Abstract
This article presents, by means of computational simulation tools, a full analysis and design of an Interferometric Fiber-Optic Gyroscope (IFOG) prototype based on a closed-loop configuration with sinusoidal bias phase- modulation. The complete design of the different blocks, optical and electronic, is presented, including some novelties as the sinusoidal bias phase-modulation and the use of an integrator to generate the serrodyne phase-modulation signal. The paper includes detailed calculation of most parameter values, and the plots of the resulting signals obtained from simulation tools. The design is focused in the use of a standard single-mode optical fiber, allowing a cost competitive implementation compared to commercial IFOG, at the expense of reduced sensitivity. The design contains an IFOG model that accomplishes tactical and industrial grade applications (sensitivity ≤ 0.055 °/h). This design presents two important properties: (1) an optical subsystem with advanced conception: depolarization of the optical wave by means of Lyot depolarizers, which allows to use a sensing coil made by standard optical fiber, instead by polarization maintaining fiber, which supposes consequent cost savings and (2) a novel and simple electronic design that incorporates a linear analog integrator with reset in feedback chain, this integrator generating a serrodyne voltage-wave to apply to Phase-Modulator (PM), so that it will be obtained the interferometric phase cancellation. This particular feedback design with sawtooth-wave generated signal for a closed-loop configuration with sinusoidal bias phase modulation has not been reported till now in the scientific literature and supposes a considerable simplification with regard to previous designs based on similar configurations. The sensing coil consists of an 8 cm average diameter spool that contains 300 m of standard single-mode optical-fiber (SMF-28 type) realized by quadrupolar winding. The working wavelength will be 1310 nm. The theoretical calculated values of threshold sensitivity and dynamic range for this prototype are 0.052 °/h and 101.38 dB (from ±1.164 × 10−5 °/s up to ±78.19 °/s), respectively. The Scale-Factor (SF) non-linearity for this model is 5.404% relative to full scale, this value being obtained from data simulation results.
Highlights
In all the electro-optical engineering areas, in the design of high cost devices likeInterferometric Fiber-Optic Gyroscopes (IFOGs), computational simulation resources can provide powerful and inestimable guidance
This type of noise stems from two causes: (1) the two interfering optical waves do not come to the photodetector with the same optical power level, due to polarization crosstalk between the two orthogonal polarizations states along the entire length of the sensing fiber-coil; and (2) the light source is low-coherence, thereby producing several beat wavelengths, which add at the photodetector optical-input, causing a variation in relative intensity on every point of photodetector’s response-curve
An IFOG prototype was theoretically designed by means of optical and electronic simulation tools
Summary
Interferometric Fiber-Optic Gyroscopes (IFOGs), computational simulation resources can provide powerful and inestimable guidance. This stems from the rapidity, the reproducibility and the reliability of this kind of hardware to obtain the finished design of a preconceived model. It is possible to realize designs for certain applications that do not need such a high grade of performance (i.e., tactical-grade, sensitivity ď0.01 ̋ /h or industrial-grade, sensitivity ď1 ̋ /h). The latter mentioned will constitute the objective of the model presented. What follow is a brief overview of the basis of IFOG performance
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