物理
振幅
噪音(视频)
加速度
残余物
惯性参考系
理论(学习稳定性)
重力加速度
验证质量
惯性测量装置
电子线路
声学
引力波
万有引力
航空航天工程
光学
经典力学
计算机科学
工程类
机器学习
图像(数学)
人工智能
量子力学
天体物理学
算法
作者
Jiawei Zhang,Peilong Yu,Shuyang Lin,Qiang Ma,Zhe Han,Jianping Huang
标识
DOI:10.1088/1361-6382/ad9c0d
摘要
Abstract The primary measure of scientific performance for inertial sensors used in space gravitational wave detection is the residual acceleration noise of the test mass (TM). This residual noise arises from both the internal circuit and the external environment. The actuation circuit, a crucial component of the internal circuit, significantly affects the TM’s residual acceleration noise through its amplitude stability, thereby impacting the scientific performance of the inertial sensor. In this study, we designed the actuation circuit for an inertial sensor, developed a mathematical model to describe its amplitude stability, and experimentally verified the model’s accuracy. Experimental results demonstrate that the current design enables the actuation circuit to achieve an amplitude stability of 3.6 ppm Hz −1/2 at 1 mHz, thereby offering theoretical support for achieving a higher amplitude stability in the millihertz frequency band.
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