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Optical waveguide analysis using
  Beam Propagation Method
Term Paper for “Introduction to Optoelectronics” spring 2006
                    Prof. Frank Barnes




Page 10: My MATLAB® implementation of double slit diffraction
              Using Beam Propagation Method




                Sri Rama Prasanna Pavani
                    pavani@colorado.edu
          Micro-Optical Imaging Systems Laboratory
              University of Colorado at Boulder




                                                                1
Introduction


C    losed form analytical solutions for the wave equation can be easily determined only

for a few symmetrical structures such as cylindrical and slab waveguides. In complicated
structures with bends such as y-couplers, analytic closed form solutions cannot be
derived.




                           Figure 1a: Cylindrical waveguide




                                 Figure 1b: Y Coupler


The Y-Coupler, as shown in Figure 1b, couples an input waveguide to two output
waveguides. As the mode would dynamically change as the wave propagates through
such structure, it is hard to determine the losses using analytical methods. Beam
propagation method can be efficiently used for analyzing such structures.




                                                                                      2
Beam propagation method

The beam propagation method is a numerical way of determining the fields inside a
waveguide. With this method, the mode profile of an unusual waveguides such as y-
couplers can be determined with ease. The dynamic mode profile can be accurately
estimated as the wave propagates through the wave guide.

The beam propagation method essentially decomposes a mode into a superposition of
plane waves, each traveling in a different direction. These individual plane waves are
propagated through a finite predetermined distance through the wave guide until the point
where the field needs to be determined has arrived. At this point, all the individual plane
waves are numerically added in order to get back the spatial mode.




        Figure 2: My simulation of the diffraction of a Gaussian beam using BPM


This process precisely corresponds to the Fourier way of analyzing. Specifically,
according to Fourier theory, any periodic signal can be decomposed into complex
sinusoids of different frequencies. When all of these sinusoids are added, we would get
back the original signal. In beam propagation method, a mode is decomposed into
different plane waves, which indeed are sinusoids of different frequencies. The basic idea
here is to split a complicated problem into a simpler problem for which solutions are
obvious. Since wave equation is linear, all these simple solutions can be added back to
obtain the complicated solution.

For instance, in Figure 2, I have numerically computed the diffraction of a Gaussian
beam as it propagates through a medium.


                                                                                         3
Principle of superposition

This principle is forms the foundation of the beam propagation theory. The principle of
superposition states that, for a linear system, a linear combination of solutions to the
system is also a solution to the same linear system.

The superposition principle applies to linear systems of algebraic equations, linear
differential equations, or systems of linear differential equations. Since we are
considering a linear medium, the superposition principle is valid.

Consider a slab waveguide as shown in Figure 3. Any guided field inside this wave guide
should necessarily satisfy the wave equation.




If the medium is isotropic, then plane waves are natural solutions of the wave equation.




                                Figure 3: Slab wave guide

Since the wave equation is linear, any linear superposition of solutions will also
constitute a valid solution. This important fact forms the foundation of the beam
propagation theory.

 In order to describe the general mode of a waveguide, a superposition of plane waves,
each with identical angular frequency, but different propagation vector, would be used.
Thus, the essence of the theory is that plane waves form a basis set for the mode
description.




                                                                                           4
Fundamental mode of a Hermite Gaussian beam

In this section, let us see, how the Gaussian amplitude profile, which is the fundamental
TEMoo mode can be represented in the form of a superposition of plane waves.
Analytically, a Gaussian can be represented as




       Figure 4a                       Figure 4b                        Figure 4c


Figure 4a: Gaussian beam profile of a HeNe laser, which I captured after spatial filtering.
Figure 4b: An ideal simulated Gaussian beam profile
Figure 4c: 3D plot of a Gaussian


The idea here is to split the above Gaussian into number of plane waves weighted by
complex factors known as Fourier coefficients. The Fourier and inverse Fourier
transforms are characterized as follows.




In the first equation, f(x) (Gaussian), is represented just as an integral of weighted
sinusoids. Note that F(k)s are mere complex numbers that act as weighting factors of the
sinusoids. In the beam propagation approach, it can be rightly said that the Fourier kernel,
that is, the sinusoids (with different k’s) are infact plane waves with different propagation
vectors. Thus, in short, with the above expression, any finite analytical function can be
represented as a sum of plane waves. Note that this is possible only since the Fourier
transform is linear.




                                                                                           5
For a Gaussian beam, the Fourier coefficients can be shown to be

                                             1              2
                                                                x0 2 k x 2
                            F (k ) =                 e −π
                                            π x0 2
The whole theory explained above is represented by the following picture (Figure 5).




Figure 5: The Gaussian beam represented in terms of multiple plane wave components.

In order to obtain an appreciation for the above picture, we should first have an
appreciation of the propagation vector K. The total magnitude of K is identical for all
components in a mode. However, the relative sizes of Kx and Kz vary.

Since Ky is assumed to be zero in the above picture, the wave propagates only in the xz
plane, and therefore

                                        2        2
                              K =    Kx + Kz

Consequently, Kz is maximum when Kx is zero, which can be clearly seen from in
Figure 5. Thus the axial propagation vector is the vector with highest magnitude. As Kx
increases, the amplitude of the plane wave decreases.

 The spatial amplitude distribution of the Gaussian is essentially comprised by the
amplitude and the direction of the individual plane waves. The length of each arrow
represents the amplitude of the K vector while the direction of each arrow represents the
direction of the K vector.

The important point in the beam propagation technique is to calculate the propagation
effects using the phase space representation, and then add phase shifts caused by the
waveguide structure using the spatial representation of the mode.




                                                                                            6
Numerical Implementation using Discrete Fourier Transforms

In order to numerically implement a beam propagation technique (as I did in Figure 2),
we need to work with digital implementations of Fourier transforms known as the
discrete Fourier transforms.

A brief introduction to discrete Fourier transforms in given below. For more detained
analysis, the interested reader is referred to standard Digital Signal Processing books,
such as the one by Alan Oppenheim.

The continuous Fourier transform is defined as


                                                                                                (1)


Now consider generalization to the case of a discrete function,             by letting
         , where       , with      , ...,     . Writing this out gives the discrete Fourier
transform                    as



                                                                                                (2)



The inverse transform                       is then


                                                                                                (3)


Discrete Fourier transforms are extremely useful because they reveal periodicities in
input data as well as the relative strengths of any periodic components. There are a few
subtleties in the interpretation of discrete Fourier transforms, however. In general, the
discrete Fourier transform of a real sequence of numbers will be a sequence of complex
numbers of the same length. In particular, if are real, then        and are related by

                                                                                                (4)

for    , 1, ..., , where denotes the complex conjugate. This means that the
component is always real for real data.

As a result of the above relation, a periodic function will contain transformed peaks in not
one, but two places. This happens because the periods of the input data become split into
"positive" and "negative" frequency complex components.


                                                                                            7
Figure 6: Introduction to discrete fourier transforms

The plots above show the real part (red), imaginary part (blue), and complex modulus
(green) of the discrete Fourier transforms of the functions             (left figure) and
                        (right figure) sampled 50 times over two periods. In the left figure,
the symmetrical spikes on the left and right side are the "positive" and "negative"
frequency components of the single sine wave.

Similarly, in the right figure, there are two pairs of spikes, with the larger green spikes
corresponding to the lower-frequency stronger component            and the smaller green
spikes corresponding to the higher-frequency weaker component. A suitably scaled plot
of the complex modulus of a discrete Fourier transform is commonly known as a power
spectrum.

Beam diffraction

In order to propagate a wave through a distance L in the z direction, we fist decompose
the spatial profile of the wave into a series of plane wave components and advance each
of these plane wave components through a distance of L. Once we have propagated to the
point, we then superimpose all these plane wave components to get back our spatial mode
at that point.




      Figure 7: Different path lengths incurred by different plane wave components




                                                                                              8
As each plane wave is traveling in a different direction, each would accumulate a
different amount of phase due to the different path lengths between the source and
destination planes along different directions.

Let us now consider a practical example. Consider the propagation of a Gaussian beam
through a homogeneous isotropic medium. In order to achieve this numerically, the
following steps should be followed.

   1. The whole process is akin to a linear system analysis, where the output of a linear
      time invariant system with impulse response h(t) is the convolution of x(t) and
      h(t), where x(t) is the applied input.




                       Figure 8: Beam propagation as a linear system

   2. The can be accomplished in the Fourier domain just as a multiplication. That is,
      we first take the Fourier transform of x(t), then multiply it with the Fourier
      transform of h(t). When we do this, we would end up with the Fourier transform
      of y(t). In order to obtain y(t) back, we’ll have to take inverse Fourier transform.

   3. Let’s extend the above theory for the propagation through free space. In general,
      the Fourier transform of h(t) is known as the transfer function. h(t) is itself known
      as the impulse response. Hence, when we have the impulse response, we convolve
      with the input function, and when we have the transfer function, we multiply with
      the Fourier transform of the input function in order to obtain the output. Clearly,
      in the second case, we’d obtain the Fourier transform of the output, while in the
      first case, we would obtain the output itself. Despite this, we like to do the
      propagation in the Fourier domain, since, multiplication, in general, is simpler to
      do than a convolution.

       The transfer function of free space is




       Where ‘d’ is the distance through which the wave needs to be propagated.




                                                                                             9
4. If f(x) is the 1D Gaussian beam to be propagated in free space, through a
    distance ‘d’, we first obtain the Fourier transform of f(x), which I call F(w). Now,
    multiply F(w) with the transfer function of free space H(w) in order to propagate
    through a distance ‘d’. Note that the distance through which the wave needs to be
    propagated‘d’ is decided while defining the transfer function of free space. After
    multiplication, we have,

                               Y(w) = X(w) x H(w)

     Where Y(w) is the Fourier transform of the field at point ‘d’ (after propagation).
     Obviously, in order to obtain the field at ‘d’, y(x), all we need to do is to apply
     Inverse Fourier transform to Y (w)




Figure 9: Two slit diffraction numerically implemented in beam propagation method




                                                                                       10
The best way to appreciate the beam propagation method is to analyze examples. In
Figure 9, I have shown my implementation of two slit diffraction using the beam
propagation method. The slits are located in the left. An incident plane wave diffracts out
of the two slits and expands as it propagates through the medium. A lens is used in order
to bring the far field closer. A screen placed after the lens would shown Young’s fringes
as shown in Figure 9.

The code that I wrote in MATLAB for implementing the above numerical models is
shown below.


Beam Propagation code: (Author: Sri Rama Prasanna Pavani)


function [Im, Power, R, SFG, CF] = bpm(G, K, N, l, dz, nz, absorb, AF)
FG = fft(G);
SFG = fftshift(FG);

figure;plot(G);figure;plot(abs(SFG));

% Transfer function of free space.
k0 = 2*pi/l;

for j = 1:N;
    H(j) = exp(i*(k0^2-(K(j))^2)^0.5 * dz);
end

figure;plot(abs(H)); title('H');figure;


%%%%% Propagation %%%%%%%
for n = 1:nz

      SFG = SFG .* H;

      R = ifft(SFG);

      if (absorb == 1)
          R = R .* AF;
          SFG = fft(R);
      end


      for cnt = 1:N;
            sR(cnt) = R(cnt) ^ (1/3);
      end

      CF(n,:) = R;
      Im(n,:) = sR;
      Power(n) = R * R';

end




                                                                                        11
Gaussian code: (Author: Sri Rama Prasanna Pavani)

function [G K N] = gaussian(l,dX)

R   =   40;
w   =   100 * l;
K   =   [-R/2:dX:R/2];
N   =   R/dX + 1;

% Gaussian
for j = 1:N

        G(j) = exp(-((K(j))^2)/w);

end
%
% figure;plot(G, K); title('Transverse Gaussian beam');
% xlabel('Intensity'); ylabel('Samples (N)');




Double slit code: (Author: Sri Rama Prasanna Pavani)

function [] = DoubleSlit(absorb)

% Size of object = 5 mm. Object samples = (5*10^-3)/(10*10^-6) = 500.
% Double slit separation = 200*10^-6. Separation samples = 200/10 = 20
% Double slit width = 40*10^-6. Width samples = 40/10 = 4

DS = [zeros(1,486), ones(1,4), zeros(1,20), ones(1,4), zeros(1,486)];

l = 0.4*10^-6;
[Im, S, P] = lbpm(DS, l, absorb, 1, 10*10^-6);

figure;imagesc(abs(Im));



Double slit diffraction code: (Author: Sri Rama Prasanna Pavani)
% All lengths are in meters
clear all; clc;

% Sample spacing.
dZ = 100 * 10^-6;

% Grid width = 1cm = 10^-2 => N = (10^-2)/(10*10^-6))
% Grid width = 1cm = 10000 * 10-6
N = 10000;

% Size of object = 5 mm = 500 samples.



                                                                         12
% Double slit separation = 200*10^-6. Separation samples = 200/10 = 20
% Double slit width = 40*10^-6. Width samples = 40/10 = 4
DS    =    [zeros(1,4860),   ones(1,40),    zeros(1,200),    ones(1,40),
zeros(1,4860)];

% Focal length = (5 * 10^-2)/(100*10^-6);
%!! f = 5cm = (5 * 10^-2) = 50000 * 10^-6
f = 50000;

l = 1 * 10^-6;

IX = [1:N];
X = (IX - N/2);

% H is the free space transfer function.
k0 = 2*pi/l;
for j = 1:N;

       H(j) = exp(i*(k0^2 - (X(j)^2))^0.5 *   f);

end

FDS = fft(DS);
SFDS = fftshift(FDS);

subplot(4,2,1);plot([1:N], DS); title('Original signal in space');
subplot(4,2,2);plot(X,abs(SFDS)); title('Original singal in freq');

%P1 = FDS .* H;

for j = 1:N
    P1(j) = SFDS(j) * H(j);
end

S1 = ifft(P1);

subplot(4,2,3);plot([1:N],   abs(S1));title('Signal  in   space   after
propagating upto lens');
subplot(4,2,4);plot(X, abs(P1));title('Signal in freq after propagating
upto lens');


% L is the lens transmission function.
 for j = 1:N;

      L(j) = exp(i*(k0)*((X(j))^2)/(2*f));

end

%S2 = S1 .* L;

for j = 1:N
    S2(j) = S1(j) * L(j);
end

P2 = fft(S2);



                                                                      13
subplot(4,2,6);plot(X, abs(P2));title('Singal in freq                    after    passing
throgh lens');
subplot(4,2,5);plot([1:N],  abs(S2));title('Signal in                     space     after
passing through lens');


P3 = P2 .* H;
S3 = ifft(P3);

subplot(4,2,8);plot(X, abs(P3));title('Final fourier spectrum');
subplot(4,2,7);plot([1:N], abs(S3));title('Final signal in space');

for j = 1:N
    DS(j) =    DS(j)^(1/3);
    S1(j) =    S1(j)^(1/3);
    S2(j) =    S2(j)^(1/3);
    S3(j) =    S3(j)^(1/3);
end

ImS = [DS; S1; S2; S3];

figure;imagesc(abs(ImS'));



Split step Beam Propagation

Now that I have given the overall idea, I’d like to get into some of the specifics involved
in the whole process of numerical implementation of beam propagation.

Firstly, we’ll have to note that the memory of a computer is not unlimited. Hence, there is
a finite fundamental limit on the resolution of the numerical implementation. As a result,
sometimes, when the diffracted beam goes near the edges, we might encounter
reflections.

The reflections can be clearly seen in Figure 10a, where the Gaussian beam hits the edges
as it propagated along z. In order to avoid this we need to have absorbing boundaries.
Absorbing boundaries are the boundary functions that do not cause reflections. This is
implemented using a technique called split step beam propagation where in the following
steps are followed.

   1. In order to propagate fro z = 0 to z = d, we should propagate step by step through
      distances delta_z ‘n’ times, such that

                                      n*delta_z = d

2. After each step of propagation, the real field is multiplied with an absorbing function,
as shown in Figure 11. The main purpose of the absorbing function is to smoothen the
edges such that the ends of the beam do not hit the edges. The beam propagation with an
absorbing function in place is shown in Figure 10b. It can be clearly seen that we no more
have the reflections we had in Figure 10a.


                                                                                        14
Figure 10a: Without absorbing boundaries




Figure 10b: Absorbing function




Figure 10c: With absorbing boundaries




                                        15
Figure 11 schematically depicts the split step beam propagation method, where the
distance to be propagated is systematically split into tiny distances of delta-z. To deal
with the most generalized case, each step is considered to have a different refractive
index. Since we are dealing only with homogeneous medium, the refractive index will
only affect the value of the propagation vector in the transfer function of the medium.

                                             2π n
                                       K =
                                              λ

Where n is the refractive index and lambda is wavelength of light.




                     Figure 11: Split step beam propagation method


Figure 12 shows the beam propagation method implementation on a triangular index
wave guide. Clearly, at z = 0, a Gaussian profile is launched. As the wave propagates
through the slab, unguided energy radiates away while the guided mode is found to
emerge after 6mm propagation.




                 Figure 12: BPM on a triangular index slab wave guide.


                                                                                        16
Coupling in waveguides

The beam propagation method is many times used to evaluate the performance of
waveguide couplers like a Y coupler. By solving the wave equation inside the wave
guide, it can be established that even confined modes have evanescent tails extending
beyond the core. The mode propagation on a waveguide that is located adjacent to an
identical guide can be analyzed with the beam propagation method.




        Figure 13: Two step index waveguides separated by a very small distance


When a Gaussian beam is launched into one of the waveguides (say, in the second one),
the beam propagation method results are as shown in Figure 14a. It is found that, because
of the proximity of the two wave guides, the following occur.

   1. Soon after a Gaussian beam is launched in the second waveguide, a part of the
      evanescent tail actually lies within the first waveguide.

   2. As the beam propagates, it is seen that the wave in the waveguide 1 starts building
      while the wave in the waveguide 2 starts decreasing.

   3. When the beam is wave guide 1 reaches its maximum, it can be clearly observed
      that the evanescent tail of the beam in waveguide 1 is actually coupled to the
      second wave guide.

   4. As the beam propagates further, the evanescent tail in the second waveguide starts
      building up, and the steps 1 to 4 repeat themselves.




                                                                                        17
Figure 14a                                Figure 14b

Figure 14a: Beam propagation results when a Gaussian beam is launched in one of the
            two waveguides located very close to each other.

Figure 14b: Fields propagated in a bent thin film wave guide calculated using beam
           Propagation method.

More results

My MATLAB implementation of propagation through a index profile as shown in Figure
13 resulted in Figure 15a and 15b. A careful observation would reveal that just when the
beam in one wave guide reaches its maximum, the beam in the other waveguide reaches
its minimum.




                                                                                      18
Figure 15a




Figure 15b



             19
Conclusion

The Beam Propagation Method was described and its use in optical waveguide analysis
was analyzed. Experimental results were provided and the results were found to agree
well with the theoretical predictions. Numerical beam propagation method, thus, is a very
handy tool for accurately determining the field at any point of a complex optical wave
guide.


Acknowledgement
Sincere thanks to Prof. Carol Cogswell’s Micro-Optical Imaging systems laboratory,
which is funding my studies in CU.


References

[1] Photonics, Optical electronics in modern communications, Amnon Yariv
[2] Fundamentals of optoelectronics, Pollock
[3] J. Van Roey, J. van der Donk, and P. E. Lagasse, Beam-propagation method: analysis
and assessment, Vol. 71, No. 7/July 1981/J. Opt. Soc. Am.
[4] R. Baets and P. E. Lagasse, Calculation of radiation loss in integrated-optic tapers and
Y-junctions, APPLIED OPTICS / Vol. 21, No. 11 / 1 June 1982
[5] Introduction to fourier optics, Joseph Goodman
[6] http://mathworld.wolfram.com/DiscreteFourierTransform.html




                                       Thank You!




                                                                                         20

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Waveguide beamprop

  • 1. Optical waveguide analysis using Beam Propagation Method Term Paper for “Introduction to Optoelectronics” spring 2006 Prof. Frank Barnes Page 10: My MATLAB® implementation of double slit diffraction Using Beam Propagation Method Sri Rama Prasanna Pavani pavani@colorado.edu Micro-Optical Imaging Systems Laboratory University of Colorado at Boulder 1
  • 2. Introduction C losed form analytical solutions for the wave equation can be easily determined only for a few symmetrical structures such as cylindrical and slab waveguides. In complicated structures with bends such as y-couplers, analytic closed form solutions cannot be derived. Figure 1a: Cylindrical waveguide Figure 1b: Y Coupler The Y-Coupler, as shown in Figure 1b, couples an input waveguide to two output waveguides. As the mode would dynamically change as the wave propagates through such structure, it is hard to determine the losses using analytical methods. Beam propagation method can be efficiently used for analyzing such structures. 2
  • 3. Beam propagation method The beam propagation method is a numerical way of determining the fields inside a waveguide. With this method, the mode profile of an unusual waveguides such as y- couplers can be determined with ease. The dynamic mode profile can be accurately estimated as the wave propagates through the wave guide. The beam propagation method essentially decomposes a mode into a superposition of plane waves, each traveling in a different direction. These individual plane waves are propagated through a finite predetermined distance through the wave guide until the point where the field needs to be determined has arrived. At this point, all the individual plane waves are numerically added in order to get back the spatial mode. Figure 2: My simulation of the diffraction of a Gaussian beam using BPM This process precisely corresponds to the Fourier way of analyzing. Specifically, according to Fourier theory, any periodic signal can be decomposed into complex sinusoids of different frequencies. When all of these sinusoids are added, we would get back the original signal. In beam propagation method, a mode is decomposed into different plane waves, which indeed are sinusoids of different frequencies. The basic idea here is to split a complicated problem into a simpler problem for which solutions are obvious. Since wave equation is linear, all these simple solutions can be added back to obtain the complicated solution. For instance, in Figure 2, I have numerically computed the diffraction of a Gaussian beam as it propagates through a medium. 3
  • 4. Principle of superposition This principle is forms the foundation of the beam propagation theory. The principle of superposition states that, for a linear system, a linear combination of solutions to the system is also a solution to the same linear system. The superposition principle applies to linear systems of algebraic equations, linear differential equations, or systems of linear differential equations. Since we are considering a linear medium, the superposition principle is valid. Consider a slab waveguide as shown in Figure 3. Any guided field inside this wave guide should necessarily satisfy the wave equation. If the medium is isotropic, then plane waves are natural solutions of the wave equation. Figure 3: Slab wave guide Since the wave equation is linear, any linear superposition of solutions will also constitute a valid solution. This important fact forms the foundation of the beam propagation theory. In order to describe the general mode of a waveguide, a superposition of plane waves, each with identical angular frequency, but different propagation vector, would be used. Thus, the essence of the theory is that plane waves form a basis set for the mode description. 4
  • 5. Fundamental mode of a Hermite Gaussian beam In this section, let us see, how the Gaussian amplitude profile, which is the fundamental TEMoo mode can be represented in the form of a superposition of plane waves. Analytically, a Gaussian can be represented as Figure 4a Figure 4b Figure 4c Figure 4a: Gaussian beam profile of a HeNe laser, which I captured after spatial filtering. Figure 4b: An ideal simulated Gaussian beam profile Figure 4c: 3D plot of a Gaussian The idea here is to split the above Gaussian into number of plane waves weighted by complex factors known as Fourier coefficients. The Fourier and inverse Fourier transforms are characterized as follows. In the first equation, f(x) (Gaussian), is represented just as an integral of weighted sinusoids. Note that F(k)s are mere complex numbers that act as weighting factors of the sinusoids. In the beam propagation approach, it can be rightly said that the Fourier kernel, that is, the sinusoids (with different k’s) are infact plane waves with different propagation vectors. Thus, in short, with the above expression, any finite analytical function can be represented as a sum of plane waves. Note that this is possible only since the Fourier transform is linear. 5
  • 6. For a Gaussian beam, the Fourier coefficients can be shown to be 1 2 x0 2 k x 2 F (k ) = e −π π x0 2 The whole theory explained above is represented by the following picture (Figure 5). Figure 5: The Gaussian beam represented in terms of multiple plane wave components. In order to obtain an appreciation for the above picture, we should first have an appreciation of the propagation vector K. The total magnitude of K is identical for all components in a mode. However, the relative sizes of Kx and Kz vary. Since Ky is assumed to be zero in the above picture, the wave propagates only in the xz plane, and therefore 2 2 K = Kx + Kz Consequently, Kz is maximum when Kx is zero, which can be clearly seen from in Figure 5. Thus the axial propagation vector is the vector with highest magnitude. As Kx increases, the amplitude of the plane wave decreases. The spatial amplitude distribution of the Gaussian is essentially comprised by the amplitude and the direction of the individual plane waves. The length of each arrow represents the amplitude of the K vector while the direction of each arrow represents the direction of the K vector. The important point in the beam propagation technique is to calculate the propagation effects using the phase space representation, and then add phase shifts caused by the waveguide structure using the spatial representation of the mode. 6
  • 7. Numerical Implementation using Discrete Fourier Transforms In order to numerically implement a beam propagation technique (as I did in Figure 2), we need to work with digital implementations of Fourier transforms known as the discrete Fourier transforms. A brief introduction to discrete Fourier transforms in given below. For more detained analysis, the interested reader is referred to standard Digital Signal Processing books, such as the one by Alan Oppenheim. The continuous Fourier transform is defined as (1) Now consider generalization to the case of a discrete function, by letting , where , with , ..., . Writing this out gives the discrete Fourier transform as (2) The inverse transform is then (3) Discrete Fourier transforms are extremely useful because they reveal periodicities in input data as well as the relative strengths of any periodic components. There are a few subtleties in the interpretation of discrete Fourier transforms, however. In general, the discrete Fourier transform of a real sequence of numbers will be a sequence of complex numbers of the same length. In particular, if are real, then and are related by (4) for , 1, ..., , where denotes the complex conjugate. This means that the component is always real for real data. As a result of the above relation, a periodic function will contain transformed peaks in not one, but two places. This happens because the periods of the input data become split into "positive" and "negative" frequency complex components. 7
  • 8. Figure 6: Introduction to discrete fourier transforms The plots above show the real part (red), imaginary part (blue), and complex modulus (green) of the discrete Fourier transforms of the functions (left figure) and (right figure) sampled 50 times over two periods. In the left figure, the symmetrical spikes on the left and right side are the "positive" and "negative" frequency components of the single sine wave. Similarly, in the right figure, there are two pairs of spikes, with the larger green spikes corresponding to the lower-frequency stronger component and the smaller green spikes corresponding to the higher-frequency weaker component. A suitably scaled plot of the complex modulus of a discrete Fourier transform is commonly known as a power spectrum. Beam diffraction In order to propagate a wave through a distance L in the z direction, we fist decompose the spatial profile of the wave into a series of plane wave components and advance each of these plane wave components through a distance of L. Once we have propagated to the point, we then superimpose all these plane wave components to get back our spatial mode at that point. Figure 7: Different path lengths incurred by different plane wave components 8
  • 9. As each plane wave is traveling in a different direction, each would accumulate a different amount of phase due to the different path lengths between the source and destination planes along different directions. Let us now consider a practical example. Consider the propagation of a Gaussian beam through a homogeneous isotropic medium. In order to achieve this numerically, the following steps should be followed. 1. The whole process is akin to a linear system analysis, where the output of a linear time invariant system with impulse response h(t) is the convolution of x(t) and h(t), where x(t) is the applied input. Figure 8: Beam propagation as a linear system 2. The can be accomplished in the Fourier domain just as a multiplication. That is, we first take the Fourier transform of x(t), then multiply it with the Fourier transform of h(t). When we do this, we would end up with the Fourier transform of y(t). In order to obtain y(t) back, we’ll have to take inverse Fourier transform. 3. Let’s extend the above theory for the propagation through free space. In general, the Fourier transform of h(t) is known as the transfer function. h(t) is itself known as the impulse response. Hence, when we have the impulse response, we convolve with the input function, and when we have the transfer function, we multiply with the Fourier transform of the input function in order to obtain the output. Clearly, in the second case, we’d obtain the Fourier transform of the output, while in the first case, we would obtain the output itself. Despite this, we like to do the propagation in the Fourier domain, since, multiplication, in general, is simpler to do than a convolution. The transfer function of free space is Where ‘d’ is the distance through which the wave needs to be propagated. 9
  • 10. 4. If f(x) is the 1D Gaussian beam to be propagated in free space, through a distance ‘d’, we first obtain the Fourier transform of f(x), which I call F(w). Now, multiply F(w) with the transfer function of free space H(w) in order to propagate through a distance ‘d’. Note that the distance through which the wave needs to be propagated‘d’ is decided while defining the transfer function of free space. After multiplication, we have, Y(w) = X(w) x H(w) Where Y(w) is the Fourier transform of the field at point ‘d’ (after propagation). Obviously, in order to obtain the field at ‘d’, y(x), all we need to do is to apply Inverse Fourier transform to Y (w) Figure 9: Two slit diffraction numerically implemented in beam propagation method 10
  • 11. The best way to appreciate the beam propagation method is to analyze examples. In Figure 9, I have shown my implementation of two slit diffraction using the beam propagation method. The slits are located in the left. An incident plane wave diffracts out of the two slits and expands as it propagates through the medium. A lens is used in order to bring the far field closer. A screen placed after the lens would shown Young’s fringes as shown in Figure 9. The code that I wrote in MATLAB for implementing the above numerical models is shown below. Beam Propagation code: (Author: Sri Rama Prasanna Pavani) function [Im, Power, R, SFG, CF] = bpm(G, K, N, l, dz, nz, absorb, AF) FG = fft(G); SFG = fftshift(FG); figure;plot(G);figure;plot(abs(SFG)); % Transfer function of free space. k0 = 2*pi/l; for j = 1:N; H(j) = exp(i*(k0^2-(K(j))^2)^0.5 * dz); end figure;plot(abs(H)); title('H');figure; %%%%% Propagation %%%%%%% for n = 1:nz SFG = SFG .* H; R = ifft(SFG); if (absorb == 1) R = R .* AF; SFG = fft(R); end for cnt = 1:N; sR(cnt) = R(cnt) ^ (1/3); end CF(n,:) = R; Im(n,:) = sR; Power(n) = R * R'; end 11
  • 12. Gaussian code: (Author: Sri Rama Prasanna Pavani) function [G K N] = gaussian(l,dX) R = 40; w = 100 * l; K = [-R/2:dX:R/2]; N = R/dX + 1; % Gaussian for j = 1:N G(j) = exp(-((K(j))^2)/w); end % % figure;plot(G, K); title('Transverse Gaussian beam'); % xlabel('Intensity'); ylabel('Samples (N)'); Double slit code: (Author: Sri Rama Prasanna Pavani) function [] = DoubleSlit(absorb) % Size of object = 5 mm. Object samples = (5*10^-3)/(10*10^-6) = 500. % Double slit separation = 200*10^-6. Separation samples = 200/10 = 20 % Double slit width = 40*10^-6. Width samples = 40/10 = 4 DS = [zeros(1,486), ones(1,4), zeros(1,20), ones(1,4), zeros(1,486)]; l = 0.4*10^-6; [Im, S, P] = lbpm(DS, l, absorb, 1, 10*10^-6); figure;imagesc(abs(Im)); Double slit diffraction code: (Author: Sri Rama Prasanna Pavani) % All lengths are in meters clear all; clc; % Sample spacing. dZ = 100 * 10^-6; % Grid width = 1cm = 10^-2 => N = (10^-2)/(10*10^-6)) % Grid width = 1cm = 10000 * 10-6 N = 10000; % Size of object = 5 mm = 500 samples. 12
  • 13. % Double slit separation = 200*10^-6. Separation samples = 200/10 = 20 % Double slit width = 40*10^-6. Width samples = 40/10 = 4 DS = [zeros(1,4860), ones(1,40), zeros(1,200), ones(1,40), zeros(1,4860)]; % Focal length = (5 * 10^-2)/(100*10^-6); %!! f = 5cm = (5 * 10^-2) = 50000 * 10^-6 f = 50000; l = 1 * 10^-6; IX = [1:N]; X = (IX - N/2); % H is the free space transfer function. k0 = 2*pi/l; for j = 1:N; H(j) = exp(i*(k0^2 - (X(j)^2))^0.5 * f); end FDS = fft(DS); SFDS = fftshift(FDS); subplot(4,2,1);plot([1:N], DS); title('Original signal in space'); subplot(4,2,2);plot(X,abs(SFDS)); title('Original singal in freq'); %P1 = FDS .* H; for j = 1:N P1(j) = SFDS(j) * H(j); end S1 = ifft(P1); subplot(4,2,3);plot([1:N], abs(S1));title('Signal in space after propagating upto lens'); subplot(4,2,4);plot(X, abs(P1));title('Signal in freq after propagating upto lens'); % L is the lens transmission function. for j = 1:N; L(j) = exp(i*(k0)*((X(j))^2)/(2*f)); end %S2 = S1 .* L; for j = 1:N S2(j) = S1(j) * L(j); end P2 = fft(S2); 13
  • 14. subplot(4,2,6);plot(X, abs(P2));title('Singal in freq after passing throgh lens'); subplot(4,2,5);plot([1:N], abs(S2));title('Signal in space after passing through lens'); P3 = P2 .* H; S3 = ifft(P3); subplot(4,2,8);plot(X, abs(P3));title('Final fourier spectrum'); subplot(4,2,7);plot([1:N], abs(S3));title('Final signal in space'); for j = 1:N DS(j) = DS(j)^(1/3); S1(j) = S1(j)^(1/3); S2(j) = S2(j)^(1/3); S3(j) = S3(j)^(1/3); end ImS = [DS; S1; S2; S3]; figure;imagesc(abs(ImS')); Split step Beam Propagation Now that I have given the overall idea, I’d like to get into some of the specifics involved in the whole process of numerical implementation of beam propagation. Firstly, we’ll have to note that the memory of a computer is not unlimited. Hence, there is a finite fundamental limit on the resolution of the numerical implementation. As a result, sometimes, when the diffracted beam goes near the edges, we might encounter reflections. The reflections can be clearly seen in Figure 10a, where the Gaussian beam hits the edges as it propagated along z. In order to avoid this we need to have absorbing boundaries. Absorbing boundaries are the boundary functions that do not cause reflections. This is implemented using a technique called split step beam propagation where in the following steps are followed. 1. In order to propagate fro z = 0 to z = d, we should propagate step by step through distances delta_z ‘n’ times, such that n*delta_z = d 2. After each step of propagation, the real field is multiplied with an absorbing function, as shown in Figure 11. The main purpose of the absorbing function is to smoothen the edges such that the ends of the beam do not hit the edges. The beam propagation with an absorbing function in place is shown in Figure 10b. It can be clearly seen that we no more have the reflections we had in Figure 10a. 14
  • 15. Figure 10a: Without absorbing boundaries Figure 10b: Absorbing function Figure 10c: With absorbing boundaries 15
  • 16. Figure 11 schematically depicts the split step beam propagation method, where the distance to be propagated is systematically split into tiny distances of delta-z. To deal with the most generalized case, each step is considered to have a different refractive index. Since we are dealing only with homogeneous medium, the refractive index will only affect the value of the propagation vector in the transfer function of the medium. 2π n K = λ Where n is the refractive index and lambda is wavelength of light. Figure 11: Split step beam propagation method Figure 12 shows the beam propagation method implementation on a triangular index wave guide. Clearly, at z = 0, a Gaussian profile is launched. As the wave propagates through the slab, unguided energy radiates away while the guided mode is found to emerge after 6mm propagation. Figure 12: BPM on a triangular index slab wave guide. 16
  • 17. Coupling in waveguides The beam propagation method is many times used to evaluate the performance of waveguide couplers like a Y coupler. By solving the wave equation inside the wave guide, it can be established that even confined modes have evanescent tails extending beyond the core. The mode propagation on a waveguide that is located adjacent to an identical guide can be analyzed with the beam propagation method. Figure 13: Two step index waveguides separated by a very small distance When a Gaussian beam is launched into one of the waveguides (say, in the second one), the beam propagation method results are as shown in Figure 14a. It is found that, because of the proximity of the two wave guides, the following occur. 1. Soon after a Gaussian beam is launched in the second waveguide, a part of the evanescent tail actually lies within the first waveguide. 2. As the beam propagates, it is seen that the wave in the waveguide 1 starts building while the wave in the waveguide 2 starts decreasing. 3. When the beam is wave guide 1 reaches its maximum, it can be clearly observed that the evanescent tail of the beam in waveguide 1 is actually coupled to the second wave guide. 4. As the beam propagates further, the evanescent tail in the second waveguide starts building up, and the steps 1 to 4 repeat themselves. 17
  • 18. Figure 14a Figure 14b Figure 14a: Beam propagation results when a Gaussian beam is launched in one of the two waveguides located very close to each other. Figure 14b: Fields propagated in a bent thin film wave guide calculated using beam Propagation method. More results My MATLAB implementation of propagation through a index profile as shown in Figure 13 resulted in Figure 15a and 15b. A careful observation would reveal that just when the beam in one wave guide reaches its maximum, the beam in the other waveguide reaches its minimum. 18
  • 20. Conclusion The Beam Propagation Method was described and its use in optical waveguide analysis was analyzed. Experimental results were provided and the results were found to agree well with the theoretical predictions. Numerical beam propagation method, thus, is a very handy tool for accurately determining the field at any point of a complex optical wave guide. Acknowledgement Sincere thanks to Prof. Carol Cogswell’s Micro-Optical Imaging systems laboratory, which is funding my studies in CU. References [1] Photonics, Optical electronics in modern communications, Amnon Yariv [2] Fundamentals of optoelectronics, Pollock [3] J. Van Roey, J. van der Donk, and P. E. Lagasse, Beam-propagation method: analysis and assessment, Vol. 71, No. 7/July 1981/J. Opt. Soc. Am. [4] R. Baets and P. E. Lagasse, Calculation of radiation loss in integrated-optic tapers and Y-junctions, APPLIED OPTICS / Vol. 21, No. 11 / 1 June 1982 [5] Introduction to fourier optics, Joseph Goodman [6] http://mathworld.wolfram.com/DiscreteFourierTransform.html Thank You! 20