2018
DOI: 10.3390/s18030696
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Analysis of Resonance Asymmetry Phenomenon in Resonant Fiber Optic Gyro

Abstract: This experiment demonstrated the resonance asymmetry phenomenon in the resonant fiber optic gyro. The asymmetry of resonant curve affects the system open-loop bias and its stability, which directly affects the accuracy of angular velocity measurement. In this paper, a new mathematic model is established. The influence of the coupler normal mode loss difference (the phase difference between the coupler cross port output optical field and direct port is less than the ideal π/2) on the symmetry of resonant curve,… Show more

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Cited by 10 publications
(8 citation statements)
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“…The optical power coupling ratio between the coupler direct port and cross port is k :(1 − k ). The remaining percentage of optical power that is caused by insertion loss of the coupler is ρ c [ 3 ].…”
Section: Theoretical Analysis and Simulation Resultsmentioning
confidence: 99%
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“…The optical power coupling ratio between the coupler direct port and cross port is k :(1 − k ). The remaining percentage of optical power that is caused by insertion loss of the coupler is ρ c [ 3 ].…”
Section: Theoretical Analysis and Simulation Resultsmentioning
confidence: 99%
“…At this moment, the output optical signal of the CCW light wave can reflect the resonant frequency difference of the CW and CCW light waves. Furthermore, the rotational angular speed can be obtained after being processed by the circuit [ 3 ].…”
Section: System Structure Of the Rfogmentioning
confidence: 99%
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“…Fiber optic gyro (FOG) is a core component of the third generation inertial measurement devices. It is widely used in military and civilian applications for its advantages of all solid state, high sensitivity, low cost and large dynamic range [1], [2], [3], [4], [5], [6], [7]. The principle of the interferometric fiber optic gyroscope (IFOG) is based on the phase change caused by the Sagnac effect.…”
Section: Introductionmentioning
confidence: 99%
“…Optical gyros based on the Sagnac effect are attractive sensors for inertial navigation systems [1,2,3,4]. However, both the Fiber Optic Gyroscope (FOG) and Ring Laser Gyroscope (RLG) have some serious disadvantages, as they are bulky, expensive, and energy intensive [5,6,7,8]. In order to overcome these shortcomings in traditional optical gyroscopes, the Micro Optic Gyroscope (MOG), which includes the Resonant Integrated Optic Gyroscope (RIOG) and the Interferometric Integrated Optical Gyroscope (IIOG), based on a waveguide ring resonator (WRR) was proposed [9,10,11,12,13,14,15,16].…”
Section: Introductionmentioning
confidence: 99%