TY - JOUR
T1 - Online Identification and Compensation of Drive and Phase Errors for Whole-Angle Hemispherical Resonator Gyroscope Based on Sinusoidal Self-Excitation
AU - Chen, Zhennan
AU - Yan, Kaichen
AU - Wang, Xiaoxu
AU - Qu, Tianliang
AU - Zhou, Jinling
AU - Zhang, Xi
AU - Che, Chicheng
AU - Gao, Pu
AU - Lu, Qianbo
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - Drive and phase errors of whole-angle hemispherical resonator gyroscope in the control circuit cannot be neglected. These two errors represent the coupling and gain mismatch between control forces and the undesired phase delays accumulating in the control loops respectively. The existing identification methods for these two errors are offline, and this non-real-time compensation causes significant fluctuations in the performance of the gyroscope with changes in error parameters. This paper proposes a novel sinusoidal self-excitation-based online error identification and compensation scheme. This scheme uses a sinusoidal self-excitation to modulate the angular incremental signal and quadrature control force carrying the drive and phase error information. Then, the real-time identification of the two errors is achieved through the modulated sinusoidal signal without affecting the angular rate detection in the low-frequency band. Experiments demonstrate that the drive and phase errors have been successfully identified and compensated for based on the proposed scheme. The peak-to-peak value of angle-dependent bias and bias instability decreased by 2.4 times and 3.77 times, to 11.84°/h and 0.0061°/h. In addition, superior results are achieved after the anisodamping error compensation, with angle-dependent bias reaching 0.1802°/h and scale factor nonlinearity reaching 1.95ppm. Compared to the 0.55°/h and 3.20ppm obtained by compensating for only anisodamping error, it decreases by 3.06 times and 1.66 times, respectively.
AB - Drive and phase errors of whole-angle hemispherical resonator gyroscope in the control circuit cannot be neglected. These two errors represent the coupling and gain mismatch between control forces and the undesired phase delays accumulating in the control loops respectively. The existing identification methods for these two errors are offline, and this non-real-time compensation causes significant fluctuations in the performance of the gyroscope with changes in error parameters. This paper proposes a novel sinusoidal self-excitation-based online error identification and compensation scheme. This scheme uses a sinusoidal self-excitation to modulate the angular incremental signal and quadrature control force carrying the drive and phase error information. Then, the real-time identification of the two errors is achieved through the modulated sinusoidal signal without affecting the angular rate detection in the low-frequency band. Experiments demonstrate that the drive and phase errors have been successfully identified and compensated for based on the proposed scheme. The peak-to-peak value of angle-dependent bias and bias instability decreased by 2.4 times and 3.77 times, to 11.84°/h and 0.0061°/h. In addition, superior results are achieved after the anisodamping error compensation, with angle-dependent bias reaching 0.1802°/h and scale factor nonlinearity reaching 1.95ppm. Compared to the 0.55°/h and 3.20ppm obtained by compensating for only anisodamping error, it decreases by 3.06 times and 1.66 times, respectively.
KW - drive error
KW - online error identification and compensation
KW - phase error
KW - sinusoidal self-excitation
KW - Whole-Angle hemispherical resonator gyroscope
UR - http://www.scopus.com/inward/record.url?scp=85210960368&partnerID=8YFLogxK
U2 - 10.1109/JSEN.2024.3504581
DO - 10.1109/JSEN.2024.3504581
M3 - 文章
AN - SCOPUS:85210960368
SN - 1530-437X
JO - IEEE Sensors Journal
JF - IEEE Sensors Journal
ER -