1 Introduction

In the year 2003 Agrawal and Mohammad [1] introduced a new sequence of linear positive operators by modifying the well-known Baskakov operators having weight functions of Szasz basis function as

D n (f,x)=n k = 1 p n , k (x) 0 s n , k 1 (t)f(t)dt+ p n , 0 (x)f(0),x[0,),
(1.1)

where

p n , k (x)= ( n + k 1 k ) x k ( 1 + x ) n + k , s n , k (t)= e n t ( n t ) k k ! .

It is observed in [1] that these operators reproduce constant as well as linear functions. Later, some direct approximation results for the iterative combinations of these operators were studied in [14].

A lot of works on q-calculus are available in literature of different branches of mathematics and physics. For systematic study, we refer to the work of Ernst [5], Kim [10, 11], and Kim and Rim [9]. The application of q-calculus in approximation theory was initiated by Phillips [13], who was the first to introduce q-Bernstein polynomials and study their approximation properties. Very recently the q-analogues of the Baskakov operators and their Kantorovich and Durrmeyer variants have been studied in [2, 3] and [7] respectively. We recall some notations and concepts of q-calculus. All of the results can be found in [5] and [8]. In what follows, q is a real number satisfying 0<q<1.

For nN,

The q-binomial coefficients are given by

[ n k ] q = [ n ] q ! [ k ] q ! [ n k ] q ! ,0kn.

The q-Beta integral is defined by [12]

Γ q (t)= 0 1 1 q x t 1 E q (qx) d q x,t>0,
(1.2)

which satisfies the following functional equation:

Γ q (t+1)= [ t ] q Γ q (t), Γ q (1)=1.

For fC[0,)q>0 and each positive integer n, the q-Baskakov operators [2] are defined as

B n , q ( f , x ) = k = 0 [ n + k 1 k ] q q k ( k 1 ) 2 x k ( 1 + x ) q n + k f ( [ k ] q q k 1 [ n ] q ) = k = 0 p n , k q ( x ) f ( [ k ] q q k 1 [ n ] q ) ,
(1.3)

where

( 1 + x ) q n :={ ( 1 + x ) ( 1 + q x ) ( 1 + q n 1 x ) , n = 1 , 2 , , 1 , n = 0 .

Remark 1 The first three moments of the q-Baskakov operators are given by

As the operators D n (f,x) have mixed basis functions in summation and integration and have an interesting property of reproducing linear functions, we were motivated to study these operators further. Here we define the q-analogue of the operators as

D n q (f,x)= [ n ] q k = 1 p n , k q (x) 0 q / ( 1 q n ) q k s n , k 1 q (t)f ( t q k ) d q t+ p n , 0 q (x)f(0),
(1.4)

where x[0,) and

p n , k q (x)=[ n + k 1 k ] q q k ( k 1 ) 2 x k ( 1 + x ) q n + k , s n , k q (t)= E q ( [ n ] q t ) ( [ n ] q t ) k [ k ] q ! .

In case q=1, the above operators reduce to the operators (1.1). In the present paper, we estimate a local approximation theorem and the rate of convergence of these new operators as well as their weighted approximation properties.

2 Moment estimation

Lemma 1 The following equalities hold:

  1. (i)

    D n q (1,x)=1,

  2. (ii)

    D n q (t,x)=x,

  3. (iii)

    D n q ( t 2 ,x)= x 2 + x [ n ] q (1+q+ x q ).

Proof The operators D n q are well defined on the function 1,t, t 2 . Then for every x[0,), we obtain

D n q (1,x)= [ n ] q k = 1 p n , k q (x) 0 q / ( 1 q n ) q k ( [ n ] q t ) k 1 [ k 1 ] q ! E q ( [ n ] q t ) d q t+ p n , 0 q (x).

Substituting [ n ] q t=qy and using (1.2), we have

D n q ( 1 , x ) = [ n ] q k = 1 p n , k q ( x ) 0 1 / ( 1 q ) q k ( q y ) k 1 [ k 1 ] q ! E q ( q y ) q d q y [ n ] q + p n , 0 q ( x ) = k = 1 p n , k q ( x ) + p n , 0 q ( x ) = B n , q ( 1 , x ) = 1 ,

where B n , q (f,x) is the q-Baskakov operator defined by (1.3).

Next, we have

D n q (t,x)= [ n ] q k = 1 p n , k q (x) 0 q / ( 1 q n ) q k ( [ n ] q t ) k 1 [ k 1 ] q ! E q ( [ n ] q t ) t q k d q t.

Again substituting [ n ] q t=qy and using (1.2), we have

D n q ( t , x ) = [ n ] q k = 1 p n , k q ( x ) 0 1 / ( 1 q ) q k ( q y ) k [ k 1 ] q ! [ n ] q E q ( q y ) q d q y [ n ] q q k = k = 0 p n , k q ( x ) q [ k ] q [ n ] q q k = B n , q ( t , x ) = x .

Finally,

D n q ( t 2 , x ) = [ n ] q k = 0 p n , k q (x) 0 q / ( 1 q n ) q k ( [ n ] q t ) k 1 [ k 1 ] q ! E q ( [ n ] q t ) t 2 q 2 k d q t.

Again substituting [ n ] q t=qy, using (1.2) and [ k + 1 ] q = [ k ] q + q k , we have

D n q ( t 2 , x ) = [ n ] q k = 1 p n , k q ( x ) 0 1 / ( 1 q ) q k ( q y ) k + 1 [ k 1 ] q ! [ n ] q 2 E q ( q y ) q 2 k q d q y [ n ] q = k = 1 p n , k q ( x ) [ k + 1 ] q [ k ] q [ n ] q 2 q 2 k 2 = k = 1 p n , k q ( x ) ( [ k ] q + q k ) [ k ] q [ n ] q 2 q 2 k 2 = B n , q ( t 2 , x ) + q [ n ] q B n , q ( t , x ) = x 2 + x [ n ] q ( 1 + q + x q ) .

 □

Remark 2 If we put q=1, we get the moments of a new sequence D n (f,x) considered in [1] as operators as

Lemma 2 Letq(0,1), then forx[0,)we have

D n q ( ( t x ) 2 , x ) = x ( x + q [ 2 ] q ) q [ n ] q .

3 Direct theorems

By C B [0,) we denote the space of real valued continuous bounded functions f on the interval [0,); the norm- on the space C B [0,) is given by

f= sup 0 x < | f ( x ) | .

The Peetre’s K-functional is defined by

K 2 (f,δ)=inf { f g + δ g : g W 2 } ,

where W 2 ={g C B [0,): g , g C B [0,)}. By [4], pp.177], there exists a positive constant C>0 such that K 2 (f,δ)C ω 2 (f, δ 1 / 2 )δ>0 and the second order modulus of smoothness is given by

ω 2 ( f , δ ) = sup 0 < h δ sup 0 x < | f ( x + 2 h ) 2 f ( x + h ) + f ( x ) | .

Also, for f C B [0,) a usual modulus of continuity is given by

ω(f,δ)= sup 0 < h δ sup 0 x < | f ( x + h ) f ( x ) | .

Theorem 1 Letf C B [0,)and0<q<1. Then for allx[0,)andnN, there exists an absolute constantC>0such that

| D n q ( f , x ) f ( x ) | C ω 2 ( f , x ( x + q [ 2 ] q ) q [ n ] q ) .

Proof Let g W 2 and x,t[0,). By Taylor’s expansion, we have

g(t)=g(x)+ g (x)(tx)+ x t (tu) g (u)du.

Applying Lemma 2, we obtain

D n q (g,x)g(x)= D n q ( x t ( t u ) g ( u ) d u , x ) .

Obviously, we have | x t (tu) g (u)du| ( t x ) 2 g . Therefore,

| D n q ( g , x ) g ( x ) | D n q ( ( t x ) 2 , x ) g = x ( x + q [ 2 ] q ) q [ n ] q g .

Using Lemma 1, we have

| D n q ( f , x ) | [ n ] q k = 1 p n , k q (x) 0 q / ( 1 q n ) q k s n , k 1 q (t) | f ( t q k ) | d q t+ p n , 0 q (x) | f ( 0 ) | f.

Thus

| D n q ( f , x ) f ( x ) | | D n q ( f g , x ) ( f g ) ( x ) | + | D n q ( g , x ) g ( x ) | 2 f g + x ( x + q [ 2 ] q ) q [ n ] q g .

Finally, taking the infimum over all g W 2 and using the inequality K 2 (f,δ)C ω 2 (f, δ 1 / 2 ), δ>0, we get the required result. This completes the proof of Theorem 1. □

We consider the following class of functions:

Let H x 2 [0,) be the set of all functions f defined on [0,) satisfying the condition |f(x)| M f (1+ x 2 ), where M f is a constant depending only on f. By C x 2 [0,), we denote the subspace of all continuous functions belonging to H x 2 [0,). Also, let C x 2 [0,) be the subspace of all functions f C x 2 [0,), for which lim | x | f ( x ) 1 + x 2 is finite. The norm on C x 2 [0,) is f x 2 = sup x [ 0 , ) | f ( x ) | 1 + x 2 . We denote the modulus of continuity of f on closed interval [0,a], a>0 as by

ω a (f,δ)= sup | t x | δ sup x , t [ 0 , a ] | f ( t ) f ( x ) | .

We observe that for function f C x 2 [0,), the modulus of continuity ω a (f,δ) tends to zero.

Theorem 2 Letf C x 2 [0,), q(0,1)and ω a + 1 (f,δ)be its modulus of continuity on the finite interval[0,a+1][0,), wherea>0. Then for everyn>2,

D n q ( f ) f C [ 0 , a ] 6 M f a ( 1 + a 2 ) ( 2 + a ) q [ n ] q +2ω ( f , a ( a + q [ 2 ] q ) q [ n ] q ) .

Proof For x[0,a] and t>a+1, since tx>1, we have

| f ( t ) f ( x ) | M f ( 2 + x 2 + t 2 ) M f ( 2 + 3 x 2 + 2 ( t x ) 2 ) 6 M f ( 1 + a 2 ) ( t x ) 2 .
(3.1)

For x[0,a] and ta+1, we have

|f(t)f(x)| ω a + 1 ( f , | t x | ) ( 1 + | t x | δ ) ω a + 1 (f,δ)
(3.2)

with δ>0.

From (3.1) and (3.2) we can write

|f(t)f(x)|6 M f ( 1 + a 2 ) ( t x ) 2 + ( 1 + | t x | δ ) ω a + 1 (f,δ)
(3.3)

for x[0,a] and t0. Thus

| D n q ( f , x ) f ( x ) | D n q ( | f ( t ) f ( x ) | , x ) 6 M f ( 1 + a 2 ) D n q ( ( t x ) 2 , x ) + ω a + 1 ( f , δ ) ( 1 + 1 δ D n q ( ( t x ) 2 , x ) ) 1 2 .

Hence, by using Schwarz inequality and Lemma 2, for every q(0,1) and x[0,a]

| D n q ( f , x ) f ( x ) | 6 M f ( 1 + a 2 ) x ( q [ 2 ] q + x ) q [ n ] q + ω a + 1 ( f , δ ) ( 1 + 1 δ x ( q [ 2 ] q + x ) q [ n ] q ) 6 M f a ( 1 + a 2 ) ( 2 + a ) q [ n ] q + ω a + 1 ( f , δ ) ( 1 + 1 δ a ( a + q [ 2 ] q ) q [ n ] q ) .

By taking δ= a ( q [ 2 ] q + a ) q [ n ] q we get the assertion of our theorem. □

4 Higher order moments and an asymptotic formula

Lemma 3 ([6])

Let0<q<1, we have

B n , q ( t 3 , x ) = 1 [ n ] q x + 1 + 2 q q 2 [ n + 1 ] q [ n ] q 2 x 2 + 1 q 3 [ n + 1 ] q [ n + 2 ] q [ n ] q 2 x 3 , B n , q ( t 4 , x ) = 1 [ n ] q 3 x + 1 q 3 ( 1 + 3 q + 3 q 2 ) [ n + 1 ] q [ n ] q 3 x 2 + 1 q 5 [ 2 ] q ( 1 + 3 q + 5 q 2 + 3 q 3 ) [ n + 1 ] q [ n + 2 ] q [ n ] q 3 x 3 + 1 q 6 [ 2 ] q [ 3 ] q [ 4 ] q ( 1 + 3 q + 5 q 2 + 6 q 3 + 5 q 4 + 3 q 5 + q 6 ) × [ n + 1 ] q [ n + 2 ] q [ n + 3 ] q [ n ] q 3 x 4 .

Now, we present higher order moments for the operators (1.4).

Lemma 4 Let0<q<1, we have

The proof of Lemma 4 can be obtained by using Lemma 3.

We consider the following classes of functions:

Theorem 3 Let q n (0,1), then the sequence{ D n q n (f)}converges to f uniformly on[0,A]for eachf C 2 [0,)if and only if lim n q n =1.

Theorem 4 Assume that q n (0,1), q n 1and q n n aasn. For anyf C 2 [0,)such that f , f C 2 [0,)the following equality holds

lim n [ n ] q n ( D n q n ( f ; x ) f ( x ) ) = ( x 2 + 2 x ) f (x)

uniformly on any[0,A], A>0.

Proof Let f, f , f C 2 [0,) and x[0,) be fixed. By using Taylor’s formula, we may write

f(t)=f(x)+ f (x)(tx)+ 1 2 f (x) ( t x ) 2 +r(t;x) ( t x ) 2 ,
(4.1)

where r(t;x) is the Peano form of the remainder, r(;x) C 2 [0,) and lim t x r(t;x)=0. Applying D n q n to (4.1), we obtain

[ n ] q n ( D n q n ( f ; x ) f ( x ) ) = 1 2 f (x) [ n ] q n D n q n ( ( t x ) 2 ; x ) + [ n ] q n D n q n ( r ( t ; x ) ( t x ) 2 ; x ) .

By the Cauchy-Schwarz inequality, we have

D n q n ( r ( t ; x ) ( t x ) 2 ; x ) D n q n ( r 2 ( t ; x ) ; x ) D n q n ( ( t x ) 4 ; x ) .
(4.2)

Observe that r 2 (x;x)=0 and r 2 (;x) C 2 [0,). Then it follows from Theorem 3 and Lemma 4, that

lim n D n q n ( r 2 ( t ; x ) ; x ) = r 2 (x;x)=0
(4.3)

uniformly with respect to x[0,A]. Now from (4.2), (4.3) and Remark 2, we get immediately

lim n [ n ] q n D n q n ( r ( t ; x ) ( t x ) 2 ; x ) =0.

Then, we get the following

 □