Transcript Document
7 雷射線寬(Linewidth)及啁啾(chirp)量測
• Measurement of the intensity dynamics can be
carried out using a photodetector and a
appropriate electronic receiver.
• Using the optical mixing and interference
techniques,the phase noise and frequency
dynamics of optical sources can be measured.
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7.1 Coherence Time and
Linewidth
• The coherence time, c , of a laser is measure of
the spectral purity of the laser frequency over time.
• In two-path interferometers, an optical wave
interferes with a time-delayed portion of itself.
• The degree of interference depends on the
coherence time of the wave with respect to the
optical delay.
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7.1 Coherence Time and
Linewidth
• Coherence time is reduced by random events, such as
spontaneous emission in the laser cavity, which alter the phase
or frequency of the laser-output field.
• In Fig 7.1(a), the coherence time is longer than that of (b) ,
since the phase is predictable during the
of time
.
T1 interval
T2
T1
(a)
T1
T2
T2
E (t)
time
(b)
E (t)
Fig.7.1 Concept
of coherence time
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time
Phase jumps
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7.1 Coherence Time and
Linewidth
• The coherence time, c ,varies inversely
with laser linewidth, .
• It is defined as 1
c
for spectra with Lorentzian line shapes
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7.1 Coherence Length and
Linewidth
• The coherence length is the coherence time
multiplied by velocity of light: Lc vg c
c
v
• g
ng is the group velocity
• ng is the refractive index,
( approximately 1.47 in optical fiber)
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7.2 Linewidth and Chirp
• The phase noise and frequency noise cause
spectral broadening in single-longitudinalmode lasers.
• Random phase noise is created when
spontaneous-emission,originating in the
laser cavity gain media,changes the phase of
the free running laser frequency.
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7.2 Linewidth and Chirp
• The effective amplitude-phase coupling factor,
eff shows the link between power changes in the
laser cavity to phase changes of the emitted light.
• A large value of eff results in increased laser
linewidth.
• It results in a broadening of the laser spectral
linewidth.
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7.2 Linewidth and Chirp
Frequency Chirp
• Laser frequency chirp results in significant
spectral broadening when the laser injection
current is modulated.
• The unwanted frequency modulation (chirp)
can broaden the laser spectrum.
• The magnitude of the chirp is proportional to
the amplitude-phase coupling factor. eff .
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7.2 Linewidth and Chirp
E(t)
time
CW optical field
E(t)
time
Chirped optical field
Lower frequency region
Fig7.2 Optical field with and without frequency chirp
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7.3 Methods of Linewidth
Measurement
• Neither OSA nor wavelength meters have
sufficient wavelength resolution to display
each longitudinal mode of a laser.
• Heterodyne and homodyne measurements
can be used to study the intensity dynamics.
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7.3 Methods of Linewidth
Measurement
Heterodyne measurements:
• The unknown signal is combined with a narrow-linewidth
local oscillator (LO) laser.
• The LO must have the same polarization as the unknown
signal.
• The intermediate frequency (IF) signal is analyzed with an
electronic signal analyzer such as a spectrum analyzer.
S o u rc e
U nder
T est
(L O )
L ocal
O s c illa to r
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C a lib ra te d R e c e iv e r
E le c tric a l
S p e c tr u m
A n a ly z e r
Fig 7.3 Measurement configuration for
Heterodyne spectrum analysis
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7.3 Methods of Linewidth
Measurement
Homodyne measurements:
• Homodyne techniques are similar to
heterodyne analysis except that the LO is a
time-delayed version of itself.
• If an optical signal is delayed in time by
more than the inverse of the source spectral
width (measured in Hz), the signal becomes
phase independent of the original signal,
allowing it to be an effective LO.
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7.3 Methods of Linewidth
Measurement
(a)Heterodyne
0
P o w e r (d B m )
P o w e r (d B m )
• The asymmetries of the
RB =1 M Hz
Fig 7.4
optical spectrum can’t
been seen in homodyne
(a) Intensity
modulation
measurement.
sideband for
-5 0
• The information about
0 .7 5
2
+ 3 .2 5
a DFB laser.
F req u e n cy
D iffe re n c e (G H z )
the center wavelength of
(b)Homodyne
(b) Unmodulated
a laser is not shown in
0
Linewidth
R B = 0 .1 M H z
homodyne method.
measurement
-3 d B
of a DFB
• Both methods can be
U n m o d u la te d
laser.
D F B la s e r
used to characterize laser
lin e w id th
-2 0
chirp .
0 .5
100
F re q u e n c y (M H z )
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
• The delayed self-heterodyne technique can perform
linewidth measurements without the requirement of a
separate local oscillator laser.
i (t )
Es (t )
E (t )
0
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Fig7.5 Delayed
self-heterodyne
Optical
measurement setup
Frequency
Shifter
(AO)
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
• Incident light is split into two paths by the interferometer.
• The optical frequency of one arm is offset with respect to
the other.
• If the delay, 0 ,of one path exceeds the coherence time, c ,
of the source, the two combining beams interfere as if they
are originated from two independent lasers offset in
frequency by
i(t)
Es(t) frequency shift
Fig7.6 Equivalent circuit when
the interferometer delay time
is larger than the signal
Coherence time( 0 c)
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E (t )
Es (t )
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
• The incoherent mixing requires a minimum delay requirement
of the interferometer with respect to the laser’s linewidth:
0 1
• When this condition is satisfied, the mixing becomes
independent of the phase of the interfering light and the
measurement is stable.
• The delayed self-heterodyne photocurrent consists of direct
detection as well as the desire mixing point:
Si ( f ) R 2 S d ( f ) 2S s ( ) S s ( )
(ESA=>direct direction + self-heterodyne spectrum)
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7.5 Delayed Self-Heterodyne
Linewidth Measurement
S E ( )
• is the shift frequency
applied to the field
traversing one arm of the
interferometer and R is the
usual detector responsivity.
• The displayed lineshape
will always be
symmetrical,even if the
original lineshape had
important asymmetries.
s
S E ( )
~ 200THz
convolution
s
Si ( f )
2
0
80MHz
frequency
Fig 7.7 The delayed self-heterodyne
mixing of the laser field with a frequency shifted replica.
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
• For the case of a Lorentizan-shaped field
spectrum, the displayed lineshape will be twice
of the actual linewidth.
• Laser sources exhibiting frequency jitter or 1/f
noise will yield larger measured linewidths.
• A larger delay yields a larger linewidth.
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
• The frequency shift in delayed selfheterodyne linewidth measurements can be
obtained a verity of devices including
acousto-optic frequency shifters, phase
modulators, and intensity modulators.
• The frequency shift should be larger than
the spectral content of the laser under study.
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7.4 Delayed Self-Heterodyne
Linewidth Measurement
An Example (from “Fiber Optic Test and Measurement”, edited by D. Derickson)
• An acousto-optic frequency provide an 80 MHz shift
frequency for a delayed self-heterodyne linewidth
measurement as shown in Fig.
• The preamplifier following the photodiode provided high
gain(~30dB)to reduce the effects if the ESA noise on the
sensitivity of the electronic spectrum analysis.
Fiber delay
PS
Fig 7.8 Optical
self-heterodyne
input
for laser linewidth Es (t )
measurement .
80MHz
0
PC
E (t )
SMF
AOFS
G
ESA
photodiode
Diffracted beam
AOFS=acousto-optic
Frequency shifter
Undiffracted beam stop
Power
oscillator
amplifier
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7.5 Delayed Self-Homodyne
Linewidth Measurement
• The delayed self-homodyne technique can
measure the linewidth of an unmodulated
laser.
• This method has high resolution afforded by
using optical interferometers with low-loss
fiber optic delays.
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7.5 Delayed Self-Homodyne
Linewidth Measurement
• Several optical circuit
implementations for
the delayed selfhomodyne method are
shown in Fig.7.9
input
(from “Fiber Optic
Test and
input
Measurement”, edited
by D. Derickson)
(a)Mach-Zehnder interferometer
Fiber
delay
0
PS
E (t )
SMF
i(t)
ESA
photodiode
PC
Fiber
delay
PS
(b)Michelson interferometer
i(t)
0
E (t )
SMF
PC
mirror
ESA
photodiode
Fig 7.9
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7.5 Delayed Self-Homodyne
Linewidth Measurement
•
The photocurrent spectrum for the delayed selfhomodyne technique consists of direct detection as
well as the desired mixing product but without the
frequency shift: 2
Si ( f ) R Sd ( f ) 2 Ss () Ss ()
(ESA=>direct direction + self-homodyne spectrum)
• The displayed lineshape will always be
symmetrical,even if the original lineshape had
important asymmetries.
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7.5 Delayed Self-Homodyne
Linewidth Measurement
• The translation of linewidth
information from the optical
spectrum to electrical
spectrum is illustrated in Fig.
• For the case of laser
lineshapes described by
Lorentzian or Gaussian
functions,the displayed
electrical power spectrum
will have identical
functional shapes to the
actual optical spectrum.
S E ( )
s
S E ( )
convolution
s
Si ( f )
2
Fig 7.10 The delayed self-homodyne
mixing of the laser field.
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7.6 Laser Chirp Measurement
• Measurement of chirp provides the dynamics of
the laser frequency excursions during intensity
modulation.
• The time dependence of frequency chirp can be
characterized using optical discriminators to
convert optical frequency variations into
detectable intensity variations.
• A linear optical component with wavelengthdependent transmission characteristics may serve
as a discriminator.
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7.6 Laser Chirp Measurement
• An interferometer circuit
for measuring laser chirp
as shown in Fig . (from
Fiber Optic Test and
Measurement, edited by D.
Derickson)
• The differential time of
flight between the two
interference path is
denoted by 0 .
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Quadrature Feedback
circuit
lens
PZT
idc idc
PC
Computer
A
SOURCE
laser
B
Es (t )
z
collimator
modulation
scope
i(t )
Bias T
E (t )
High-speed
receiver
to:scope trigger
Fig 7.11 Time-domain laser chirp measurement using
A Mach-Zehnder interferometer followed by
A high-speed receiver.
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7.6 Laser Chirp Measurement
• A feedback circuit maintains quadrature by adjusting the
delay 0 .
• This delay adjustment is small,on the order of an optical
wavelength.
• This delay can be realized using piezo-electric(PZT)
devices.
• The measurements apparatus uses a sampling oscilloscope
which is triggered by the laser modulation source.
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7.6 Laser Chirp Measurement
Analysis.
• For interferometers with two optical paths,the average
output power interferometer is the sum of the path power
contributions and an interference term:
P (t ) P (t ) P (t ) 2 P (t ) P (t ) cos( (t , ) 2 )
0
1
2
1 2
0
0 0
0 is the average optical carrier frequency and 0 is the
differential interferometer delay.
• In the absence of any frequency modulation,
(t ) is zero
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7.6 Laser Chirp Measurement
Interferometer Delay Requirement.
• To maintain unambiguous chirp measurement,the
peak frequency excursion peak must be less than
one-forth the interferometer free-spectral range.
• To reduce the effects of noise on the chirp
measurement ,the maximum chirp is confined to
the approximately linear region of the
interferometer characteristic :
peak
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7.6 Laser Chirp Measurement
(a) 1Gb/s
200ps
Example. (from “Fiber
Optic Test and
Measurement”, edited
by D. Derickson)
(b)
10
.
5
0
Fig 7.12 Optical discriminator used to
measure DFB laser.(a) Intensity
Modulation.(b)Frequency chirp.
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time
-5
-10
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7.6 Laser Chirp Measurement
• Since the measurement is made in the time
domain, both the magnitude and the phase of
the amplitude and frequency modulation are
measured.
• This technique can also be applied towards
frequency domain measurements of the FM
response by characterizing laser FM response
as a function of modulation frequency applied
to the laser.
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