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Analysis of optical-signal processing using an arrayed-waveguide grating

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Abstract

We analyzed optical-signal processing based on time-space conversion in an arrayed-waveguide grating (AWG). General expressions for the electric fields needed to design frequency filters were obtained. We took into account the effects of the waveguides and clearly distinguished the temporal frequency axis from the spatial axis at the focal plane, at which frequency filters were placed. Using the analytical results, we identified the factors limiting the input-pulse width and clarified the windowing effect and the effect ofphase fluctuation in the arrayed waveguide.

©2000 Optical Society of America

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Figures (5)

Figure 1.
Figure 1. Schematic diagrams of time-space-conversion optical-signal processing using (a) DGs and (b) AWGs.
Figure 2.
Figure 2. Model and axes used for analysis. Spatial frequency axes were used instead of spatial axes at the interface between the I/O waveguide and the first slab waveguide and at the focal plane.
Figure 3.
Figure 3. Spectral filtering using narrow-stripe mirror: (a) profile of narrow stripe mirror, (b) electric field near ξ=0, (c) temporal frequency spectrum reflected by narrow stripe mirror, (d) temporal output waveform. The shape of the output waveform reflects crosstalk at the focal plane.
Figure 4.
Figure 4. Figure of merit (flatness of envelope of temporal waveform) and loss versus shape of distribution function (a/Nd). Envelope of temporal waveform became flatter as a/Nd became larger, but the loss became larger. There is thus a trade-off relation between loss and the figure of merit. The a/Nd of the previously reported AWG was 0.57.
Figure 5.
Figure 5. Number-of-waveguides dependence on coefficient of determination (R 2) calculated from output pulse shape for m=72. A phase error of 0.8×10-2 rad/mm is a typical standard deviation in a silica-based waveguide with a relative refractive index difference of 0.75%.

Tables (1)

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Table 1 Parameters used in AWG simulation

Equations (34)

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f ( t ) = u ( t ) exp ( i 2 π ν 0 t ) ,
F ( ν ) = U ( ν ν 0 ) U ν .
F 0 , ν ( x 0 ) = U ν · e ( x 0 ) = U ν w IO π · exp ( x 0 2 w IO 2 ) .
β ( x 1 ) = w IO π i α exp { ( π w IO ) 2 ( x 1 α ) 2 } ,
α = c L f n s ν 0 ,
f 1 , ν ( x 1 ) = U ν · [ { β ( x 1 ) · rect ( x 1 Nd ) } * δ S ( x 1 ) ] * exp ( π x 1 2 w AW 2 ) ,
δ S ( x ) p = N 2 N 2 1 δ ( x 1 pd ) ,
rect ( x ) = { 1 ( x < 1 2 ) 0 ( otherwize ) ,
θ ( x , ν ) = 2 π m ν ν 0 d x · δ S ( x ) .
f 2 , ν ( x 2 ) = exp { i θ ( x 2 , ν ) } · f 1 , ν ( x 2 )
= U ν · [ { β ( x 2 ) · rect ( x 2 Nd ) · exp ( i 2 π m ν ν 0 d x 2 ) } * δ S ( x 2 ) ]
* exp ( π x 2 2 w AW 2 ) .
F 3 , ν ( ξ ) = π w AW 2 i α U ν { B ( ξ ) * sinc ( Nd ξ ) * δ ( ξ m ν ν 0 d ) } Δ Sum ( ξ ) exp ( π 2 w AW 2 ξ 2 ) ,
ξ ν 0 n s c L f x 3 = x 3 α ,
Δ S ( ξ ) = p = N 2 N 2 1 exp ( i 2 π pd ξ )
B ( ξ ) = α 3 2 i π w IO exp { ( α ξ ) 2 w IO 2 } .
ξ = m ν ν 0 d
γ = ν x 3 = ν 0 2 n s d mc L f = ν 0 d m α .
ν FSR = ν 0 m .
Δ ν = ν 0 Nm .
Δ ν = ν 0 d m Δ ξ ν 0 N eff · m ,
G 3 , ν ( ξ ) = π w AW 2 i α · U ν · H ( ξ ) · { B ( ξ ) * sinc ( Nd ξ ) * δ ( ξ m ν ν 0 d ) }
× Δ S ( ξ ) · exp ( π 2 w AW 2 ξ 2 ) ,
g 2 , ν ( x 2 ) = U ν · { h ( x 2 ) * ( β ( x 2 ) · rect ( x 2 Nd ) · exp ( i 2 π m ν ν 0 d x 2 ) ) * δ S ( x 2 ) }
* exp ( π x 2 2 w 2 )
g 1 , ν ( x 1 ) = U ν · [ { h ( x 1 ) * ( β ( x 1 ) . rect ( x 1 Nd ) · exp ( i 2 π m ν ν 0 d x 1 ) ) * δ S ( x 1 ) }
× exp ( i 2 π m ν ν 0 d x 1 ) ] * exp ( π x 1 2 w 2 ) .
G 0 , ν ( ξ ) = π w AW 2 i α · U ν · { H ( ξ + m ν ν 0 d ) · ( B ( ξ ) * sinc ( Nd ξ ) ) · Δ S ( ξ + m ν ν 0 d ) }
× exp ( π 2 w AW 2 ξ 2 ) .
V ν = e ( α ξ ) · G 0 , ν ( ξ ) d ξ
= π w AW 2 i α · U ν e ( α ξ ) · H ( ξ + m ν ν 0 d ) · ( B ( ξ ) * sinc ( Nd ξ ) ) · Δ S ( ξ + m ν ν 0 d )
× exp ( π 2 w AW 2 ξ 2 ) d ξ .
Δ t = 1 ν FSR = m ν 0 .
T 0 = 1 Δ ν = Nm ν 0 .
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