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用于天琴计划的弱光星际航天器时钟抖动读出的实验演示。

Experimental demonstration of weak-light inter-spacecraft clock jitter readout for TianQin.

作者信息

Zeng Hanyu, Yan Hao, Xie Siyuan, Jiang Sicheng, Li Yingzi, Pan Yuhang, He Diaomin, Du Yuanbo, Yeh Hsien-Chi

出版信息

Opt Express. 2023 Oct 9;31(21):34648-34666. doi: 10.1364/OE.503164.

Abstract

The space-based gravitational wave detection mission, TianQin, requires high-level synchronization between independent clocks of all spacecrafts to extract the gravitational wave signals. It is necessary to measure the inter-spacecraft relative clock jitter based on laser phase-sideband clock transfer. The main challenge is the tracking and locking of clock sideband beatnote signals with low signal-to-noise ratio and frequency variation. In this paper, a systematic scheme of inter-spacecraft clock jitter readout is reported. The requirement of the clock transfer link for TianQin based on the time-delay interferometry algorithm is derived. A bi-directional laser interferometer system with a transmission optical power below 1 nW and a time delay of ∼50 µs is built up to demonstrate the weak-light clock transfer. In this scheme, frequency modulation is performed on the laser to simulate the inter-spacecraft Doppler frequency shift and its variation. Based on electrical and optical clock transfer comparison experiments, it is demonstrated that the GHz frequency synthesizer is the main noise source below the 50 mHz frequency range. The residual clock jitter noise introduced by the optical transfer link is below 40 fs/Hz above the 6 mHz frequency range, and the fractional frequency instability is less than 6.7 × 10 at 1000 s, which meets the requirement of the TianQin mission. Ultimately, The carrier phase measurement accuracy reaches 1 × 10 cycles/Hz above 6 mHz after differential clock noise correction using measured clock jitter.

摘要

天琴空间引力波探测任务要求所有航天器的独立时钟之间实现高度同步,以提取引力波信号。有必要基于激光相位边带时钟传递来测量航天器间的相对时钟抖动。主要挑战在于跟踪和锁定信噪比低且频率变化的时钟边带拍频信号。本文报道了一种航天器间时钟抖动读出的系统方案。推导了基于时延干涉测量算法的天琴时钟传递链路要求。搭建了一个发射光功率低于1 nW且时延约为50 µs的双向激光干涉仪系统,以演示弱光时钟传递。在该方案中,对激光进行频率调制,以模拟航天器间的多普勒频移及其变化。基于电时钟传递和光时钟传递比较实验,证明GHz频率合成器是50 mHz频率范围以下的主要噪声源。光传递链路引入的残余时钟抖动噪声在6 mHz频率范围以上低于40 fs/Hz,在1000 s时分数频率不稳定度小于6.7×10,满足天琴任务要求。最终,使用测量的时钟抖动进行差分时钟噪声校正后,在6 mHz以上载波相位测量精度达到1×10周期/Hz。

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