Amplitude-Phase Inconsistency Extraction and In Situ Calibration Technique of Six-Degree-of-Freedom Capacitance Sensor for Space Gravitational Wave Detection

• Published in: IEEE sensors journal 2024-07, Vol.24 (14), p.22539-22552
• Main Authors: Zhang, Yuerong, Ma, Hong, Zhang, Hua, Yang, Hong, Wang, Xiongwei, Huang, Kun, Zang, Jie, Chen, Liyuan
• Format: Article
• Language: English
• Subjects: Amplitude-phase inconsistency; Amplitudes; Calibration; Capacitance; Carrier frequencies; Circuits; Degrees of freedom; Demodulation; Electrodes; gravitational wave (GW) detection; Gravitational waves; in situ calibration; Inertial sensing devices; inertial sensors; multiple degree-of-freedom (DoF) capacitive displacement sensing; Probes; Quadratures; Sensors; Transformers
• ISSN: 1530-437X; 1558-1748
• DOI: 10.1109/JSEN.2024.3408146

The high precision multiple degree-of-freedom (DoF) capacitance sensor operating in milli-hertz band is critical for satellite platform inertial sensing of space gravitational wave (GW) detection mission, and the amplitude-phase characteristics inconsistency among the capacitive sensing channels may seriously deteriorate the displacement sensing performance. In this article, a novel architecture of 6-DoF capacitive sensing circuits (CSCs) with digital quadrature demodulation is proposed, and the impact of 6-channel displacement sensing front-ends (DSFs) parameters inconsistency on the output signals and displacement sensing performance is also analyzed. The amplitude-phase inconsistency extraction and in-orbit in situ calibration technique for the 6-channel capacitance sensor is proposed and verified by an invented ground-equivalent evaluation scheme. Finally, a 6-DoF CSCs prototype for the inertial sensors of "China TianQin Project" has been developed and tested. The results show the mean values and the standard deviations of the translational and rotational displacement detection errors are reduced from 1.32~\mu m, 5.67 mdeg to 30.86 nm, 86.92~\mu deg, and from 18.22 nm, 76.51~\mu deg to 12.23 nm, 32.97~\mu deg, at the specific carrier frequency, respectively. The method may be utilized to periodically calibrate CSCs to significantly improve the prolonged in-orbit running performance of the inertial sensor.