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FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

FIBEROPTIC SENSOR TECHNOLOGY HANDBOOK

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the aingle-sideband phaae noiae intercepts the 120 dB<br />

level at about 1 kHz. The acoustooptic modulator drive<br />

requirement is approximately +33 dBm. Asauming an output<br />

of +10 dBm from the oscillator the amplifier shown<br />

must provide 23 dBm of gain.<br />

Fig. 4.21<br />

cy noise. Phase trackers and the associated circuits<br />

are not required. An interferometer employing heterodyne<br />

detection is ahown in Fig. 4.21. The aystem difr<br />

UJO+<br />

SolMHz<br />

aLINEARFM<br />

DISCRIMINATOR<br />

‘A<br />

OU;PUT<br />

A interferornetric fiberoptic senaor employing<br />

heterodyne detection.<br />

fers from the usual heterodyne syatem in that uae is<br />

made of two Bragg cells. The firat cell also serves<br />

as a 3-dB coupler. By placing a star coupler (or plaited<br />

3-dB fiber coupler) at points A and B it should be<br />

possible for a single diode laser and one pair of Bragg<br />

cells to serve as the optical source for several dozen<br />

aenaors. For the Bragg frequencies indicated in Fig.<br />

4.21, bulk Bragg cells are required. In thia caae GRIN<br />

rods must be used to focus the light in and out of the<br />

fiber. If surface acoustic wave (SAW) Bragg cella are<br />

employed, they must be operated at approximately 600<br />

klllz (with a difference of 100 kHz). If the lowest signal<br />

frequency of interest is fs, the oscillator must<br />

exhibit phase noise less than -120 dB/Hz at an offset<br />

of fs from the carrier frequency. The plot of single<br />

sideband phase noise versus displacement from the carrier<br />

frequency for two oscillators is shown in Fig.<br />

4.22. The curve that corresponds to 600 MHz shows that<br />

5<br />

u -70<br />

u<br />

~ -80<br />

$1<br />

-90<br />

w<br />

~ -1oo<br />

z -110<br />

n<br />

z -120<br />

<<br />

flj -130<br />

Q<br />

m -140<br />

y -150<br />

60-100 MHz<br />

a ~ -160<br />

m<br />

I<br />

1 , ! !<br />

101 102<br />

,03 ,04<br />

105<br />

,.6<br />

FREQUENCY REMOVED FROM CARRIER<br />

Fig. 4.22 Typical single-sideband phaae noise measured<br />

relative to the carrier in a 1 Hz bandwidth<br />

in a fiberoptic interferornetric<br />

heterodyne sensor using fixed-frequency<br />

crystal osallators as shown in Fig. 4.12.<br />

4-11<br />

The maximum optical power that a channel waveguide<br />

will handle is about 120 uW. One pair of Bragg<br />

modulators configured as shown in Fig 4.21 could supply<br />

several sensors. However, with only 120 pW into the<br />

first Bragg cell it would not be possible to provide<br />

sufficient optical intensity to the detectors to insure<br />

quantum-limited operation for more than four sensors.<br />

Thua, for the operation of several dozen senaors from a<br />

aingle laser and one pair of bulk Bragg cells, heterodyne<br />

detection must be uaed.<br />

The difference frequency constitutes a heterodyne<br />

frequency of 100 kHz for the heterodyne detection<br />

configuration shown in Fig. 4.21. This permits the use<br />

of low-frequency, low-noise electronic circuits, such<br />

as low-noise amplifiers and FM discriminators. Since<br />

heterodyne detection is relatively insensitive to optical<br />

intensity fluctuation and low frequency noise,<br />

phase tracker circuits are not required. As in the<br />

case of homodyne detection, there may be a need for<br />

polarization-preserving fiber in order to prevent signal<br />

loss. Also, Bragg cells that are highly atable relative<br />

to each other, are required. Finally, in heterodyne<br />

detection, aa in homodyne detection, optical feedback<br />

into the diode laser greatly increases the laaer<br />

noise. Thus it is necessary to employ the aame precautions<br />

as were indicated above for homodyne detection.<br />

A number of other detection schemes have been<br />

suggested and are currently being considered. These<br />

include simple homodyning employing a 3 x 3 coupler in<br />

place of the input coupler (see Ref. 5 in Subsection<br />

4.2.8). It can be ahown that this resulta in an operating<br />

condition very close to quadrature. Synthetic<br />

heterodyne operation is another. A high frequency dither<br />

is employed on the phase stretcher. The output of<br />

such an interferometer can be shown to exhibit the characteristics<br />

of a heterodyne system.<br />

In view of the significant effort being applied<br />

to the detection problem further improvements can<br />

be expected; however, such effort la also an indication<br />

that the optimal detection acheme haa not been achieved.<br />

Numerous trade-offs are required. Theae include frequency<br />

range, sensitivity, dynamic range, cost, and complexity<br />

of the detection circuitry.<br />

4.2.8 References<br />

1.<br />

2.<br />

3.<br />

4.<br />

5.<br />

A. Dandridge, A. Tveten, R. Miles, D. Jackson, and<br />

T. Giallorenzi, “Single-Mode Diode Laser Phaae<br />

Noise”, Appl. Phya. Lett. — 38, 77 (1981).<br />

A. Dandridge and A. Tveten, “Noise Reduction in<br />

Fiber-Optic Interferometer Systems”, Appl. Opt.<br />

20-, 2337 (1981).<br />

R. Miles, A. Dandridge, A. Tveten, H. Taylor, and<br />

T. Giallorenzi, “Feedback-Induced Line Broadening<br />

in Cw Channel-Substrate Planar Laser Diodes”, Appl.<br />

Physica. Lett. — 37, 990 (1980).<br />

K. Fritsch and G. Adamovsky, “Simple Circuit for<br />

Feedback Stabilization of a Singlemode Optical<br />

Fiber Interferometer”, Rev. Sci. Instrum. ~, 996<br />

(1981).<br />

S. Sheem, “Fiber-Optic Gyroscope with [3x3] Directional<br />

Coupler”, Appl. Phys. Lett. 37, 869 (1980). —

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