I. Introduction
Nuclear magnetic resonance (NMR) gyroscopes, which have the advantages of small size and high accuracy, and are unaffected by environmental factors, have great potential in the field of inertial navigation [1], [2], [3]. NMR gyroscopes operate on the principle of Larmor precession, utilizing the embedded magnetometer and signal processing system to capture rotational information [4], [5], [6]. Compared with single-species, dual-species can eliminate the impact of the static magnetic field on measurement accuracy [7]. To ensure continuous measurement of the angular velocity, the system needs to work in a closed-loop system to address real-time phase detuning and compensate for the transverse driving field [6]. In the case of a closed-loop NMR gyroscope based on87Rb–129Xe/131Xe, by demodulating at the first harmonic of the rubidium atomic magnetic moment component, the signal containing the progression phase can be obtained. The complexity of the NMR gyroscope system encompasses tasks, such as vapor cell temperature control, laser frequency stabilization, three-axis magnetic field control, and angular velocity resolution [8]. This intricate system needs extensive digital signal processing and substantial hardware resources underscoring the importance of accurately determining the precession phase with minimal resource consumption.