Squeezed-Light-Enhanced Dispersive
Gyroscope based Optical Microcavities
XIAOYANG CHANG,1 WENXIU LI1 , HAO ZHANG2*, YANG ZHOU2, ANPING
HUANG1,AND ZHISONG XIAO1,2,3
1 School of Physics, Beihang University, Beijing 100191, China
2 Research Institute of Frontier Science, Beihang University, Beijing 100191, China
3 Beijing Academy of Quantum Information Sciences, Beijing 100193, China
*Corresponding author: haozhang@buaa.edu.cn
Abstract: Optical gyroscope based on the Sagnac effect have excellent potential in the
application of high-sensitivity inertial rotation sensors. In this paper, we demonstrate that for
an optical resonance gyroscope with normal dispersion, the measurement sensitivity can be
increased by two orders of magnitude through coupling into a squeezed vacuum light, which
is different from that in the classical situation. When the system is operated under critical
anomalous dispersion condition, injecting a squeezed vacuum light allows the measurement
sensitivity beyond the corresponding standard quantum limit by five orders of magnitude,
with a minimum value of 3.8×10-5 Hz. This work offers a promising possibility for
developing optical gyroscopes that combine high sensitivity with tiny size.
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1. Introduction
Optical gyroscopes based on microcavity have remarkable advantages in weight, size, cost,
and power consumption and have become one of the focuses of inertial rotation sensors[1].
Physically, the optical gyroscope is based on the Sagnac effect[2]. That is to say, if two
beams are counter-propagating in an optical loop, a phase or frequency shift between the
clockwise (CW) and counterclockwise (CCW) beams is generated when the loop is rotating
around the axis, which is proportional to the angular rotation rate of the loop. The
accumulated phase or frequency shift in the loop, which comes from the Sagnac effect, is
proportional to the effective area of the optical cavity. Therefore, the Sagnac phase shift
accumulated in an optical microcavity gyro is seriously bounded, limiting its measurement
sensitivity due to the tiny effective area. In many applications such as vehicles, spacecraft,
and satellites, the size and weight of the gyro are strictly limited, but high sensitivity is
required simultaneously.
In order to make a microcavity optical gyro have high measurement sensitivity, various
coupled resonator optical waveguides (CROWs) were proposed, and the normal dispersion
effect in these structures is also discussed[3–8]. Subsequent studies have shown that even
with optimized parameters, the sensitivity of the CROW gyro is equal to that of a Ring laser
gyro under equal loop loss conditions. Physically, normal dispersion is a resultant feature of
the CROW structure and is not directly correlated with sensitivity enhancement. In addition,
the sensitivity of a resonator-based optical gyroscope can be enhanced by introducing
anomalous dispersion effect[9]. Typically, there are two experimental regimes for achieving
anomalous dispersion, utilizing the alkali metal vapors and optical coupled resonators[9–24].
However, the alkali metal vapors approach is unsuitable for reducing the weight and size of a
gyro because the experimental system is rather complex. Optical coupled microresonators can
achieve anomalous dispersion only by using passive elements, thus avoiding the complexities
of modulating the dispersion in alkali metal vapors.
Nevertheless, most of the previous research on dispersion enhancing the sensitivity of an
optical gyroscope is based on classical light. As a result, these devices are forcing an