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Mean-square angle-of-arrival difference between two counter-propagating spherical waves in the presence of atmospheric turbulence

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Abstract

The mean-square angle-of-arrival (AOA) difference between two counter-propagating spherical waves in atmospheric turbulence is theoretically formulated. Closed-form expressions for the path weighting functions are obtained. It is found that the diffraction and refraction effects of turbulent cells make negative and positive contributions to the mean-square AOA difference, respectively, and the turbulent cells located at the midpoint of the propagation path have no contributions to the mean-square AOA difference. If the mean-square AOA difference is separated into the refraction and diffraction parts, the refraction part always dominates the diffraction one, and the ratio of the diffraction part to the refraction one is never larger than 0.5 for any turbulence spectrum. Based on the expressions for the mean-square AOA difference, formulae for the correlation coefficient between the angles of arrival of two counter-propagating spherical waves in atmospheric turbulence are derived. Numerical calculations are carried out by considering that the turbulence spectrum has no path dependence. It is shown that the mean-square AOA difference always approximates to the variance of AOA fluctuations. It is found that the correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves ranges from 0.46 to 0.5, implying that the instantaneous angles of arrival of two counter-propagating spherical waves in atmospheric turbulence are far from being perfectly correlated even when the turbulence spectrum does not vary along the path.

© 2015 Optical Society of America

1. Introduction

Over the past years, many researchers have focused attention on counter-propagation of two optical waves along a common path in atmospheric turbulence because of the need for knowledge of the relation between the two counter-propagating waves in relevant engineering applications [1–11 ]. An important practical example of such engineering applications is a bidirectional optical link through the earth’s atmosphere; recently, several efforts have been made to clarify the statistical correlation between the received instantaneous signal power at one link end and that at the other end [6–11 ]. In fact, it has been found for several decades that even though there exits atmospheric turbulence, the field at an observation point, due to a point source located at a given distance from the observation point, remains unchanged if we interchange the positions of the point source and observation point [1,2 ]. This phenomenon has been referred to as the point-source point-receiver (PSPR) reciprocity [8]. Fluctuations in the angle of arrival (AOA) of an optical wave have an important impact on a heterodyne detection system [12]. For a bidirectional optical link using heterodyne detection, an analysis of the relation between the instantaneous AOA fluctuations of two counter-propagating optical waves may be useful in understanding the statistical correlation between the output signals of the detection systems at both link ends.

In accordance with the literature [13–15 ], it is found that the AOA of an optical wave at an observation point is actually determined by the corresponding transverse gradient of the wave front at that observation point. Atmospheric turbulence causes wave-front distortions in propagating optical waves, which further lead to fluctuations in the AOA of the waves at the observation plane. The variance of AOA fluctuations depends heavily on the inner scale of turbulence. Consortini et al. [16] presented a method for measuring the inner scale based on simultaneous measurements of both the AOA and irradiance fluctuations of an optical wave propagating in the atmospheric turbulence. By considering a target-in-the-loop propagation geometry, Churnside and Lataitis [17] investigated the AOA fluctuations of a reflected laser beam from a reflector at a distance from the transmitter in the presence of atmospheric turbulence; many studies of wave-front tilt measurement with a laser guide star (LGS) also considered a similar propagation geometry; i.e., a beam is launched from the ground to create a LGS at a certain altitude in the sky and the wave-front tilt of the returned wave from the LGS is measured at the ground [18–21 ]. Nevertheless, the propagation geometry under consideration in this paper is essentially a point-to-point case, meaning that the two counter-propagating spherical waves are generated by two independent point sources at each end of the path. Recently, the variance of AOA fluctuations for both plane and spherical waves propagating through non-Kolmogorov turbulence has also been theoretically formulated based on the geometrical optics method [22,23 ]. Examination of the published formulations concerning the AOA fluctuations reveals that the variances of AOA fluctuations of two counter-propagating waves at both ends of a path will be identical if the turbulence spectrum has no path dependence; however, we cannot infer directly from this fact that the instantaneous angles of arrival of the two counter-propagating waves are always the same. As is well known, the turbulence-induced AOA fluctuations have a close connection with the phase disturbances in propagating optical fields. In the aforementioned PSPR case, interchanging the point source and observation point does not lead to any changes in the phase of the wave. The above consideration stimulates us to deliberate on other new questions as to whether the mean-square difference between the instantaneous angles of arrival of two counter-propagating spherical waves can reach zero in a specific situation, e.g., the one in which the turbulence spectrum has no path dependence, and how the propagation and turbulence parameters affect it.

The purpose of this paper is to gain an insight into the relation between the instantaneous AOA fluctuations of two counter-propagating spherical waves in atmospheric turbulence, and hence to understand optical wave counter-propagation in atmospheric turbulence from a different point of view. The propagation geometry considered by us is essentially the same as that in the PSPR situation. In the later sections, we begin by detailing the development of general expressions for the mean-square difference and correlation coefficient between the instantaneous angles of arrival of two counter-propagating spherical waves in atmospheric turbulence, then present the numerical calculations and discussions, and finally give the concluding remarks.

2. Theoretical formulations

Figure 1 illustrates a diagram of the counter-propagation geometry under consideration in this work. We will refer to the propagation from a point source positioned at the point (x = 0, y = 0, z = 0) to the observation point (x = 0, y = 0, z = L) as the ‘forward propagation’ and that from a point source positioned at the point (x = 0, y = 0, z = L) to the observation point (x = 0, y = 0, z = 0) as the ‘inverse propagation’. Without loss of generality, here the z-axis has been directed from the forward-propagation point source to the inverse-propagation point source.

 figure: Fig. 1

Fig. 1 Counter-propagation of two spherical waves along a common path in atmospheric turbulence.

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Let us first consider the forward-propagation case. By employing the Rytov approximation method [13–15,24 ], the phase fluctuations of the wave at the observation point can be given by ([13], Sec. 2.3)

S^F(r,z=L)=k0Ldzdv(κ,z)cos[κ2z(Lz)2kL]exp(izLκr),
where k=2π/λ is the optical wave number with λ denoting the wavelength, r = (x, y) is a two-dimensional point in the z = L plane, dv(κ,z) represents the random amplitude of refractive-index fluctuations, κ is a two-dimensional wave vector, and the subscript ‘F’ on the left-hand side means ‘forward propagation’. It is noted that dv(κ,z) is obtained by expressing the refractive-index fluctuations in a spectral representation, and dv(κ,z) = dv*(κ,z). We define the AOA of a wave at an observation point (r, z ) as the angle that the local propagation direction of the wave at that observation point, i.e., the local ray direction in a geometric sense, makes with the z-axis. In accordance with the literature [13–15 ], the AOA of the forward-propagating spherical wave, shown by Fig. 1, at the point (r = 0, z = L) can be expressed in the form
βF=tφF(r)|r=0,
where t represents the transverse gradient operator, and φF(r) = [SF(0)(r,z=L) + S^F(r,z=L)]/k denotes the wave front with SF(0)(r,z=L) being the phase of the wave at the z = L plane in the absence of atmospheric turbulence. With tSF(0)(r,z=L)|r=00 in mind, combination of Eqs. (1) and (2) leads to the expression for the AOA of the forward-propagating spherical wave at the point (r = 0, z = L) given by
βF=i0Ldzdv(κ,z)κzLcos[κ2z(Lz)2kL].
In a similar manner, for the inverse-propagation case, the expression for the AOA of the wave at the point (r = 0, z = 0) can be developed to give
βI=i0Ldzdv(κ,z)κLzLcos[κ2z(Lz)2kL].
where the subscript ‘I’ on the left-hand side implies ‘inverse propagation’.

In what follows, we begin to formulate the mean-square AOA difference between two counter-propagating spherical waves in the presence of atmospheric turbulence. As in [9–11 ], for simplicity, the wavelengths associated with the two counter-propagating waves are assumed to be identical. It is noted that both βF and βI are random quantities due to the existence of atmospheric turbulence. Based on Eqs. (3) and (4) , by utilizing the Markov approximation [13–15,24 ] and following the same procedure used to obtain Eq. (2.110) in [13], the mean-square difference between βF and βI can be formulated to give (see Appendix A)

δFI2=2π0L(2zL1)2dzd2κΦn(κ,z)κ2cos2[κ2z(Lz)2kL],
where Φn() is the turbulence spectrum and κ = |κ|. In arriving at Eq. (5), we have indeed assumed that the atmospheric turbulence is isotropic, which can further lead us to
δFI2=4π2L01dξ(12ξ)20dκκ3Φn(κ,ξL)cos2[κ2Lξ(1ξ)2k].
In fact, the AOA can be conceptually separated into two orthogonal components, i.e., the x- and y-components. Notice that, δFI2 appearing in Eq. (5) denotes the total mean-square AOA difference between two counter-propagating spherical waves, which is equal to the sum of the mean-square AOA differences in the x and y directions. The magnitude of Φn(·) for atmospheric turbulence with a finite inner scale l 0 falls off rapidly to zero when κ increases beyond a value κm (~1/l 0). In the limit of the geometrical optics approximation [24], i.e., κ 2 L/k ≈0 for all κ smaller than κm, the squared cosine term in Eq. (6) can be replaced by 1. Below, we rewrite Eq. (6) as follows:
δFI2=δFI,r2δFI,d2
with
δFI,r2=4π2L01dξ(12ξ)20dκκ3Φn(κ,ξL),
δFI,d2=4π2L01dξ(12ξ)20dκκ3Φn(κ,ξL)sin2(κ2Lξ(1ξ)2k).
It is easy to find that δFI,r2 and δFI,d2 arise from the refraction and diffraction effects of turbulent cells, respectively. Based on Eqs. (7)–(9) , we find that the refraction and diffraction effects of turbulent cells make positive and negative contributions to δFI2, respectively. In the two limits (L/k)1/2 → 0 and (L/k)1/2 → ∞, one finds
δFI,d2={0L/k0δFI,r2/2L/k.
Combination of Eqs. (7) and (10) leads to
δFI2={δFI,r2L/k012δFI,r2L/k.
Equation (11) shows that the two asymptotic values of δFI2 differ by a factor of 1/2 for any turbulence spectrum. As is well known, the diffraction phenomenon of a wave associated with a larger wavelength λ is easier to observe. In fact, for a given finite L, (L/k)1/2 → 0 implies λ → 0, which corresponds to the case that the diffraction effects can be completely ignored; on the other hand, for a given finite L, (L/k)1/2 → ∞ means λ → ∞, which corresponds to the situation that the diffraction effects become most prominent. As a result, we can infer that δFI,d2/δFI,r20.5 for any turbulence spectrum.

A turbulence spectrum model taking the form [22]

Φn(κ,z)=A(α)C˜n2(z)(κ2+κ02)α/2exp(κ2/κm2)
has been widely employed in the literature concerning optical wave propagation through atmospheric turbulence, where C˜n2(z) is the refractive-index structure constant in units of m3− α, κ0=2π/L0 with L 0 being the outer scale of turbulence, κm=c(α)/l0, c(α) = {2πΓ[(5−α)/2] A(α)/3}1/( α −5), A(α)=Γ(α1)cos(απ/2)/(4π2), Γ(∙) denotes the gamma function, and αis referred to as the spectral index with 3 < α< 4. As was well known, the inner scale of turbulence is critical for AOA fluctuations. However, the outer scale of turbulence is not critical for AOA fluctuations except when (L/k)1/2 ~L 0, which generally corresponds to an extremely large propagation distance and holds no interest for us. To simplify the mathematical presentation, in the following development we will drop the outer scale from the turbulence spectrum model, i.e., let L 0 → ∞. This does not affect the final conclusions. By introducing Eq. (12) into Eqs. (8) and (9) and meanwhile letting κ 0 = 0, one finds
δFI,r2=2π2A(α)Γ(2α2)κm4αL01dξC˜n2(ξL)Wr(ξ),
δFI,d2=2π2A(α)Γ(2α2)κm4αL01dξC˜n2(ξL)Wd(ξ)
with
Wr(ξ)=(12ξ)2,
Wd(ξ)=12Wr(ξ)[1Q(θ)],
Q(θ)=cos[(2α2)arctan(θ)](1+θ2)α/41,
where θ = (1−ξ) and q = κm2 L/k. In what follows, q will be called the Fresnel number; Wr(ξ) and Wd(ξ) will be referred to as the refraction and diffraction path weighting functions, respectively. Physically speaking, Wr(ξ) and Wd(ξ) characterize the weight of the refraction- and diffraction-induced contributions, respectively, to the mean-square AOA difference from turbulent cells located at various positions on the propagation path. As could have been expected, Wr(ξ) is independent of the wavelength, and Wd(ξ) is a function of the wavelength. At the middle point of the path, it is found that Wr(ξ = 0.5) = Wd(ξ = 0.5) = 0, meaning that the turbulent cells located at the middle point do not contribute to the mean-square AOA difference. Moreover, examination of Eqs. (15) and (16) reveals that the curve corresponding to either Wr(ξ) or Wd(ξ) in terms of ξ has a symmetric shape with respect to ξ = 0.5. Note that Q(θ) = 0 and 1 when θ → ∞ and 0, respectively. It is easy to verify that 0 ≤ Q(θ) ≤ 1. Thus, it can be deduced that Wd(ξ) / Wr(ξ) ≤ 0.5 except for ξ = 0.5, implying that δFI,d2/δFI,r20.5; this verifies once again our previous inference.

The unit of C˜n2(z) depends on the spectral index α. This fact may cause some difficulties when one analyzes various optical-wave statistics based on numerical calculations [25,26 ]. To avoid the unit choice inconsistency [25] in the representation of calculation results concerning δFI2 in the form of dependence on α, below we normalize the mean-square AOA difference between two counter-propagating spherical waves by the variances of AOA fluctuations. Following the procedure used to obtain Eq. (6), the variance of AOA fluctuations for the forward-propagating spherical wave at the observation point (r = 0, z = L) can be expressed as

βF2=4π2L01dξξ20dκκ3Φn(κ,ξL)cos2[κ2Lξ(1ξ)2k].
Similarly, the variance of AOA fluctuations for the inverse-propagating spherical wave at the observation point (r = 0, z = 0) can be expressed by
βI2=4π2L01dξ(1ξ)20dκκ3Φn(κ,ξL)cos2[κ2Lξ(1ξ)2k].
After evaluating the integrations over κ in Eqs. (18) and (19) , we can obtain the normalized mean-square AOA difference given by
δ^FI2=δFI2βF2βI2=01dξC˜n2(ξL)(12ξ)2[1+Q(θ)]01dξC˜n2(ξL)ξ2[1+Q(θ)]01dξC˜n2(ξL)(1ξ)2[1+Q(θ)],
where θ = ′(1−ξ′). If Φn(∙) has no path dependence, i.e., C˜n2(∙) does not vary over the propagation path and βF2βI2, Eq. (20) reduces to

δ^FI2=01dξ(12ξ)2[1+Q(θ)]01dξ(1ξ)2[1+Q(θ)].

According to the normalized mean-square AOA difference between two counter-propagating spherical waves, the correlation coefficient between the angles of arrival in the x or y direction can be readily expressed as follows (see Appendix B):

γFI,v=βF,vβI,vβF,v2βI,v2=12(βF2βI2+βI2βF2)12δ^FI2,
where βF , v and βI , v are the instantaneous angles of arrival in the v direction associated with the forward and inverse propagation, respectively (v = x or y). Here, we emphasize that Eq. (22) has been obtained by assuming that atmospheric turbulence is isotropic. Moreover, if Φn(∙) has no path dependence, one finds
γFI,v=1δ^FI2/2.
It should be pointed out that the definitions shown by Eqs. (20) and (22) are not meaningful for α = 3 because Φn(∙) ≡ 0 with α = 3, resulting in βF2 = βI2 ≡ 0.

3. Numerical calculations and discussions

In this section, we discuss the results obtained in the previous section with the help of numerical calculations. Figure 2 illustrates the path weighting functions shown by Eqs. (15) and (16) in terms of ξ with various q. As has been pointed out, we can see from Fig. 2 that at the middle point of the propagation path, viz., ξ = 0.5, both the refraction and diffraction weighting functions are equal to zero. It is apparent that Wr(ξ) achieves its maximum value at ξ = 0 and 1; however, Wd(ξ) becomes zero at ξ = 0 and 1, causing its curve to take on a double-peak appearance. Furthermore, although Wr(ξ) does not depend on the Fresnel number q, it can be found from Fig. 2 that Wd(ξ) can have an appreciable value only when q ≳ 1. The physical interpretation about this phenomenon is as follows: q ≳ 1 means (L/k)1/2l 0; it has been known that turbulent cells with scale sizes larger than the first Fresnel zone (L/k)1/2 do not diffract an optical wave through a large enough angle to arrive at the observation point [24]; that is, only the diffraction effects produced by those turbulent cells with scale sizes smaller than the first Fresnel zone (L/k)1/2 are important; meanwhile, theoretically speaking, the inner scale l 0 describes the smallest scale size of turbulent cells; consequently, if (L/k)1/2 < l 0 (i.e., all the scale sizes of turbulent cells are larger than the first Fresnel zone (L/k)1/2), none of the turbulent cells can produce important diffraction effects, resulting in that Wd(ξ) has an inappreciable value. In addition, when the Fresnel number q increases steadily beyond 1, there are increasing turbulent cells that can produce important diffraction effects, causing a rise in the value of Wd(ξ), which can be clearly seen in Figs. 2(b)–2(d). It is easy to find by numerical calculations that with a given θ > 0, a larger α leads to a greater value of Q(θ). This is the reason why Figs. 2(b)–2(d) show that Wd(ξ) diminishes as α increases with the same q and ξ, except for ξ = 0, 0.5 and 1. Indeed, when α → 4, the structure function of the turbulence tends to take a quadratic form, resulting in that the wave-front distortions mainly manifest themselves as tilts and the turbulence-induced higher-order wave-front distortions become really tiny [25,27–29 ]; the tilts can be regarded as the turbulence-induced deflections of propagating waves, which should be related to the refraction effects; accordingly, the diffraction effects become less significant when α grows larger with fixed q.

 figure: Fig. 2

Fig. 2 The path weighting functions in terms of ξ with various q. (a) the refraction path weighting function Wr(∙); (b) the diffraction path weighting function Wd(∙) with α = 3.1; (c) the diffraction path weighting function Wd(∙) with α = 11/3; (d) the diffraction path weighting function Wd(∙) with α = 3.9.

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When C˜n2() has path dependence, Eq. (20) can be used to determine the normalized mean-square AOA difference between two counter-propagating spherical waves in atmospheric turbulence. In the literature concerning optical wave propagation, almost all the cases, in which one needs to consider the variation of C˜n2() over the propagation path, involve a vertical or slant path in the earth’s atmosphere. Strictly speaking, for the earth’s atmospheric turbulence, both the inner scale l 0 and spectral index α are dependent on the altitude ([15,30 ], Eq. (5)), implying that these two parameters indeed change over a vertical or slant path. However, we note that the turbulence spectrum shown by Eq. (12) assumes that both the inner scale and spectral index have no path dependence. Hence, although Eq. (20) allows us formally to consider the path dependence of C˜n2(), it is not a very suitable mathematical model which can be used to carry out a rigorous analysis of the normalized mean-square AOA difference between two counter-propagating spherical waves if a vertical or slant path in the earth’s atmosphere needs to be considered. On the other hand, the variance of AOA fluctuations of a wave propagating from the earth’s ground to a position in the space is apparently different from that of a wave propagating from the position in the space to the earth’s ground; thus it is straightforward to deduce that the mean-square AOA difference between two counter-propagating waves in the vertical- or slant-propagation case cannot be zero. However, for a horizontal path, it is common to assume that the turbulence spectrum has no path dependence, and in this case, the variances of AOA fluctuations of two counter-propagating waves at both ends of the path will be the same. Below we focus our attention on the horizontal propagation case, in which the parameters C˜n2(), l 0 and α are assumed to remain constant over the path. Figure 3 shows the normalized mean-square AOA difference between two counter-propagating spherical waves in atmospheric turbulence as a function of the Fresnel number q and spectral index α. It is seen from Fig. 3 that all the curves corresponding to δ^FI2 in terms of q take on a single-peak appearance; a smaller α leads to a higher peak. It is found that δ^FI2 quickly approaches 1 when q decreases below 1 for all α. It is also observed that δ^FI2 gradually becomes close to 1 when q steadily increases to a large enough value. Note that, if the first Fresnel zone (L/k)1/2 is fixed, an increase in q means a decrease in l 0. Furthermore, we find by numerical calculations that the maximum value of δ^FI2 is smaller than 1.08, implying that 1 ≤ δ^FI2 < 1.08. Accordingly, a statement can be made that the mean-square AOA difference between two counter-propagating spherical waves is indeed approximately equal to the variance of AOA fluctuations. Figure 4 shows the correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves as a function of q and α. As could been expected, all the curves in Fig. 4 take on a single-valley appearance. Based on the analysis of Fig. 3, it can be readily deduced that 0.46 < γFI,v ≤ 0.5. These findings reveal that the angles of arrival of two counter-propagating spherical waves in atmospheric turbulence cannot be perfectly correlated under any conditions of practical interest and the correlation coefficient only shows a slight dependence on q and α.

 figure: Fig. 3

Fig. 3 Normalized mean-square AOA difference between two counter-propagating spherical waves as a function of q and α. 3 < α < 4. The turbulence spectrum is assumed to have no path dependence.

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 figure: Fig. 4

Fig. 4 Correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves as a function of q and α. The subscript v can be specified as x or y. 3 < α < 4. The turbulence spectrum is assumed to have no path dependence.

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At this point, we present a brief discussion about the validity domain of our theoretical formulations. Because the preceding formulations have been developed based on the Rytov approximation, it may be expected that they are applicable only in the weak fluctuation regime. On the other hand, because the theoretical technique we used to formulate the mean-square AOA difference is essentially the same as that used to develop the expressions for the variance of AOA fluctuations based on the Rytov approximation, we believe that our theoretical formulations should have the same validity domain as that of the expressions for the variance of AOA fluctuations obtained by making use of the Rytov approximation. The experimental study concerning the AOA fluctuations carried out by Gurvich and Kallistratova [31] has proved that the formulation of AOA fluctuations developed by employing the Rytov approximation remains valid within a range wider than the weak fluctuation regime. For this reason, it is believed that our formulations may also be applicable beyond the weak fluctuation regime. This result does not surprise us. Indeed, it can be found from [24,25,32 ] that for a spherical wave propagating in atmospheric turbulence, the expression for the mutual coherence function obtained by making use of the Rytov approximation is identical to that derived based on the Markov approximation, which is a method applicable to the strong fluctuation regime; in other words, the expression for the mutual coherence function of spherical waves obtained by employing the Rytov approximation is also applicable in the strong fluctuation regime. Furthermore, it is interesting to note that Eq. (21) is even independent of the refractive-index structure constant.

4. Conclusions

In this paper, general formulations for the mean-square AOA difference between two counter-propagating spherical waves in atmospheric turbulence have been developed by making use of the Rytov approximation method. Based on these formulations, expressions for the correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves have been derived. Both the refraction and diffraction effects of turbulent cells can play a role in determining the mean-square AOA difference; the former and the latter make positive and negative contributions to the mean-square AOA difference, respectively. The turbulent cells located at the midpoint of the propagation path do not contribute to the mean-square AOA difference. If the mean-square AOA difference is separated into the refraction and diffraction parts, the ratio of the diffraction part to the refraction one is never larger than 0.5 for any turbulence spectrum. By consider the cases that the turbulence spectrum has no path dependence, numerical calculations have been carried out. The findings are the following. The normalized mean-square AOA difference only changes slightly within a very narrow range when the Fresnel number or the spectral index varies, and its value can be regarded as being always approximately equal to 1, implying that the mean-square AOA difference always approximates to the variance of AOA fluctuations. The Fresnel number and spectral index only have a slight impact on the value of the correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves, which ranges from 0.46 to 0.5 for all values of the Fresnel number and spectral index. The obtained analytical expressions may still remain valid in relatively strong fluctuation regimes. As a final comment, we note that the theoretical models developed here apply to both Kolmogorov and non-Kolmogorov atmospheric turbulence.

Appendix A

According to Eqs. (3) and (4) , it follows that

δFI2=(βFβI)2=0Ldz0Ldzdv(κ,z)dv*(κ,z)κκ×{(2zL1)cos[κ2z(Lz)2kL]}{(2zL1)cos[κ2z(Lz)2kL]}
with
dv(κ,z)dv*(κ,z)=C˜n2(z/2+z/2)En(κ,|zz|)δ(κκ)dκdκ,
where the angle brackets stand for an ensemble average, κ′ = |κ′|, C˜n2() represents the refractive-index structure constant, En(∙) is the two-dimensional spatial power spectrum of refractive-index fluctuations scaled by C˜n2(), and δ() denotes the Dirac delta function. By introducing Eq. (25) into Eq. (24), making the change of variables zs=(z+z)/2 and zd=zz, employing the relation [13,24,33 ]
C˜n2(zs)0En(κ,zd)dzd=πΦn(κ,zs),
and recalling the arguments on page 51 of [13], one can obtain the result shown by Eq. (5).

Appendix B

Under the condition that atmospheric turbulence is isotropic, it is easy to find that

δFI2=δFI,x2+δFI,y2=βF,x2+βI,x22βF,xβI,x+βF,y2+βI,y22βF,yβI,y=βF2+βI22βF,xβI,x2βF,yβI,y=βF2+βI24βF,vβI,v,
where βF , v and βI , v denote the instantaneous angles of arrival in the v direction for the forward and inverse propagation, respectively (v = x or y). Note that, βF,x2=βF,y2, βI,x2=βI,y2, and βF,xβI,x=βF,yβI,y due to the assumption of isotropic atmospheric turbulence. Moreover, it is apparent that the correlation coefficient can be written by
γFI,v=βF,vβI,vβF,v2βI,v2=2βF,vβI,vβF2βI2.
Based on Eqs. (20), (27) and (28) , one can yield the result shown by Eq. (22).

Acknowledgments

The authors are very grateful to the reviewers for valuable comments. This work was supported by the National Natural Science Foundation of China (61007046, 61275080, 61475025), the Natural Science Foundation of Jilin Province of China (20150101016JC), and the Specialized Research Fund for the Doctoral Program of Higher Education of China (20132216110002).

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Figures (4)

Fig. 1
Fig. 1 Counter-propagation of two spherical waves along a common path in atmospheric turbulence.
Fig. 2
Fig. 2 The path weighting functions in terms of ξ with various q. (a) the refraction path weighting function Wr (∙); (b) the diffraction path weighting function Wd (∙) with α = 3.1; (c) the diffraction path weighting function Wd (∙) with α = 11/3; (d) the diffraction path weighting function Wd (∙) with α = 3.9.
Fig. 3
Fig. 3 Normalized mean-square AOA difference between two counter-propagating spherical waves as a function of q and α. 3 < α < 4. The turbulence spectrum is assumed to have no path dependence.
Fig. 4
Fig. 4 Correlation coefficient between the angles of arrival in the x or y direction of two counter-propagating spherical waves as a function of q and α. The subscript v can be specified as x or y. 3 < α < 4. The turbulence spectrum is assumed to have no path dependence.

Equations (28)

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S ^ F ( r , z = L ) = k 0 L d z d v ( κ , z ) cos [ κ 2 z ( L z ) 2 k L ] exp ( i z L κ r ) ,
β F = t φ F ( r ) | r = 0 ,
β F = i 0 L d z d v ( κ , z ) κ z L cos [ κ 2 z ( L z ) 2 k L ] .
β I = i 0 L d z d v ( κ , z ) κ L z L cos [ κ 2 z ( L z ) 2 k L ] .
δ F I 2 = 2 π 0 L ( 2 z L 1 ) 2 d z d 2 κ Φ n ( κ , z ) κ 2 cos 2 [ κ 2 z ( L z ) 2 k L ] ,
δ F I 2 = 4 π 2 L 0 1 d ξ ( 1 2 ξ ) 2 0 d κ κ 3 Φ n ( κ , ξ L ) cos 2 [ κ 2 L ξ ( 1 ξ ) 2 k ] .
δ F I 2 = δ F I , r 2 δ F I , d 2
δ F I , r 2 = 4 π 2 L 0 1 d ξ ( 1 2 ξ ) 2 0 d κ κ 3 Φ n ( κ , ξ L ) ,
δ F I , d 2 = 4 π 2 L 0 1 d ξ ( 1 2 ξ ) 2 0 d κ κ 3 Φ n ( κ , ξ L ) sin 2 ( κ 2 L ξ ( 1 ξ ) 2 k ) .
δ F I , d 2 = { 0 L / k 0 δ F I , r 2 / 2 L / k .
δ F I 2 = { δ F I , r 2 L / k 0 1 2 δ F I , r 2 L / k .
Φ n ( κ , z ) = A ( α ) C ˜ n 2 ( z ) ( κ 2 + κ 0 2 ) α / 2 exp ( κ 2 / κ m 2 )
δ F I , r 2 = 2 π 2 A ( α ) Γ ( 2 α 2 ) κ m 4 α L 0 1 d ξ C ˜ n 2 ( ξ L ) W r ( ξ ) ,
δ F I , d 2 = 2 π 2 A ( α ) Γ ( 2 α 2 ) κ m 4 α L 0 1 d ξ C ˜ n 2 ( ξ L ) W d ( ξ )
W r ( ξ ) = ( 1 2 ξ ) 2 ,
W d ( ξ ) = 1 2 W r ( ξ ) [ 1 Q ( θ ) ] ,
Q ( θ ) = cos [ ( 2 α 2 ) arc tan ( θ ) ] ( 1 + θ 2 ) α / 4 1 ,
β F 2 = 4 π 2 L 0 1 d ξ ξ 2 0 d κ κ 3 Φ n ( κ , ξ L ) cos 2 [ κ 2 L ξ ( 1 ξ ) 2 k ] .
β I 2 = 4 π 2 L 0 1 d ξ ( 1 ξ ) 2 0 d κ κ 3 Φ n ( κ , ξ L ) cos 2 [ κ 2 L ξ ( 1 ξ ) 2 k ] .
δ ^ F I 2 = δ F I 2 β F 2 β I 2 = 0 1 d ξ C ˜ n 2 ( ξ L ) ( 1 2 ξ ) 2 [ 1 + Q ( θ ) ] 0 1 d ξ C ˜ n 2 ( ξ L ) ξ 2 [ 1 + Q ( θ ) ] 0 1 d ξ C ˜ n 2 ( ξ L ) ( 1 ξ ) 2 [ 1 + Q ( θ ) ] ,
δ ^ F I 2 = 0 1 d ξ ( 1 2 ξ ) 2 [ 1 + Q ( θ ) ] 0 1 d ξ ( 1 ξ ) 2 [ 1 + Q ( θ ) ] .
γ F I , v = β F , v β I , v β F , v 2 β I , v 2 = 1 2 ( β F 2 β I 2 + β I 2 β F 2 ) 1 2 δ ^ F I 2 ,
γ F I , v = 1 δ ^ F I 2 / 2.
δ F I 2 = ( β F β I ) 2 = 0 L d z 0 L d z d v ( κ , z ) d v * ( κ , z ) κ κ × { ( 2 z L 1 ) cos [ κ 2 z ( L z ) 2 k L ] } { ( 2 z L 1 ) cos [ κ 2 z ( L z ) 2 k L ] }
d v ( κ , z ) d v * ( κ , z ) = C ˜ n 2 ( z / 2 + z / 2 ) E n ( κ , | z z | ) δ ( κ κ ) d κ d κ ,
C ˜ n 2 ( z s ) 0 E n ( κ , z d ) d z d = π Φ n ( κ , z s ) ,
δ F I 2 = δ F I , x 2 + δ F I , y 2 = β F , x 2 + β I , x 2 2 β F , x β I , x + β F , y 2 + β I , y 2 2 β F , y β I , y = β F 2 + β I 2 2 β F , x β I , x 2 β F , y β I , y = β F 2 + β I 2 4 β F , v β I , v ,
γ F I , v = β F , v β I , v β F , v 2 β I , v 2 = 2 β F , v β I , v β F 2 β I 2 .
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