 5 ( R 2 ) , we use the Gagliardo–Nirenberg inequality and Young’s inequality to deduce
u L 5 ( R 2 ) 5 =   u 2 L 5 2 ( R 2 ) 5 2 C G N u 2 L 2 ( R 2 ) 3 2 u 2 L 1 ( R 2 ) ε 3 u 2 L 2 ( R 2 ) 2 + C ( ε 3 , C G N ) u L 2 ( R 2 ) 8 ,
where 0 < ε 3 < 1 has yet to be determined. Using the estimate (10) again, there exist a constant C 2 > 0 such that
v 2 L 5 ( R 2 ) C 2 5 w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 ) .
Taking the appropriate ε 3 such that 3 4 81 ( χ 1 χ 2 ) 4 + 256 δ 4 + 4 5 ε 3 = min 5 δ 8 , 3 4 ε 3 * > 0 , we can obtain
d d t 1 4 u 2 L 2 ( R 2 ) 2 + 1 5 w L 5 ( R 2 ) 5 + 4 min 5 δ 8 , 3 4 ε 3 * 1 4 u 2 L 2 ( R 2 ) 2 + 1 5 w L 5 ( R 2 ) 5 C 3
for all 0 < ε 3 * < 3 4 , where C 3 > 0 depends on u 0 L 1 ( R 2 ) L 2 ( R 2 ) , w 0 L 1 ( R 2 ) L 3 ( R 2 ) and C 2 . Similarly to (23), there is a constant C 4 > 0 such that
u 2 L 2 ( R 2 ) 2   u 2 L 2 ( R 2 ) 2 + C 4 u 0 L 2 ( R 2 ) 4 .
Combining (28) with (29) and applying Gronwall’s inequality yields
u L 4 ( R 2 ) + w L 5 ( R 2 ) C ,
where C > 0 depends on ε 3 , δ , χ 1 , χ 2 , C G N , u 0 L 1 ( R 2 ) L 2 ( R 2 ) L 4 ( R 2 ) , w 0 L 1 ( R 2 ) L 3 ( R 2 ) L 5 ( R 2 ) .
Using (8) and (9) in Lemma 2 and (30), we complete the proof of Lemma 6. □
In what follows, we will give the boundedness of u , v i and w.
Lemma 7. 
Assume χ 1 χ 2 holds. Then, for any p [ 1 , ] , we have
u L p ( R 2 ) + i = 1 2 v i W 2 , p ( R 2 ) + w L p ( R 2 ) C , i = 1 , 2 ,
where the constant C depends on χ i , λ i , u 0 L ( R 2 ) L 1 ( R 2 ) and w 0 L ( R 2 ) .
Proof. 
To obtain the L estimate of u, we first employ an energy inequality and Moser’s iteration technique. Next, we utilize the ODE comparison principle and classical elliptic theory to derive the estimates of w and v j .
Recalling (16) and (2), we integrate by parts for the right-hand side and use Young’s inequality to obtain
1 p d d t u L p ( R 2 ) p + 4 ( p 1 ) p 2 u p 2 2 2 = R 2 u p 1 · χ 1 u v 1 + · ( χ 2 u v 2 ) d x = ( p 1 ) R 2 u p 1 ( χ 1 v 1 χ 2 v 2 ) · u d x ( p 1 ) ( χ 1 + χ 2 ) M R 2 u p 1 | u | d x = 2 ( χ 1 + χ 2 ) ( p 1 ) M p R 2 u p 2 | u p 2 | d x 2 ( χ 1 + χ 2 ) ( p 1 ) M p u p 2 L 2 ( R 2 ) u p 2 L 2 ( R 2 ) 2 ( p 1 ) p 2 u p 2 2 2 + 2 ( p 1 ) ( χ 1 + χ 2 ) 2 M 2 u L p ( R 2 ) p .
That is,
d d t u L p ( R 2 ) p + p ( p 1 ) u L p ( R 2 ) p + 2 ( p 1 ) p u p 2 2 2 p ( p 1 ) 2 ( χ 1 + χ 2 ) 2 M 2 + 1 u L p ( R 2 ) p .
On the other hand, we can use the Gagliardo–Nirenberg inequality to deduce
u L p ( R 2 ) p = u p 2 L 2 ( R 2 ) 2 C G N u p 2 L 2 ( R 2 ) u p 2 L 1 ( R 2 ) 2 p 2 2 ( χ 1 + χ 2 ) 2 M 2 + 1 u p 2 2 2 + p 2 2 ( χ 1 + χ 2 ) 2 M 2 + 1 C G N 2 2 u p 2 L 1 ( R 2 ) 2 .
Substituting (33) into (32) gives
d d t u L p ( R 2 ) p + p ( p 1 ) u L p ( R 2 ) p p 3 ( p 1 ) 2 ( χ 1 + χ 2 ) 2 M 2 + 1 C G N 2 2 u L p 2 ( R 2 ) p .
Using Gronwall’s inequality, we have
u L p ( R 2 ) p e p ( p 1 ) t u 0 L p ( R 2 ) p + p 2 2 ( χ 1 + χ 2 ) 2 M 2 + 1 C G N 2 2 sup 0 t < u ( t ) L p 2 ( R 2 ) p .
Let B ( p ) = max u 0 L 1 ( R 2 ) , u 0 L ( R 2 ) , sup 0 t < u ( t ) L p ( R 2 ) . This yields
B ( p ) C 5 1 p p 2 p B ( p 2 ) for all p 2 ,
where C 5 = 1 + 2 ( χ 1 + χ 2 ) 2 M 2 + 1 C G N 2 2 is a constant.
Taking p = 2 j ( j = 1 , 2 , ) and applying the above iterative inequality, we see that
B ( 2 j ) C 5 2 j 2 j · 2 1 j B ( 2 j 1 ) C 5 2 j 2 j · 2 1 j · C 5 2 j + 1 2 ( j 1 ) · 2 2 j B ( 2 j 2 ) C 5 ( 2 j + 2 j + 1 + + 2 2 + 2 1 ) × 2 j · 2 1 j + ( j 1 ) 2 2 j + + 2 × 2 1 + 1 × 2 0 B ( 1 ) 4 C 5 B ( 1 ) .
By virtue of (34) and the boundedness of B ( 1 ) , we have
u L ( R 2 ) = lim j + B ( 2 j ) 4 C 5 B ( 1 ) 4 C 5 max u 0 L 1 ( R 2 ) , u 0 L ( R 2 ) .
Recalling (17) and applying interpolation inequality and Young’s inequality, we further have
1 p + 1 d d t w L p + 1 ( R 2 ) p + 1 + δ w L p + 1 ( R 2 ) p + 1 = R 2 u w p d x δ 2 w L p + 1 ( R 2 ) p + 1 + 2 p δ p u L p + 1 ( R 2 ) p + 1 δ 2 w L p + 1 ( R 2 ) p + 1 + 2 p δ p u L 1 ( R 2 ) u L ( R 2 ) p .
This means that
d d t w L p + 1 ( R 2 ) p + 1 + δ ( p + 1 ) 2 w L p + 1 ( R 2 ) p + 1 ( p + 1 ) ( 2 C 6 ) p δ p ,
where C 6 is a constant independent of p. Applying Gronwall’s inequality and the Lemma 2.1 in [29], we obtain
w L p + 1 ( R 2 ) w 0 L p + 1 ( R 2 ) p + 1 + 2 p + 1 C 6 p δ p + 1 1 p + 1 w 0 L p + 1 ( R 2 ) + 2 δ C 6 p p + 1 .
Letting p + , we can obtain the boundedness of w L ( R 2 ) . Finally, we use the classical elliptic estimate to obtain
D 2 v i L p ( R 2 ) C 7 w L p ( R 2 ) .
Applying the boundedness of w in (37), the proof is complete. □
Proof of Theorem 1. 
By virtue of Lemma 6 and Lemma 7 being complete, we complete the proof of the Theorem 1. □

4. Boundedness of Radial Solutions

In this section, we focus on the case of radial solutions. We assume that the non-negative initial data u 0 , w 0 are radially symmetric with respect to the spatial variable x and satisfy (3). We redefine the function u ˜ ( t , s ) , v ˜ j ( t , s ) ( j = 1 , 2 ) and w ˜ ( t , s ) as
u ( t , x ) = u ˜ ( t , s ) , v j ( t , x ) = v ˜ j ( t , s ) , w ( t , x ) = w ˜ ( t , s ) , s = π | x | 2
and the initial data as u 0 ( x ) = u ˜ ( s ) , w 0 ( x ) = w ˜ ( s ) . We denote the following:
U ( t , s ) = 0 s u ˜ ( t , σ ) d σ , V j ( t , s ) = 0 s u ˜ ( t , σ ) d σ , W ( t , s ) = 0 s w ˜ ( t , σ ) d σ ( j = 1 , 2 )
and U 0 ( s ) = 0 s u ˜ 0 ( σ ) d σ , W 0 ( s ) = 0 s u ˜ 0 ( σ ) d σ .
Similarly to Lemma 1, we have
U ( t , ) = 0 u ˜ ( t , s ) d s = 2 π 0 u ˜ ( t , π r 2 ) r d r = R 2 u ( t , x ) d x = u 0 L 1 ( R 2 )
and
W ( t , ) = 0 w ˜ ( t , s ) d s = R 2 w ( t , x ) d x w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 )
as well as
V j ( t , ) = 0 v ˜ j ( t , s ) d s = R 2 v j ( t , x ) d x 1 λ j w 0 L 1 ( R 2 ) + 1 λ j δ u 0 L 1 ( R 2 ) ( j = 1 , 2 ) .
Lemma 8. 
If the spatial variable x is a radial region and U is defined by (38), it holds that
𝜕 t U 4 π s 𝜕 s 2 U + χ 2 λ 2 V 2 + ( χ 1 χ 2 ) M 0 𝜕 s U .
Proof. 
By straightforward calculations, we have
𝜕 x j u = 𝜕 s u ˜ 𝜕 x j s = 2 π x j 𝜕 s u ˜
and
𝜕 x i x j 2 u = 𝜕 x j ( 2 π x i 𝜕 s u ˜ ) = 2 π δ i j 𝜕 s u ˜ + 4 π 2 x i x j 𝜕 s 2 u ˜ .
Therefore, we obtain
Δ u = j = 1 2 𝜕 x j 2 u = 4 π 𝜕 s u ˜ + 4 π 2 | x | 2 𝜕 s 2 u ˜ = 4 π 𝜕 s u ˜ + 4 π s 𝜕 s 2 u ˜ = 4 π 𝜕 s ( s 𝜕 s u ˜ )
and
· ( u v j ) = i = 1 2 𝜕 i ( u 𝜕 i v j ) = i = 1 2 𝜕 i u 𝜕 i v j + u i = 1 2 𝜕 i 2 v j = 4 π 2 | x | 2 𝜕 s u ˜ 𝜕 s v ˜ j + 4 π u ˜ 𝜕 s ( s 𝜕 s v ˜ j ) = 4 π s 𝜕 s u ˜ 𝜕 s v ˜ j + 4 π u ˜ 𝜕 s ( s 𝜕 s v ˜ j ) = 4 π 𝜕 s ( s u ˜ 𝜕 s v ˜ j )
as well as
𝜕 t u ˜ = 𝜕 t u = Δ u · ( χ 1 u v 1 ) + · ( χ 2 u v 2 ) = 4 π 𝜕 s ( s 𝜕 s u ˜ ) 4 π χ 1 𝜕 s ( s u ˜ 𝜕 s v ˜ 1 ) + 4 π χ 2 𝜕 s ( s u ˜ 𝜕 s v ˜ 2 ) = 4 π 𝜕 s ( s 𝜕 s u ˜ ) 4 π 𝜕 s s u ˜ 𝜕 s ( χ 1 v ˜ 1 χ 2 v ˜ 2 ) .
Integrating both sides of (2) from 0 to s and combining (43)–(45) yields
𝜕 t U = 4 π ( s 𝜕 s u ˜ ) 4 π s u ˜ 𝜕 s ( χ 1 v ˜ 1 χ 2 v ˜ 2 ) = 4 π s 𝜕 s 2 U 4 π s 𝜕 s U 𝜕 s ( χ 1 v ˜ 1 χ 2 v ˜ 2 ) = 4 π s 𝜕 s 2 U 𝜕 s U 4 π χ 1 s 𝜕 s v ˜ 1 4 π χ 2 s 𝜕 s v ˜ 2 .
Applying the second equations of (2) and (43), we can deduce
Δ v j = 4 π 𝜕 s ( s 𝜕 s v ˜ j ) = λ j v j w ( j = 1 , 2 ) .
Similarly to (46), integrating both sides of (47), we see that
4 π s 𝜕 s v ˜ j = λ j V j W .
Substituting (48) into (46), we have
𝜕 t U = 4 π s 𝜕 s 2 U 𝜕 s U χ 1 ( λ 1 V 1 W ) χ 2 ( λ 2 V 2 W ) = 4 π s 𝜕 s 2 U + ( χ 1 χ 2 ) W 𝜕 s U ( χ 1 λ 1 V 1 χ 2 λ 2 V 2 ) 𝜕 s U .
Using the third equation of (2) again, we can solve the ODE to obtain
w ( t , x ) = w 0 ( x ) e δ t + 0 t e δ ( τ t ) u ( τ , x ) d τ .
So, we can integrate the both sides of (50) to obtain
W ( t , s ) = e δ t · 0 s w ˜ 0 ( σ ) d σ + 0 t e δ ( τ t ) 0 s u ˜ ( τ , σ ) d σ d τ = e δ t W 0 ( s ) + 0 t e δ ( τ t ) U ( τ , s ) d τ .
Combining (49) and (51) and using the first mean-value theorem and 𝜕 s U 0 , we have
𝜕 t U = 4 π s 𝜕 s 2 U + ( χ 1 χ 2 ) W 𝜕 s U ( χ 1 λ 1 V 1 χ 2 λ 2 V 2 ) 𝜕 s U = 4 π s 𝜕 s 2 U + ( χ 1 χ 2 ) e δ t W 0 ( s ) + 0 t e δ ( τ t ) U ( τ , s ) d τ 𝜕 s U ( χ 1 λ 1 V 1 χ 2 λ 2 V 2 ) 𝜕 s U = 4 π s 𝜕 s 2 U + ( χ 1 χ 2 ) e δ t W 0 ( s ) + 1 δ 1 e δ t U ( θ t , s ) 𝜕 s U ( χ 1 λ 1 V 1 χ 2 λ 2 V 2 ) 𝜕 s U = 4 π s 𝜕 s 2 U + χ 1 χ 2 δ 1 e α t U ( θ t , s ) 𝜕 s U χ 1 λ 1 V 1 χ 2 λ 2 V 2 ( χ 1 χ 2 ) e δ t W 0 ( s ) 𝜕 s U 4 π s 𝜕 s 2 U + ( χ 1 χ 2 ) u 0 L 1 ( R 2 ) δ + w 0 L 1 ( R 2 ) + χ 2 λ 2 V 2 𝜕 s U .
It means that
𝜕 t U 4 π s 𝜕 s 2 U + χ 2 λ 2 V 2 + ( χ 1 χ 2 ) M 0 𝜕 s U .
Therefore, we complete the proof of Lemma 8. □
Recalling (31), regarding the construction of iterative techniques, we need to sup t > 0 v j L < ( j = 1 , 2 ) . By virtue of (48) and s = π | x | 2 , we have
| 𝜕 i v j ( t , x ) | =   | 𝜕 s 𝜕 x · 𝜕 s v j ( t , x ) | = 2 π | x | | 𝜕 s v ˜ j ( t , s ) | = 1 2 π s | λ j V j ( t , s ) W ( t , s ) | ( j = 1 , 2 ) .
Lemma 9. 
Suppose that the spatial variable is a radial region and M 0 2 π χ 1 χ 2 holds. Then, we have
i = 1 2 sup t > 0 v j L < .
Proof. 
First, for the term V j ( t , s ) , applying the Hölder’s inequality, the estimate of (10) and (41), we deduce that
0 V j ( t , s ) = 0 s v ˜ j ( t , σ ) d σ s 1 2 0 v j 2 ( t , σ ) d σ 1 2 s 1 2 C ( 2 ) w ( t ) L 1 ( R 2 ) C ( 2 ) s 1 2 w 0 L 1 ( R 2 ) + 1 δ u 0 L 1 ( R 2 ) = C ( 2 ) M 0 s ( j = 1 , 2 ) .
For convenience, taking the operator N g : = 4 π s 𝜕 s 2 g + C ( 2 ) s + χ 1 χ 2 M 0 𝜕 s g , we can obtain the equivalent form
𝜕 t U N U , t > 0 , s > 0 , U ( t , 0 ) = 0 , U ( t , + ) = u 0 L 1 ( R 2 ) , t > 0 , U ( 0 , s ) = U 0 ( s ) , s 0 .
Next, we define a comparison function G(s) as G ( s ) = R s 1 ( χ 1 χ 2 ) M 0 4 π e α s , where α : = C ( 2 ) M 0 2 π and R are two positive constants. Let β : = 1 ( χ 1 χ 2 ) M 0 4 π 1 2 . That is,
G ( s ) = R s β e α s for α > 0 , β 1 2 .
We can take a R > 0 value that is suitably large such that
U 0 ( s ) u 0 L 1 ( R 2 ) < R s 0 1 ( χ 1 χ 2 ) M 0 4 π e α s 0 for 0 < s s 0 .
Through a direct calculation, we can obtain
N G ( s ) = 4 π s d 2 G ( s ) d s 2 + C ( 2 ) s + χ 1 χ 2 M 0 d G ( s ) d s = 0 .
Therefore, we have the following gradient flow
𝜕 t U N U , N G = 0 , 0 < t < , 0 < s < s 0 , U ( t , 0 ) = G ( 0 ) = 0 , U ( t , s 0 ) u 0 L 1 ( R 2 ) < G ( s 0 ) 0 t < , U ( 0 , s ) = U 0 ( s ) < G ( s ) , 0 s s 0 .
Applying the comparison principle, we have
U ( t , s ) G ( s ) R s β e α s .
Thus, applying (51), we see that
W ( t , s ) = e δ t 0 s w 0 ( σ ) d σ + 0 t e τ t U ( τ , s ) d τ w 0 ( x ) L 2 ( R 2 ) s e δ t + R s β e α s w 0 ( x ) L 1 ( R 2 ) 1 2 w 0 ( x ) L ( R 2 ) 1 2 s + R s β e α s .
Noticing (53) and applying (54) and (60), we complete the proof of Lemma 9. □
Proof of Theorem 2. 
Thanks to the results obtained from Lemmas 8 and 9, and by employing the iterative technique described in Lemma 7, we complete the proof of Theorem 2. □

Author Contributions

J.W. contributed methods, ideas and writing; Y.H. was responsible for checking and revising the manuscript. All authors have read and agreed to the published version of the manuscript.

Funding

J. Wu was supported by Scientific Research Funds of Chengdu University under grant No. 2081921030, which also was supported funding of the Visual Computing and Virtual Reality Key Laboratory of Sichuan Province under grant No. SCVCVR2023.09VS.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The authors declare no conflicts of interest.

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Wu, J.; Huang, Y. Boundedness of Solutions for an Attraction–Repulsion Model with Indirect Signal Production. Mathematics 2024, 12, 1143. https://doi.org/10.3390/math12081143

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Wu J, Huang Y. Boundedness of Solutions for an Attraction–Repulsion Model with Indirect Signal Production. Mathematics. 2024; 12(8):1143. https://doi.org/10.3390/math12081143

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Wu, Jie, and Yujie Huang. 2024. "Boundedness of Solutions for an Attraction–Repulsion Model with Indirect Signal Production" Mathematics 12, no. 8: 1143. https://doi.org/10.3390/math12081143

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