Note: Descriptions are shown in the official language in which they were submitted.
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BACK~R_D A~D SUMMARY OF T_INVF~NTION
The present invention relates generally to an apparatus and
method for measuring power and power losses of light transmissionc
in fiber optic cables, and more specifically, the power and power
losses resulting from the transmissions of known wavelengths of
light. -
Fiber optic cables have been finding increased applica~ions ir.a variety of industries as a result of-their ligntweight
composition and effectiveness in transferring information. The
use of fiher optic cables has, for instance, become co~non in the
telecommunications industTy, where many of the bulkier and less
efficient wire data lines are be.ing replaced with fiber optic
cables. To assure accurac~ of the data transmitted b~ light
signals, however, these fiber optic cables are tested by m~asurina
the power losses associated with the light transmissions, and
th~s, determine the potential error in the data transmissions.
Lignt signals constituting data transmissions are transmitted
through fiber optic cables using specific nominal wavelengths of
light for the transmission. Because different ~avelengths of
light have varying attenuating characteristics, it is important to
determine the attenuation of the iber optic cable with respect t~
the spec;fic wavelength of light which will be used for the
particular data transmission.
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In U.S. Patent 4,234,253 to Higginbotham et al., an
attenuation measuring system is described 25 having a transmitter
and receiver which are operativeiy connected to opposite ends of a
fiber optic cable under test. A r~ference signal comprised o a
timing pulse is superimposed upon a square wave pulse. This
modified square wave~signa-l is then transmitted through the fiber
optic cable where it is detected by a receiver attached to a
second end of the cable. ~he receiver separates the timing pulse
from the transmitted pulse for use in demodulating the transmitted
signal and compares the demodulated square wave signal to a
reference signal contained wi~hin the receiver; The use of a
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modified square wavë pulsë as a test signal, however, has the
disadvantages of signal noise and limited bandwidth which are
characteristic of DC s~gnals.
U.S. Patent 4,2BO,765 to Pophillat et al. describes a
measuring system for measuring the transmission bandwidth of the
fiber optic cable using a plurality of sinusoidal test signals as
opposed to square wave pulses. ~ophillat, therefore, avoids some
of the disadvantages of Higginbotham. This system comprises a
frequency generator for producing a first composite signal having
discrete distribution of predetermined sinusoidal frequencies. A
single laser is provided by which the first composite signal
modulates the light signal for transmission through the optical
,
fiber under test. An op~ical detector is positioned at a
~eceiving end for converting the light signal into a second
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composite signal and directing the same to a spectrum analyzer.
The analyzer provides a requency spectrum display of the
composîte o the electrical sinusoidal signals which is compared
with the spectrum of the first siqnal for determining the power
attenuation of the first composite of signal transmîssions. While
the prior art has concentrated on techniques o measuring the
response to the specific wavelength of light that is being
transmitted, they have failed ~o address the problem of providing
a tester which is capable of being adapted for the varying nu~ers
of wavelengths which may be used. As more and more different
sources of light become available, and the quality of light fibe.rs
increases, a single tester at a single wavelength will not be
sufficient.
It is, therefore, an object of the present disclosure to
provide a means for determining the power losses associated with
any specific wavelengths of light transmissions.
Another object o~ the presentdisclosure is to provide a means
for identifying the wavelength of light signals transmitted
through a fiber optic cable under test and for aetermining the
power losses associated with the respective light wavelengths.
Yet another object is to provide a
means for determining the power losses associated with specific
wavelengths of light transmissions, using either a laser or an LED
as a source for the light transmissions.
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Still another object is to provide a
means for measuring the optical power transmitted through a fiber
optic cable.
A further o~ject is to provide a
microprocessor control tester for measuring the power attenuation
at each specific ~avelength of light transmissions in fiber optics.
Here described is a
transmitter for modulating the power intensities of known
wavelengths of light with identifying or signature AC signals.
The modulated light.is transmitted through a length of fiber under -
test.where the modulated light is then detected and the signature
identified ~y a receiver. The transmitted AC signa} is compared
with a reference~signal stored in a microprocessor or the
specific signature to determine the power attenuation of the
transmitted signal, thereby determining the transfer
characteristics of the fiber optic cable as a function of light
wavelengths. By using AC signals to modulate the light
wavelength, the pro~lem of noise and limited bandwiath associated
with DC signal transmissions are avoided. Nevertheless, a
specially preferred embodiment of the tester also includes the
capabilities of also measuring the DC power of the transmitted
signal.
A specially prefer'red emhodiment of the tester is designed as
a modular sys~em,~and thus, may be operated~as either a single
unit (local mode~ or a plurality of separate units (remote mode).
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For fiber optic cables of relatively short length, a single tester
unit having both a transmitter module and a receiver module is
used, such that the single tester unit attaches to both ends of
the cable under test. For cables of longer length, separate
tester units having respective transmitting and receiving modules
contained therein are provided, whereby the receiver unit includes
independently calibrated reference signals for comparison with the
received transmitted signal.
Preferred embodiments of the transmitting part of the tester
in both single and separate tester operations may include a
plurality of laser or light emitting diode ~LED) source modules,
each module designed Lo produce a predètermined known mean
wavelength o light. Because fiber optic cables do not attenuate
the power intensities of different wavelengths o light uniformly,
a more accurate xepresentation of the fiber optic cable
transmission characteristics results with the use of a plurality
of light sources. Each laser or LED source module has assigned to
it a modulating AC signal of a specified frequency. After
transmission of a nominal wavelength o light modulated on the
assigned known frequency, the microprocessor controlled receiver
module identifies the modulating frequency for determining which
wavelength of light was transmitted, and thereby associate the
power loss measurement with the~transmitted wavelength of light.
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In specially preferred embodiments with a laser light
source, the transmitter includes a photodetector for providing
input to two feedback circuits, which provide stabilization of
the test signal amplitude and wavelength. These feedback loops
stabilize the average power or DC level of the light source and
maintains the percentage modulation constant. A third feedback
which is utilized when the light source is either an LED or a
laser, includes a temperature compensation circuit for
maintaining the ambient temperature surrounding the light source
at a selected temperature. This assures that the light source
will have as consistent output as possible. Thus, the feedback
circuits assure that during testLng, the microprocessor
controlled drive unit~ o~ tha respective light sources provide a
proper modulation of the assigned wavelength of light.
A unique temperature compensating circuit for a light
source is described. This includes a heater/cooler in a four
switch bridge which determines the direction of current through
the heater~cooler as a function of temperature ~ariations and,
thus, the heating or cooling cycle of the heater/cooler.
In accordance with a first aspect of the invention
there is provided a temperature compensation circuit comprising:
a cooler and heater means haYing a first and a second
terminal for providing cooling when current flows into said first
terminal and out of said second terminal, and providing heating
when current flows into said second ~erminal and out of said first
; terminal;
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a four switch bridge having two pairs o opposed
terminals, a power supply connected across one pair of opposed
terminals and said cooler and heater means across th~ other pair
of opposed terminals;
. error means for sensing a ~emperatuxe, comparing the
: sensed temperature to a desired temperature and producing a
temperature error signal; and
control means connected to said error means and said four
switch bridge for activating diagonally opposed pairs of switches
in said bridge to control the direction of current flow through
said cooler and heater means as a function of said error signal.
Embodiments of the invention will now be described
; with reference to the accompanying drawings wherein;
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BRIEF DESCRIPTIO~ OF THE DRAWINGS
Figure 1 is a schematic diagram of the tester unit accordiny
to a preferred embodiment of the present invention.
Figure 2 is a more detailed schematic diagram of ~he ~eedback
and status circuits as shown in Figure 1.
Figure 3 is' a more detailed s,chematic diagram of the variable
frequency generator and demodula~or as shown in Figure 1.
- DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
-
, Reerring to Figure 1, a modular test unit includes a main
,frame unit ll, a source.module 10 and a detector module 12. ~n
optical cable 15 is connected to source module 10 at 13 and to,
detector module 12 at 1~. The main frame test unit 11 includes a
microprocessor 18, a frequency generating circuitry for providing
a modulating frequency or the source module 10, and an
identifying and demodulating circuitry for identifying the
modulating frequency of the signal received by the detector module
12, and demodulating the signal for further processing for input
into the microprocessor 18. Each main frame unit 11 includes a
microprocessor lB for controlling the various analog circuits, for
storing calibration parameters and for determining the power loss
of a transmitted light wavelength signal. The analog circuitry of
the main frame unit 11, the detector module 12, and source module
10, are interfaced through an I/O board 111 to the microprocessor
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The source module 10 includes a light source 28 having a known
center wavelength of light output. The source module 10 receives
a specified modulation frequency from the mainframe unit for
providing signature modulation, e.g. modulating a known wavelength
of light by a known modulating frequency. Each source module is
assigned a different modulating frequency, depending upon its
wavelength, its type of source, e.g. laser or LED and the
calibrated output power. This modulating frequency assignment is
stored in each ~ester's microprocessor's memory 17. In order to
insure accuracy of testing by simulating normal operational
conditions for fiber optic cable systems which use either laser or
LED light sources for their data transmissions, source modules 10
are available which include LED light sources or laser light
sources.
The detector module 12 includes microprocessor controlled
circuitry for detecting the modulated light signai of a speci~ic
wavelength and amplifying the same for receipt by the demodulator
circuitry 23 in the main frame unit 11. Because the detector
modules 12 each have their own Yarying responses to different
wavelengths of light received, each module 12 is calibrated at the
factory for determining this response, which response is stored in
the respecti~e PROM's 75 located in thè detector module 12. Upon
the demodulator 23 in the main frame unit 11 determining the
modulating frequency received by the detector module, the
microprocessor 18 will match the frequency with its assigned
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wavelength of light. The microprocessor 18 will then retrieve
from the detector module P~O~ 75 the corresponding calibrated
parameters associated with the detector's responsiveness to the
light wave received, and will use t~ese parameters in any
calculations the microprocessor will perform regarding the
received signal. ~
The tester unit is capable of measuring the optical power of
the transmitted light signal received at a second position, or it
can determine the power loss of a transmitted light wavelength
signal by comparing the power level o~ the received signal with
the power level of a reference signal. The comparison of siqnals
is performed by the microprocessor 18 with the reference signal
having been store~ in the microprocessor's memory~
By flipping a switch (not shown) on the front panel of the
main frame unit 11, the operator may choose between a relative or
absolute mode for determining the power loss measurement. In the
relative mode, the tester is set up to make a power measurement of
any received signal and use this measurement as a relative value
for comparing with a second received signal. In an absolute mode,
the microprocessor uses as a reference signal, stored information
regarding the specific light wave which was transmitted. Each
tester main frame unit 11 has stored in its memory the power
intensities of all available light signal transmissions. Thus,
upon the demodulator circuitry 23 identifying the modulating
frequency, the microprocessor retrieves from its memory the
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reference signal corresponding to the transmitted light wavelength
signal and uses the same for determining the received iight
wavelength signal's power loss.
In onepreferred embodiment, the source module 10 transmits an
AC signal having a DC bias. The tester system proYides the
ability to measure the DC'~optical power by fi:ltering out the AC
components~ or it can measure the peak AC power of the received
signal or determining the power loss associated with the same;
By attaching or remo~ing different source and aetector
modules, the configuration of the test system can be changed. By
including ~oth source lO 'and detector 14 modules in a signal te.st
unit, the tester is set up in a local mode, whereby the tester
provides a test signal at the source module output 2~ to a first
end 13 of a fiber optic cable lS and detects the transmitted
signal at 2 second end 14 of the fiber optic cable 15 by an input
to the detector module 74.
If the fiber optic cable 15 under test is too lon~ for''local
or single tester applicability, a second main frame unit (not '
shown) will be required at the second end of the fiber optic ca~le
15 under test. In this remote mode of testing, the first main
frame unit 11 with a source module 10 can be set up to transmit
the test signal to the first end 13 of the cable 15. The second
main frame unit (not shown) is set up as the receiver requiring
only a receiver module 12 for detecting and measuring the power of
the received wavelength test signal. The second main frame uses
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its microprocessor to identify the signature of the transmitted
signal and provides the appropriate controls and re~erence signal
for the detector module. If source 10 and detector 12 modules are
duplicated in both main frame units, the test signal may be sent
in either direction of the cable length, thereby providing a
testing system having bi-directional test capabilities.
The modularity of the testing system also allows for the
interchangability of different source modules 10, having different
wavelength test signals. This allows for a fle~ibility in testing
any number of available wavelengths by merely interchanging the
source module 10.- Each dëtector module 12 is calibrated at the
factory for responding to all available light sources. A
modulating AC signal is generated b~ a microproc~ssor controlled
frequency generator lfi located in the main frame 11 of the tester
unit. The frequency of the modulating AC signal is controlled by
data signals received from the microprocessor 18 through I/O ports
20a and 20b of the microprocessor 18 and generator 16
respectively. In the preferred embodiment shown, the frequency
generator 16 provides a nominal ou~put frequency of lO KHz. The
output of the frequency generator 16 is provided to an input of a
phase lock loop (PLL) 22 having a voltage control oscillator
(VCO), as well as to an input to a demodulator and low pass filter
23. The output of the PL~ 22 provides an AC signal of a known
frequency to the input of a voltage control amplifier (VCA) 24
which serves as the input to the source module 10. The VCA in
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turn provides an AC signal of a specified average voltage to a
driver circuit 26. The output of the PLL 22 is also provided at a
terminal 25 on the rear panel o the main frame unit 11 for
re~erencing the AC signal. The driver circuit 26 then pro~ides a
light source 28 with a nominal bias current having frequency
corresponding to the frequency of the AC signal provided by the
frequency generator 16, an average AC power determined by the VCA
24 and a DC bias level determined by the driver circuit 26. The
light source 28 comprising either a laser or light emitting diode
(LED), then provides a modulated light signal of a known
wavelength modulating frequency and power leve~ to the fiber optic
cable 13.
The output o~ the light source 28 is provided as a feedback
circuit to control the light source. If a laser source is used, a
photodetector 30 senses the output of the laser and provides it on
line 33b to switch 33 which is connected during assembly of the
source module. If a I.ED is used as a source, a current measuring
circuit 31 is provided and connected to line 30a. The selected
feedback signal is provided to the AC level set circuit 32 which
should adjust the gain of the VCA 24 and to DC level set 34 to
adjust the driver circuit 26. A temperature compensation circuit
S8 is also provided to control the temperature of either laser or
LED sources 28. Status circuitry 5g is connected to the
temperature compensation circuit 5~, the DC level circuit 34 and
the AC level circuit 32 to provide a visual indication of the
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proper operating status of this system as well as communicating
the status to the CPU via I/O port 20d~ -
A sourc~ identification circuit 47 is includPd in every sourcemodule lO to identify to the main frame testler unit ll the type of
light source the particular source module lO represents via I/O
por~ 20e. The microproces~sor 18; can therefore, retrieve from its
memory, the necessary data for programming the respective
components of the source module lO via-I/O ports 20.
The details of the eedback and status circuitry are
illustrated specifically in Figure 2. The DC level set circuit 32.
includes a low pass filter 35 and an integrator 36. Their output
is provided to a window dëtector 37 in the status circuitry 59.
If the signal is within the high and low value determined by the
. . .
window detector 37, a positive indication is given on terminal
20dl to the CPU. The AC level set circuit 34 includes a full wave
rectifier 38 and an integrator 39 providing a signal to window
detector 40 of the status control circuitry 59. If this value is
within the high and low limits set by the window detector, it will
provïde a positive output on terminal 20d2 to the I/O port. The
visual indication in LED 64 is connected to the terminal ~Od2 and
is lit if the DC level is within the acceptable limits.
The temperature compensation circuit 58 is included in the
source module lO when a laser or LED source is used, for
maintaining a preselected temperature surrounding the laser or LED
source 28. In the preferred embodiment, a temperature of
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appro~imately 25C is maintained about the light sou~ce. The
compensation circuit 58 includes a resistive bridge 60 including a
thermistor RT. An integrator 61 connected across the output o~
resistor bridge 60 provides an input to the control circuit 62 for
peltier 45 for heating or cooling the light source and an input to
window comparator 63 nf t~e status circuitry 59. The control
circuitry 62 for the peltier 45 is constructed as a current
switching bridg~ including serially connected P-channel transistor
41 and N-channel transistor 42 in parallel with series connected
P-channel transistor 47 and N-channel transistor 48 betwe~n a
current limiter and groun^d. The peltier device 45 is connected
between the two parallel iegs. The output from the integrator 61
is provided as an input to the gates o~ the transistor pairs 41
and 42 via amplifier 43. The signals on the drain of the
transistor pairs are provided as a second input to the amplifier
43. A capacitor 46 is connected between the gates and sources of
the transistors 41 and 42 for providing stability. The output of
integrator 50 is connected as an input signal to amplifier 49, and
in turn, the output of amplifier 49 is connected to the gates of
transistor pair 47 and 48. The sources of the transistor pair 47
and 48 are also connected as a second input to the amplifier 49.
A capacitor 51 is connected between the common gates and sources
of the transistor pair 47 and 48 for providing stability.
Depending upon the high or low value of the output signal sensed
by the resistor bridge 60, diagonally opposing transistors of the
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control circuit will be activated to control the degree and
direction of current through the peltier device. For current in
one direction, the peltier device will heat up and for current in
the other direction, it will cool. By way of e~ample, if a
positive signal is provided on amplifier 43, the N-channel device
42 will be on and the P-c~annel device 41 will be of~. The
inverted signal on amplifier 49 will turn on P-channel device 47
and turn off N-channel device 48. Thus, the current path will be
from the voltage regulator 44 through P-channel device 47, laser
peltier 4S, N-channel device 42 to ground. The low voltage signal
at the source of 42.is fed back to amplifier 43 to further
increase its differential as will the current signal on t:he source
oE transistor 53 be provided to the amplifier 49. For a low input
signal, the inverse occurs, namely P-channel 41 and N-channel 48
are on providing a current path through peltier 45 in the opposite
direction. The inverted and non-inverted input signals are
provided to the window detector 63 which provides an output signal
to I/O port 2~d2 as well as to the LED 64.
The detector module 12 of the receiving part of the test.
system includes a photodetector 74 arranged at a second end 14 o~
the fiber optic cable 15. A detector prom module 75 is included
in each detector module 12 for storing information relating to the
responsivity of the specific photodetector 74 to different
:: wavelengths of light, also gain, absolute calibration factors,
type of detector, and parity checker bits. Because the
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photodetector 7~ will respond diferently to different ~avelengths
of light, the detector 74 is tested during the manufacturing and
assembly of the detector module i2 for det~rmining this variance,
with the resulting information stored in the detector prom 75.
This information is retrieved by the microprocessor 18 via I/0
port 20f from the detecto~ prom 75 during the normal testing
operation as compensat;ng factors in order to eliminate the
responsivity of the photodetector 74 to light wavelengths in
determining the power of attenuation o the test signals.
The photodetector 74 provides a current equi~alent to the
power intensity of the detected transmitted si~nal to a
microprocessor controlied variable gain current-to-voltage IfV
converter 76. The microprocessor 18 via D/A converter 79 and I~0
ports 20g controls the reference signal for IfV converter 76 and
via I/0 20h the gain of resistors 77 by switching different
resistors into the feedback of the I~V converter 76. The output
of the IfV converter 76 is then supplied either directly to
amplifier B0 whose gain is microprocessor controller via I~0 20i
or supplied indirectly to the same via amplifier 78, as determined
by switch 82 controlled by I/0 20j. The output of amplifier 80 in
turn provides the input to a demodulator 84 located in the main
frame test unit 11. Additionally, this output is provided to a
speaker 92 via serially connected voltage control oscillator B8
and buffers 89. An output of a demodulator 23 in the main frame
11 provides the input to a continuity indicator circuit 86 located
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in the detector module 12. The indicator 86 includes an ~ED for
indicating the presence of a detected signal by pho~odetector 74. - -
The demodulator 23 receives an AC reference signal from thefrequency generator 16. In local mode, the transmitter and
receiver components are in one unit and, thus, the demodulator 23
merely references the out~ut o~ the frequency generator 16 to
determine the frequency o~ modulation. In remote mode, the main
frame unit which is at the recei~ing end of the cable, does not
have this initial information, and thus, must step the frequency
generator 16 through all the possible modulating frequencies of
the transmitter which are stored in the microprocessar's memory in
the receiving unit, an~ compare the same with the raGeived signal
to determine the AC modulating frequency of the transmitter. The
demodulator 23 then receives the necessary frequency components.
The output of the demodulator 23 provides the input to a
sample and hold circuit 101 and A/D converter 102. The A~D
converter 102 in turn provides the input to a buffer and decoder
104 and to an alphanumeric display 106. The buffer and decoder
104 is further coupled to a data bus 108 which connects to the I/0
circuit 111 and General Purpose Interface Bus (GPIB) 112. The I/0
circuit 111 is also coupled to the central processing unit (CPU)
18.
Figure 3 shows a more detailed schematic diagram of a
preferred embodiment of the frequency generator 16 and demodulator
23. The frequency generator 16 includes a temperature compensated
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crystal oscillator (TCXO) 16 which provides the input, e.g. 10 KHz
to a first microprocessor controlled multiple divider 118 haYing
I/O ports 20a connected ~o the microprocessor 18. In the
preferred embodiment, the multiple divider 118 provides assigned
frequencies in steps of 40 Hz from the nominal frequency of 10 KHz
for assigning a specific ~C frequency of modulation to each
wavelength of'light to identify the wavelength with a signature or
identifying AC frequency. The output of the multiple divider 118
is then provided to a divide-by-four divider 120 for pro~iding an
output signal to the PLL circuit 22 and frequency components ~, q,
i, i,representing-the genërated frequency to the demodulator 23.
The demodulator 23'includes an amplifier 122 whose output is
connected to ground via variable resistance 124 for providing DC
gain, and via capacitance 126 and varia~le resistance 128 for
pro~iding AC gain. A circuit for providing the e~uivalent peak
value of the received AC component is connected between the output
connections of amplifier 122 and the sample and hold circuits
101. This circuit comprises parallel mixers 130 and 132 having
inputs connected to the respective output signals of the
divide-by-four divider 120 or to the microprocessor, depending
upon the mode the system is operating under. The mixers 130, 132
have a common connection with variable resistance 128 for
receiving the received'transmitted signal from amplifier 122. The
respective outputs of mixers 130, 132 are connected to respective
microprocessor controlled low pass filters 134, 136 and to
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respective ampliiers 138, 140~ The output of the amplifiers 138,
140 provide the Q and I components respectively, which are then~
provided to respecti~e inputs to the sample and hold circuit 101,
and A/D converter 102, respectively of Figure 1.
In the operation of the measuring systenn, the frequency
generator 16 is programme~ to produce a specific frequency
output. The requency output of the general:or 16 will then be
processed through the phase lock loop ~2 and further processed by
a voltage control amplifier 24 and driver circuit 26. A bias
current provided by the driver circuit 26 will modulate the light
source 28 at the assigned frequency of the generator~s OlltpUt, and
at the power intensity provided by ~he VCA and driver circuits.The
light source 2~ comprises either a laser or LED having a known
central wavelength associated with its light signal output. The
source module 10 includes at least one of these light sources 28
with each of the sources providing a light signal of a distinct
central waYelength. The microprocessor 18 programs the freguency
generating system 16 to generate a specific frequency to
correspond to each of the ligh~ sources 28, thereby providing an
identification or signature modulation for the particular light
wavelength of each source. Because the modules and main frame
units are calibrated to a common standard in the loss absolute
mode of measurement, further calibration is no longer required of
the tester system in the field or in the lab.
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A photodetector 30 is arranged near the light source 28 or a
current senser 31 for providing a feedback signal to the ---
respective AC and DC level controls, 32, 34. The respective
circuits provide for stabilizing the amplitude and frequency of
the AC signal by controlling the AC level of the VCA 24 and the DC
level of the driver circuit 26. The status circuit 59 receives
output signals from the feedback circuits 32, 34, 58 and compares
the sum of the output signals for comparing with ma~imum and
minimum parameters provided in each feedback circuit. If the
status signal ~alls,outside the limit of the parameters of the
comparator ci,rcuits., an L'ED 63 will light up and the
microprocessor will provide a message on the display means 106
indicating that the status of the transmitter is out of
specification.
Once the modulated light signal is transmitted through the
fiber cable 15, the photodetector 74 o the detector module 12
detects the signal at a second end 14 of the fiber cable 15 and
converts the light signal into an equivalent current signal. This
current signal is then supplied to a microprocessor control
current-to-voltage converter 76. The output voltage of the
amplifier 76 ;s directed to microprocessor controlled-amplifiers
78 and 80 which serve as an auto-ranging circuit.
The output of amplifier 80 provides the input to a demodulator
23, and the voltage control oscillator (VCO) 88. The VCO drives a
speaker 92 via buffer 89 for aurally indicating the signal
strength received at the photodetector 74.
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If the apparatus is set up in a local or internal mode e.g.
having only a single unit, then the necessary information for~
determining a frequency of modulation or demodulating the received
signal in the modulator 23 is provided directly from ~he frequency
generator 16. I~ the apparatus is operated in a remote or
external mode e.g. having-two separate units for the transmitter
and receiver, then the receiving unit's microprocessor 18 will
step its frequency generator 1~ through the various frequency to
determine a match and loc~ it in to provide the necessary signals
to the receiving unit demodulator 23.
Upon identifying the ^modulating frequency, the microprocessor
in the receiver.main framë unit 11 will provide through respective
I/O ports 20a the necessar~ signals for adjusting.the gain of
respective current-to-voltage amplifier 76 in the detector module
12. Additionally, the microprocessor 18 will identify from its
memory the particular light wavelength assigned to the detected
modulating frequency, and thereby incorporate compensating
parameters from the detector PROM 75 of the detector module 12
which correspond to the specific photodetector's 74 responsivity
to that particular light wavelength.
The demodulation and low pass filter 23 will provide the
equivalent peak value of the received modulating signal in the
external mode. These values are determined originally during the
manufacturing an~ calibration process of the apparatus system, and
stored within the microprocessor's memory for each assigned
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frequency. The output of the demodulator and low pass filter 23
will then be supplied to a sample and hold 101 and an
analog-to-digital converter 102. This information is further
processed by the microprocessor 18 by compar;ng the receiYed
values corresponding to the power intensity of the recei~ed signal
to that of a reference signal stor~ed in the microprocessor 18.
This reference signal may be an absolute value determined during
the calibration of the system at the assembly plant, or may be a
relative value determined by tPsting a reference cable immediately
be~ore the present test for using the result of the reference
cable as a relative value. The microprocessor 18 will calculate
the difference between;the received transmitted signal oE known
wavelength of light and the reerence value for determlning the
attenuation associated'with the transmission of the particular
light wavelength. ~his attenuation will then be displayed on the
display means 106 and may be stored within the microprocessor's
mëmory for further analysis. The micr~processor will then start
the above procedure over for new wavelengths of light transmitted
by a new laser or LED source. Also, through the use of the
General Purpose Interf~ce Bus (GPIB), the resulting information
may be outputted to a printer or other digital controlled
mechanism.
Although certain p'referred embodiments provide for modulated
light signals having the same power levels prior to transmission,
the tester is capable of having varying power levels assigned to
the specific modulated light signals.
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~ . ~ ~
~5(~36
From the preceding description of the preferred embodiments,
it is evîdent that the objects of the inven~ion are attained,-and --
~although the invention has been described and illustrated in
detail~ it is to be clearly understood that the same is by way of
illustra~i.on and example only and is not to ]be taken by way of
limitation. The spirit an-d scope of the invention are to be
limited only-by the terms of the appended cl,aims.
,;,
. .
.
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