Expand this Topic clickable element to expand a topic
Skip to content
Optica Publishing Group

Comprehensive theoretical analysis of the period chirp in laser interference lithography

Open Access Open Access

Abstract

We present a theoretical investigation on laser interference lithography used for the exposure of linear gratings. The focus is on the geometry of the arising interference lines on the substrate, in particular on their period and orientation, depending on the illumination geometry as determined by the setup. The common approach with point sources emitting spherical wavefronts is considered for the illumination. Three different cases are discussed, namely the interference between two point sources with either two convex, two concave or mixed, i.e., convex and concave wavefronts. General equations focusing mainly on the calculation of the period and the orientation of the grating lines are derived for each of the three exposure cases considering arbitrarily positioned point sources and arbitrarily shaped substrates. Additionally, the interference of symmetrically positioned point sources illuminating plane substrates is investigated, as these boundary conditions significantly simplify the derived equations.

Published by Optica Publishing Group under the terms of the Creative Commons Attribution 4.0 License. Further distribution of this work must maintain attribution to the author(s) and the published article's title, journal citation, and DOI.

1. INTRODUCTION

Within the last decade, diffraction gratings, i.e., grating waveguide structures, have become essential in laser development. They can be used to serve various purposes, such as intra-cavity stabilization of polarization and wavelength [1,2] or spectral beam combining for power-scaling [3]. Furthermore, they play a particularly important role in the field of chirped pulse amplification (CPA), where they are used in optical pulse compressors. Pulse compressors based on diffraction gratings are state of the art and allow for high dispersions, which in turn form the basis of high-power lasers operating in the megajoule and petawatt range [46]. The periodic structures of diffraction gratings are usually produced using well-established technologies in the micro- and nano-electronic industry. The step in the production that mainly defines the geometry of the structures is the lithography, where various techniques are common. Electron-beam lithography, where the structures are directly written into the photo-resist, is very flexible but comparatively slow [710]. Nano imprint is faster but less flexible, as the geometry of the structures is fixed by the master stamp [7,11,12]. A technique that is very suitable to produce periodic linear structures is laser interference lithography (LIL), as it is both fast and flexible. The exposure of the photo-resist exploits the interference of two coherent beams, which form a standing intensity pattern inside the photo-resist [13,14]. Two configurations are commonly used for the experimental implementation, which are briefly described in the following. In the first one, the laser beam is split into two beams using a beam splitter. The two coherent beams are then divergently guided toward the substrate, illuminating it with the laser’s far field. The second approach is the so-called Lloyds-mirror approach, where the laser beam is not split up but interferes with itself using a mirror placed perpendicular to the substrate [1317]. Another approach that cannot be left unmentioned is scanning beam interference lithography (SBIL). However, since its underlying principle is not the one of a one-shot illumination but consists in writing the grating lines similar to electron-beam lithography [18], it is usually not included in classical LIL and, hence, also not in the context of this publication.

On the one hand, the simple generation of the standing intensity pattern and the one-shot illumination is what makes LIL so attractive; on the other hand, it is also its biggest weakness. By principle, only plane wavefronts can create a standing intensity pattern with constant period on a plane substrate. In practice, the incident waves are divergently propagated over long distances, with the planarity being only an approximation [15]. The consequence is called chirp or hyperbolic periodicity, which are both synonyms for the spatially dependent change of the period of the standing intensity pattern on the photo-resist coated substrate.

The term chirp was already used in 1977 by Katzir et al. [19] to describe structures that were produced by interfering plane and convex wavefronts. Since the chirp is usually undesired in the production of periodic structures, various groups have reported on its consequences. For example, Hibino and Hegedus investigated the effects on wavefronts diffracted by period-chirped gratings when modeling the lithographic process with two point sources emitting convex wavefronts that interfere on a plane substrate [20]. Noda et al. [21] presented a theoretical work on holographic and mechanically ruled gratings and considered the exposure of a substrate to the convex waves emitted from two arbitrarily positioned point sources but did neither derive an expression for the two-dimensional distribution of the period and the orientation of the grating lines nor consider the interference patterns generated by combinations with concave spherical waves. In 1996, Ferrera and Schattenburg gave an equation to calculate the grating period across the entire surface of a substrate when the convex wavefronts of two point sources are symmetrically incident on a plane substrate [22]. Kim et al., who deliberately produced chirped gratings, addressed the exposure using mixed wavefronts, i.e., convex and concave, on a plane substrate. The given equations, however, only allow to calculate the period in one axis [23]. In addition to these theoretical investigations on the chirp, various techniques have been developed to detect such periodicity errors during the process [22] or in the final grating [2426]. Compensation techniques have also been developed, for example, by deliberately bending the substrate during the exposure to reduce the resulting period chirp [27]. The spatially dependent period, however, is not the only consequence when interfering non-planar wavefronts. It also leads to a spatially dependent curvature of the grating lines. Since this effect cannot be separated from the spatially dependent period, the term chirp is typically used to refer to both effects. This spatially dependent curvature has already been investigated for the case of symmetrically positioned point sources with convex wavefronts incident on a plane substrate [28]. The chirp is a prominent problem, but it has only been investigated in part and for specific special cases. Depending on the publications, plane substrates or symmetrically placed point sources were assumed, and equations were often only derived for one axis and based on simplifications. Furthermore, the focus mainly lies on the grating period but hardly on the curvature of the grating lines.

In the present publication, we aim to analyze both the cause and the effects of the chirp in a holistic way, and we present a new mathematical approach, which enables us to incorporate the various cases of exposures with combinations of convex and concave spherical waves into one model. The exposure to aspheric wavefronts as discussed by Noda et al. [29] is beyond the scope of the present report. Considering spherical waves, we derive generally applicable analytical equations, i.e., without any simplifications, to describe the spatial distribution of the period and the orientation of the grating lines on arbitrarily shaped substrates for the general case of arbitrarily positioned point sources. Additionally, a simplified mathematical formalism derived for few special cases (described in Sections 3.C and 5.C) with symmetrically positioned point sources illuminating a plane substrate iso9 described. This holistic mathematical description of LIL is of high interest for many reasons. On the one hand, it serves the manufacturers, who can derive improvement strategies for the fabrication process. On the other hand, it serves the users, who can derive implementation hints from the given equations and models. As we will show, depending on the application, there are preferred areas on chirped gratings.

2. MODELING OF THE SETUPS

The model constituting the basis of all derivations presented in the following is the interference of the spherical wavefronts emitted by two coherent point sources. This model is considered to be valid, since the common LIL setups (not SBIL) use the far field of a laser beam for the exposure of photo-resist-coated substrates, as shown in Fig. 1. A spectrally narrow beam emitted by a fiber-coupled laser is collimated and subsequently evenly divided by a beam splitter. The two replicas of the beam are both focused through an aperture and directed toward the sample, which is to be exposed. The focusing serves both to clean up the beam and to create the divergence required to illuminate the full surface of the sample.

 figure: Fig. 1.

Fig. 1. Simplified sketch of a LIL setup comprising a beam splitter to create two coherent laser beams. The setup is modeled with two coherent point sources $A$ and $B$, located at the foci of the beams. They emit convex spherical wavefronts illuminating the substrate.

Download Full Size | PDF

Since the distance $z \gg {z_R}$. between the substrate and the focus of the laser beam is much larger than the beam’s Rayleigh length ${z_R}$, the curvature of the spherical wavefronts at the substrate is equal to the distance $z$. The focus of the laser beam can, therefore, be viewed as a point source emitting convex spherical wavefronts. Considering other setups and further implementations of imaging optics, three exposure cases are possible based on the interference of the waves emitted from two coherent point sources. As shown in Fig. 2(a) the first exposure arrangement involves the interference of two waves with convex wavefronts at the substrate. This is considered to be the most common arrangement and is the abstraction of the system shown in Fig. 1.

 figure: Fig. 2.

Fig. 2. Three possible arrangements for the exposure in LIL, based on the model of the interference of spherical waves emitted from two coherent point sources $A$ and $B$. (a) Convex case, direct interference of the waves with convex wavefronts as emitted from the point sources. (b) Concave case, the waves of the two point sources are focused by means of two lenses, thus creating concave wavefronts that converge to the virtual point sources ${A^*}$ and ${B^*}$. (c) Mixed case, inference between a wave with a convex and a wave with a concave wavefront. Only point source $A$ is imaged to ${A^*}$.

Download Full Size | PDF

The second case, shown in Fig. 2(b), involves the interference of two beams with concave wavefronts. The concave waves are obtained by additional imaging. The third case, shown in Fig. 2(c), corresponds to a combination of the previous two.

3. EXPOSURE WITH TWO CONVEX WAVES

The following derivations for the interference of two convex waves as sketched in Fig. 2(a) are presented in detail as they are the foundation for the two other exposure cases discussed in Sections 4 and 5.

A. Fundamentals

The interference of two convex waves emerging from the point sources $A$ and $B$ is modeled by considering the arrangement shown in Fig. 3. Since the resulting interference pattern is rotationally symmetric around the axis connecting the two point sources, it is sufficient to consider the system in two dimensions to start with. Without loss of generality, a coordinate system is, therefore, chosen in which the two point sources $A$ and $B$ lie on the $x$ axis with the origin exactly in the middle between the two sources. The distance from this axis is denoted by the radial coordinate $r$.

 figure: Fig. 3.

Fig. 3. Cross-sectional (2D) sketch explaining the interference of the two convex spherical waves emitted from the two coherent point sources $A$ and $B$ at a given instant of time $t$. Constructive interference occurs along the curve ${F_{\rm{vex}}}$. The other variables are explained in the text.

Download Full Size | PDF

It is assumed that, at the time $t = 0$, two waves emitted from the point sources $A$ and $B$ constructively interfere at the point ${P_O}$ on the $x$ axis; the corresponding wavefronts with the radii ${R_A}({t = 0})$ and ${R_B}({t = 0})$ are shown by the solid circles. These wavefronts expand with time $t$, as shown by the dashed circles with the radii ${R_A}(t)$ and ${R_B}(t)$. The point at which these two wavefronts experience constructive interference, therefore, moves from ${P_O} = {P_{I,{\rm vex}}}({t = 0})$ to

$${P_{I,{\rm vex}}}(t ) = \left({\begin{array}{*{20}{c}}{{x_{I,{\rm vex}}}(t )}\\{{r_{I,{\rm vex}}}(t )}\end{array}} \right),$$
along the curve ${F_{\rm{vex}}}$, with ${x_{I,{\rm vex}}}(t)$ and ${r_{I,{\rm vex}}}(t)$ being the coordinates of the point ${P_{I,{\rm vex}}}(t)$ on the $x$ and $r$ axis, respectively. According to Pythagoras’ law, it can be stated that
$${R_A}{(t )^2} = {\left({{x_{\rm{PS}}} + {x_{I,{\rm vex}}}(t )} \right)^2} + {r_{I,{\rm vex}}}{(t )^2},$$
$${R_B}{(t )^2} = {\left({{x_{\rm{PS}}} - {x_{I,{\rm vex}}}(t )} \right)^2} + {r_{I,{\rm vex}}}{(t )^2}$$
for the point ${P_{I,{\rm vex}}}(t)$ on the curve ${F_{\rm{vex}}}$, where ${x_{\rm{PS}}} \gt 0$ is the distance of the point sources from the origin. Since time was set to $t = 0$ for the moment when the two considered wavefronts meet at the Point ${P_O} = {P_I}({t = 0})$ at $x = {x_O}$ and $r = 0$, their radii of curvature are given by
$${R_A}(t ) = {x_{\rm{PS}}} + {x_O} + {v_A} \cdot t,$$
$${R_B}(t ) = {x_{\rm{PS}}} - {x_O} + {v_B} \cdot t,$$
where ${v_A}$ and ${v_B}$ are the propagation speeds of the two waves. By assuming the same speed of the wavefronts, i.e., ${v_A} = {v_B}$, Eqs. (1)–(5) can be combined as shown in Appendix A to find that constructive interference occurs along the curve ${F_{\rm{vex}}}$ defined by
$${F_{\rm{vex}}}:\; \frac{{{x^2}}}{{x_O^2}} - \frac{{{r^2}}}{{x_{\rm{PS}}^2 - x_O^2}} = 1,$$
which exhibits a hyperbolic geometry. Considering the rotational symmetry around the $x$ axis of what is shown as a two-dimensional cross section in Fig. 3, ${r^2}$ may be replaced by
$${r^2} = {y^2} + {z^2}$$
to express the three-dimensional geometry $H$ of the intensity pattern in Cartesian coordinates as
$$H:\;\;\frac{{{x^2}}}{{x_O^2}} - \frac{{{y^2}}}{{x_{\rm{PS}}^2 - x_O^2}} - \frac{{{z^2}}}{{x_{\rm{PS}}^2 - x_O^2}} = 1,$$
which evidences that the geometry of the intensity pattern is described by two-sheeted hyperboloids. When the two coherent point sources are assumed to be in phase (or emit with a phase difference of an integer multiple of ${{2}}\pi$), the point ${P_O}$ at which the curve ${F_{\rm{vex}}}$ for constructive interference and, hence, the corresponding hyperboloid crosses the $x$ axis is located at one of the discrete positions,
$${x_{O,n}} = n \cdot \frac{\lambda}{2}\;\;|\;n \in {\mathbb{Z}},$$
where $\lambda$ is the wavelength of the waves. Replacing ${x_O}$ in Eq. (8) by the discrete values ${x_{O,n}}$ yields the hyperboloids ${H_n}$ shown in Fig. 4. Both Figs. 4(a) and 4(b) contain an additional surface $S$, which shall represent the surface of the resist-coated substrate that is to be illuminated. The lines of intersections ${G_{\rm{vex}}}$ between the hyperboloids and the substrate’s surfaces correspond to the resulting grating lines (assuming a negative photo-resist from now on). A symmetrical illumination case is shown in Fig. 4(a), where a plane substrate is exposed, which is arranged symmetrically to the point sources. This case will be the concern of Section 3.C. The general illumination case, i.e., the exposure of an arbitrarily shaped substrate depicted in Fig. 4(b), is discussed in the following Section 3.B. Independent of the case, the grating lines in both subfigures already show that the chirp leads to a spatially dependent grating period and a curvature of the grating lines.
 figure: Fig. 4.

Fig. 4. Hyperboloids ${H_n}$ where the waves of the two coherent point sources $A$ and $B$ experience constructive interference. For illustrative purposes they were calculated with $\lambda = 4\;{\rm{mm}}$ and ${x_{\rm{PS}}} = 20\;{\rm{mm}}$. (a) Hyperboloids and their cross sections at $y = 0$ (black lines) as well as their intersections ${G_{{\rm vex,sym},n}}$ (red lines) with a plane substrate ${S_{\rm vex,sym}}$ (gray sheet). (b) Hyperboloids and their intersections ${G_{{\rm vex,gen},n}}$ (red lines) with an arbitrarily shaped substrate ${S_{\rm vex,gen}}$ (gray sheet).

Download Full Size | PDF

B. General Case of the Convex Arrangement

For the general case, we consider the intersection of the hyperboloids ${H_n}$ with an arbitrarily shaped and arbitrarily positioned substrate as shown in Fig. 4(b). Without loss of generality, we describe its surface ${S_{\rm vex,gen}}$ by defining its $z$ position with the following function,

$${S_{\rm vex,gen}}\!:\;\;\;{z_{\rm vex,gen}}({x,y} ).$$

The grating lines ${G_{{\rm vex,gen},n}}$ arising from the intersection of the hyperboloids ${H_n}$ and the surface ${S_{\rm vex,gen}}$ are then defined by

$${G_{{\rm vex,gen},n}}\!:\; \frac{{{x^2}}}{{x_{O,n}^2}} - \frac{{{y^2}}}{{x_{\rm{PS}}^2 - x_{O,n}^2}} - \frac{{{z_{\rm vex,gen}}{{({x,y} )}^2}}}{{x_{\rm{PS}}^2 - x_{O,n}^2}} = 1,$$
resulting from the insertion of Eq. (10) into Eq. (8). In the application, it is mainly not the grating lines themselves that are of importance, but two of their properties. These are the grating period, i.e., the spacing between the grating lines, and the orientation or the curvature of the grating lines. Of course, these two properties can be determined by calculating every single grating line using Eq. (11), but depending on the geometry of the substrate, this requires a high level of mathematical and computational effort. Simple analytical equations are, therefore, derived in the following, with which the grating period and the orientation of the grating lines can be described in a much easier way.

First, the determination of the period in a two-dimensional system is considered, as shown in Fig. 5(a). The period $\Lambda$ is to be determined at a point $P$ on an axis ${a_S}$, resulting from the interference of the point sources $A$ and $B$. In an infinitesimally small region around the point $P$ the wavefronts of the two point sources can be approximated by plane waves. This assumption is valid for a single point and, therefore, does not contradict the intention of this publication to rigorously consider the curvature of the wavefronts. Without loss of generality, it is furthermore assumed that the wavefronts (represented by the thin red and blue lines) are in phase at point $P$, thus creating a constructive interference pattern as marked by the green lines.

 figure: Fig. 5.

Fig. 5. Model for the derivation of equations describing the grating period and the orientation of the grating lines for the general case. (a) Determination of the period $\Lambda$ at a point $P$ in a two-dimensional system. (b) Transfer of the model shown in (a) into three dimensions.

Download Full Size | PDF

From the geometrical relations depicted in Fig. 5(a) and as already shown by Kim et al. [23] in a similar way, the period can then be defined as

$${\Lambda _{\rm vex,plane}}({\beta ,\theta ,\lambda} ) = \frac{\lambda}{{2\sin (\theta ) \cdot \cos (\beta )}},$$
where $\theta$ is half of the aperture angle between the normals of the wavefronts and $\beta$ is the angle between the bisector $b$ and the normal of the axis ${a_S}$. Alternatively, the period can be expressed by
$${\Lambda _{\rm vex,plane}}({\lambda ,{\varphi _A},{\varphi _B}} ) = \frac{\lambda}{{\sin ({{\varphi _A}} ) + \sin ({{\varphi _B}} )}},$$
using the angles ${\varphi _A}$ and ${\varphi _B}$ between the normals of the wavefronts and the normal of the axis ${a_S}$. In the next step, a three-dimensional system is considered with $P$ being a point on the arbitrary-shaped surface ${S_{\rm vex,gen}}$, as shown in Fig. 5(b). In order to determine the period at the point $P$, the goal is to transfer this three-dimensional system to the two-dimensional system shown in Fig. 5(a). Therefore, we span the illumination plane ${K_{\rm{IP}}}$ between the points $A$, $B$, and $P$ with its normal vector defined by
$${\vec n_{\rm{IP}}} = {\vec{a}_B} \times {\vec{a}_A},$$
with the vectors
$${\vec{a}_A} = \overrightarrow {AP}$$
and
$${\vec{a}_B} = \overrightarrow {BP} .$$

The orientation of the substrate’s surface, i.e., the tangential plane at the point $P$, is referred to as ${K_S}$ and is defined by its normal vector ${\vec n_S}$. The vector ${\vec{a}_S}$, which describes the orientation of the intersection line between the surface plane ${K_S}$, and the illumination plane ${K_{\rm{IP}}}$ can be calculated by the vectorial product,

$${\vec{a}_S} = {\vec n_S} \times {\vec n_{\rm{IP}}}.$$

This vector corresponds to the axis ${a_S}$ from Fig. 5(a) and, thus, enables the transfer of the three-dimensional system into the two-dimensional system. Using this vector, the angles ${\varphi _A}$ and ${\varphi _B}$ in the illumination plane ${K_{\rm{IP}}}$ can be defined as

$${\varphi _A} = \arcsin \left({\frac{{{{\vec{a}}_S} \cdot {{\vec{a}}_A}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_A}} \right|}}} \right)$$
and
$${\varphi _B} = \arcsin \left({- \frac{{{{\vec{a}}_S} \cdot {{\vec{a}}_B}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_B}} \right|}}} \right).$$

By inserting Eqs. (18) and (19) into Eq. (13), the period at the point $P$ with which the vector ${\vec{a}_S}$ intersects the planes ${K_{\rm{CI}}}$ in which constructive interference occurs is given by

$${\Lambda _{{{\vec{a}}_S}}} = \frac{\lambda}{\displaystyle{\frac{{{{\vec{a}}_S} \cdot {{\vec{a}}_A}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_A}} \right|}} - \frac{{{{\vec{a}}_S} \cdot {{\vec{a}}_B}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_B}} \right|}}}}.$$

This period is illustrated in Fig. 6 where the area around the point $P$ with a top-view on the substrate plane ${K_S}$ and only a small section of the illumination plane ${K_{\rm{IP}}}$ is shown. The three green planes symbolize the planes where constructive interference occurs at and around the point, respectively. They correspond to the three green lines shown in Fig. 5(a), whereby the central plane was also depicted in Fig. 5(b). Applying Eq. (20) to the exposure of a plane substrate yields the same result as published by Noda et al. [21] and by Ferrera [22]. However, the real period ${{{\Lambda}}_{\rm vex,gen}}$ in the substrate plane needs to be measured perpendicular to the grating lines. In order to obtain this period ${{{\Lambda}}_{\rm vex,gen}}$ (shown in orange), the angle $\alpha$ between the vectors ${\vec{a}_S}$ and ${\vec g_{\rm{vex}}}$ defined as

$${{\alpha}} = {\rm{arccos}}\left({\frac{{{{\vec{a}}_S} \cdot {{\vec g}_{\rm{vex}}}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec g}_{\rm{vex}}}} \right|}}} \right)$$
has, therefore, to be considered.
 figure: Fig. 6.

Fig. 6. Close-up on the region near the point $P$ with top-sight on the substrate plane ${K_S}$ showing the difference between the periods ${\Lambda _{{{\vec{a}}_S}}}$ and ${{{\Lambda}}_{\rm vex,gen}}$ as well as the derivation of the latter.

Download Full Size | PDF

The vector ${\vec g_{\rm{vex}}}$ describes the orientation of the grating line on the substrate and is mathematically given by the intersection line between the substrate plane ${K_S}$ and the plane ${K_{\rm{CI}}}$ where constructive interference occurs. It is, therefore, given by the cross-product of their normal vectors as

$${\vec g_{\rm{vex}}} = {\vec n_{\rm{CI}}} \times {\vec n_S}.$$

By definition, the plane ${K_{\rm{CI}}}$ contains the bisector $\vec b$ between ${\vec{a}_A}{}$ and ${\vec{a}_B}$ and is perpendicular to the illumination plane ${K_{\rm{IP}}}$. The normal vector ${\vec n_{\rm{CI}}}$ of the plane ${K_{\rm{CI}}}$ is, therefore, defined by

$${\vec{n}_{\rm{CI}}} = {\vec n_{\rm{IP}}} \times {\vec b},$$
with
$${\vec{b}} = \frac{{{{\vec{a}}_A}}}{{\left| {{{\vec{a}}_A}} \right|}} + \frac{{{{\vec{a}}_B}}}{{\left| {{{\vec{a}}_B}} \right|}}.$$

Therefore, the orientation of the grating lines at a point $P$ on an arbitrarily shaped surface can now be determined by combining Eqs. (22)–(24), which yields

$${\vec g_{\rm{vex}}} = \left({{{\vec n}_{\rm{IP}}} \times \left({\frac{{{{\vec{a}}_A}}}{{\left| {{{\vec{a}}_A}} \right|}} + \frac{{{{\vec{a}}_B}}}{{\left| {{{\vec{a}}_B}} \right|}}} \right)} \right) \times {{\vec{n}}_S}.$$

With the help of this vector ${\vec g_{\rm{vex}}}$, Eqs. (20) and (21), and the angular relations of the triangle shown in Fig. 6, the period on the substrate is finally found to be

$$\begin{split}{\Lambda _{\rm vex,gen}} &= \frac{{\lambda \cdot \sin \left({\arccos \left({\frac{{{\vec{a}_{S}} \cdot {\vec{g}_{\rm{vex}}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{g}_{\rm{vex}}}|}}} \right)} \right)}}{\displaystyle{\frac{{{\vec{a}_{S}} \cdot {\vec{a}_{A}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{a}_{A}}|}} - \frac{{{\vec{a}_{S}} \cdot {\vec{a}_{B}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{a}_{B}}|}}}}\\ & = \frac{{\lambda \cdot \sqrt {1 - {{\left({\frac{{{\vec{a}_{S}} \cdot {\vec{g}_{\rm{vex}}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{g}_{\rm{vex}}}|}}} \right)}^2}}}}{\displaystyle{\frac{{{\vec{a}_{S}} \cdot {\vec{a}_{A}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{a}_{A}}|}} - \frac{{{\vec{a}_{S}} \cdot {\vec{a}_{B}}}}{{|{\vec{a}_{S}}| \cdot |{\vec{a}_{B}}|}}}}.\end{split}$$

Equations (25) and (26), thus, enable the calculation of the orientation and the period of an interference pattern along an arbitrarily shaped surface created by two arbitrarily placed point sources.

An example is presented in the following, aiming to show both the application as well as the validity of the derived equations. The two point sources $A$ and $B$ are placed at (–340.2 mm, 0 mm, 940.4 mm) and (340.2 mm, 0 mm, 940.4 mm), respectively, illuminating a substrate ${S_{\rm vex,gen}}$, which is arbitrarily defined by

$${S_{\rm vex,gen}}\!:\;{z_{\rm vex,gen}}({x,y} ) = - 5 \cdot \sin ({x \cdot 0.06} ) - 5 \cdot \sin ({y \cdot 0.07} )$$
and shown in Fig. 7(a). This yields a distance of $d = 1000\;{\rm{mm}}$ between each of the point sources and the center of the substrate with an angle of incidence of $\theta = 19.89^\circ$. The wavelength of the sources was chosen to be $\lambda = 415\;{\rm{nm}}$, thus aiming for a period of ${{\Lambda}} = 610\;{\rm{nm}}$ in case the substrate was flat.
 figure: Fig. 7.

Fig. 7. Example of a wavy surface that is illuminated by the spherical waves of two coherent point sources. (a) Geometry of the surface. The color-scale refers to the $z$ position of the surface. (b) Period of the interference pattern on the illuminated surface as calculated with Eq. (26). The color-scale refers to the value of the period. (c) Orientation of the grating lines as calculated using Eq. (25). The black lines show the local orientation of the grating lines, and the color-scale shows their deviation to the ideal orientation in the $x-y$ plane.

Download Full Size | PDF

The resulting period calculated with Eq. (26) is shown in Fig. 7(b). The period’s inhomogeneity is a direct consequence of the surface’s waviness. When analyzing it, it becomes apparent that the period is mainly influenced by the orientation ($\partial z/\partial x$) of the surface in $x$ direction rather than its orientation ($\partial z/\partial y$) in the $y$ direction or the overall height $z$. This can be well seen at the two blue areas, for example, where the surface has a different $z$ position and different orientation ($\partial z/\partial y$) in the $y$ direction but a similar orientation ($\partial z/\partial x$) in the $x$ direction. Figure 7(c) shows the orientation of the grating lines as calculated with Eq. (25). The orientation is represented by the black lines on the one hand and by the color-scale on the other hand. While the lines represent the spatially resolved vector ${\vec g_{\rm{vex}}}$ on the surface, the color-scale shows the angular deviation of this vector from the ideal orientation of ${{\vec{g}}_{\rm{ideal}}} = [{0,\;1,\;0}]$ in the $x-y$ plane. It can be seen that the tilt of the lines along the $y$ axis is close to zero since the hyperboloids of constructive interference are almost parallel to the $y-z$ plane here (see Fig. 4). Moreover, the results show that the tilt of the grating lines becomes stronger toward the edges, which is due to an increase of the curvatures of the hyperboloids (see Fig. 4).

C. Symmetric Case of the Convex Arrangement

While the previous section treated the general illumination case, this part is devoted to the examination of the special case of symmetrical illumination of a plane substrate, i.e., where the point sources are aligned symmetrically on the $x$ axis while the plane substrate is orientated parallel to the $x-y$ plane as depicted in Fig. 8(a). In this configuration, the plane substrate’s surface is defined by

$${S_{\rm vex,sym}}:\;\;{z_{\rm vex,sym}}({x,y} ) = {z_S},$$
where ${z_S}$ is the distance of the substrate’s surface to the origin. Inserting Eq. (28) into Eq. (11) yields the description of the grating lines (shown in red in Fig. 8). Solving this for $x$, the grating lines ${G_{\rm vex,sym}}$ for the symmetric case are found to be given by
$$\begin{split}&{G_{{\rm vex,sym},n}}\!:\;{x_{\rm vex,sym}}({{x_{O,n}},{x_{\rm{PS}}},y,{z_S}} )\\&\quad = \pm \sqrt {x_{O,n}^2\left({1 + \frac{{{y^2}}}{{x_{\rm{PS}}^2 - x_{O,n}^2}} + \frac{{z_S^2}}{{x_{\rm{PS}}^2 - x_{O,n}^2}}} \right)} .\end{split}$$
 figure: Fig. 8.

Fig. 8. (a) Symmetric arrangement of the two coherent point sources and a plane substrate. The sources are placed on the $x$ axis with equal distance to the origin while the substrate is orientated parallel to the $x-y$ plane at a distance ${z_S}$. The hyperboloids of constructive interference are shown by the colored surfaces, and their intersections with the substrate are shown in red. (b) Section of (a) showing a small region around the point $P$ serving for the derivation of the period ${{{\Lambda}}_{\rm vex,sym}}$ from the period ${{{\Lambda}}_{{\rm vex,sym},x}}$, which is parallel to the $x$ axis.

Download Full Size | PDF

In principle, the period of the interference resulting in this symmetric arrangement can of course be calculated with the generally valid Eq. (26). Thanks to the symmetrical configuration, the much simpler equation

$${{{\Lambda}}_{{\rm vex,sym},x}}({x,{x_{\rm{PS}}},y,{z_S},\lambda} ) = \frac{\lambda}{{\frac{{{x_{\rm{PS}}} + x}}{{\sqrt {z_S^2 + {y^2} + {{({{x_{\rm{PS}}} + x} )}^2}}}} + \frac{{{x_{\rm{PS}}} - x}}{{\sqrt {z_S^2 + {y^2} + {{({{x_{\rm{PS}}} - x} )}^2}}}}}}$$
can be derived. The derivation of this equation is not discussed here since it was already shown in a similar way by Ferrera et al. [22]. What was, however, not considered by Ferrera et al. is that this equation only describes the period parallel to the $x$ axis. This is depicted in Fig. 8(b), where a small section of the substrate’s surface from Fig. 8(a) is shown. Similar to the period derived for the general case, the inclination of the lines requires further consideration. To this end, we consider a point $P = (x,y,{z_S})$ on a grating line ${G_{{\rm vex,sym},n}}$ on the substrate’s surface as shown in Fig. 8(a). In order for this point to lie on the grating line at a given $y$ position, its $x$ coordinate needs to be
$$\begin{split}x &= {x_{\rm vex,sym}}\left({{x_{O,n}},{x_{\rm{PS}}},y,{z_S}} \right)\\& = \pm \sqrt {x_{O,n}^2\left({1 + \frac{{{y^2}}}{{x_{\rm{PS}}^2 - x_{O,n}^2}} + \frac{{z_S^2}}{{x_{\rm{PS}}^2 - x_{O,n}^2}}} \right)} .\end{split}$$

The orientation of the grating line ${G_{{\rm vex,sym},n}}$ at the point $P$ is found by differentiating Eq. (29) with respect to $y$, resulting in

$$\frac{{{\rm d}{x_{\rm vex,sym}}}}{{{\rm d}y}}({{x_{O,n}},{x_{\rm{PS}}},y,{z_S}} ) = \frac{{{x_{O,n}} \cdot y}}{{\left({\;x_{\rm{PS}}^2 - x_{O,n}^2} \right)\sqrt {\frac{{{y^2} + z_S^2}}{{\;x_{\rm{PS}}^2 - x_{O,n}^2}} + \;1}}}.$$

Solving Eq. (31) for ${x_{O,n}}$ yields

$${x_{O,n}}\left({{x_{\rm{PS}}},{x_P},y,{z_s}} \right) = \frac{{x \cdot {x_{\rm{PS}}}}}{{\sqrt {{x^2} + {y^2} + z_S^2 + x_{\rm{PS}}^2}}}.$$

Inserting this in Eq. (32), one finds

$$\begin{split}&\frac{{{\rm d}{x_{\rm vex,sym}}}}{{{\rm d}y}}({x,{x_{\rm{PS}}},y,{z_S}} )\\ &\quad = \frac{{x \cdot y \cdot \sqrt {z_S^2 + {y^2} + x_{\rm{PS}}^2 + {x^2}}}}{{\sqrt {\big({{x^2}z_S^2 + {x^2}{y^2} + {{\big({x_{\rm{PS}}^2 + {y^2} + z_S^2} \big)}^2}} \big)\big({x_{\rm{PS}}^2 + {y^2} + z_S^2} \big)}}}.\end{split}$$

Using this equation for the inclination of the lines and the angle $\epsilon$ from Fig. 8(b), one finds

$${{{\Lambda}}_{\rm vex,sym}}({x,{x_{\rm{PS}}},y,{z_S},\lambda} ) = {{{\Lambda}}_{{\rm vex,sym},x}} \cdot \cos \left({\arctan \left({\frac{{{\rm d}{x_{\rm vex,sym}}}}{{{\rm d}y}}} \right)} \right).$$

Combining this with Eq. (30) and applying trigonometrical simplifications to the term $\cos ({\arctan ({{\rm d}{x_{\rm vex,sym}}/dy})})$, the period is found to be

$${{{\Lambda}}_{\rm vex,sym}}({x,{x_{\rm{PS}}},y,{z_S},\lambda} ) = \frac{{\lambda \cdot {{\left({1 + {{\left({\frac{{{\rm d}{x_{\rm vex,sym}}}}{{{\rm d}y}}} \right)}^2}} \right)}^{- 1/2}}}}{{\frac{{{x_{\rm{PS}}} + x}}{{\sqrt {z_S^2 + {y^2} + {{({{x_{\rm{PS}}} + x} )}^2}}}} + \frac{{{x_{\rm{PS}}} - x}}{{\sqrt {z_S^2 + {y^2} + {{\left({{x_{\rm{PS}}} - x} \right)}^2}}}}}}.$$

Two illumination examples of this symmetric case are presented in the following to illustrate the application of the derived equations and particularly to show the effects of the chirp. The period, the orientation, and the grating lines themselves were calculated using Eqs. (36), (34), and (29), respectively. For both examples, the same wavelength of $\lambda = 415\;{\rm{nm}}$ and angle of incident of $\theta = 19.89^\circ$ are chosen as already used for the example in the previous section depicted in Fig. 7. The two examples presented in the following only differ in the distance $d$ between the point sources and the center of the substrate, cf. Fig. 8(a). This distance was set to $d\; = 50\;{\rm{mm}}$ for the first example as shown in Fig. 9(a).

 figure: Fig. 9.

Fig. 9. Example of a symmetric illumination with two convex waves. (a) Arrangement of the sources placed at a distance of $d = 50\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) including parabolic fits. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from the ideal direction (color-coded).

Download Full Size | PDF

The targeted period ${\Lambda _{\rm{Target}}} = 610\;{\rm{nm}}$ is obtained at the center of the substrate but strongly increases with the distance from the center, as shown in Fig. 9(b). This increase, which is mainly meant by the term chirp, is much stronger in the $x$ direction, which is emphasized by the cross-sectional view in Fig. 9(c). By comparing these cross sections with the additionally shown parabolic fits, it can be concluded that the distribution $\Lambda ({x,y})$ of the period for this case roughly represent a three-dimensional paraboloid. The root mean square error (RMSE) of the fits in the $x$ and $y$ axis are ${{\rm{RMSE}}_x} = \;7.2\;{\rm{nm}}$ and ${{\rm{RMSE}}_y} = 0.32\;{\rm{nm}}$, respectively. Figure 9(d) depicts every 5000th grating line arising from the interference of the two sources. The distances between the lines increase with increasing distance from the center showing the chirp in both the $x$ and $y$ directions. The color-coding in Fig. 9(d) shows the orientation of the grating lines, respectively, and their absolute deviation from the ideal orientation (parallel to the $y$ axis). It is noticeable that the orientation of the grating lines is ideal both along the $x$ axis ($y = 0$) and $y$ axis ($x = 0$), but deteriorates with increasing distance with deviations of up to about 15°. A larger distance of $d = 1000\;{\rm{mm}}$ between the sources and the substrate is applied for the second example shown in Fig. 10.

 figure: Fig. 10.

Fig. 10. Example of a symmetric illumination with two convex waves. (a) Arrangement of the sources placed at a distance of $d = 1000\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) including parabolic fits. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from the ideal direction (color-coded).

Download Full Size | PDF

It is noticeable by comparing Figs. 9(b) to 10(b) that the spatial variation of the period looks qualitatively similar but has become smaller by orders of magnitude. While the period of the previous example increased by approximately 500 nm (82% increase) toward the corners, the period of the present example only increases by approximately 1 nm (0.2% increase), due to the larger exposure distance. When looking at the cross-sectional views in Fig. 10(c), it is also noticeable that the parabolic fits match much better than before, only having residual errors of ${{\rm{RMSE}}_x} = 52.4 \cdot {10^{- 6}}\;{\rm{nm}}$ and ${{\rm{RMSE}}_y} = 2.36 \cdot {10^{- 6}}\;{\rm{nm}}$. In Fig. 10(d) it can be seen that the grating lines no longer show any apparent curvature with deviations of the orientation of less than about 0.05°, while the pattern of the tilt is qualitatively similar.

From these two examples, it can already be concluded that gratings produced under such a symmetrical illumination contain an ideal area in the center where both period and curvature are optimal, and that the next best areas are located along the $x$ axis ($y = 0$) and the $y$ axis ($x = 0$). The examples furthermore show that the spatial distribution of the period can be approximated by a paraboloid and that the chirp is reduced by increasing the distance of the point sources.

4. EXPOSURE WITH TWO CONCAVE WAVES

Only the exposure arrangement with interfering convex waves shown in Fig. 2(a) has been considered so far. Interference of concave wavefronts can occur, e.g., when optical imaging is applied as shown in Fig. 2(b). The easiest way to derive the equations for the period and the orientation of the grating lines resulting in this situation is to consider the two virtual point sources ${A^*}$ and ${B^*}$ below the substrate. While the point sources $A$ and $B$ emit the wavefronts, the virtual point sources ${A^*}$ and ${B^*}$ have to be viewed as if they attracted the wavefronts. By means of this observation, the same derivations can be used as above, while only the sign of the velocities of the wavefronts need to be changed. However, since only the time-independent paths along which constructive interferences occurs are considered in the final result, see Appendix A, Eqs. (6) to (9) are not affected by this change of sign. All the equations presented for the convex exposure case can, therefore, also be applied to the concave exposure case just by using the new point sources ${A^*}$ and ${B^*}$ instead of the previously used sources $A$ and $B$.

5. EXPOSURE WITH ONE CONVEX AND ONE CONCAVE WAVE

For the third and final case, the photo-resist is exposed to the interference of convex and concave wavefronts. This mixed exposure arrangement is shown in Fig. 2(c) where the interference between the waves from the real point source $B$ and the virtual point source ${A^*}$ needs to be considered. As shown in the following subsection, this arrangement unfortunately does not allow to use the equations derived for the previous two cases.

A. Fundamentals

In order to consider the interference of one expanding and one contracting spherical wave, we place the two point sources symmetrically around the origin on the $z$ axis, since they are arranged approximately vertically, as shown in Fig. 2(c). This assumption does not limit the generality of the derivation as one may later define an arbitrarily tilted and shaped surface of the illuminated substrate. Due to the rotational symmetry of the system around the chosen $z$ axis, we denote the transversal coordinate(s) with the radial coordinate $r$, as shown in Fig. 11(a). Analogous to the procedure in Section 3.A, we consider a starting point ${P_O}$ on the transversal $r$ axis where two wavefronts (solid lines) experience constructive interference at the time $t = 0$. After a time $t$, this intersection point has moved from ${P_O} = {P_{I,{\rm mix}}}({t = 0})$ to the point

$${P_{I,{\rm mix}}}(t ) = \left({\begin{array}{*{20}{c}}{{r_{I,{\rm mix}}}(t )}\\{{z_{I,{\rm mix}}}(t )}\end{array}} \right),$$
along the curve ${F_{\rm{mix}}}$. From the arrangement shown in Fig. 11(a) and by applying Pythagoras’s law, it follows that the two equations,
$${R_{{A^*}}}{(t )^2} = {\left({{z_{I,{\rm mix}}}(t ) + {z_{\rm{PS}}}} \right)^2} + {r_{I,{\rm mix}}}{(t )^2},$$
$${R_B}{(t )^2} = {\left({{z_{I,{\rm mix}}}(t ) - {{\rm{z}}_{\rm{PS}}}} \right)^2} + {r_{I,{\rm mix}}}{(t )^2},$$
apply for any point on the curve ${F_{\rm{mix}}}$, where ${R_{{A^*}}}$ and ${R_B}$ are the radii of the wavefronts emitted from the sources ${A^*}$ and $B$, respectively, and ${z_{\rm{PS}}}$ is the distance of the point sources to the origin. The curve ${F_{\rm{mix}}}$ is defined such that its origin lies on the Point ${P_O} = ({{r_O}, {}0})$ at $t = 0$. The radii of the wavefronts of the sources ${A^*}$ and $B$ can, therefore, be defined as
$${R_{{A^*}}}(t ) = \sqrt {r_O^2 + z_{\rm{PS}}^2} + {v_{{A^*}}} \cdot t,$$
$${R_B}(t ) = \sqrt {r_O^2 + z_{\rm{PS}}^2} + {v_B} \cdot t.$$
 figure: Fig. 11.

Fig. 11. (a) Cross-sectional (2D) view explaining the interference of a convex and a concave spherical wave. While the wavefronts of the point source $B$ expand with time, the wavefronts of the virtual point source ${A^*}$ contract. Constructive interference arises along the curve ${F_{\rm{mix}}}$. The other variables are explained in the text. (b) Sketch used to determine the origin of the curves ${F_{\rm{mix}}}$ regarding the wavelength of the emitted waves.

Download Full Size | PDF

By setting ${v_{{A^*}}} = - {v_B}$ and by eliminating the parameterization variable $t$ from Eqs. (38) to (41), as shown in the Appendix B, the curve ${F_{\rm{mix}}}$ is found to be defined by

$${F_{\rm{mix}}}\!:\;\;{r^2} = r_O^2 + {z^2}\left({\frac{{z_{\rm{PS}}^2}}{{r_O^2 + z_{\rm{PS}}^2}} - 1} \right).$$

The location ${r_O}$ marks the starting point ${P_O}$ of the curve ${F_{\rm{mix}}}$. By considering the wavelength $\lambda$ of the point sources, these points are limited to a set of discrete values ${r_{0,n}}$, which can be calculated considering the geometrical relationships shown in Fig. 11(b). Let us assume that the two point sources are in phase in such a way that constructive interference occurs exactly at the origin, which lies in the middle between them. This point is noted by ${r_{O,n = 0}}$. The next point at which constructive interference occurs is denoted as ${r_{O,n = 1}}$, the following one as ${r_{O,n = 2}}$, and so on. The locations of these points can be defined using Pythagoras’ theorem,

$$R_{\rm{WF}}^2(n ) = r_{O,n}^2 + z_{\rm{PS}}^2,$$
where the radius ${R_{\rm{WF}}}(n)$ of the corresponding wavefront $n$ is given by
$${R_{\rm{WF}}}\left(n \right) = n \cdot \frac{\lambda}{2} + {z_{\rm{PS}}}\;|\;n \in {\mathbb{Z}}.$$

By combining Eqs. (43) and (44), the origin(s) of the discrete curve(s) ${F_{{\rm mix},n}}$ can be defined as

$${r_{O,n}} = \sqrt {{{\left({n \cdot \frac{\lambda}{2} + {z_{\rm{PS}}}} \right)}^2} - z_{\rm{PS}}^2} \;\;|\;n \in {\mathbb{Z}}.$$

The presented cross-sectional formulation can be transferred into the Cartesian coordinate system of the three-dimensional space by using

$${r^2} = {x^2} + {y^2}.$$

In this system, the curves ${F_{\rm{mix}}}$ are found to be the cross sections of the ellipsoids,

$${E_n}:\;\;{x^2} + {y^2} = r_{O,n}^2 + {z^2}\left({\frac{{z_{\rm{PS}}^2}}{{r_{O,n}^2 + z_{\rm{PS}}^2}} - 1} \right),$$
which exhibit an “onion”-like geometry, as shown in Fig. 12. For a better view, this set of stratified ellipsoids is shown in different cross sections in Figs. 12(a) and 12(b) with an arbitrarily shaped [Fig. 12(a)] and a flat [Fig. 12(b)] substrate surface, respectively. The positioning of the substrate on the left side might be confusing on first sight but corresponds to the geometry shown in Fig. 2(c), since the ellipsoids are created by the interference between the real point source $B$ and the virtual point source ${A^*}$. In Fig. 12(b), the grating lines ${G_{{\rm mix,sym},n}}$ resulting from the intersections between the ellipsoids ${E_n}$ and the substrate surface are shown in red.
 figure: Fig. 12.

Fig. 12. 3D representation of the ellipsoids ${E_n}$ where the waves of the two coherent point sources ${A^*}$ and $B$ experience constructive interference. For illustrative purposes, the distance of the point sources to the origin was set to ${z_{\rm{PS}}} = \;50\;{\rm{mm}}$, and a wavelength of $\lambda = 8\;{\rm{mm}}$ was chosen. (a) Ellipsoids with an arbitrarily shaped and positioned substrate ${S_{\rm mix,sym}}$ (gray sheet). The curves ${F_{{\rm mix},n}}$ are marked in the cross section at $y = {{0}}$. (b) Ellipsoids and their intersections ${G_{\rm mix,sym}}$ (red lines) with a plane substrate ${S_{\rm mix,sym}}$ (gray sheet) parallel to the $x-y$ plane.

Download Full Size | PDF

B. General Case of the Mixed Arrangement

As already done for the exposure with two convex waves, a distinction is again made here between the illumination of an arbitrarily shaped surface depicted in Fig. 12(a) and the symmetrical illumination of a plane surface depicted in Fig. 12(b). For the general case, the arbitrarily shaped surface of the illuminated substrate is defined by

$${S_{\rm mix,gen}}\!:\;\;{z_{\rm mix,gen}}({x,y} ).$$

The grating lines $G_{{\rm mix,gen},n}$ (still assuming a negative photo-resist) are then given by

$$G_{{\rm mix,gen},n}\!:\;\; {x^2} + {y^2} = r_{O,n}^2 + z_{\rm mix,gen}^2({x,y} )\left({\frac{{z_{\rm{PS}}^2}}{{r_{O,n}^2 + z_{\rm{PS}}^2}} - 1} \right).$$

As mentioned before, it is mainly the grating period and the local orientation of the grating lines that are of interest. Rather than deriving a new model, we adapt the vectorial model used for the above case of interfering convex waves and consider the real point source $B$, the virtual point source ${A^*}$, and an arbitrarily shaped surface ${S_{\rm mix,gen}}$ as shown in Fig. 13(a).

 figure: Fig. 13.

Fig. 13. Vectors needed for the derivation of the period and the orientation of the grating generated by the interference of a concave and a convex wave on (a) an arbitrarily shaped or (b) a symmetrically arranged plane surface.

Download Full Size | PDF

The local period and orientation of the grating lines is determined at an arbitrary point $P$ on the illuminated surface. The ray vector of the wave coming from the real point source $B$ is denoted by ${\vec{a}_B},$ and the one of the wave originating from the virtual point source ${A^*}$ is denoted by

$${\vec{a}_{{A^*}}} = \overrightarrow {{A^*}P} .$$

The comparison of the current model with that of the two interfering convex waves can be made considering the ray vector,

$${\vec{a}_A} = - {\vec{a}_{{A^*}}} = \overrightarrow {P{A^*}} ,$$
originating from the real point source $A$. By applying this relation [Eq. (51)] to Eqs. (26) and (25), the period and the orientation of the grating lines resulting from the interference of a convex and a concave spherical wave are found to be
$${\Lambda _{\rm mix,gen}} = \frac{{\lambda \sqrt {1 - {{\left({\frac{{{{\vec{a}}_S} \cdot {{\vec g}_{\rm{mix}}}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec g}_{\rm{mix}}}} \right|}}} \right)}^2}}}}{{\displaystyle\frac{{{{\vec{a}}_S} \cdot - {{\vec{a}}_{{A^*}}}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_{{A^*}}}} \right|}} - \frac{{{{\vec{a}}_S} \cdot {{\vec{a}}_B}}}{{\left| {{{\vec{a}}_S}} \right| \cdot \left| {{{\vec{a}}_B}} \right|}}}}$$
and
$${\vec g_{\rm{mix}}} = \left({{{\vec n}_{\rm{IP}}} \times \left({\frac{{- {{\vec{a}}_{{A^*}}}}}{{\left| {{{\vec{a}}_{{A^*}}}} \right|}} + \frac{{{{\vec{a}}_B}}}{{\left| {{{\vec{a}}_B}} \right|}}} \right)} \right) \times {\vec n_S},$$
respectively.

C. Symmetrical Case of the Mixed Arrangement

For the consideration of the grating generated on a symmetrically arranged plane surface, we replace the arbitrarily shaped surface ${S_{\rm mix,gen}}$ from Eq. (48) by

$${S_{\rm mix,sym}}\!:\;{z_{\rm mix,sym}}({x,y} ) = {z_S},\;$$
cf. Figs. 12(b) and 13(b). The grating lines
$$G_{{\rm mix,sym},n}\!:\;\;{x^2} + {y^2} = r_{O,n}^2 + z_S^2\left({\frac{{z_{\rm{PS}}^2}}{{r_{O,n}^2 + z_{\rm{PS}}^2}} - 1} \right)$$
are then found by inserting Eq. (54) in Eq. (47). As seen from Fig. 13(b), the period of the grating at a point $P$ is given analogously to Eq. (13) by
$${\Lambda _{\rm mix,sym}}({\lambda ,{\varphi _A},{\varphi _B}} ) = \frac{\lambda}{{\sin ({{\varphi _A}} ) + \sin ({{\varphi _B}} )}},$$
with
$${\varphi _A} = \arctan \left({\frac{{- r}}{{{z_{\rm{PS}}} + {z_S}}}} \right)$$
and
$${\varphi _B} = \arctan \left({\frac{{- r}}{{{z_{\rm{PS}}} - {z_S}}}} \right).$$

By combining Eq. (56) to Eq. (58), the period is found to be

$$\begin{split}&{\Lambda _{\rm mix,sym}}({r,{z_S},{z_{\rm{PS}}},\lambda} )\\[-3pt]&\quad = \lambda \cdot {\left({\frac{r}{{\sqrt {{r^2} + {{({{z_{\rm{PS}}} + {z_S}} )}^2}}}} + \frac{r}{{\sqrt {{r^2} + {{\left({{z_{\rm{PS}}} - {z_S}} \right)}^2}}}}} \right)^{- 1}}.\end{split}$$

This equation shows that the spatial distribution of the grating’s period is radially symmetric around the $z$ axis, as already seen in Fig. 12(b). Using Eq. (46), the distribution of the period can again be expressed in Cartesian coordinates,

$$\begin{split}&{\Lambda _{\rm mix,sym}}({x,y,{z_{\rm{PS}}},{z_S},\lambda} )\\[-3pt]&\quad = \lambda {\left({\frac{{\sqrt {{x^2} + {y^2}}}}{{\sqrt {{x^2} + {y^2} + {{({{z_{\rm{PS}}} + {z_S}} )}^2}}}} + \frac{{\sqrt {{x^2} + {y^2}}}}{{\sqrt {{x^2} + {y^2} + {{({{z_{\rm{PS}}} - {z_S}} )}^2}}}}} \right)^{\!- 1}}\!.\end{split}$$

Due to the radial symmetry of the grating lines around the $z$ axis, their local orientation is simply given by

$$\frac{{d{x_{\rm mix,sym}}}}{{dy}}({x,y} ) = - \frac{y}{x},$$
where ${x_{\rm mix,sym}}$ is the $x$ coordinate of a point along one of the grating lines. The following example serves both to understand the interference pattern produced by the interaction of a concave and a convex spherical wave and to compare it to the pattern produced by two convex waves. The same illumination parameters, therefore, are used as above, i.e., a wavelength of $\lambda = 415\;{\rm{nm}}$, a distance between the point sources of $d = 1000\;{\rm{mm}}$, and an angle of incidence of $\theta = 19.89^\circ$. The results are shown in Fig. 14. They can directly be compared to the results obtained for two convex waves shown in Fig. 10. Since the exposure with convex waves is identical to the one with concave waves, which was proven in Section 4, the results presented in Fig. 10 also apply to the latter.
 figure: Fig. 14.

Fig. 14. Example of a symmetric illumination of a plane surface by a concave and a convex wave. (a) Arrangement of the sources placed at a distance of $d = 1000\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) compared to the cross sections of the period distribution of the interference pattern produced by two convex waves. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from their ideal direction (color-coded).

Download Full Size | PDF

The arrangement of the two point sources ${A^*}$ and $B$ is shown in Fig. 14(a). The distribution of the period of the resulting interference pattern depicted in Fig. 14(b) exhibits a strong gradient in the radial direction (here shown along the $x$ direction). The targeted period is obtained only in the center, and the gradient is much stronger than in the case of two interfering convex waves. This can particularly be seen in Fig. 14(c) giving cross-sectional views of the period’s distributions for the two respective cases. The orientation of the grating lines is shown in Fig. 14(d). The lines show a visible curvature whose center lies at the origin of the underlying coordinate system. It is noticeable that the maximum curvature is an order of magnitude larger than that obtained for the interfering convex waves, cf. Fig. 10(d). In summary, this analysis shows that the interference of a convex with a concave wave produces a much stronger chirp and that it should be avoided if homogeneous gratings with constant period are targeted.

6. CONCLUSION AND OUTLOOK

In summary, we have presented an extensive and general theoretical investigation on the period chirp, which is a prominent problem in the fabrication of linear gratings using LIL. The considered arrangements of point sources are applicable for all setups that are based on far-field illumination of the substrate. Exact analytical equations were derived describing the grating period and the orientation of the grating lines both for a general case having an arbitrarily shaped substrate illuminated by arbitrarily positioned point sources and for a symmetrical case having a plane substrate illuminated by symmetrically positioned point sources. In future publications, we will focus on a modeling of the illumination by Gaussian beams in order to precisely describe the chirp for SBIL as well, and we will address the elimination of the chirp by seizing the idea of Walsh and Smith [27] of bending the substrate for the illumination process.

APPENDIX A: DERIVATION OF EQ. (6)

First, Eqs. (2) and (3) are combined to

$${R_A}{(t )^2} - {\left({{x_{\rm{PS}}} + {x_{I,{\rm vex}}}(t )} \right)^2} = {R_B}{(t )^2} - {\left({{x_{\rm{PS}}} - {x_{I,{\rm vex}}}(t )} \right)^2},$$
and they simplified to
$${x_{I,{\rm vex}}}(t ) = \frac{{{R_A}{{(t )}^2} - {R_B}{{(t )}^2}}}{{4{x_{\rm{PS}}}}}.$$

Then Eqs. (4) and (5) are inserted into Eq. (A2), resulting in

$${x_{I,{\rm vex}}}(t ) = \frac{{{{\left({{x_{\rm{PS}}} + {x_O} + {v_A} \cdot t} \right)}^2} - {{\left({{x_{\rm{PS}}} - {x_O} + {v_A} \cdot t} \right)}^2}}}{{4{x_{\rm{PS}}}}}.$$

Using the relationship ${v_{\rm{A}}} = {v_B}$, Eq. (A3) can be transformed to

$${v_A} \cdot t = \frac{{{x_{I,{\rm vex}}}(t ){x_{\rm{PS}}}}}{{{x_O}}} - {x_{\rm{PS}}}.$$

Inserting Eqs. (4) into (2) yields

$${\left({{x_{\rm{PS}}} + {x_O} + {v_A} \cdot t} \right)^2} = {\left({{x_{\rm{PS}}} + {x_{I,{\rm vex}}}(t )} \right)^2} + {r_{I,{\rm vex}}}{(t )^2}.$$

By inserting Eq. (A4) into Eq. (A5),

$$\begin{split}&{\left({{x_{\rm{PS}}} + {x_O} + \frac{{{x_{I,{\rm vex}}}(t ){x_{\rm{PS}}}}}{{{x_O}}} - {x_{\rm{PS}}}} \right)^2}\\&\quad = {\left({{x_{\rm{PS}}} + {x_{I,{\rm vex}}}(t )} \right)^2} + {r_{I,{\rm vex}}}{(t )^2},\end{split}$$
one finds
$$\frac{{{x_{I,{\rm vex}}}{{(t )}^2}}}{{x_O^2}} - \frac{{{r_{I,{\rm vex}}}{{(t )}^2}}}{{x_{\rm{PS}}^2 - x_O^2}} = 1.$$

The intersection points, where the two waves experience constructive interference, therefore move along the path ${F_{\rm{vex}}}$ defined by

$$\frac{{{x^2}}}{{x_O^2}} - \frac{{{r^2}}}{{x_{\rm{PS}}^2 - x_O^2}} = 1,$$
which defines the geometry of the standing intensity pattern.

APPENDIX B: DERIVATION OF EQ. (42)

Equations (38) and (39) are combined to

$${R_{{A^*}}}{(t )^2} - {\left({{z_{I,{\rm mix}}}(t ) + {z_{\rm{PS}}}} \right)^2} = {R_B}{(t )^2} - {\left({{z_{I,{\rm mix}}}(t ) - {z_{\rm{PS}}}} \right)^2},$$
and they are simplified to
$${z_{I,{\rm mix}}}(t ) = \frac{{{R_{{A^*}}}{{(t )}^2} - {R_B}{{(t )}^2}}}{{4{z_{\rm{PS}}}}}.$$

Then Eqs. (40) and (41) are inserted into Eq. (B2), resulting in

$${z_{I,{\rm mix}}}(t ) = \frac{{{{\left({\sqrt {r_O^2 + z_{\rm{PS}}^2} + {v_{{A^*}}} \cdot t} \!\right)}^2} - {{\left({\sqrt {r_O^2 + z_{\rm{PS}}^2} + {v_B} \cdot t} \!\right)}^2}}}{{4{z_{\rm{PS}}}}}.$$

Using the relationship ${v_{{{\rm{A}}^{\rm{*}}}}} = - {v_B}$, Eq. (B3) can be transformed to

$${v_B} \cdot t = \frac{{- {z_{I,{\rm mix}}}(t ){z_{\rm{PS}}}}}{{\sqrt {r_O^2 + z_{\rm{PS}}^2}}}.$$

Inserting Eqs. (38) into (40) results in

$$\begin{split}{r_{I,{\rm mix}}}{(t )^2}& = r_O^2 - 2\sqrt {r_O^2 + z_{\rm{PS}}^2} \cdot {v_B} \cdot t + v_B^2 \cdot {t^2} \\&\quad- {z_{I,{\rm mix}}}{(t )^2} - 2{z_{I,{\rm mix}}}(t ) \cdot {z_{\rm{PS}}}.\end{split}$$

The time and velocity can be removed from the result by inserting Eq. (B4) into Eq. (B5). After simplification, this finally results in

$${r_{I,{\rm mix}}}{(t )^2} = r_O^2 + {z_{I,{\rm mix}}}{(t )^2}\left({\frac{{z_{\rm{PS}}^2}}{{r_O^2 + z_{\rm{PS}}^2}} - 1} \right).$$

The path ${F_{\rm{mix}}}$ on which the points of constructive interference move along is, therefore, given by

$${r^2} = r_O^2 + {z^2}\left({\frac{{z_{\rm{PS}}^2}}{{r_O^2 + z_{\rm{PS}}^2}} - 1} \right).$$

Funding

Horizon 2020 Framework Programme (687880, 825246).

Disclosures

The authors declare no conflicts of interest.

Data availability

No data were generated or analyzed in the presented research.

REFERENCES

1. T. Dietrich, S. Piehler, M. Rumpel, P. Villeval, D. Lupinski, M. A. Ahmed, and T. Graf, “Highly-efficient continuous-wave intra-cavity frequency-doubled Yb:LuAG thin-disk laser with 1 kW of output power,” Opt. Express 25, 4917–4925 (2017). [CrossRef]  

2. M. M. Vogel, M. Rumpel, B. Weichelt, A. Voss, M. Haefner, C. Pruss, W. Osten, M. Abdou Ahmed, and T. Graf, “Single-layer resonant-waveguide grating for polarization and wavelength selection in Yb:YAG thin-disk lasers,” Opt. Express 20, 4024–4031 (2012). [CrossRef]  

3. C. Wirth, O. Schmidt, I. Tsybin, T. Schreiber, R. Eberhardt, J. Limpert, A. Tünnermann, K. Ludewigt, M. Gowin, E. ten Have, and M. Jung, “High average power spectral beam combining of four fiber amplifiers to 8.2 kW,” Opt. Lett. 36, 3118–3120 (2011). [CrossRef]  

4. C. Danson, D. Hillier, N. Hopps, and D. Neely, “Petawatt class lasers worldwide,” High Power Laser Sci. Eng.3 (2015). [CrossRef]  

5. N. Bonod and J. Neauport, “Diffraction gratings: from principles to applications in high-intensity lasers,” Adv. Opt. Photon. 8, 156–199 (2016). [CrossRef]  

6. S. Fu, W. Zhang, W. Kong, G. Wang, F. Xing, F. Zhang, and H. Zhang, “Review of pulse compression gratings for chirped pulse amplification system,” Opt. Eng. 60, 020902 (2021). [CrossRef]  

7. X. Dai and H. Xie, “New methods of fabricating gratings for deformation measurements: a review,” Opt. Laser Eng. 92, 48–56 (2017). [CrossRef]  

8. T. R. Groves, D. Pickard, B. Rafferty, N. Crosland, D. Adam, and G. Schubert, “Maskless electron beam lithography: prospects, progress, and challenges,” Microelectron. Eng. 61–62, 285–293 (2002). [CrossRef]  

9. Y. Chen, “Nanofabrication by electron beam lithography and its applications: a review,” Microelectron. Eng. 135, 57–72 (2015). [CrossRef]  

10. U. D. Zeitner, M. Oliva, F. Fuchs, D. Michaelis, T. Benkenstein, T. Harzendorf, and E. B. Kley, “High performance diffraction gratings made by e-beam lithography,” Appl. Phys. A 109, 789–796 (2012). [CrossRef]  

11. L. J. Guo, “Recent progress in nanoimprint technology and its applications,” J. Phys. D 37, R123 (2004). [CrossRef]  

12. D. L. Voronov, E. M. Gullikson, and H. A. Padmore, “Large area nanoimprint enables ultra-precise x-ray diffraction gratings,” Opt. Express 25, 23334–23342 (2017). [CrossRef]  

13. C. J. M. Van Rijn, “Laser interference as a lithographic nanopatterning tool,” J. Micro/Nanolithogr. MEMS MOEMS 5, 1–6 (2006). [CrossRef]  

14. C. Lu and R. H. Lipson, “Interference lithography: a powerful tool for fabricating periodic structures,” Laser Photon. Rev. 4, 568–580 (2010). [CrossRef]  

15. C. G. Chen, P. T. Konkola, R. K. Heilmann, G. S. Pati, and M. L. Schattenburg, “Image metrology and system controls for scanning beam interference lithography,” J. Vac. Sci. Technol. B 19, 2335 (2001). [CrossRef]  

16. D. Ma, S. Wang, and L. Zeng, “Wavefront aberration of plane diffraction gratings fabricated in a Lloyd’s mirror interferometer,” J. Micro/Nanolithogr. MEMS MOEMS 16, 023503 (2017). [CrossRef]  

17. R. R. Hershey and E. N. Leith, “Grating interferometers for producing large holographic gratings,” Appl. Opt. 29, 937–943 (1990). [CrossRef]  

18. C. G. Chen, P. T. Konkola, R. K. Heilmann, C. Joo, and M. L. Schattenburg, “Nanometer-accurate grating fabrication with scanning beam interference lithography,” Nano- Microtechnol. Mater. Process. Packag. Syst. 4936, 126 (2002) [CrossRef]  .

19. A. Katzir, A. C. Livanos, J. B. Shellan, and A. Yariv, “Chirped gratings in integrated optics,” IEEE J. Quantum Electron. 13, 296–304 (1977). [CrossRef]  

20. K. Hibino and Z. S. Hegedus, “Hyperbolic holographic gratings: analysis and interferometric tests,” Appl. Opt. 33, 2553–2559 (1994). [CrossRef]  

21. H. Noda, T. Namioka, and M. Seya, “Geometric theory of the grating,” J. Opt. Soc. Am. 64, 1031–1036 (1974). [CrossRef]  

22. J. Ferrera, “Analysis of distortion in interferometric lithography,” J. Vac. Sci. Technol. B 14, 4009 (1996). [CrossRef]  

23. H. Kim, H. Jung, D.-H. Lee, K. B. Lee, and H. Jeon, “Period-chirped gratings fabricated by laser interference lithography with a concave Lloyd’s mirror,” Appl. Opt. 55, 354–359 (2016). [CrossRef]  

24. T. H. Yoon, C. Il Eom, M. S. Chung, and H. J. Kong, “Diffractometric methods for absolute measurement of diffraction-grating spacings,” Opt. Lett. 24, 107–109 (1999). [CrossRef]  

25. B. Sheng, G. Chen, Y. Huang, and L. Luo, “Measurement of grating groove density using multiple diffraction orders and one standard wavelength,” Appl. Opt. 57, 2514–2518 (2018). [CrossRef]  

26. Z. R. Wu, T. C. Kao, C. W. Kao, P. C. Chang, W. Lin, and Y. J. Hung, “Wafer-scale grating mapping system for rapid pitch and diffraction efficiency measurement,” in OECC/PSC 2019 - 24th OptoElectronics Communications Conference and 2019 International Conference on Photonics in Switching and Computing (2019).

27. M. E. Walsh and H. I. Smith, “Method for reducing hyperbolic phase in interference lithography,” J. Vac. Sci. Technol. B 19, 2347 (2001). [CrossRef]  

28. S.-T. Zhou, Z.-Q. Lin, and W. S. C. Chang, “Precise periodicity control in the fabrication of holographic gratings,” Appl. Opt. 20, 1270–1272 (1981). [CrossRef]  

29. H. Noda, Y. Harada, and M. Koike, “Holographic grating recorded using aspheric wavefronts for a Seya-Namioka monochromator,” Appl. Opt. 28, 4375–4380 (1989). [CrossRef]  

Data availability

No data were generated or analyzed in the presented research.

Cited By

Optica participates in Crossref's Cited-By Linking service. Citing articles from Optica Publishing Group journals and other participating publishers are listed here.

Alert me when this article is cited.


Figures (14)

Fig. 1.
Fig. 1. Simplified sketch of a LIL setup comprising a beam splitter to create two coherent laser beams. The setup is modeled with two coherent point sources $A$ and $B$ , located at the foci of the beams. They emit convex spherical wavefronts illuminating the substrate.
Fig. 2.
Fig. 2. Three possible arrangements for the exposure in LIL, based on the model of the interference of spherical waves emitted from two coherent point sources $A$ and $B$ . (a) Convex case, direct interference of the waves with convex wavefronts as emitted from the point sources. (b) Concave case, the waves of the two point sources are focused by means of two lenses, thus creating concave wavefronts that converge to the virtual point sources ${A^*}$ and ${B^*}$ . (c) Mixed case, inference between a wave with a convex and a wave with a concave wavefront. Only point source $A$ is imaged to ${A^*}$ .
Fig. 3.
Fig. 3. Cross-sectional (2D) sketch explaining the interference of the two convex spherical waves emitted from the two coherent point sources $A$ and $B$ at a given instant of time $t$ . Constructive interference occurs along the curve ${F_{\rm{vex}}}$ . The other variables are explained in the text.
Fig. 4.
Fig. 4. Hyperboloids ${H_n}$ where the waves of the two coherent point sources $A$ and $B$ experience constructive interference. For illustrative purposes they were calculated with $\lambda = 4\;{\rm{mm}}$ and ${x_{\rm{PS}}} = 20\;{\rm{mm}}$ . (a) Hyperboloids and their cross sections at $y = 0$ (black lines) as well as their intersections ${G_{{\rm vex,sym},n}}$ (red lines) with a plane substrate ${S_{\rm vex,sym}}$ (gray sheet). (b) Hyperboloids and their intersections ${G_{{\rm vex,gen},n}}$ (red lines) with an arbitrarily shaped substrate ${S_{\rm vex,gen}}$ (gray sheet).
Fig. 5.
Fig. 5. Model for the derivation of equations describing the grating period and the orientation of the grating lines for the general case. (a) Determination of the period $\Lambda$ at a point $P$ in a two-dimensional system. (b) Transfer of the model shown in (a) into three dimensions.
Fig. 6.
Fig. 6. Close-up on the region near the point $P$ with top-sight on the substrate plane ${K_S}$ showing the difference between the periods ${\Lambda _{{{\vec{a}}_S}}}$ and ${{{\Lambda}}_{\rm vex,gen}}$ as well as the derivation of the latter.
Fig. 7.
Fig. 7. Example of a wavy surface that is illuminated by the spherical waves of two coherent point sources. (a) Geometry of the surface. The color-scale refers to the $z$ position of the surface. (b) Period of the interference pattern on the illuminated surface as calculated with Eq. (26). The color-scale refers to the value of the period. (c) Orientation of the grating lines as calculated using Eq. (25). The black lines show the local orientation of the grating lines, and the color-scale shows their deviation to the ideal orientation in the $x-y$ plane.
Fig. 8.
Fig. 8. (a) Symmetric arrangement of the two coherent point sources and a plane substrate. The sources are placed on the $x$ axis with equal distance to the origin while the substrate is orientated parallel to the $x-y$ plane at a distance ${z_S}$ . The hyperboloids of constructive interference are shown by the colored surfaces, and their intersections with the substrate are shown in red. (b) Section of (a) showing a small region around the point $P$ serving for the derivation of the period ${{{\Lambda}}_{\rm vex,sym}}$ from the period ${{{\Lambda}}_{{\rm vex,sym},x}}$ , which is parallel to the $x$ axis.
Fig. 9.
Fig. 9. Example of a symmetric illumination with two convex waves. (a) Arrangement of the sources placed at a distance of $d = 50\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) including parabolic fits. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from the ideal direction (color-coded).
Fig. 10.
Fig. 10. Example of a symmetric illumination with two convex waves. (a) Arrangement of the sources placed at a distance of $d = 1000\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) including parabolic fits. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from the ideal direction (color-coded).
Fig. 11.
Fig. 11. (a) Cross-sectional (2D) view explaining the interference of a convex and a concave spherical wave. While the wavefronts of the point source $B$ expand with time, the wavefronts of the virtual point source ${A^*}$ contract. Constructive interference arises along the curve ${F_{\rm{mix}}}$ . The other variables are explained in the text. (b) Sketch used to determine the origin of the curves ${F_{\rm{mix}}}$ regarding the wavelength of the emitted waves.
Fig. 12.
Fig. 12. 3D representation of the ellipsoids ${E_n}$ where the waves of the two coherent point sources ${A^*}$ and $B$ experience constructive interference. For illustrative purposes, the distance of the point sources to the origin was set to ${z_{\rm{PS}}} = \;50\;{\rm{mm}}$ , and a wavelength of $\lambda = 8\;{\rm{mm}}$ was chosen. (a) Ellipsoids with an arbitrarily shaped and positioned substrate ${S_{\rm mix,sym}}$ (gray sheet). The curves ${F_{{\rm mix},n}}$ are marked in the cross section at $y = {{0}}$ . (b) Ellipsoids and their intersections ${G_{\rm mix,sym}}$ (red lines) with a plane substrate ${S_{\rm mix,sym}}$ (gray sheet) parallel to the $x-y$ plane.
Fig. 13.
Fig. 13. Vectors needed for the derivation of the period and the orientation of the grating generated by the interference of a concave and a convex wave on (a) an arbitrarily shaped or (b) a symmetrically arranged plane surface.
Fig. 14.
Fig. 14. Example of a symmetric illumination of a plane surface by a concave and a convex wave. (a) Arrangement of the sources placed at a distance of $d = 1000\;{\rm{mm}}$ from the substrate’s center. (b) Calculated spatial distribution of the period on the substrate’s surface. (c) Cross-sectional view of the period distribution shown in (b) compared to the cross sections of the period distribution of the interference pattern produced by two convex waves. (d) Graph showing every 5000th grating line (black lines) and the spatial distribution of the absolute deviation of their orientation from their ideal direction (color-coded).

Equations (76)

Equations on this page are rendered with MathJax. Learn more.

P I , v e x ( t ) = ( x I , v e x ( t ) r I , v e x ( t ) ) ,
R A ( t ) 2 = ( x P S + x I , v e x ( t ) ) 2 + r I , v e x ( t ) 2 ,
R B ( t ) 2 = ( x P S x I , v e x ( t ) ) 2 + r I , v e x ( t ) 2
R A ( t ) = x P S + x O + v A t ,
R B ( t ) = x P S x O + v B t ,
F v e x : x 2 x O 2 r 2 x P S 2 x O 2 = 1 ,
r 2 = y 2 + z 2
H : x 2 x O 2 y 2 x P S 2 x O 2 z 2 x P S 2 x O 2 = 1 ,
x O , n = n λ 2 | n Z ,
S v e x , g e n : z v e x , g e n ( x , y ) .
G v e x , g e n , n : x 2 x O , n 2 y 2 x P S 2 x O , n 2 z v e x , g e n ( x , y ) 2 x P S 2 x O , n 2 = 1 ,
Λ v e x , p l a n e ( β , θ , λ ) = λ 2 sin ( θ ) cos ( β ) ,
Λ v e x , p l a n e ( λ , φ A , φ B ) = λ sin ( φ A ) + sin ( φ B ) ,
n I P = a B × a A ,
a A = A P
a B = B P .
a S = n S × n I P .
φ A = arcsin ( a S a A | a S | | a A | )
φ B = arcsin ( a S a B | a S | | a B | ) .
Λ a S = λ a S a A | a S | | a A | a S a B | a S | | a B | .
α = a r c c o s ( a S g v e x | a S | | g v e x | )
g v e x = n C I × n S .
n C I = n I P × b ,
b = a A | a A | + a B | a B | .
g v e x = ( n I P × ( a A | a A | + a B | a B | ) ) × n S .
Λ v e x , g e n = λ sin ( arccos ( a S g v e x | a S | | g v e x | ) ) a S a A | a S | | a A | a S a B | a S | | a B | = λ 1 ( a S g v e x | a S | | g v e x | ) 2 a S a A | a S | | a A | a S a B | a S | | a B | .
S v e x , g e n : z v e x , g e n ( x , y ) = 5 sin ( x 0.06 ) 5 sin ( y 0.07 )
S v e x , s y m : z v e x , s y m ( x , y ) = z S ,
G v e x , s y m , n : x v e x , s y m ( x O , n , x P S , y , z S ) = ± x O , n 2 ( 1 + y 2 x P S 2 x O , n 2 + z S 2 x P S 2 x O , n 2 ) .
Λ v e x , s y m , x ( x , x P S , y , z S , λ ) = λ x P S + x z S 2 + y 2 + ( x P S + x ) 2 + x P S x z S 2 + y 2 + ( x P S x ) 2
x = x v e x , s y m ( x O , n , x P S , y , z S ) = ± x O , n 2 ( 1 + y 2 x P S 2 x O , n 2 + z S 2 x P S 2 x O , n 2 ) .
d x v e x , s y m d y ( x O , n , x P S , y , z S ) = x O , n y ( x P S 2 x O , n 2 ) y 2 + z S 2 x P S 2 x O , n 2 + 1 .
x O , n ( x P S , x P , y , z s ) = x x P S x 2 + y 2 + z S 2 + x P S 2 .
d x v e x , s y m d y ( x , x P S , y , z S ) = x y z S 2 + y 2 + x P S 2 + x 2 ( x 2 z S 2 + x 2 y 2 + ( x P S 2 + y 2 + z S 2 ) 2 ) ( x P S 2 + y 2 + z S 2 ) .
Λ v e x , s y m ( x , x P S , y , z S , λ ) = Λ v e x , s y m , x cos ( arctan ( d x v e x , s y m d y ) ) .
Λ v e x , s y m ( x , x P S , y , z S , λ ) = λ ( 1 + ( d x v e x , s y m d y ) 2 ) 1 / 2 x P S + x z S 2 + y 2 + ( x P S + x ) 2 + x P S x z S 2 + y 2 + ( x P S x ) 2 .
P I , m i x ( t ) = ( r I , m i x ( t ) z I , m i x ( t ) ) ,
R A ( t ) 2 = ( z I , m i x ( t ) + z P S ) 2 + r I , m i x ( t ) 2 ,
R B ( t ) 2 = ( z I , m i x ( t ) z P S ) 2 + r I , m i x ( t ) 2 ,
R A ( t ) = r O 2 + z P S 2 + v A t ,
R B ( t ) = r O 2 + z P S 2 + v B t .
F m i x : r 2 = r O 2 + z 2 ( z P S 2 r O 2 + z P S 2 1 ) .
R W F 2 ( n ) = r O , n 2 + z P S 2 ,
R W F ( n ) = n λ 2 + z P S | n Z .
r O , n = ( n λ 2 + z P S ) 2 z P S 2 | n Z .
r 2 = x 2 + y 2 .
E n : x 2 + y 2 = r O , n 2 + z 2 ( z P S 2 r O , n 2 + z P S 2 1 ) ,
S m i x , g e n : z m i x , g e n ( x , y ) .
G m i x , g e n , n : x 2 + y 2 = r O , n 2 + z m i x , g e n 2 ( x , y ) ( z P S 2 r O , n 2 + z P S 2 1 ) .
a A = A P .
a A = a A = P A ,
Λ m i x , g e n = λ 1 ( a S g m i x | a S | | g m i x | ) 2 a S a A | a S | | a A | a S a B | a S | | a B |
g m i x = ( n I P × ( a A | a A | + a B | a B | ) ) × n S ,
S m i x , s y m : z m i x , s y m ( x , y ) = z S ,
G m i x , s y m , n : x 2 + y 2 = r O , n 2 + z S 2 ( z P S 2 r O , n 2 + z P S 2 1 )
Λ m i x , s y m ( λ , φ A , φ B ) = λ sin ( φ A ) + sin ( φ B ) ,
φ A = arctan ( r z P S + z S )
φ B = arctan ( r z P S z S ) .
Λ m i x , s y m ( r , z S , z P S , λ ) = λ ( r r 2 + ( z P S + z S ) 2 + r r 2 + ( z P S z S ) 2 ) 1 .
Λ m i x , s y m ( x , y , z P S , z S , λ ) = λ ( x 2 + y 2 x 2 + y 2 + ( z P S + z S ) 2 + x 2 + y 2 x 2 + y 2 + ( z P S z S ) 2 ) 1 .
d x m i x , s y m d y ( x , y ) = y x ,
R A ( t ) 2 ( x P S + x I , v e x ( t ) ) 2 = R B ( t ) 2 ( x P S x I , v e x ( t ) ) 2 ,
x I , v e x ( t ) = R A ( t ) 2 R B ( t ) 2 4 x P S .
x I , v e x ( t ) = ( x P S + x O + v A t ) 2 ( x P S x O + v A t ) 2 4 x P S .
v A t = x I , v e x ( t ) x P S x O x P S .
( x P S + x O + v A t ) 2 = ( x P S + x I , v e x ( t ) ) 2 + r I , v e x ( t ) 2 .
( x P S + x O + x I , v e x ( t ) x P S x O x P S ) 2 = ( x P S + x I , v e x ( t ) ) 2 + r I , v e x ( t ) 2 ,
x I , v e x ( t ) 2 x O 2 r I , v e x ( t ) 2 x P S 2 x O 2 = 1.
x 2 x O 2 r 2 x P S 2 x O 2 = 1 ,
R A ( t ) 2 ( z I , m i x ( t ) + z P S ) 2 = R B ( t ) 2 ( z I , m i x ( t ) z P S ) 2 ,
z I , m i x ( t ) = R A ( t ) 2 R B ( t ) 2 4 z P S .
z I , m i x ( t ) = ( r O 2 + z P S 2 + v A t ) 2 ( r O 2 + z P S 2 + v B t ) 2 4 z P S .
v B t = z I , m i x ( t ) z P S r O 2 + z P S 2 .
r I , m i x ( t ) 2 = r O 2 2 r O 2 + z P S 2 v B t + v B 2 t 2 z I , m i x ( t ) 2 2 z I , m i x ( t ) z P S .
r I , m i x ( t ) 2 = r O 2 + z I , m i x ( t ) 2 ( z P S 2 r O 2 + z P S 2 1 ) .
r 2 = r O 2 + z 2 ( z P S 2 r O 2 + z P S 2 1 ) .
Select as filters


Select Topics Cancel
© Copyright 2024 | Optica Publishing Group. All rights reserved, including rights for text and data mining and training of artificial technologies or similar technologies.