arrayed waveguide gratings application and design
TRANSCRIPT
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Chapter 2 Arrayed Waveguide Gratings, Application and Design
2.1 Introduction
2.1.1 Optical Communications
Optical fibre is a popular carrier of long distance communications due to its
potential speed, flexibility and reliability. Attenuation and dispersion problems in
fibre, which limit the practical speed and distance of communication, were partially
resolved with the advent of the Erbium Doped Fibre Amplifier (EDFA)[2.1],
eliminating problems caused by attenuation. However, the dispersion qualities of an
optical fibre still force a compromise between transmission distance and bandwidth,
making it necessary to refresh high-speed signals at intervals using opto-electronic
repeaters. Solving the dispersion problem in this manner is expensive, due to the
additional cost of high-speed electronics, and maintaining and upgrading the link is
made more difficult and costly (especially with a buried or under-water link). A more
elegant solution is found using Dense Wavelength Division Multiplexing (DWDM),
which effectively increases the useable bandwidth in a system without electronic
repeaters, and allows realisation of a true photonic network.
2.1.2 Arrayed Waveguide Gratings
Dense Wavelength Division Multiplexing (DWDM) is an efficient method
where several channels, each carried by a different wavelength, are transmitted
through a single optical fibre, utilising more of the available bandwidth without
increasing the effects of dispersion. Each channel, since it is effectively separated
from the others, can be independent in protocol, speed, and direction of
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communication. DWDM also helps realise an all-optical network architecture where
signals are routed according to wavelength without the need for electro-optical
conversion. As a result, this type of network is potentially faster and more flexible,
and can be less costly to maintain when compared to other methods.
Figure 2.1 : (from [2.2]), An Add/Drop Multiplexer (ADM). Made reconfigurable by using space
division switches (top in “crossed” state)
Figure 2.2 : (from [2.2]) An Optical Cross Connect (OXC) employing a space division switch for
each wavelength. Switch settings determine where each wavelength is routed.
Arrayed Waveguide Gratings (AWGs) are optical wavelength
(de)multiplexers used in DWDM. As well as performing basic (de)multiplexing
functions, they can be combined with other components to create add/drop
multiplexers, Figure 2.1 [2.2], used to pipe single wavelengths on and off the
A D
Demux Mux
MUX
MUX
S W I
T C
H
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network, and Cross Connects, Figure 2.2, used for routing. These devices can be
passive, where the signal routing is fixed according to wavelength, or active, as in
Figures 2.1 and 2.2, where optical switches are utilised to dynamically route the
signals. Both circuits shown are transparent to the data format, can allow bi-
directional transfer of information, and function entirely in the optical domain. These
functions allow the construction of different transparent optical network topologies,
examples of the three major types of these are described in the following subsection.
2.1.3 Forms of Photonic Network
The simplest form of optical network is the point-to-point network. Optical
multiplexers and de-multiplexers are required at each end of the link. In this
configuration, DWDM simply increases the number of channels available through
one fibre. Passive Optical Networks (PONs) (Figure 2.3) [2.2] use a wavelength
(de)multiplexer as a passive optical router, each wavelength servicing an Optical
Network Unit (ONU). This allows the ONUs to share a single long optical fibre link
back to the central office (CO).
Figure 2.3: A Passive Optical Network
Long haul networks tend to have more than one point where channels are added to
and removed from the system, for example to provide a bi-directional channel to an
optical network unit. To add and remove channels optical add drop multiplexers
(OADMs) and Optical Cross Connects (OXCs) are utilised (Figures 2.1 and 2.2),
λ1
λ2
λ4
λ3
λ1 + λ2 + λ3 + λ4
Passive Router Central Office
ONUs
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[2.2], to allow single channels to be individually piped off the network, and to route
channels between sections of the network respectively. Figure 2.4 shows an example
configuration of a Long Haul network.
Figure 2.4 : A Long Haul Network, utilising Add-Drop Multiplexers (ADMs) and Optical Cross
Connects (OXCs)
2.1.4 Summary
The Arrayed Waveguide Grating (AWG) plays a crucial role in the realisation of
modern optical networks. The next section introduces the principles of operation of
the AWG, and then examines the design process.
OXC
ADM
ADM
ADM
ADM
ADM
ADM
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2.2 Arrayed Waveguide Grating (AWG) Operation Principles
2.2.1 Basic Operation of The AWG
In the previous section we established that AWGs are essential components
for the realisation of DWDM and optical networks. In this section, the basic
operation of an AWG as a de-multiplexer is described.
Figure 2.5 shows the structure of an AWG. The input (a) consists of several
channels, typically between 8 and 40 in commercial devices, carried on separate
frequencies. Channel spacings of 100GHz or 50 GHz are common in commercial
devices, although 25GHz [2.3] and 10GHz [2.4] spacings have been achieved under
laboratory conditions. The operational wavelength is commonly around 1.55µm
where attenuation is lowest in optical fibres. All waveguides in the AWG tend to be
single-moded to ensure predictable propagation through the device.
Light couples from the input waveguide (a) into the Free Propagation Region
(FPR) (b) and disperses to illuminate the arrayed waveguides (AWs) starting on a
curved plane as shown in Figure 2.6, along which the light exhibits a constant phase
profile. Each AW increases in length by ∆L compared to the previous one in the
array, where ∆L = m λw / neff, m is an integer number, λw is the central operational
(c) Arrayed Waveguides
(a) Input Waveguide
(b) Input FPR
(d) Output FPR
(e)
Figure 2.5 :[2.2] The structure of an Arrayed Waveguide Grating de-multiplexer.
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wavelength, and neff the effective refractive index, (β/k0), of the single mode
supported by each waveguide forming the AWG. Consequently, at the central
wavelength, a constant phase profile is exhibited at the end of the AWs, an integer
number of cycles out of phase, along the same plane, as shown in Figure 2.6.
Therefore, at the central frequency, the light focuses at the centre of the plane (e),
where an output waveguide is positioned to capture the focussed light. Different
wavelengths of light will exhibit different amounts of phase change and, due to the
increments in length of each waveguide, the phases will change along the AW output
plane, causing the focal point to move along the focal plane (e) at the end of the FPR.
An output waveguide is positioned on the output plane to pick up each input
frequency (channel).
Figure 2.6 : The Input / Output Free Propagation Region.
2.2.2 AWG tolerances
An AWG is a very large and inherently complex structure, typically several
square centimetres in area and comprised of multiple waveguides. The AWG is
clearly also very sensitive to any phase error, particularly at the end of the Arrayed
Waveguides. Consequently, careful and rigorous design is critical for its correct
θ RFPR ∆s
Arrayed Waveguides
Input / Output
Waveguides
Focal Plane
Ape
ture
Wid
th
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operation. A design process based on prototyping is prohibitively expensive, both in
terms of cost and time, so it is highly desirable to develop modelling tools that can
provide a detailed analysis of the device operation. However, due to the component
size, even relatively detailed analyses have previously resorted to approximate semi-
analytical methods, e.g. [2.5][2.6], which do not fully characterise the structure
(Chapter 1). Some of the current design methods are reviewed in the following
section.
2.3 Current Design Process of an AWG (Basic De-multiplexer)
2.3.1 Introduction
This section looks at the analytical methods used to design an AWG. The
design of an AWG is covered in detail in [2.2], [2.5], [2.7], and [2.8]. An AWG is
specified by the following characteristics:
• Number of Channels
• Central Frequency fc, and Channel spacing ∆fch
• Free Spectral Range ∆fFSR
• Channel bandwidth
• Maximum insertion loss
• Maximum non-uniformity
• Maximum crosstalk level
• Polarisation dependence
We concentrate first on the basic design rules that govern AWG dimensions.
2.3.2 Receiver Waveguide Spacing
The spacing of the receiver waveguides affects the adjacent-channel crosstalk
of the system and is covered in detail in [2.5] and [2.6]. A calculated crosstalk of
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around -30dB is normally considered sufficient, where other sources of crosstalk,
resulting from flaws in design and manufacture, normally become dominant.
2.3.3 Free Propagation Region (FPR) length
The length of the Free Propagation Region is determined by the maximum
acceptable channel non-uniformity (expressed in dB). Channel non-uniformity is
defined in [2.5] as the difference in intensity of the central and edge channels of the
AWG, and is the result of the variation of the waveguide mode far field with angle.
Channel non-uniformity can be estimated analytically, as described in [2.5], or
determined through numerical simulation (as will be described in Chapter 8). By
specifying the maximum channel non-uniformity, a value for the maximum
dispersion angle (θMAX) can be obtained. If the distance to the outermost output
waveguide, smax, is known, then the minimum length of the Free Propagation Region,
RFPR, is calculated by using RFPR = smax / θMAX.
2.3.4 Arrayed Waveguide Length Increment, ∆L
The increment in length of the Arrayed Waveguides (AWs) is determined
from the required dispersion D = ds / df, where ds is the displacement of the focal
spot on the image plane, and df is the change in frequency to cause this displacement.
Minimum dispersion is related to the receiver waveguide spacing and the free
propagation length. Dispersion is calculated from [2.7]:
dfdR
dfdsD FPR
θ== (2.1a)
where,
( )aFPRa
FPR
dm
dma
βπφβπφθ 2/2sin −∆
≈⎟⎟⎠
⎞⎜⎜⎝
⎛ −∆= (2.1b)
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where ∆Ф = β∆L, β is the propagation constant in the waveguides (in rads m-1), and
βFPR that in the Free Propagation Region. The waveguide spacing, da, is chosen to be
as small as possible to maximise coupling efficiency from the FPR to the AWs. m is
the order of the phased array.
2.3.5 Arrayed Waveguide Aperture Width
The aperture width, shown on Figure 2.6, is the effective capture width of the
AWs. The number of AWs, is determined by the aperture width and the crosstalk
characteristics of the waveguides used in the AWG, which affects the separation
between the AWs. It is covered in depth in [2.5] and [2.7]. The aperture size also
affects the amount of light captured by the grating and is normally chosen to capture
the majority of the expanded field at the end of the input FPR.
2.3.6 Free Spectral Range (FSR)
The required frequency range for the arrayed waveguide grating is a
fundamental design factor. FSR is defined as the frequency shift, for which the
phase-shift, ∆Φ, equals 2π, i.e.:
ππ 2~2=∆
∆ LgNcfFSR (2.2a)
where gN~ is the group index of the waveguide mode and c the velocity of light in
free space. The FSR has to be sufficiently large to accommodate the required
operating frequency range. Two frequencies separated by the Free Spectral Range
FSR and input into an AWG de-multiplexer will focus and leave though the same
output waveguide, since their phase at the outputs is the same. It follows from 2.2a
that
dfdN
fNgN gg +=~ (2.2b)
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so
LNcfg
FSR ∆=∆ ~ (2.2c)
Since the FSR is not constant with frequency the analysis above is only approximate,
but in most cases it is sufficient.
2.3.7 Summary
The parameters described in this section determine the basic dimensions for
the AWG. Although the procedures outlined provide a basic guidance for a working
design, a good design requires the consideration of many other issues, as detailed in
the next section.
2.4 Issues Affecting the Performance of Arrayed Waveguide Gratings
2.4.1 Crosstalk
The causes of inter-channel crosstalk are many, and may be a result of the
design or imperfect fabrication of the AWG. The primary source taken into account
in initial design is the inter-channel crosstalk, caused by the overlap of the focussed
spot in the output FPR with adjacent output waveguides, as covered in [2.5].
Approaches that are more rigorous take into account potential AW phase
inaccuracies, caused by design or fabrication anomalies, which cause the spot to
spread, increasing crosstalk. This form of crosstalk, however, is easily controlled by
increasing the separation of the output waveguides. Often, as evaluated in [2.9], there
are design tradeoffs between crosstalk and other desirable characteristics, such as
insertion loss or channel spacing.
Crosstalk is also likely to occur as a consequence of more complex effects in
the AWs, such as through light propagating in the AWs in modes other than the
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single-waveguide fundamental modes. This would adversely affect the phase and
amplitude distributions at the output of the Arrayed Waveguides. Due to the
assumptions inherent within AW design using current design tools, these effects are
difficult to evaluate completely. This is an area where an improved understanding is
presented in this Thesis, particularly in Chapters 6 and 7, gained through the
application of advanced numerical design tools.
2.4.2 Insertion Loss
The primary cause for insertion loss in the AWG is due to inefficient
coupling at the interface between the first FPR and the AWs. Due to reciprocity
[2.2], identical loss occurs at the second AW - FPR interface into higher diffraction
orders. Coupling efficiency, and therefore insertion loss is largely determined by the
separation of the AWs at these interfaces, where smaller separations increase the
coupling efficiency [2.2]. However, at small separations, coupling between the AWs
becomes significant. This effect has to be carefully quantified through the Finite
Difference- Beam Propagation Method (FD-BPM) or another simulation method to
avoid phasing errors in the AWs. Other areas that cause loss may include
• Material losses
• Scattering due to fabrication errors and waveguide roughness
• De-focussing of the spot on the output plane due to phase errors, decreasing
coupling efficiency into the output waveguide.
2.4.3 Polarisation Dependent Dispersion
Unless specifically engineered, waveguide boundary conditions cause quasi-
TE and quasi-TM polarised modes to propagate at different speeds (birefringence),
particularly in the case of strongly confining waveguides. As well as birefringence
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due to waveguide geometry, stresses within the structure may occur due to
fabrication processes that can cause anisotropy and stress birefringence [2.2].
Birefringence causes a second “shadow” spot on the output plane of the FPR, where
the TE- and TM- like polarisations have experienced different phase shifts,
potentially coupling with the wrong output waveguide and causing inter-channel
crosstalk. Several methods have been presented to reduce this polarisation
dependence, such as making the Free Spectral Range equal the difference between
the phase change between TE and TM polarised modes, hence overlapping the
TE/TM spots [2.10], or using a polarisation converting lambda half-plate half way
along the AWs [2.11], causing both polarisations to undergo the same phase change.
Stress birefringence in the waveguides is treated to some extent by coating the
waveguides with a stress inducing film or, as covered in [2.12], in the case of silicon
on Silica waveguides, stress-relieving grooves can be cut either side of the
waveguide.
2.4.4 Polarisation Rotation
Curved waveguides by their nature will exhibit a certain amount of
Polarisation Rotation, where the light energy is transferred from one polarisation to
the other. This effect is exploited in polarisation conversion devices in [2.13][2.14].
Polarisation rotation in the curved waveguides of the AWG is an effect that has not
presently been covered by any paper on the subject of AWGs even though it may be
in some cases a contributor to dispersion in the device.
2.4.5 Passband Shape
A sharp passband, such as the one illustrated schematically in Figure 2.7a,
allows very little error in laser frequency and AWG wavelength tolerance. It is
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desirable in most circumstances to flatten the passband, as illustrated in Figure 2.7b
so that the device produces a similar output for small changes in laser wavelength.
As stated in [2.2], the ideal shape for the passband of an AWG is to have a flat top,
with a deviation of less than 1dB, for over 70% of the channel separation, and as
wide a -3dB bandwidth (Full Width Half Maximum (FWHM)) as possible without
increasing crosstalk.
Various methods are used to flatten the pass band [2.15], such as broadening
the capture width of the receiver waveguide by using wide, multimode waveguides.
Another approach is to create a spot that has a broad flat centre with steep cut-off at
either side. The latter is achieved by using Multi-Mode Interference Devices (MMIs)
[2.16], y-junctions or a parabolic tapered horn [2.17]. Using these methods, a pass
band of over 50% of the channel separation of 200GHz is achieved in [2.18].
Alternative methods of flattening the spectral response of the AWG are
covered in [2.19], where the spectral response is manipulated by altering the
respective lengths of each arm of the AWG and their positions at the edge of the Free
Propagation Regions (FPRs). The authors of [2.20] take a similar approach through
de-focussing the phase profile in the AWG, to make it near parabolic, again widening
Frequency Gain
Figure 2.7 : (a) a typical AWG channel passband & 2.7b, with
flattened, widened, passband
Frequency Gain
3dB Passband
-3dB -3dB
(a) (b)
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the pass band. In all cases, flattening the pass band response also increases the
insertion loss of the AWG and often increases crosstalk.
2.4.6 Passband Position
Design or fabrication errors cause a phase error at the end of the AWs which
may shift the focal point away from the expected position, hence affecting the pass-
band position. To compensate for this, the position of the focal point may be shifted
by adjusting the temperature of the AWG [2.4]. If the phase error for each waveguide
is random, causing the spot to defocus, then separate heaters for each individual
Arrayed Waveguide may be implemented. However this approach increases the
energy consumed by the device and requires additional control circuitry, increasing
the cost of manufacture.
2.4.7 Summary
In this section issues that affect the performance of the AWG have been
discussed. All issues that occur in Arrayed Waveguide Gratings brought up in this
section can be attributed to issues with the Arrayed Waveguide part of the structure.
However, due to the complexity of the structure, the Arrayed Waveguides (AWs)
have not previously been fully modelled. Consequently, issues such as crosstalk are
not accurately predicted, since complex propagation mechanisms in the AWs are not
taken into account. It was suggested in Chapter 1 that FD methods, and in particular
the FD-BPM, may be adapted to allow a more thorough investigation into AW
structures, in order to predict or even reduce the impact of unwanted properties of the
AWs, ultimately improving performance and simplifying AWG design. The next
section summarises areas which the FD algorithms can improve analysis of the
AWG, to allow more thorough simulation of the AWs.
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2.5 Conclusion
This chapter described the basic operation of the AWG and summarised the
methods used for AWG design. However it is highlighted that current methods of
analysis do not accurately predict effects observed in fabricated structures, such as
increased inter-channel crosstalk. It is concluded that although the semi-analytical
analysis methods presented in Section 2.3 are sufficient to design an Arrayed
Waveguide Grating (AWG), these techniques, due to the number of assumptions
made, limit the analysis so that levels of inter-channel crosstalk, and other effects
summarised in Section 2.4, cannot be predicted. Assumptions that are made include:
• Propagation of power in the waveguides of the AW structure is to be wholly
in the fundamental mode of the waveguide
• The field at the end of the first FPR is assumed not to excite modes other than
the fundamental mode of each waveguide in the AW set, such as higher order
and grating modes.
• Coupling, and other propagation effects in the AW structure is normally
ignored
• The propagation is assumed to be constant in waveguides of varying radius.
To improve the analysis, and allow fewer assumptions to be made, a numerical
method may be used, such as the FD-BPM, introduced in Chapter 3, which is popular
due to its relative speed and accuracy. However even FD-BPM has hitherto not
widely been considered to be a viable simulation tool for the full simulation of large
components such as the AWG, due to its memory and processing requirements
although successful simulations of the output Free Propagation Regions and coupling
areas of AWGs have been conducted 2D, and in [2.6] a 3D model of the coupling
regions of the AWs is used to assist in the analysis of coupling and defocusing
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effects in the AWG. (In this case, for speed of simulation, a Fourier optics modelling
approach is used in conjunction with FD-BPM). However, even in [2.6], the
modelling of the AW structure relies on semi-analytical methods, with all light
energy in the AW structure assumed to propagate in the fundamental mode.
Consequently, in this Thesis, the goal is to improve the understanding of the AW
region of the AWG through the use of improved FD techniques. To achieve this the
basic FD-BPM is extended and improved together with an accompanying FD mode
solver, to allow efficient and accurate modelling of the complex mechanisms present
in the AWs of the AWG.
The next Chapter introduces the theory behind the FD-BPM and FD Mode
Solver in Cartesian co-ordinates, and develops the basic algorithms.
2.6 References
[2.1] P. C. Becker, N.A. Olsson, J.R. Simpson, “Erbium-Doped Fibre Amplifiers”,
Academic Press, 1st edition, May 1999
[2.2] K. A. McGreer, “Arrayed Waveguide Gratings for Wavelength Routing”,
University of Manitoba and TRLabs, IEEE commications Magazine, December
1998.
[2.3] Research by Nippon Telegraph and Telephone Corporation, “400-channel
arrayed waveguide grating with 25GHz spacing”, 2002.
[2.4] Hiroaki Yamada, Kazumasa Takada and Seiko Mitachi, “Crosstalk Reduction
in a 10 GHz Spacing Arrayed-Waveguide Grating by Phase-Error
Compensation”, Journal of Lightwave Technol., vol. 16, no. 3, March 1998
[2.5] M. K. Smit, C van Dam, “Phasar based WDM-devices: principles, design and
applications”, IEEE J Selected Topics in Quantum Electron., Vol. 2, No. 2,
June 1996, pp. 236-250
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[2.6] A Klekamp and R Munzer, “Imaging Errors in Arrayed Waveguide Gratings”,
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multiplexer / demultiplexer in WDM systems”, 3ªConferência Nacional de
Telecomunicações, Figueira da Foz, Portugal, 2001, pp. 164-168.
[2.9] J Lam and L Zhao “Design Trade-offs For Arrayed Grating DWDM
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Devices for Network Applications, April 2000, pp. 90-98
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[2.15] C. Dragone, “Efficient Techniques for widening the passband of a
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[2.16] P. Munoz, D. Pastor and J. Capmany, “Analysis and design of arrayed
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an Arrayed-Waveguide Grating with Flat Spectral Response”, J Lightwave
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