1 Introduction

The q-difference equations initiated in the beginning of the 20th century [14], is a very interesting field in difference equations. In the last few decades, it has evolved into a multidisciplinary subject and plays an important role in several fields of physics, such as cosmic strings and black holes [5], conformal quantum mechanics [6], and nuclear and high-energy physics [7]. For some recent work on q-difference equations, we refer the reader to [812]. However, the theory of boundary value problems (BVPs) for nonlinear q-difference equations is still in an early stage and many aspects of this theory need to be explored. To the best of our knowledge, for the BVPs of nonlinear third-order q-difference equations, a few works were done, see [13, 14] and the references therein.

Recently, in [15], El-Shahed has studied the existence of positive solutions for the following nonlinear singular third-order BVP:

{ u ( t ) + λ a ( t ) f ( u ( t ) ) = 0 , 0 t 1 , u ( 0 ) = u ( 0 ) = 0 , α u ( 1 ) + β u ( 1 ) = 0 ,

by Krasnoselskii’s fixed-point theorem on a cone.

More recently, in [13] Ahmad has studied the existence of positive solutions for the following nonlinear BVP of third-order q-difference equations:

{ D q 3 u ( t ) = f ( t , u ( t ) ) , 0 t 1 , u ( 0 ) = 0 , D q u ( 0 ) = 0 , u ( 1 ) = 0 ,

by Leray-Schauder degree theory and some standard fixed-point theorems.

Motivated by the work above, in this paper, we will study the following BVP of nonlinear singular third-order q-difference equations:

{ D q 3 u ( t ) + λ a ( t ) f ( u ( t ) ) = 0 , t I q , u ( 0 ) = 0 , D q u ( 0 ) = 0 , α D q u ( 1 ) + β D q 2 u ( 1 ) = 0 ,
(1.1)

where λ>0 is a positive parameter, a:(0,1)[0,) is continuous and 0< 0 1 a(t) d q t<, f is a continuous function, I q ={ q n :nN}{0,1}, q(0,1) is a fixed constant, and α,β0, α+β>0.

Obviously, when q 1 , BVP (1.1) reduces to the standard BVP in [15].

Throughout this paper, we always suppose the following conditions to hold:

(C1) fC([0,1],[0,+));

(C2) α,β0, α+β>0 and α β α + β q.

2 Preliminary results

In this section, firstly, let us recall some basic concepts of q-calculus [16, 17].

Definition 2.1 For 0<q<1, we define the q-derivative of a real-value function f as

D q f(t)= f ( t ) f ( q t ) ( 1 q ) t ,t I q {0}, D q f(0)= lim t 0 D q f(t).

Note that lim q 1 D q f(t)= f (t).

Definition 2.2 The higher-order q-derivatives are defined inductively as

D q 0 f(t)=f(t), D q n f(t)= D q D q n 1 f(t),nN.

For example, D q ( t k )= [ k ] q t k 1 , where k is a positive integer and the bracket [ k ] q =( q k 1)/(q1). In particular, D q ( t 2 )=(1+q)t.

Definition 2.3 The q-integral of a function f defined in the interval [a,b] is given by

a x f(t) d q t:= n = 0 x(1q) q n f ( x q n ) af ( a q n ) ,x[a,b],

and for a=0, we denote

I q f(x)= 0 x f(t) d q t= n = 0 x(1q) q n f ( x q n ) ,

then

a b f(t) d q t= 0 b f(t) d q t 0 a f(t) d q t.

Similarly, we have

I q 0 f(t)=f(t), I q n f(t)= I q I q n 1 f(t),nN.

Observe that

D q I q f(x)=f(x),

and if f is continuous at x=0, then I q D q f(x)=f(x)f(0).

In q-calculus, the product rule and integration by parts formula are

D q (gh)(t)= D q g(t)h(t)+g(qt) D q h(t),
(2.1)
0 x f(t) D q g(t) d q t= [ f ( t ) g ( t ) ] 0 x 0 x D q f(t)g(qt) d q t.
(2.2)

Remark 2.1 In the limit q 1 , the above results correspond to their counterparts in standard calculus.

Definition 2.4 Let E be a real Banach space. A nonempty closed convex set PE is called a cone if it satisfies the following two conditions:

  1. (i)

    xP, λ0 implies λxP;

  2. (ii)

    xP, xP implies x=0.

Theorem 2.1 (Krasnoselskii) [18]

Let E be a Banach space and let KE be a cone in E. Assume that Ω 1 and Ω 2 are open subsets of E with 0 Ω 1 and Ω ¯ 1 Ω 2 . Let T:K( Ω ¯ 2 Ω 1 )K be a completely continuous operator. In addition, suppose either

(H1) Tuu, uK Ω 1 and Tuu, uK Ω 2 or

(H2) Tuu, uK Ω 2 and Tuu, uK Ω 1

holds. Then T has a fixed point in K( Ω ¯ 2 Ω 1 ).

Lemma 2.1 Let yC[0,1], then the BVP

{ D q 3 u ( t ) + y ( t ) = 0 , t I q , u ( 0 ) = 0 , D q u ( 0 ) = 0 , α D q u ( 1 ) + β D q 2 u ( 1 ) = 0 ,
(2.3)

has a unique solution

u(t)= 0 1 G(t,s;q)y(s) d q s,

where

G(t,s;q)= 1 ( 1 + q ) ( α + β ) { α t 2 ( 1 q s ) + β t 2 ( t q s ) ( t q 2 s ) ( α + β ) , 0 s t 1 , α t 2 ( 1 q s ) + β t 2 , 0 t s 1 .

Proof Integrate the q-difference equation from 0 to t, we get

D q 2 u(t)= 0 t y(s) d q s+ a 2 .
(2.4)

Integrate (2.4) from 0 to t, and change the order of integration, we have

D q u(t)= 0 t (tqs)y(s) d q s+ a 2 t+ a 1 .
(2.5)

Integrating (2.5) from 0 to t, and changing the order of integration, we obtain

u(t)= 0 t ( t 2 + q 3 s 2 1 + q q t s ) y(s) d q s+ a 2 1 + q t 2 + a 1 t+ a 0 ,
(2.6)

where a 2 , a 1 , a 0 are arbitrary constants. Using the boundary conditions u(0)=0, D q u(0)=0, α D q u(1)+β D q 2 u(1)=0 in (2.6), we find that a 0 = a 1 =0, and

a 2 = 1 α + β ( α 0 1 ( 1 q s ) y ( s ) d q s + β 0 1 y ( s ) d q s ) .

Substituting the values of a 2 , a 1 , and a 0 in (2.6), we obtain

u ( t ) = 0 t ( t 2 + q 3 s 2 1 + q q t s ) y ( s ) d q s + t 2 ( 1 + q ) ( α + β ) ( α 0 1 ( 1 q s ) y ( s ) d q s + β 0 1 y ( s ) d q s ) = 0 1 G ( t , s ; q ) y ( s ) d q s ,

where

G(t,s;q)= 1 ( 1 + q ) ( α + β ) { α t 2 ( 1 q s ) + β t 2 ( t q s ) ( t q 2 s ) ( α + β ) , 0 s t 1 , α t 2 ( 1 q s ) + β t 2 , 0 t s 1 .

This completes the proof. □

Remark 2.2 For q1, equation (2.6) takes the form

u(t)= 1 2 0 t ( t s ) 2 y(s) d q s+ a 2 2 t 2 + a 1 t+ a 0 ,

which is the solution of a classical third-order ordinary differential equation u (t)+y(t)=0 and the associated form of Green’s function for the classical case is

G(t,s)= 1 2 ( α + β ) { α t 2 ( 1 s ) + β t 2 ( t s ) 2 ( α + β ) , 0 s t 1 , α t 2 ( 1 s ) + β t 2 , 0 t s 1 .

It is obvious that, when (C2) holds, G(t,s;q)0, and G(t,s;q)G(1,s;q), 0t,s1.

Lemma 2.2 Let (C2) hold, then G(t,s;q)g(t)G(1,s;q) for 0t,s1, where g(t)= 4 β 5 ( α + β ) t 2 .

Proof If ts, then

G ( t , s ; q ) G ( 1 , s ; q ) = α t 2 ( 1 q s ) ( 1 + q ) ( α + β ) + β t 2 ( 1 + q ) ( α + β ) α ( 1 q s ) ( 1 + q ) ( α + β ) + β ( 1 + q ) ( α + β ) = t 2 α q s α + β t 2 1 α q s α + β t 2 α α + β t 2 = β α + β t 2 4 β 5 ( α + β ) t 2 .

If ts, then

G ( t , s ; q ) G ( 1 , s ; q ) = α t 2 ( 1 q s ) ( 1 + q ) ( α + β ) + β t 2 ( 1 + q ) ( α + β ) t 2 + q 3 s 2 1 + q + q t s α ( 1 q s ) ( 1 + q ) ( α + β ) + β ( 1 + q ) ( α + β ) 1 + q 3 s 2 1 + q + q s = α q s α + β t 2 q 3 s 2 + ( 1 + q ) q t s α q s α + β q 3 s 2 + ( 1 + q ) q s ( 1 + q ) q t 2 α q s α + β t 2 q 3 s 2 ( 1 + q ) q s q 3 s 2 = ( 1 + q ) t 2 α s α + β t 2 q 2 s 2 ( 1 + q ) s q 2 s 2 t 2 α α + β t 2 1 + q q 2 4 β 5 ( α + β ) t 2 .

The proof is complete. □

We consider the Banach space C q =C( I q ,R) equipped with standard norm u=sup{|u(t)|,t I q }, u C q . Define a cone P by

P= { u C q | u ( t ) 0 , u ( t ) g ( t ) u , t I q } .

It is easy to see that if uP, then u=u(1).

Define an integral operator T:P C q by

Tu(t)=λ 0 1 G(t,s;q)a(s)f ( u ( s ) ) d q s,t I q ,uP.
(2.7)

Obviously, T is well defined and uP is a solution of BVP (1.1) if and only if u is a fixed point of T.

Remark 2.3 By Lemma 2.2, we obtain, for uP, Tu(t)0 on I q and

T u ( t ) = λ 0 1 G ( t , s ; q ) a ( s ) f ( u ( s ) ) d q s λ g ( t ) 0 1 G ( 1 , s ; q ) a ( s ) f ( u ( s ) ) d q s λ g ( t ) sup t I q 0 1 G ( t , s ; q ) a ( s ) f ( u ( s ) ) d q s = g ( t ) T u .

Thus T(P)P.

We adopt the following assumption:

(C3) a(t)C((0,1), R + ) may be singular at t=0,1, 0< 0 1 a(t) d q t<+, and 0< 0 1 G(1,s;q)a(t) d q t<+.

Lemma 2.3 Assume (C1), (C2), and (C3) hold, then T:PP is completely continuous.

Proof Define the functions a n (t) for n2 by

a n (t)= { inf { a ( t ) , a ( 1 n ) } , 0 t 1 n , a ( t ) , 1 n t 1 1 n , inf { a ( t ) , a ( 1 1 n ) } , 1 1 n t 1 .

Next, for n2, we define the operator T n :PP by

T n u(t)=λ 0 1 G(t,s;q) a n (s)f ( u ( s ) ) d q s,t I q ,uP.

Obviously, T n is completely continuous on P for any n2 by an application of the Ascoli-Arzelá theorem. Denote B K ={uP:uK}. Then T n converges uniformly to T as n. In fact, for any t I q , for each fixed K>0 and u B K , from (C1), we obtain

| T n u ( t ) T u ( t ) | = | λ 0 1 G ( t , s ; q ) [ a ( s ) a n ( s ) ] f ( u ( s ) ) d q s | λ 0 1 n G ( 1 , s ; q ) | a ( s ) a n ( s ) | f ( u ( s ) ) d q s + λ 1 n 1 1 n G ( 1 , s ; q ) | a ( s ) a n ( s ) | f ( u ( s ) ) d q s + λ 1 1 n 1 G ( 1 , s ; q ) | a ( s ) a n ( s ) | f ( u ( s ) ) d q s 0 ( n ) ,

where we have used the fact that G(t,s;q)0, and G(t,s;q)G(1,s;q), 0t,s1. Hence, T n converges uniformly to T as n, and therefore T is completely continuous also. This completes the proof. □

3 Main results

In this section, we will apply Krasnoselskii’s fixed-point theorem to the eigenvalue problem (1.1). First, we define some important constants:

A q = 0 1 G ( 1 , s ; q ) a ( s ) g ( s ) d q s , B q = 0 1 G ( 1 , s ; q ) a ( s ) d q s , F 0 = lim u 0 + sup f ( u ) u , f 0 = lim u 0 + inf f ( u ) u , F = lim u + sup f ( u ) u , f = lim u + inf f ( u ) u .

Here we assume that 1 A q f =0 if f = and 1 B q F 0 = if F 0 =0 and 1 A q f 0 =0 if f 0 = and 1 B q F = if F =0.

The main result of this paper is the following.

Theorem 3.1 Suppose that (C1), (C2) and (C3) hold and A q f > B q F 0 . Then for each λ( 1 A q f , 1 B q F 0 ), BVP (1.1) has at least one positive solution.

Proof By the definition of F 0 , we see that there exists an l 1 >0, such that f(u)( F 0 +ε)u for 0u l 1 . If uP with u= l 1 , we have

Tu=Tu(1)=λ 0 1 G(1,s;q)a(s)f ( u ( s ) ) d q sλ( F 0 +ε)u B q .

Choose ε>0 sufficiently small such that λ( F 0 +ε) B q 1. Then we obtain Tuu. Thus if we let Ω 1 ={u C q |u< l 1 }, then Tuu for uP Ω 1 .

From the definition of f , we see that there exist an l 3 >0 and l 3 > l 1 , such that f(u)( f ε)u for u> l 2 . Let l 2 > l 3 , if uP with u= l 2 we have

T u = T u ( 1 ) = λ 0 1 G ( 1 , s ; q ) a ( s ) f ( u ( s ) ) d q s λ 0 1 G ( 1 , s ; q ) a ( s ) g ( s ) f ( u ( s ) ) d q s λ ( f ε ) u A q .

Choose ε>0 sufficiently small such that λ( f ε) A q 1. Then we have Tuu. Let Ω 2 ={u C q |u< l 2 }, then Ω 1 Ω ¯ 2 and Tuu for uP Ω 2 .

Condition (H1) of Krasnoselskii’s fixed-point theorem is satisfied. Hence, by Theorem 2.1, the result of Theorem 3.1 holds. This completes the proof of Theorem 3.1. □

Theorem 3.2 Suppose that (C1), (C2) and (C3) hold and A q f 0 > B q F . Then for each λ( 1 A q f 0 , 1 B q F ), BVP (1.1) has at least one positive solution.

Proof It is similar to the proof of Theorem 3.1. □

Theorem 3.3 Suppose that (C1), (C2) and (C3) hold and λ B q f(u)<u for u(0,+). Then BVP (1.1) has no positive solution.

Proof Assume to the contrary that u is a positive solution of BVP (1.1). Then

u ( 1 ) = λ 0 1 G ( 1 , s ; q ) a ( s ) f ( u ( s ) ) d q s < 1 B q 0 1 G ( 1 , s ; q ) a ( s ) u ( s ) d q s u ( 1 ) B q 0 1 G ( 1 , s ; q ) a ( s ) d q s = u ( 1 ) .

This is a contradiction and completes the proof. □

Theorem 3.4 Suppose that (C1), (C2) and (C3) hold and λ A q f(u)>u for u(0,+). Then BVP (1.1) has no positive solution.

Proof It is similar to the proof of Theorem 3.3. □

4 Example

Consider the following BVP:

{ D 1 2 3 u ( t ) + λ t 1 2 10 u 2 + u u + 1 ( 5 + sin u ) = 0 , t I q , u ( 0 ) = 0 , D 1 2 u ( 0 ) = 0 , D 1 2 u ( 1 ) + 3 D 1 2 2 u ( 1 ) = 0 .
(4.1)

Then F 0 =6, f 0 =4, F =60, f =40, and 4uf(u)60u. By direct calculations, we obtain A q =0.110963 and B q =0.271661. From Theorem 3.1 we see that if λ(0.225299,0.613510) then the problem (4.1) has a positive solution. From Theorem 3.3 we see that if λ<0.061351 then the problem (4.1) has no positive solution. By Theorem 3.4 we see that if λ>2.252986 then the problem (4.1) has no positive solution.