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1Introduction

In this chapter we will study how light propagates as a wave. In the study of the double-slit experiment we concluded from the interference pattern observed on a screen that light is a wave. To demonstrate more convincingly that light is indeed a wave, we require a detailed quantitative model of the propagation of light, which gives experimentally verifiable predictions.

But a precise description of the propagation of light is not only important for fundamental science; it also has many practical applications. For example, if a sample must be analyzed by illuminating it and measuring the scattered light, the fact that the detected light has been affected not only by the sample but also by propagation has to be taken into account. Another example is lithography. If a pattern has to be printed onto a substrate using a mask that is illuminated and there is a certain distance between the mask and the photoresist, the light which reaches the resist does not have the exact shape of the mask due to propagation effects. Thus, the mask needs to be designed to compensate for these effects.

Two examples: light diffracts after passing through slits, and light scattered from a sample travels to a detector.

Figure 1:A quantitative model of the propagation of light is required to predict the properties of propagation and to apply it in sample analyses and lithography.

From electromagnetic theory, we know that in homogeneous matter (i.e. the permittivity is constant), every component UU of a time-harmonic electromagnetic field satisfies the scalar Helmholtz Eq. (1):

(∇2+k2)U(r)=0,\begin{align*} \left( \nabla ^2 + k^2\right) U(\mathbf{r})=0, \end{align*}

where k=ωϵμ0k=\omega\sqrt{\epsilon \mu_0} is the wave number of the light in matter with permittivity ϵ\epsilon and refractive index n=ϵ/ϵ0n=\sqrt{\epsilon/\epsilon_0}.

When the refractive index is not constant, Maxwell’s equations are no longer equivalent to the wave equation for the individual electromagnetic field components and there is then coupling between the components due to the curl operators in Maxwell’s equation. When the variation of the refractive index is slow on the scale of the wavelength, the scalar wave equation may still be a good approximation, but for structures that vary on a scale comparable to the wavelength, vector effects can make a scalar model inaccurate.

2Propagation of light through a homogeneous medium

We will describe two equivalent methods to compute the propagation of the field through homogeneous matter, namely the angular spectrum method and the Rayleigh-Sommerfeld diffraction formula. Our goal is to derive the field at some point (x,y,z)(x,y,z) with z>0z>0, given the field in the plane z=0z=0, as is illustrated in Figure 2. Although both methods ultimately describe the same propagation, they give physical insight into different aspects of propagation.

2.1Angular Spectrum Method

A wave field on the plane z equals zero propagates to a second plane at positive z.

Figure 2:Given the field U(x,y,0)U(x,y,0), we want to find UU at a point (x,y,z)(x,y,z) with z>0z>0. It is assumed that the field propagates in the positive zz-direction, which means that all sources are in the region z<0z<0.

F(U0)(ξ,η)=∫ ⁣∫U0(x,y)e−2πi(ξx+ηy) dxdy,\begin{align*} \mathcal{F}(U_0)(\xi,\eta) = \int\!\int U_0(x,y) e^{-2\pi i(\xi x + \eta y)} \, \text{d}x \text{d} y, \end{align*}

The inverse Fourier transform implies:

U0(x,y)=∫ ⁣∫F(U0)(ξ,η)e2πi(ξx+ηy) dξdη=F−1{F(U0)}(x,y).\begin{align*} U_0(x,y)&= \int\!\int {\cal F}(U_0)(\xi,\eta) e^{2\pi i (\xi x + \eta y)}\, \text{d}\xi \text{d} \eta \\ &= \mathcal{F}^{-1}\{{\cal F}(U_0)\}(x,y). \end{align*}

The Fourier transform has important properties that are essential for this analysis. By defining kx=2πξk_x=2\pi \xi, ky=2πηk_y=2\pi \eta, Eq. (3) can be written as

U0(x,y)=14π2∫ ⁣∫F(U0)(kx2π,ky2π)ei(kxx+kyy) dkxdky.\begin{align*} U_0(x,y)= \frac{1}{4\pi^2} \int\!\int {\cal F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) e^{ i (k_x x + k_y y)}\, \text{d} k_x \text{d} k_y. \end{align*}

The variables in the Fourier plane, (ξ,η)(\xi,\eta) and (kx,ky)(k_x, k_y), are called spatial frequencies.

Eq. (4) says that we can write U0(x,y)=U(x,y,z=0)U_0(x,y)=U(x,y,z=0) as an integral (a sum) of plane waves[1] with wave vector k=(kx,ky,kz)T\mathbf{k}=(k_x,k_y, k_z)^T, each with its own weight (i.e. complex amplitude) F(U0)(kx2π,ky2π){\cal F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right). We know how each plane wave with complex amplitude F(U0)(kx2π,ky2π){\cal F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) and wave vector k=(kx,ky,kz)T\mathbf{k}=(k_x,k_y,k_z)^T propagates over a distance z>0z>0

F(U0)(kx2π,ky2π)ei(kxx+kyy)→F(U0)(kx2π,ky2π)ei(kxx+kyy+kzz),\begin{align*} {\cal F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)e^{i (k_x x + k_y y)} \to \mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) e^{i (k_x x + k_y y + k_z z)}, \end{align*}

Therefore, the field U(x,y,z)U(x,y,z) in the plane zz (for some z>0z>0) is given by

U(x,y,z)=14π2∫∫F(U0)(kx2π,ky2π)ei(kxx+kyy+kzz) dkx dky,\begin{align*} U(x,y,z)=\frac{1}{4\pi^2} \int\int {\cal F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)e^{i (k_x x + k_y y+k_z z)} \,\text{d}k_x\,\text{d}k_y, \end{align*}

where

kz=(2πλ)2−kx2−ky2,\begin{align*} k_z =\sqrt{\left(\frac{2\pi }{\lambda}\right)^2-k_x^2-k_y^2}, \end{align*}

with λ\lambda the wavelength of the light as measured in the material (hence, λ=λ0/n\lambda=\lambda_0/n, with λ0\lambda_0 the wavelength in vacuum). The sign in front of the square root in Eq. (7) could in principle be chosen negative: one would then also obtain a solution of the Helmholtz equation. The choice of the sign of kzk_z is determined by the direction in which the light propagates, which in turn depends on the location of the sources and on the convention chosen for the time dependence. We have to choose here the + sign in front of the square root because the sources are in z<0z<0 and the time dependence of time-harmonic fields is (as always in this book) given by e−iωte^{-i\omega t} with ω>0\omega >0.

Eq. (6) can be written alternatively as

U(x,y,z)=F−1{F(U0)(ξ,η)eikzz}(x,y),\begin{align*} U(x,y,z)=\mathcal{F}^{-1}\{\mathcal{F}(U_0)(\xi,\eta)e^{i k_z z}\}(x,y), \end{align*}

where now kzk_z has to be considered as a function of (ξ,η)(\xi, \eta):

kz=2π(1λ)2−ξ2−η2.\begin{align*} k_z = 2\pi \sqrt{ \left( \frac{1}{\lambda}\right)^2- \xi^2-\eta^2}. \end{align*}

Note that one can interpret this as a diagonalization of the propagation operator.

We can observe something interesting: if kx2+ky2>(2πλ)2k_x^2+k_y^2 > \left(\frac{2\pi }{\lambda}\right)^2, then kzk_z becomes imaginary, and exp⁡(ikzz)\exp(i k_z z) decays exponentially for increasing zz:

ei(kxx+kyy+kzz)=ei(kxx+kyy)e−zkx2+ky2−(2π/λ)2,kx2+ky2>(2π/λ)2.e^{i(k_xx+k_yy+k_zz)} =e^{i(k_xx+k_yy)} e^{-z\sqrt{k_x^2+k_y^2-(2\pi/\lambda)^2}}, \qquad k_x^2+k_y^2>(2\pi/\lambda)^2.

These exponentially decaying waves are called evanescent in the positive zz-direction. We have met evanescent waves already in the context of total internal reflection. The physical consequences of evanescent waves in the angular spectrum decomposition are important for understanding diffraction limits.

The waves for which kzk_z is real have constant amplitude: only their phase changes due to propagation. These waves therefore are called propagating waves.

A circle in transverse wave-number space separates propagating plane waves inside from evanescent components outside.

Figure 3:The spatial frequencies kxk_x, kyk_y of the plane waves in the angular spectrum of a time-harmonic field which propagates in the zz-direction. There are two types of waves: the propagating waves with spatial frequencies inside the circle kx2+ky2<k=2π/λ\sqrt{k_x^2+k_y^2}<k=2\pi/\lambda and which have phase depending on the propagation distance zz but constant amplitude, and the evanescent waves for which kx2+ky2>k\sqrt{k_x^2+k_y^2}>k and whose amplitude decreases exponentially during propagation.

Remark. In homogeneous source-free space, every electric-field component satisfies a scalar Helmholtz equation. The components must also obey Maxwell’s transversality condition. We may propagate each component ExE_x, EyE_y, and EzE_z with the angular spectrum method if the starting fields satisfy that constraint. If the data in the plane z=0z=0 of these field components are physically consistent, the electric field thus obtained will automatically satisfy the condition that the electric field is free of divergence, i.e.

∇⋅E=0,\begin{align*} \mathbf{\nabla} \cdot \mathbf{E}=0, \end{align*}

everywhere in z>0z>0. This is equivalent to the statement that the electric vectors of the plane waves in the angular spectrum are perpendicular to their wave vectors. Alternatively, one can propagate only the ExE_x- and EyE_y-components and afterwards determine EzE_z from the condition that Eq. (11) must be satisfied.

2.2Rayleigh-Sommerfeld Diffraction Integral

Another method to propagate a wave field is by using the Rayleigh-Sommerfeld integral. A very good approximation of this integral states that each point in the plane z=0z=0 emits spherical waves with amplitude proportional to the field in the plane z=0z=0. To find the field at a point (x,y,z)(x, y,z), we have to add the contributions from all these point sources together. This corresponds to the Huygens-Fresnel principle postulated earlier in the Spatial Coherence section of the Interference chapter. Because a more rigorous derivation starting from the Helmholtz equation[2] would be rather lengthy, we will just give the final result:

where we wrote again U0(x,y)=U(x,y,0)U_0(x,y)=U(x,y,0) and where

r=(x−x′)2+(y−y′)2+z2.\begin{align*} r=\sqrt{(x-x')^2+(y-y')^2+z^2}. \end{align*}

Remarks.

  1. The formula Eq. (12) is not completely rigorous because a term that is a factor 1/(kr)1/(kr) smaller (and which in practice therefore is very much smaller) has been omitted.

  2. In Eq. (12) there is an additional factor z/rz/r that has been omitted in the standard time-harmonic spherical wave formulation. This factor means that the amplitudes of the spherical waves in the Rayleigh-Sommerfeld diffraction integral depend on direction (although their wave fronts are spherical), the amplitudes being largest in the forward direction.

  3. The angular spectrum method amounts to a multiplication by exp⁡(izkz)\exp(i z k_z) in Fourier space, while the Rayleigh-Sommerfeld integral is a convolution with respect to (x,y)(x,y). It is a property of the Fourier transform that a multiplication in Fourier space corresponds to a convolution in real space and vice versa. Indeed a mathematical result called Weyl’s identity implies that the rigorous Rayleigh-Sommerfeld formulation and the plane wave expansion (i.e. the angular spectrum method) give identical results.

3Intuition for the Spatial Fourier Transform in Optics

Since spatial Fourier transformations play an important role in our discussion of the propagation of light, it is important to understand them not just mathematically, but also intuitively.

What happens when an object is illuminated and the reflected or transmitted light is detected at some distance from the object? Let us look at transmission for example. When the object is much larger than the wavelength, a transmission function τ(x,y)\tau(x,y) is often defined and the field transmitted by the object is then assumed to be simply the product of the incident field and the function τ(x,y)\tau(x,y). For example, for a hole in a metallic screen with diameter large compared to the wavelength, the transmission function would be 1 inside the hole and 0 outside. However, if the object has features of the order of the wavelength, this simple model of multiplying by a transmission function breaks down and the transmitted field must instead be determined by solving Maxwell’s equations. This is not easy, but some software packages can do it.

Now suppose that the transmitted electric field has been obtained in a plane z=0z=0 very close to the object (a distance within a fraction of a wavelength). This field is called the transmitted near field and it may have been obtained by simply multiplying the incident field with a transmission function τ(x,y)\tau(x,y) or by solving Maxwell’s equations. This transmitted near field is a kind of footprint of the object. But it should be clear that, although it is quite common in optics to speak in terms of “imaging an object”, strictly speaking we do not image an object as such, but we image the transmitted or reflected near fields which are a kind of copy of the object. After the transmitted near field has been obtained, we apply the angular spectrum method to propagate the individual plane waves through homogeneous matter (e.g. air) from the object to the detector plane or to an optical element like a lens.

Let U0(x,y)=U(x,y,0)U_0(x,y)=U(x,y,0) be a component of the transmitted near field. The first step is to Fourier transform it, by which the field component is decomposed into plane waves. To each plane wave, characterized by the wave numbers kxk_x and kyk_y, the Fourier transform assigns a complex amplitude F(U0)(kx2π,ky2π)\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right), the magnitude of which indicates how important a role this particular wave plays in the formation of the near field. So what can be said about the object field U0(x,y)U_0(x,y), by looking at the magnitude of its spatial Fourier transform ∣F(U0)(kx2π,ky2π)∣|\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)|?

Suppose U0(x,y)U_0(x,y) has sharp features, i.e. there are regions where U0(x,y)U_0(x,y) varies rapidly as a function of xx and yy. To describe these features as a combination of plane waves, these waves must also vary rapidly as a function of xx and yy, which means that the length of their wave vectors kx2+ky2\sqrt{k_x^2+k_y^2} must be large. Thus, the sharper the features that U0(x,y)U_0(x,y) has, the larger we can expect ∣F(U0)(kx2π,ky2π)∣|\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)| to be for large kx2+ky2\sqrt{k_x^2+k_y^2}, i.e. high spatial frequencies can be expected to have large amplitude. Similarly, the slowly varying, broad features of U0(x,y)U_0(x,y) are described by slowly fluctuating waves, i.e. by F(U0)(kx2π,ky2π)\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) for small kx2+ky2\sqrt{k_x^2+k_y^2}, i.e. for low spatial frequencies. This is illustrated in Figure 4.

To investigate these concepts further we choose a certain field, take its Fourier transform, remove the higher spatial frequencies and then invert the Fourier transform. We then expect that the resulting field has lost its sharp features and only retains its broad features, i.e. the image is blurred. Conversely, if we remove the lower spatial frequencies but retain the higher, then the result will only show its sharp features, i.e. its contours. These effects are shown in Figure 6. Recall that when kx2+ky2>(2πλ)2k_x^2+k_y^2 > \left(\frac{2\pi}{\lambda}\right)^2, the plane wave decays exponentially as the field propagates. During propagation through homogeneous space, evanescent components are exponentially attenuated. At an ordinary far-field detector they are overwhelmed by noise, so conventional far-field imaging has limited resolution. Near-field methods can measure some of this detail before it decays.

It is this fact that motivates near-field microscopy, which tries to detect these evanescent waves by scanning close to the sample, thus obtaining subwavelength resolution.

So we have seen how we can guess properties of some object field U0(x,y)U_0(x,y) given the amplitude of its spatial Fourier transform ∣F(U0)(kx2π,ky2π)∣|\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)|. But what about the phase of F(U0)(kx2π,ky2π)\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)? Although one cannot really guess properties of U0(x,y)U_0(x,y) by looking at the phase of F(U0)(kx2π,ky2π)\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) the same way as we can by looking at its amplitude, it is in fact the phase that plays a larger role in defining U0(x,y)U_0(x,y). This is illustrated in Figure 8: if the amplitude information of F(U0)(kx2π,ky2π)\mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right) is removed, features of the original U0(x,y)U_0(x,y) may still be retrieved. Knowing only Fourier magnitude generally does not uniquely determine the original field. Additional measurements or constraints can sometimes recover the phase. Thus, the phase of a field F(U0)\mathcal{F}(U_0) is very important, arguably often more important than its amplitude. However, we cannot measure the phase of a field directly, only its intensity I=∣F(U0)∣2I=|\mathcal{F}(U_0)|^2 from which we can calculate the amplitude ∣F(U0)∣|\mathcal{F}(U_0)|. It is this fact that makes phase retrieval an entire field of study on its own: how can we find the phase of a field, given that we can only perform intensity measurements? This question is related to a new field of optics called “lensless imaging”, where amplitudes and phases are retrieved from intensity measurements and the image is reconstructed computationally. Interesting as this topic may be, we will not treat it in these notes and refer instead to master’s courses in optics [3].

Remark. The importance of the phase for the field can also be seen by looking at the plane wave expansion Eq. (6). We have seen that the field in a plane z=constantz=\text{constant} can be obtained by propagating the plane waves by multiplying their amplitudes by the phase factors exp⁡(izkz)\exp(i z k_z), which depend on the propagation distance zz. If one leaves the evanescent waves out of consideration (since after some distance they hardly contribute to the field anyway), it follows that only the phases of the plane waves change upon propagation, while their amplitudes (the moduli of their complex amplitudes) do not change. Yet, depending on the propagation distance zz, widely differing light patterns are obtained (see e.g. Figure 12).

Central Fourier components correspond to broad image features while distant components correspond to fine detail.

Figure 4:A qualitative interpretation of spatial Fourier transforms. The low spatial frequencies (i.e. small kx2+ky2\sqrt{k_x^2+k_y^2}) represent slow fluctuations, and therefore contribute to the broad features of the real-space object. The high spatial frequencies (i.e. large kx2+ky2\sqrt{k_x^2+k_y^2}) fluctuate rapidly, and can therefore form sharp features in the real-space object.

Removing high spatial frequencies from a photograph blurs its edges; the retained Fourier spectrum is a central disk.

(a) Removing the high spatial frequencies

Removing low spatial frequencies leaves mostly outlines; the Fourier spectrum has a dark central disk.

Figure 6:(b) Removing the low spatial frequencies

Demonstration of the roles of different spatial frequencies. By removing the high spatial frequencies, only the broad features of the image remain and resolution is lost. If the low spatial frequencies are removed, only the sharp features (i.e. the contours) remain.

A photograph reconstructed with Fourier phase retained but most magnitude information removed still shows recognizable structure.

(a) Removing the amplitude information by setting the amplitude of propagating and evanescent waves to 1 and 0, respectively.

A photograph reconstructed after setting Fourier phase to zero loses most recognizable structure.

Figure 8:(b) Removing the phase information by setting the phase equal to 0.

Demonstration of the role of the phase of the spatial Fourier transform. If the amplitude information is removed, but phase information is kept, some features of the original image are still recognizable. Removing Fourier phase destroys most recognizable structure in this example; magnitude-only measurements require additional constraints to recover an image.

Another aspect of the Fourier transform is the uncertainty principle. It states that many waves of different frequencies have to be added to get a function that is confined to a small space[4]. Stated differently, if U(x,y)U(x,y) is confined to a very small region, then F(U)(kx,ky)\mathcal{F}(U)(k_x,k_y) must be very spread out. This can also be illustrated by the scaling property of the Fourier transform:

ifh(x)=f(ax)thenF(h)(kx2π)=1∣a∣F(f)(kx2πa),\begin{align*} \text{if} \quad h(x)=f(ax) \quad \text{then} \quad \mathcal{F}(h)\left(\frac{k_x}{2\pi}\right)=\frac{1}{|a|}\mathcal{F}(f)\left(\frac{k_x}{2\pi a}\right), \end{align*}

which simply states that the more h(x)h(x) is squeezed by increasing aa, the more its Fourier transform F(h)\mathcal{F}(h) spreads out. This principle is illustrated in Figure 9. The uncertainty principle is familiar from quantum physics where it is stated that a particle cannot have both a definite momentum and a definite position. In fact, this is just one particular manifestation of the uncertainty principle just described. A quantum state ∣ψ⟩|\psi\rangle can be described in the position basis ψx(x)\psi_{x}(x) as well as in the momentum basis ψp(p)\psi_p(p). Up to normalization and the change of variable k=p/ℏk=p/\hbar, the basis transformation between these representations is a Fourier transform

ψp(p)=12πℏ∫−∞∞ψx(x)e−ipx/ℏ dx.\begin{align*} \psi_p(p)=\frac{1}{\sqrt{2\pi\hbar}} \int_{-\infty}^{\infty}\psi_x(x)e^{-ipx/\hbar}\,\mathrm dx. \end{align*}

Hence, the two are obviously subject to the uncertainty principle! In fact, any two quantum observables which are related by a Fourier transform (also called conjugate variables), such as position and momentum, obey this uncertainty relation. The uncertainty relation states:

After substantial propagation, the detectable spectrum is effectively limited to propagating transverse wave numbers kx2+ky2≤k2k_x^2+k_y^2\le k^2. A conventional focused field therefore has a characteristic transverse scale of order 1/k1/k, with an exact spot size set by its aperture and by the chosen width criterion.

This sets the scale of the conventional far-field diffraction limit.

As a circular field spot becomes smaller, its Fourier pattern spreads into a wider ringed distribution.

Figure 9:Demonstration of the uncertainty principle. The more confined U(x,y)U(x,y) is, the larger the spread of F(U)(kx2π,ky2π)\mathcal{F}(U)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right).

4Fresnel and Fraunhofer Approximations

The Fresnel and Fraunhofer approximations are two approximations of the Rayleigh-Sommerfeld integral Eq. (12). The approximations are accurate provided the propagation distance zz is sufficiently large. In the Fraunhofer approximation, zz has to be quite large, i.e. larger than for the Fresnel approximation, which is already accurate for typical distances occurring in optical systems. Putting it differently: in order of most accurate to least accurate (i.e. only valid for large propagation distances), the diffraction integrals would rank as:

4.1Fresnel Approximation

We assume that zz in Eq. (12) is so large that in the denominator we can approximate rr by zz:

U(x,y,z)≃1iλ∬U0(x′,y′)zreikrr dx′dy′≃1iλz∬U0(x′,y′)eikr dx′dy′.\begin{aligned} U(x,y,z) &\simeq\frac{1}{i\lambda}\iint U_0(x',y') \frac{z}{r}\frac{e^{ikr}}{r}\,\mathrm dx'\mathrm dy'\\ &\simeq\frac{1}{i\lambda z}\iint U_0(x',y')e^{ikr}\,\mathrm dx'\mathrm dy'. \end{aligned}

The reason why we cannot apply the same approximation for rr in the exponent is that in the exponent rr is multiplied by k=2π/λk= 2\pi /\lambda, which is a very large number at optical frequencies, so any error introduced by approximating rr would be drastically magnified by multiplying by kk which can easily lead to a completely different value of exp⁡(ikr)=cos⁡(kr)+isin⁡(kr)\exp(ikr)=\cos(kr)+i\sin(kr). To approximate rr in exp⁡(ikr)\exp(ikr) we must be more careful and apply a Taylor expansion. Recall that

r=(x−x′)2+(y−y′)2+z2=z (x−x′)2+(y−y′)2z2+1.\begin{align*} r&= \sqrt{(x-x')^2+(y-y')^2+z^2} &= z\, \sqrt{\frac{(x-x')^2+(y-y')^2}{z^2}+1}. \end{align*}

We know that the Taylor expansion around s=0s=0 implies:

s+1=1+s2−s28+… .\begin{align*} \sqrt{s+1}=1+\frac{s}{2}-\frac{s^2}{8}+\dots. \end{align*}

Since we assume that zz is large, (x−x′)2+(y−y′)2z2\frac{(x-x')^2+(y-y')^2}{z^2} is small, so we have

r=z1+(x−x′)2+(y−y′)2z2≃z+(x−x′)2+(y−y′)22z(Fresnel approximation).\begin{aligned} r &=z\sqrt{1+\frac{(x-x')^2+(y-y')^2}{z^2}}\\ &\simeq z+\frac{(x-x')^2+(y-y')^2}{2z} \qquad\text{(Fresnel approximation)}. \end{aligned}

With this approximation, we arrive at the Fresnel diffraction integral, which can be written in the following equivalent forms:

U(x,y,z)≈eikziλz∫ ⁣∫U0(x′,y′)eik2z[(x−x′)2+(y−y′)2] dx′ dy′=eikzeik(x2+y2)2ziλz∫ ⁣∫U0(x′,y′)eik(x′2+y′2)2ze−ik(xzx′+yzy′) dx′ dy′=eikzeik(x2+y2)2ziλzF{U0(x′,y′)eik(x′2+y′2)2z}(xλz,yλz)\begin{align*} \begin{split} U(x,y,z) &\approx \frac{e^{ikz}}{i\lambda z}\int\!\int U_0(x',y')e^{\frac{ik}{2z}\left[(x-x')^2+(y-y')^2\right]}\,\text{d}x'\,\text{d}y' \\ &= \frac{ e^{ikz}e^{\frac{ik(x^2+y^2)}{2z}}}{i\lambda z}\int\!\int U_0(x',y') e^{\frac{ik(x'^2+y'^2)}{2z}}e^{-ik\left(\frac{x}{z}x'+\frac{y}{z}y'\right)}\,\text{d}x'\,\text{d}y' \\ &= \frac{e^{ikz}e^{\frac{ik(x^2+y^2)}{2z}}}{i\lambda z} \mathcal{F}\left\{U_0(x',y')e^{\frac{ik(x'^2+y'^2)}{2z}}\right\}\left(\frac{x}{ \lambda z },\frac{y}{\lambda z}\right) \end{split} \end{align*}

Especially the last expression is interesting, because it shows that

Note that this propagator depends on the distance of propagation zz.

Remark. By Fourier transforming Eq. (20), one can get the plane wave amplitudes of the Fresnel approximation. It turns out that these amplitudes are equal to F(U0){\cal F}(U_0) multiplied by a phase factor which is obtained from a paraxial approximation of the exact phase factor exp⁡(izkz)\exp(i z k_z), i.e. kzk_z is approximated by a quadratic function of kx,kyk_x, k_y. Therefore the Fresnel approximation is also called the paraxial approximation. In fact, it can be shown that the Fresnel diffraction integral is a solution of the paraxial wave equation and conversely, that every solution of the paraxial wave equation can be written as a Fresnel diffraction integral[5].

4.2Fraunhofer Approximation

To obtain the Fraunhofer approximation, we will make one further approximation to rr in exp⁡(ikr)\exp(ikr) in addition to the Fresnel approximation:

r≃z+(x−x′)2+(y−y′)22z(Fresnel approximation).r\simeq z+\frac{(x-x')^2+(y-y')^2}{2z} \qquad\text{(Fresnel approximation)}.
r≃z+x2+y2−2xx′−2yy′2z(Fraunhofer approximation).r\simeq z+\frac{x^2+y^2-2xx'-2yy'}{2z} \qquad\text{(Fraunhofer approximation)}.

Hence we have omitted the quadratic terms x′2+y′2x'^2+y'^2, and in comparison with the Fresnel diffraction integral, we omit the factor exp⁡[ik(x′2+y′2)/(2z)] \exp\left[ik(x'^2+y'^2)/(2z)\right] to obtain the Fraunhofer diffraction integral:

U(x,y,z)≈eikzeik(x2+y2)2ziλzF(U0)(xλz,yλz).\begin{align*} U(x,y,z)\approx \frac{e^{ikz}e^{\frac{ik(x^2+y^2)}{2z}}}{i\lambda z} \mathcal{F}(U_0)\left(\frac{x }{ \lambda z}, \frac {y}{\lambda z }\right). \end{align*}

This leads to the following important observation:

Note that to obtain the Fraunhofer field in (x,y,z)(x,y,z), the Fourier transform has to be evaluated at spatial frequencies x/(λz)x/(\lambda z) and y/(λz)y/(\lambda z). These spatial frequencies scale with 1/z1/z and the overall field U(x,y,z)U(x,y,z) is proportional to 1/z1/z. This implies that when zz is increased the field pattern spreads out without changing its shape while its amplitude goes down so that the total energy is preserved. Stated differently, apart from the factor 1/z1/z in front of the integral, the Fraunhofer field depends on the angles x/zx/z and y/zy/z. Therefore for large propagation distances zz for which the Fraunhofer approximation is accurate, the field becomes broader (it diverges) when the propagation distance increases.

Remarks.

  1. The Fresnel approximation is, like the Fraunhofer approximation, a Fourier transform of the field in the starting plane (z=0z=0), evaluated at spatial frequencies which depend on the point of observation:

ξ=xλz,η=yλz.\begin{align*} \xi = \frac{x}{\lambda z}, \quad \eta=\frac{y}{\lambda z}. \end{align*}

However, in contrast to the Fraunhofer approximation, the Fresnel approximation depends additionally in a different way on the propagation distance zz, namely through the exponent of the Fresnel propagator in the integrand. Therefore the Fresnel approximation gives quite diverse patterns depending on the propagation distance zz, as is shown in Figure 12.

  1. In the Rayleigh-Sommerfeld diffraction integral, the field is written as a superposition of spherical waves. In the Fresnel approximation the spherical waves are approximated by parabolic waves. Finally, in the Fraunhofer approximation the propagation distance is so large that the parabolic waves can be approximated by plane waves.

  2. Let fa,b(x,y)=f(x−a,y−b)f_{a,b}(x,y)=f(x-a,y-b) be the function obtained from ff by translation. From the general property of the Fourier transform:

F(fa,b)(ξ,η)=e−2πi(ξa+ηb)F(f)(ξ,η),\begin{align*} {\cal F}(f_{a,b})(\xi,\eta) = e^{ -2\pi i (\xi a + \eta b)} {\cal F}(f)(\xi,\eta), \end{align*}

it follows that when the field U0U_0 is translated, the intensity in the Fraunhofer far field is not changed. In contrast, due to the additional quadratic phase factor in the integrand of the Fresnel integral, the intensity of the Fresnel field in general changes when U0U_0 is translated.

  1. Suppose that U0U_0 is the field immediately behind an aperture A{\cal A} with diameter DD in an opaque screen. It can then be shown that points (x,y,z)(x,y,z) of observation, for which the Fresnel and Fraunhofer diffraction integrals are sufficiently accurate, satisfy:

zλ≫(max⁡(x′,y′)∈A(x−x′)2+(y−y′)2λ)4/3(Fresnel).\frac{z}{\lambda}\gg \left(\frac{\max_{(x',y')\in\mathcal A} \sqrt{(x-x')^2+(y-y')^2}}{\lambda}\right)^{4/3} \qquad\text{(Fresnel)}.
zλ≫(Dλ)2(Fraunhofer).\frac{z}{\lambda}\gg\left(\frac D\lambda\right)^2 \qquad\text{(Fraunhofer)}.

The Fresnel number is defined by

NF=D2λz,      Fresnelnumber.\begin{align*} N_F = \frac{D^2}{\lambda z}, \;\;\; \mathbf{Fresnel number}. \end{align*}

A small Fresnel number, such as NF<0.1N_F<0.1 with this definition of DD, usually makes the Fraunhofer approximation accurate over paraxial observation angles; larger values call for the Fresnel or exact treatment (see Figure 12). Suppose that D=1 mmD= 1~\text{mm} and the wavelength is that of green light: λ=550 nm\lambda=550~\text{nm}. Then the illustrative NF<0.1N_F<0.1 criterion requires z>18 mz>18~\text{m}, so a distance above about 20 m is appropriate.

  1. The paraxial Fraunhofer formula used here assumes:

∣xz∣≪1,∣yz∣≪1(paraxial observation).\left|\frac{x}{z}\right|\ll1,\qquad \left|\frac{y}{z}\right|\ll1 \qquad\text{(paraxial observation)}.

Here x/zx/z and y/zy/z approximate direction angles only in the paraxial regime. A large value of x/zx/z does not imply an evanescent wave; it means this approximation is invalid. For example, keeping both ratios below about 0.3 limits the angular error.

  1. In any expression for an optical field, one may always omit factors of constant phase, i.e. an overall phase which does not depend on position. If one is only interested in the field in certain planes z=constantz=\text{constant}, then a factor like exp⁡(ikz)\exp(ikz) may also be omitted. Further, in some cases also a position dependent phase factor in front of the Fresnel and Fraunhofer diffraction integrals is omitted, namely when only the intensity is of interest. In exercises it is usually mentioned that this factor may be omitted: if this is not stated, it should be retained in the formulae.

4.3Examples of Fresnel and Fraunhofer approximations

Fresnel approximation of the field of two point sources.

Consider two mutually coherent time-harmonic point sources at rs+=(a/2,0,0)\mathbf{r}_s^+=(a/2,0,0) and rs−=(−a/2,0,0)\mathbf{r}_s^-=(-a/2,0,0). The fields in r=(x,y,z)\mathbf{r}=(x,y,z) emitted are according to the time-harmonic field equation (see the Interference chapter) proportional to

U±(r)=eik∣r−rs±∣∣r−rs±∣.U_{\pm}(\mathbf{r}) = \frac{e^{i k |\mathbf{r}-\mathbf{r}_s^\pm|}}{|\mathbf{r} -\mathbf{r}_s^\pm|}.

We apply the Fresnel approximation for large zz:

∣r−rs±∣=z1+(x∓a/2)2+y2z2≃z+(x∓a/2)2+y22z=z+x2+y2+a2/42z∓ax2z.\begin{aligned} |\mathbf r-\mathbf r_s^\pm| &=z\sqrt{1+\frac{(x\mp a/2)^2+y^2}{z^2}}\\ &\simeq z+\frac{(x\mp a/2)^2+y^2}{2z}\\ &=z+\frac{x^2+y^2+a^2/4}{2z}\mp\frac{ax}{2z}. \end{aligned}

Hence,

U±(r)≈eikzzeikx2+y22zeika28z e∓ikax2z,U_\pm(\mathbf{r}) \approx \frac{e^{ikz}}{z} e^{i k \frac{x^2+y^2}{2z} } e^{ i k\frac{ a^2}{8z}} \, e^{∓ i k \frac{a x}{2z}},

where in the denominator we replaced ∣r−rs±∣|\mathbf{r}-\mathbf{r}_s^\pm| by zz. Note that the Fraunhofer approximation amounts to eika2/(8z)≈1e^{ i k a^2/(8z)} \approx 1 while the phase factor eikx2+y22ze^{i k \frac{x^2+y^2}{2z} } remains. The intensity on a screen z=constantz=\text{constant} of the sum of the two fields for the case that the sources have equal strength and emit in phase is:

Itot(r)=∣U+(r)+U−(r)∣2=1z2∣e−ikax2z+eikax2z∣2=2z2[1+cos⁡(2πaxλz)].\begin{align*} I_{tot}(\mathbf{r}) &= | U_+(\mathbf{r})+U_{-}(\mathbf{r}) |^2 = \frac{1}{z^2} |e^{-i k \frac{a x}{2z}} + e^{i k \frac{a x}{2z}}|^2 \\ &= \frac{2}{z^2} \left[ 1 + \cos\left(2 \pi \frac{a x}{\lambda z}\right)\right]. \end{align*}

In the far field, the intensity results from interference of two approximately plane waves with phase factors exp⁡[±ikax/(2z)]\exp[\pm i k ax/(2z)] and is given by a cosine function (see Figure 10). For these symmetric, equal-amplitude point sources, the common quadratic source phase cancels from the intensity, so the Fresnel and Fraunhofer expressions agree within their shared paraxial range. For more sources at different positions, the Fresnel phases need not be common. The leading paraxial intensity is independent of yy. Formally, its minima satisfy

xz=(2m+1)λ2a,\frac{x}{z}=(2m+1)\frac{\lambda}{2a},

and its maxima satisfy

xz=mλa,\frac{x}{z}=m\frac{\lambda}{a},

for integers mm within the valid small-angle range. If a<λ/2a<\lambda/2, the first formal minimum lies outside that range and no true far-field zero is accessible. The figure below also includes the near field, where these far-field formulas do not apply.

Near-field intensity map of two closely spaced point sources, with interference lobes that evolve over a few wavelengths.

Figure 10:Near-field intensity from two mutually coherent point sources of equal strength and phase at λ=600\lambda=600 nm. The far-field trend follows Eq. (33). Their separation is 200 nm. The image shows distances of only a few wavelengths and therefore is not a Fraunhofer-pattern example.

Fraunhofer approximation of a rectangular aperture in a screen.

Let the screen be z=0z=0 and the aperture be given by −a/2<x<a/2-a/2 < x < a/2, −b/2<y<b/2-b/2 < y < b/2. The transmission function τ(x,y)\tau(x,y) is:

τ(x,y)=1[−a/2,a/2](x)1[−b/2,b/2](y),\begin{align*} \tau(x,y)= 1_{[-a/2,a/2]}(x) 1_{[-b/2, b/2]}(y), \end{align*}

where

1[−a/2,a/2](x)={1, if −a2≤x≤a2,0, otherwise,\begin{align*} 1_{[-a/2, a/2]}(x) = \left\{ \begin{array}{l}1, \text{ if } -\frac{a}{2} \leq x \leq\frac{a}{2}, \\0, \text{ otherwise}, \end{array}\right. \end{align*}

and similarly for 1[−b/2,b/2](y)1_{[-b/2, b/2]}(y). Let the aperture be illuminated by a perpendicular incident plane wave with unit amplitude. Then the field immediately behind the screen is:

U0(x,y)=τ(x,y)=1[−a/2,a/2](x)1[−b/2,b/2](y),\begin{align*} U_0(x,y)=\tau(x,y) = 1_{[-a/2,a/2]}(x) 1_{[-b/2, b/2]}(y), \end{align*}

We have

F(1[−a/2,a/2])(ξ)=∫−a/2a/2e−2πiξx dx=eπiaξ−e−πiaξ2πiξ=a sinc(πaξ),\begin{align*} {\cal F}\left( 1_{[-a/2,a/2] }\right)(\xi) &= \int_{-a/2}^{a/2} e^{-2\pi i\xi x} \, \text{d} x \\ &= \frac{ e^{\pi i a \xi}-e^{-\pi i a\xi}}{2\pi i \xi} \\ &= a \text{ sinc}(\pi a \xi), \end{align*}

where  sinc(u)=sin⁡(u)/u\text{ sinc}(u)=\sin(u)/u. Hence,

F(U0)(xλz,yλz)=ab sinc(πaxλz) sinc(πbyλz).\begin{align*} {\cal F}(U_0)\left(\frac{x}{\lambda z},\frac{y}{\lambda z}\right) = a b \text{ sinc}\left(\frac{\pi a x}{\lambda z}\right) \text{ sinc}\left(\frac{\pi b y}{\lambda z}\right). \end{align*}

The Fraunhofer far field at a large distance zz from a rectangular aperture in a mask is obtained by substituting Eq. (40) into Eq. (23).

Remarks.

  1. The first zero along the xx-direction from the center x=0x=0 occurs for

x=±λza.\begin{align*} x= \pm \frac{\lambda z}{a}. \end{align*}

The distance between the first two zeros along the xx-axis is 2λz/a2\lambda z/a and is thus larger when the width along the xx-direction of the aperture is smaller.

  1. The single-slit first zero requires ∣sin⁡θ∣=λ/a≤1|\sin\theta|=\lambda/a\le1. Thus no angular zero is possible for a<λa<\lambda. A subwavelength aperture still affects the measured far field, but inferring its width becomes sensitive to a model, signal-to-noise ratio, and calibration.

  2. As illustrated in Figure 11, the Fraunhofer diffraction pattern as a function of diffraction angle is narrowest in the direction in which the aperture is widest.

Three rectangular apertures with increasing height produce diffraction patterns increasingly narrow in the vertical direction.

Figure 11:Fraunhofer diffraction pattern of a rectangular aperture in an opaque screen. Left: the width of the aperture in the yy-direction is twice that in the xx-direction; middle: the width in the yy-direction is 5 times that in the xx-direction; right: the width in the yy-direction is 10 times that in the xx-direction.

Fresnel approximation of a rectangular aperture in a mask

The integral in the Fresnel approximation for the field of a rectangular aperture in a mask can be computed analytically and leads to functions that are actually called “Fresnel integrals” which can be studied using the Cornu spirals. We will not go deeper in this matter but simply show the results of the simulations in Figure 12. The distance to the mask increases (NFN_F decreases), from very close to the mask at the bottom right, to further from the mask at the bottom left, to rather far from the mask in the upper right, to the Fraunhofer distance in the upper left figures. Note the change in scale along the axis in the figures and the decrease of intensity with propagation distance. It is seen that the pattern changes and broadens drastically with distance from what is more or less a copy of the aperture, to a pattern that is equal to the Fourier transform of the aperture. Once the Fraunhofer approximation is accurate, a further increase of distance only results in a widening of the pattern and a decrease of overall amplitude without change of shape. In contrast, in the region where the Fresnel approximation is accurate, the shape of the pattern is seen to change a lot with distance to the mask.

Four square-aperture intensity maps show how the pattern changes from a near-field square to a far-field diffraction spot.

Figure 12:Diffraction patterns of a square opening in a mask with corresponding cross-sections along the xx-axis, showing the transition from Fresnel to Fraunhofer approximations. The distance to the mask increases as the Fresnel number NFN_F decreases from the near field pattern close to the mask in the right bottom figures to the Fraunhofer diffraction pattern in the upper left. Note the different scales along the axis in the figures.

Fraunhofer approximation of a periodic array of slits

We can now predict the diffraction pattern of an array of slits of finite width. It follows from the Fraunhofer pattern of a single rectangular aperture that, if the sides parallel to the yy-direction are very long, the Fraunhofer diffraction pattern as a function of angle in the yy-direction is very narrow. In Figure 11b the Fraunhofer diffraction pattern of a rectangular aperture is shown, of which the width in the yy-direction is 10 times the width in the xx-direction. The diffraction pattern is then strongly concentrated along the xx-axis. If we only consider the Fraunhofer pattern for y/z=0y/z=0 while still considering it as a function of x/zx/z, it suffices to compute the Fourier transform only with respect to xx. The problem then becomes a diffraction problem for a one-dimensional slit.

We consider now an array of such slits of which the long sides are all parallel to the yy-axis and we neglect from now on the yy-variable. Suppose Wslit(x)W_{\text{slit}}(x) is the function that describes the transmission of a single slit. Then the transmission function of MM equidistant slits is

τ(x)=∑m=1MWslit(x+(M+1)p2−mp),\begin{align*} \tau(x)=\sum_{m=1}^{M} W_{\text{slit}}\left(x+ (M+1)\frac{p}{2}- mp\right), \end{align*}

where pp is the distance between neighboring slits, i.e. pp is the period of the row. If the illumination is by a perpendicular incident plane wave with unit amplitude, the transmitted near field U0(x)U_0(x) is simply τ(x)\tau(x). Then

F(U0)(ξ)=F(τ)(ξ)=∑m=1MF(Wslit)(ξ) eπi(M+1)pξe−2πimp ξ,\begin{align*} {\cal F}(U_0)(\xi) = {\cal F}(\tau)(\xi)=\sum_{m=1}^M {\cal F}(W_{slit})(\xi)\, e^{\pi i (M+1)p\xi } e^{-2\pi i m p \, \xi}, \end{align*}

where for a slit with width aa we have according to Eq. (39):

F(Wslit)(ξ)=asin⁡(πaξ)πaξ.{\cal F}(W_{slit})(\xi) = a \frac{\sin(\pi a \xi)}{\pi a \xi}.

The condition a<pa < p must hold. Using

∑m=1Me−2πimp ξ=e−2πipξ1−e−2πiMp ξ1−e−2πip ξ=e−πi(M+1)p ξ eiπMp ξ−e−iπMp ξeiπp ξ−e−iπp ξ=e−πi(M+1)p ξ sin⁡(πMp ξ)sin⁡(πp ξ),\begin{align*} \sum_{m=1}^M e^{-2\pi i m p \, \xi } &= e^{-2\pi i p\xi } \frac{ 1- e^{-2\pi i M p \, \xi}}{1-e^{-2\pi i p \, \xi}} \\ &= e^{-\pi i (M +1) p \, \xi}\, \frac{ e^{i \pi M p \, \xi} - e^{-i \pi M p \, \xi}}{e^{i \pi p \, \xi}- e^{-i \pi p \, \xi}} \\ &= e^{-\pi i (M+1) p \, \xi} \, \frac{ \sin( \pi Mp \, \xi)}{\sin(\pi p \, \xi)}, \end{align*}

we get

F(U0)(ξ)=F(Wslit)(ξ)sin⁡(πMpξ)sin⁡(πpξ).{\cal F}(U_0)(\xi) = {\cal F}(W_{slit})(\xi) \frac{\sin( \pi M p \xi)}{ \sin(\pi p \xi)}.

The intensity of the Fraunhofer far field is:

I(x,z)=∣1λzF(U0)(xλz)∣2=1λ2z2 ∣F(Wslit)(θλ)∣2 sin⁡2(πMpλ θ)sin⁡2(πpλ θ).\begin{align*} I(x,z)= \left| \frac{1}{\lambda z}\mathcal{F}(U_0)\left(\frac{x}{\lambda z}\right) \right|^2 = \frac{1}{\lambda^2 z^2}\, \left|{\cal F}(W_{slit})\left(\frac{\theta}{\lambda}\right)\right|^2 \, \frac{\sin^2\left( \pi M\frac{p}{\lambda} \, \theta \right)}{ \sin^2\left(\pi \frac{p}{\lambda}\, \theta \right)}. \end{align*}

where θ≃x/z\theta\simeq x/z is the small diffraction angle. The factor

sin⁡2(πMpλ θ)sin⁡2(πpλ θ),\frac{\sin^2\left( \pi M \frac{p}{\lambda} \, \theta \right)}{ \sin^2\left(\pi \frac{p}{\lambda}\, \theta \right)},

oscillates rapidly with θ\theta because the sine argument in the numerator contains the factor MM of θ\theta while ∣F(Wslit)(θ/λ)∣2|{\cal F}(W_{slit})(\theta/\lambda)|^2 is a slowly varying envelope. This is a manifestation of the property of the Fourier transform that small details of a structure (e.g. the size of a single slit) cause large scale features of the far field pattern, whereas large scale properties such as the length MpM p of the total structure cause quickly changing features. This is illustrated in Figure 13.

The grating interference factor is maximum for directions where both the denominator and numerator of Eq. (48) vanish:

θm≃mλp,m=0,±1,±2,…(paraxial diffraction orders).\theta_m\simeq\frac{m\lambda}{p}, \qquad m=0,\pm1,\pm2,\ldots \quad\text{(paraxial diffraction orders)}.

These directions are called diffraction orders. The exact ray path condition is sin⁡θm=mλ/p\sin\theta_m=m\lambda/p; the formulas here use θm≃sin⁡θm\theta_m\simeq\sin\theta_m for small angles. At the paraxial order directions,

sin⁡2(πMpλ θm)sin⁡2(πpλ θm)=M2,\frac{\sin^2\left( \pi M\frac{p}{\lambda} \, \theta_m \right)}{ \sin^2\left(\pi \frac{p}{\lambda}\, \theta_m \right)} = M^2,

The sine ratio tends to M2M^2 at an order. Therefore the intensity of the mmth order is

M2λ2z2 ∣F(Wslit)(mp)∣2,\begin{align*} \frac{M^2}{\lambda^2 z^2} \, \left| {\cal F}(W_{slit})\left(\frac{m}{p}\right) \right|^2, \end{align*}

hence it is proportional to the square of the number of periods and to the squared modulus of the envelope in θm\theta_m.

Between two adjacent diffraction orders, Eq. (48) has M−1M-1 zeros and M−2M-2 secondary maxima (see Figure 13). The angular width of a diffraction order is half the angular distance to the nearest zeros next to the order, i.e.

Δθ=λMp,angularwidthofadiffractionorder.\begin{align*} \Delta \theta = \frac{\lambda}{M p}, \hspace{1cm} \mathbf{angular width of a diffraction order.} \end{align*}

If there are more slits, the intensity peaks into which the energy is diffracted are narrower and the peaks are higher.

Five illuminated slits produce narrow bright grating peaks under a broad single-slit envelope.

Figure 13:An illustration of a diffraction pattern of a series of five slits.

The exact grating condition sin⁡θm=mλ/p\sin\theta_m=m\lambda/p requires ∣sin⁡θm∣≤1|\sin\theta_m|\le1. This limits the propagating orders:

∣m∣≤pλfor propagating grating orders.|m|\le\frac p\lambda \qquad\text{for propagating grating orders}.

Hence, the larger the ratio of the period to the wavelength, the more diffraction orders.

The property Eq. (49) that the diffraction orders m≠0 m\neq 0 depend on wavelength is used to separate wavelengths. Grating spectrometers use periodic structures such as an array of slits to very accurately separate and measure wavelengths. The mmth diffraction orders of two wavelengths λ1\lambda_1 and λ2>λ1\lambda_2>\lambda_1 are just separated if

mλ2p>mλ1p+Δθ=mλ1p+λ1Mp,m\frac{\lambda_2}{p} > m\frac{\lambda_1}{p} + \Delta \theta = m\frac{\lambda_1}{p } + \frac{\lambda_1}{M p},

which implies with Δλ=λ2−λ1\Delta \lambda=\lambda_2-\lambda_1 and λ=λ1\lambda=\lambda_1 that

Δλλ>1mM.\frac{\Delta \lambda}{\lambda}> \frac{1}{m M}.

It follows that the resolution is higher when there are more slits and for a larger diffraction order. However, the disadvantage of using higher diffraction orders is that often their intensity is less. For a grating with 1000 periods one can obtain a resolution of Δλ/λ=10−3\Delta \lambda/\lambda =10^{-3} in the first order.

It should be remarked that a grating is obtained for any periodic variation of the refractive index. If the proper transmission function for the unit cell of the grating is substituted for WslitW_{slit}, the formulae above also give the Fraunhofer far field of such more general diffraction gratings. By changing the unit cell, the envelope of the diffraction pattern can be changed and a certain order can be given more intensity. In Figure 14 a so-called blazed grating is shown which is used in reflection and which has a strong first diffracted order for a certain angle of incidence.

A sawtooth reflection grating directs an incident beam into several orders, with one order favored by the blaze angle.

Figure 14:Diffraction grating used in reflection with a so-called blazed unit cell.

Remark. A periodic row of slits is an example of a diffraction grating. A grating is a periodic structure, i.e. the refractive index is a periodic function of position. Structures can be periodic in one, two and three directions. A crystal acts as a three-dimensional grating whose period is the period of the crystal, which typically is a few Angstroms. X-rays have wavelengths comparable to atomic spacings, ranging across and below the ångström scale. When a beam of x-rays illuminates a crystal, a detector in the far field measures the Fraunhofer diffraction pattern given by the intensity of the Fourier transform of the refracted near field. These diffraction orders of crystals for x-rays were discovered by Von Laue and are used to study the atomic structure of crystals.

Screenshot of the Optics Lab simulation

Figure 15:Transmission and reflection gratings on an optical bench. Change the grating period and the illuminating wavelength and watch the diffracted orders move — a geometric-optics preview of the far-field grating condition used for crystals and for laboratory diffraction gratings.

Interactive simulation: Optics Lab

5Fraunhofer Diffraction Revisited

Screenshot of the Wave Interference simulation

Figure 16:An aperture and the far-field pattern it produces, with size, shape, and wavelength adjustable. Everything narrow in the aperture is wide in the pattern — the θ∼λ/a\theta\sim\lambda/a scaling of Fraunhofer diffraction, seen whole rather than one angle at a time.

Interactive simulation: Wave Interference

Fraunhofer diffraction patterns can qualitatively be explained by considering directions in which destructive and constructive interference occur. Consider two mutually coherent point sources S1S_1, S2S_2 on the xx-axis as shown in Figure 17. We assume that these point sources are in phase. On a screen at large distance zz an interference pattern is observed. If the distance zz of the screen is very large, the spherical wave fronts emitted by the point sources are almost plane at the screen and the field is the Fraunhofer far field of the two point sources. At point PP on the screen at a distance xx above the zz-axis the optical path difference of the waves emitted by the two sources is approximately given by S2Q=aθS_2Q=a \theta, where θ=x/z\theta=x/z is assumed small. Hence constructive interference occurs for angles θ\theta such that S2Q=mλS_2Q=m\lambda for some integer mm, i.e. when

θ=mλa,constructive interference.\begin{align*} \theta = m \frac{\lambda}{a}, \hspace{1cm} \text{constructive interference}. \end{align*}

Destructive interference occurs when the path length difference satisfies S2Q=λ/2+mλS_2Q=\lambda/2 + m \lambda for some integer mm, hence for angles

θ=(1/2+m)λadestructive interference.\begin{align*} \theta = ( 1/2 + m)\frac{\lambda}{a} \hspace{1cm} \text{destructive interference}. \end{align*}

If the point sources have the same strength, their fields perfectly cancel for these angles.

Two point sources separated by a send rays to a distant screen at angle theta.

Figure 17:Interference of two mutually coherent point sources. For very large zz, points PP where constructive or destructive interference occurs satisfy for some integer mm: S2Q=mλS_2Q=m \lambda and S2Q=(1/2+m)λS_2Q=(1/2 + m) \lambda, respectively.

Now consider a slit as shown in Figure 18 which is illuminated by a perpendicular incident plane wave. By the Huygens-Fresnel principle, the field at a screen far from the slit is the sum of the fields of point sources in the aperture, with strengths proportional to the field in the slit at the position of the point sources. When the slit is illuminated by a plane wave at perpendicular incidence, all point sources are in phase and have equal strength. Divide the slit into two equal halves as shown in Figure 18. The point sources in the slit can be arranged into pairs, of which one point source is in the upper half of the slit and the other is at the equivalent position (at distance a/2a/2 from the other point source) in the lower half of the slit. Let θ\theta be an angle for which the two point sources of a pair cancel each other i.e.

θ=(1/2+m)λa/2=(1+2m)λa,\begin{align*} \theta= (1/2+ m) \frac{\lambda}{a/2} = (1+ 2m)\frac{\lambda}{a}, \end{align*}

since the distance between the point sources is a/2a/2. By translating the pair of point sources through the slit, it follows that both half slits perfectly cancel each other for these angles. In this way we have found the angles θ=mλ/a\theta = m\lambda/a with mm odd for which destructive interference occurs. Destructive interference for mm even can be derived by further subdivisions of the aperture.

A slit of width a is divided into paired points separated by a over two to explain destructive interference.

Figure 18:By dividing the slit into two slits of size a/2a/2 each and considering pairs of point sources of which one is in the upper half of the slit and the other is at the corresponding position in the lower half, angles where destructive interference occurs between these point sources lead to minima in the diffraction pattern. Note that the point sources have corresponding positions in the two parts of the slit if their distance is a/2a/2.

In general it is easier to find the angles for which the far field vanishes than to find (local) maxima of the field. An exception is the case of a diffraction grating. It follows from Figure 19 that there will be constructive interference between adjacent periods, and hence for all periods, for angles for which the distance SQSQ in Figure 19 is a multiple of the wavelength, i.e. for

sin⁡θm=mλp(θm≃mλp for small angles).\sin\theta_m=\frac{m\lambda}{p} \qquad\left(\theta_m\simeq\frac{m\lambda}{p} \text{ for small angles}\right).

which corresponds to the direction of the diffraction orders. For other angles the phases of the fields of the different periods differ widely and therefore the fields almost cancel at these angles when there are many periods. This explains that for a diffraction grating of many periods, the far field intensity is highly concentrated in particular directions given by the orders Eq. (59) which depend only on the ratio of the wavelength and the period.

Adjacent points on a grating separated by period p send rays to the same far-field direction.

Figure 19:If the angle θ\theta is such that SQSQ is a multiple of the wavelength, two adjacent periods, and hence all periods of the grating, constructively interfere. These angles correspond to the diffraction orders.

6Fourier Optics

In this section we apply diffraction theory to a lens. We consider in particular the focusing of a parallel beam and the imaging of an object.

6.1Focusing of a Parallel Beam

A lens induces a local phase change to an incident field in proportion to the local thickness of the lens. Let a plane wave which propagates parallel to the optical axis be incident on a positive lens. In Gaussian geometrical optics the incident rays are all focused into the image focal point. According to the Principle of Fermat, all rays have traveled the same optical distance when they intersect in the image focal point where they constructively interfere and cause an intensity maximum. In the focal region, the wavefronts are parts of spheres centered at the focal point and cut off by the cone with the focal point as top and opening angle 2a/f2 a/f, as shown in Figure 20. Behind the focal point, there is a second cone with again spherical wavefronts, but there the light is propagating away from the focal point. According to Gaussian geometrical optics, image space is completely dark outside the two cones in Figure 20. However, as we will show, in diffraction optics this is not true.

We assume that the lens is thin and choose as origin of the coordinate system the center of the thin lens with the positive zz-axis along the optical axis. Let fif_i be the zz-coordinate of the image focal point according to Gaussian geometrical optics. Then (0,0,fi)(0,0,f_i) is the image focal point. Let (x,y,z)(x,y,z) be a point between the lens and this focal point. According to geometrical optics the field in (x,y,z)(x,y,z) is proportional to

{e−ikx2+y2+(z−fi)2−iωtx2+y2+(z−fi)2,if (x,y,z) is inside the cone,0, if (x,y,z) is outside the cone,\left\{ \begin{array}{lr} \frac{e^{- i k \sqrt{x^2 + y^2 + (z-f_i)^2}-i\omega t}}{\sqrt{x^2 + y^2 + (z-f_i)^2}}, &\text{if } (x,y,z) \text{ is inside the cone}, \\ 0, &\text{ if } (x,y,z) \text{ is outside the cone}, \end{array}\right.

where we have included the time-dependence. Indeed the surfaces of constant phase:

−x2+y2+(z−fi)2−ωt=constant,\begin{align*} -\sqrt{x^2 + y^2 + (z-f_i)^2}-\omega t=\text{constant}, \end{align*}

are spheres centered at the focal point. For increasing time, these spheres converge to the focal point, while the amplitude increases as the distance to the focal point decreases, so that energy is preserved.

Remark. For a point (x,y,z)(x,y,z) to the right of the focal point, i.e. for z>fiz>f_i, the spherical wave fronts propagate away from the focal point and therefore there −ik-ik should be replaced by +ik+ik in the exponent in Eq. (60).

The exit pupil of the lens is in the plane z=0z=0 where, according to Eq. (60), the field is

1⊙a(x,y)e−ikx2+y2+fi2x2+y2+fi2,\begin{align*} 1_{⊙_a}(x,y) \frac{e^{-i k \sqrt{x^2 + y^2 + f_i^2}}}{ \sqrt{ x^2 + y^2 + f_i^2}}, \end{align*}

where the time dependence has been omitted and

1⊙a(x,y)={1       if x2+y2<a2,0       otherwise\begin{align*} 1_{⊙_a}(x,y)= \left\{ \begin{array}{l}1 \;\;\; \text{ if } x^2+y^2< a^2, \\0 \;\;\; \text{ otherwise} \end{array} \right. \end{align*}

i.e. 1⊙a(x,y)=11_{⊙_a}(x,y)=1 for (x,y)(x,y) in the exit pupil of the lens and =0=0 otherwise. If a/fia/f_i is sufficiently small, we may replace the distance x2+y2+fi2\sqrt{x^2 +y^2 + f_i^2} between a point in the exit pupil and the image focal point in the denominator of Eq. (62) by fif_i. This is not allowed in the exponent, however, because of the multiplication by the large wave number kk. In the exponent we therefore use instead the first two terms of the Taylor series Eq. (18):

x2+y2+fi2=fi1+x2+y2fi2≈fi+x2+y22fi,\begin{align*} \sqrt{x^2 + y^2 + f_i^2} = f_i \sqrt{ 1 + \frac{x^2 + y^2 }{f_i^2}} \approx f_i + \frac{x^2 + y^2}{2f_i}, \end{align*}

which is valid for a/fia/f_i sufficiently small. Then Eq. (62) becomes:

1⊙a(x,y)e−ikx2+y22fi,\begin{align*} 1_{⊙_a}(x,y) e^{-i k \frac{x^2 + y^2}{2 f_i}}, \end{align*}

where we dropped the constant factors eikfie^{i k f_i} and 1/fi1/f_i. For a general field U0(x,y)U_0(x,y) incident on the lens, i.e. in the entrance pupil, the lens applies a transformation such that the field in the exit plane becomes:

U0(x,y)→U0(x,y)1⊙a(x,y)e−ikx2+y22fi,\begin{align*} & U_0(x,y) \to U_0(x,y) 1_{⊙_a}(x,y) e^{- i k \frac{x^2 + y^2}{2 f_i}}, \end{align*}

The function that multiplies U0(x,y)U_0(x,y) is the transmission function of the lens:

τlens(x,y)=1⊙a(x,y)e−ikx2+y22fi.\begin{align*} \tau_{\text{lens}}(x,y) = 1_{⊙_a}(x,y) e^{-ik \frac{x^2 + y^2}{2 f_i}}. \end{align*}

This result makes sense: in the center (x,y)=0(x,y)=0 the lens is thickest, so the phase is shifted the most (but we can define this phase shift to be zero because only phase differences matter, not absolute phase). As is indicated by the minus-sign in the exponent, the further you move away from the center of the lens, the less the phase is shifted. For shorter fif_i, the lens focuses more strongly, so the phase shift changes more rapidly as a function of the radial coordinate. Note that the transmission function Eq. (67) has modulus 1 so that energy is conserved.

The field on the right-hand side of Eq. (66) is used in diffraction optics as the field in the exit pupil. But instead of using ray tracing, the field in the focal region is computed using diffraction integrals. We substitute the field in the exit pupil in the Fresnel diffraction integral Eq. (20) and obtain:

U(x,y,z)=eikzeik(x2+y2)2ziλzF{U0(x′,y′)1⊙a(x′,y′)eikx′2+y′22(1z−1fi)}(xλz,yλz).\begin{align*} U(x,y,z)=\frac{e^{ikz}e^{\frac{ik(x^2+y^2)}{2z}}}{i\lambda z} \mathcal{F}\left\{U_0(x',y') 1_{⊙_a}(x',y') e^{ik\frac{x'^2+y'^2}{2}\left(\frac{1}{z}-\frac{1}{f_i}\right)}\right\}\left(\frac{x}{\lambda z },\frac{y}{ \lambda z }\right). \end{align*}

The intensity I=∣U∣2I=|U|^2 is shown at the bottom left of Figure 20. It is seen that the intensity does not monotonically increase for decreasing distance to the focal point. Instead, secondary maxima occur along the optical axis. Also the boundary of the light cone is not sharp, as predicted by geometrical optics, but diffuse. The bottom right of Figure 20 shows the phase in the focal region. The wave fronts are close to but not exactly spherical inside the cones.

A lens focuses plane wavefronts into a cone; simulated panels show the blurred intensity boundary and phase near focus.

Figure 20:Top: wavefronts of the incident plane wave and the focused field according to Gaussian geometrical optics. There is no light outside of the two cones. Bottom left: amplitude as predicted by diffraction optics. The boundary of the cones is diffuse and it is not absolutely dark outside of the cones. Furthermore, the intensity does not increase monotonically with decreasing distance to the focal point, as predicted by geometrical optics. Bottom right: phase of the focused field as predicted by diffraction optics.

For points in the image focal plane of the lens, i.e. z=fiz=f_i, we have

U(x,y,fi)=eikfieik(x2+y2)2fiiλfiF{U0(x′,y′)1⊙a(x′,y′)}(xλfi,yλfi),\begin{align*} U(x,y,f_i)= \frac{e^{ikf_i}e^{\frac{ik(x^2+y^2)}{2f_i}}}{i\lambda f_i} \mathcal{F}\left\{U_0(x',y')1_{⊙_a}(x',y') \right\}\left(\frac{ x}{ \lambda f_i},\frac{ y}{ \lambda f_i }\right), \end{align*}

which is the same as the Fraunhofer integral for propagation over the distance fif_i!

It can be shown that the fields in the front focal plane U(x,y,−fi)U(x,y,-f_i) and the back focal plane U(x,y,fi)U(x,y,f_i) are related exactly by a Fourier transform, i.e. without the quadratic phase factor[6]. So a lens performs a Fourier transform. Let us see if that agrees with some of the facts we know from geometrical optics.

  1. We know from Gaussian geometrical optics that if we illuminate a positive lens with rays parallel to the optical axis, these rays all intersect in the image focal point. This corresponds with the fact that for U0(x,y)=1U_0(x,y)=1 (i.e. plane wave illumination, neglecting the finite aperture of the lens, i.e. neglecting diffraction due to the finite size of the pupil), the Fourier transform of the pupil field is a delta peak:

F(U0)(kx2π,ky2π)=δ(kx2π)δ(ky2π),\begin{align*} \mathcal{F}(U_0)\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi}\right)=\delta\left(\frac{k_x}{2\pi}\right)\delta\left(\frac{k_y}{2\pi}\right), \end{align*}

which represents the perfect focused spot (without diffraction).

  1. If in Gaussian geometrical optics we illuminate a lens with tilted parallel rays of light (a plane wave propagating in an oblique direction), then the point in the back focal plane where the rays intersect is laterally displaced. A tilted plane wave is described by U0(r)=exp⁡(ik0⋅r)U_0(\mathbf{r})=\exp(i\mathbf{k}_0\cdot\mathbf{r}), and its Fourier transform with respect to (x,y)(x,y) is given by

F{U0}(kx2π,ky2π,z)=δ(kx−k0,x2π)δ(ky−k0,y2π),\mathcal{F}\{U_0\}\left(\frac{k_x}{2\pi},\frac{k_y}{2\pi},z\right)=\delta\left(\frac{k_x-k_{0,x}}{2\pi}\right)\delta\left(\frac{k_y-k_{0,y}}{2\pi}\right),

which is indeed a shifted delta peak (i.e. a shifted focal spot).

It seems that the diffraction model of light confirms what we know from geometrical optics. But in the previous two examples we discarded the influence of the finite size of the pupil, i.e. we have left out of consideration the function 1⊙a1_{⊙_a} in calculating the Fourier transform. If U0(x,y)=1U_0(x,y)=1 in the entrance pupil and we take the finite size of the pupil properly into account, the δ\delta-peaks become blurred: the focused field is then given by the Fourier transform of the circular disc with radius aa, evaluated at spatial frequencies ξ=xλfi\xi = \frac{x}{\lambda f_i}, η=yλfi\eta =\frac{ y}{\lambda f_i}. This field is called the Airy spot and is given by Eq. (72):

U(x,y,fi)∝πa2 2J1(q)q,q=2πaλfix2+y2.U(x,y,f_i)\propto \pi a^2\,\frac{2J_1(q)}{q}, \qquad q=\frac{2\pi a}{\lambda f_i}\sqrt{x^2+y^2}.

where J1J_1 is the Bessel function of the first kind and where the phase factors in front of the Fourier transform have been omitted. The pattern is shown in Figure 21. It is circularly symmetric and consists of a central maximum surrounded by concentric rings of alternating zeros and secondary maxima with decreasing amplitudes. In cross-section, as a function of r=x2+y2r=\sqrt{x^2+y^2}, the Airy pattern is similar (but not identical) to the  sinc\text{ sinc}-function. From the uncertainty principle illustrated in Figure 9 it follows that the size of the focal spot decreases as aa increases, and from Eq. (72) we see that the Airy function is a function of the dimensionless variable ar/(λfi)a r/(\lambda f_i). Hence the focal spot becomes narrower as a/(λfi)a/(\lambda f_i) increases. For this paraxial lens in air, its numerical aperture is approximately

NA=sin⁡ ⁣(arctan⁡afi)≃afi.\begin{align*} \mathrm{NA}=\sin\!\left(\arctan\frac{a}{f_i}\right)\simeq\frac{a}{f_i}. \end{align*}

Since the first zero of the Airy pattern occurs at r≃0.61λfi/ar\simeq0.61\lambda f_i/a, its first-zero radius in this paraxial air-space model is

rAiry≃0.61λNA\begin{align*} r_{\mathrm{Airy}}\simeq0.61\frac{\lambda}{\mathrm{NA}} \end{align*}
The Airy field cross-section has a central lobe and side lobes; its two-dimensional intensity has a bright central disk and rings.

Figure 21:Left: cross section of the field of the Airy pattern. Right: intensity of the Airy pattern.

Remark. In the simple case of a single thin lens, the entrance and exit pupils coincide with the lens itself. As has been explained in the Stops section of the Geometrical Optics chapter, the exit pupil in systems consisting of several lenses is the real or virtual image of the aperture stop under all optical lenses to the right of the stop. To model the effect of diffraction in such more complicated systems, diffraction is assumed to take place entirely in the exit pupil. The field in the exit pupil is first determined by non-paraxial ray tracing and is then integrated over the exit pupil using the Fresnel diffraction integral.

6.2Imaging by a lens

It follows from the derivations in the previous section that the Airy pattern is the image of a point source infinitely far in front of a lens. In this section we study the imaging of a general object at a finite distance from the lens. Consider first a real point object on the optical axis with coordinate z=so<foz=s_o<f_o to the left of the object focal point of a positive lens with image focal coordinate fi>0f_i>0. This lens will form a real image with positive coordinate si>0s_i>0.

The field in image space is derived using the Fresnel diffraction integral, similar to the focused field in the previous section. We postulate that the lens transforms the field radiated by the point object into a spherical wave in the exit pupil, which converges to the ideal image point of Gaussian geometrical optics. We substitute this spherical pupil field in the Fresnel diffraction integral to compute the field in image space. Then for an object point on the optical axis we find the same Airy pattern as in Figure 21, except that the variable ar/(λfi)a r/(\lambda f_i) is replaced by ar/(λsi)a r/(\lambda s_i), where sis_i is the image coordinate found from the lens equation. This field is called the Point Spread Function (PSF):

PSF⁡(x,y)∝2J1(qi)qi,qi=2πaλsix2+y2.\operatorname{PSF}(x,y)\propto \frac{2J_1(q_i)}{q_i}, \qquad q_i=\frac{2\pi a}{\lambda s_i}\sqrt{x^2+y^2}.

For object points that are not on the optical axis, the PSF is translated such that it remains centered on the ideal Gaussian image point.

A general object field Uo(x,y)U_o(x,y) can be considered a superposition of point objects, and the images of these points are given by translated PSFs:

PSF(x−xi,y−yi),\text{PSF}(x-x_i, y-y_i),

where (xi,yi)(x_i, y_i) are the transverse coordinates of the image point according to Gaussian geometrical optics. The total image field is obtained by summing (integrating) over these PSFs, weighted by the field at the object points:

Ui(x,y,si)∝∬PSF⁡(x−Mxo,y−Myo)Uo(xo,yo,so) dxo dyo.U_i(x,y,s_i)\propto \iint\operatorname{PSF}(x-Mx_o,y-My_o) U_o(x_o,y_o,s_o)\,\mathrm dx_o\,\mathrm dy_o.

Here MM is the signed transverse magnification. An overall scale factor is omitted from the field integral. The integral can be made into a convolution by using the coordinates xi,yix_i, y_i as integration variables.

It is clear from Eq. (75) that a larger radius aa of the lens and a smaller wavelength λ\lambda imply a narrower PSF. This in turn implies that the kernel in the convolution is more sharply peaked and hence that the resolution of the image is higher [7].

Remark.

  1. If laser light is used to illuminate the object, the object field may be considered perfectly coherent. This implies that a detector in the image plane would measure the squared modulus of the complex field Eq. (77):

Ii(x,y,si)∝∣∬PSF⁡(x−Mxo,y−Myo)Uo(xo,yo,so) dxo dyo∣2.I_i(x,y,s_i)\propto \left|\iint\operatorname{PSF}(x-Mx_o,y-My_o) U_o(x_o,y_o,s_o)\,\mathrm dx_o\,\mathrm dy_o\right|^2.

In this case the system is called a coherent imaging system.

  1. If the object is a spatially incoherent extended source, the cross terms between independent source points vanish after averaging. Therefore, in this case the intensity in the image plane is given by the incoherent sum:

Ii(x,y,si)∝∬∣PSF⁡(x−Mxo,y−Myo)∣2Io(xo,yo,so) dxo dyo.I_i(x,y,s_i)\propto \iint\left|\operatorname{PSF}(x-Mx_o,y-My_o)\right|^2 I_o(x_o,y_o,s_o)\,\mathrm dx_o\,\mathrm dy_o.

where Io=⟨∣Uo∣2⟩I_o=\langle|U_o|^2\rangle is the mean intensity distribution of the extended source. Hence the image intensity is expressed in terms of the intensity of the source by a convolution with the intensity of the PSF. This system is called an incoherent imaging system.

  1. An object is often illuminated by a spatially incoherent extended light source and then imaged. According to the discussion in the Propagation of Mutual Coherence section of the Interference chapter, the field that illuminates the object is then partially coherent. It is more coherent when the angle that the source extends at the object is smaller. The intensity in the image plane can be computed by splitting the spatially incoherent source into sufficiently many mutually incoherent point sources and computing the intensities in the image plane due to the illumination of the object by each individual point source. The total intensity in the image plane is then the sum of these intensities.

  2. We have considered only scalar diffraction theory. However, for a lens with numerical aperture larger than 0.6, the change of polarization can be important. Then a more general diffraction theory is needed [8].

6.3Spatial Light Modulators and Optical Fourier Filtering

Two lenses separated by their focal distances put a Fourier filtering plane between an input and an output field.

Figure 22:Set-up for Fourier filtering. The first lens creates a Fourier transform of U(x,y)U(x,y), to which we can apply some operation (e.g. applying different phase shifts to different parts of the field). The second lens then applies another Fourier transform (which gives an inverted image after the second transform, up to scale and phase factors).

7Super-resolution

Ordinary far-field imaging is limited by the propagating spatial frequencies admitted by the pupil. Evanescent components decay with distance, and a finite numerical aperture rejects some propagating components as well. The Airy first-zero radius in image space is

rAiry≃0.61 λ0NAi(circular pupil in air).r_{\mathrm{Airy}}\simeq0.61\,\frac{\lambda_0}{\mathrm{NA}_i} \qquad\text{(circular pupil in air)}.

For a single thin lens in air, NAi≃a/si\mathrm{NA}_i\simeq a/s_i and the object-side numerical aperture is approximately NAo≃∣M∣NAi≃a/∣so∣\mathrm{NA}_o\simeq|M|\mathrm{NA}_i\simeq a/|s_o|. In a general optical system, entrance and exit pupil sizes must be treated separately. These formulas describe the conventional linear, diffraction-limited image of a point. The examples below gain different kinds of resolution by changing the illumination, detection, medium, or response of the specimen.

An ideal negative-index slab forms one image point inside the slab and another beyond it.

Figure 23:Pendry’s perfect lens consists of a slab of a material with negative permittivity and negative permeability such that their absolute values are equal to the positive permittivity and positive permeability of the surrounding medium. In the ideal lossless, exactly matched model, a source point has image points inside and beyond the slab.

The ideal slab proposal dates to 2000 [10]. Artificial composites can approximate a negative refractive index over a limited bandwidth, but finite loss and imperfect matching prevent a perfect image.

Six examples of layered, patterned, and nanowire structures used to approximate anisotropic optical materials.

Figure 24:Examples of composite materials consisting of thin (sub-wavelength) layers of metals and dielectrics. These artificial materials are called metamaterials. (A. Poddubny, I. Iorsh, P. Belov, & Y. Kivshar, Hyperbolic Metamaterials, {N}at. {P}hoton., 7(12), 948-957 (2013)).

A few natural hyperbolic media exist for visible frequencies, but there are more in the mid-infrared. Researchers try to approximate hyperbolic media by metamaterials, made of, for example, multilayers consisting of alternating thin metallic and dielectric layers, so that the effective permittivity has the desired hyperbolic property. Also metallic nanopillars embedded in a dielectric are used.

Excitation and doughnut depletion beams leave a small fluorescent center; paired images compare confocal and STED resolution.

Figure 25:Spot used for excitation (top left) and for depletion (top middle). Fluorescence signal top right. In the lower figure the confocal image is compared to the STED image. (P.F. Rodriguez and al., Building a fast scanning stimulated emission depletion microscope, Materials Science (2012))

8Chapter Summary

Footnotes
  1. Sixty Symbols (2012) Basic explanation of Fourier transforms. Also see Section 3.

  2. For a rigorous derivation see e.g. Goodman (2005), §3.3, §3.4, §3.5 - and Lecture Notes of Advanced Photonics, Delft University of Technology.

  3. See the course Advanced Photonics given at TUDelft.

  4. Sixty Symbols (2012) Basic explanation of the uncertainty principle (though in the context of quantum physics)

  5. For a proof see Siegman (1986)

  6. Goodman (2005), §5.2.2 - Several calculations on the Fourier transforming properties of lenses.

  7. Hecht (2017) §10.2.6 ‘Resolution of imaging systems’.

  8. Braat & Török (2019)

  9. See Liu et al. (2008)

  10. Pendry (2000)

References
  1. Poddubny, A., Iorsh, I., Belov, P., & Kivshar, Y. (2013). Hyperbolic metamaterials. Nature Photonics, 7(12), 948–957. 10.1038/nphoton.2013.243
  2. Sixty Symbols. (2012). Every picture is made of waves - Sixty Symbols. https://www.youtube.com/watch?v=mEN7DTdHbAU
  3. Sixty Symbols. (2012). Heisenberg’s Microscope - Sixty Symbols. https://www.youtube.com/watch?v=dgoA_jmGIcA
  4. Goodman, J. W. (2005). Introduction to Fourier Optics (3rd ed.). Roberts.
  5. Siegman, A. E. (1986). Lasers. University Science Books.
  6. Hecht, E. (2017). Optics (5th ed.). Pearson.
  7. Braat, J., & Török, P. (2019). Imaging Optics. Cambridge University Press.
  8. Liu, Z., Lee, H., Xiong, Y., Sun, C., & Zhang, X. (2008). Far-field optical hyperlens magnifying sub-diffraction-limited objects. Physical Review Letters, 100(12), 123904.
  9. Pendry, J. B. (2000). Negative refraction makes a perfect lens. Physical Review Letters, 85(18), 3966.