Precision assembly method of HRG harmonic oscillator based on Huygens bridge

被引:0
作者
Wang, Jianqing [1 ]
Wang, Xiaoxu [1 ]
Wu, Liao [2 ]
Dong, Yonghong [2 ]
He, Xiaoxia [2 ]
Xue, Tengyuan [2 ]
机构
[1] School of Automation, Northwestern Polytechnical University, Xi’an
[2] The 16th, China Aerospace Science and Technology Corporation, Xi’an
来源
Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology | 2025年 / 33卷 / 01期
关键词
assembly precision; gain inconsistency; hemispherical resonator gyro; Huygens bridge;
D O I
10.13695/j.cnki.12-1222/o3.2025.01.012
中图分类号
学科分类号
摘要
In order to solve the problem that the gain of detection loop is inconsistent due to the asymmetric assembly gap of hemispherical resonator gyroscope (HRG), which leads to additional gyro drift in full Angle mode, a gap detection model based on Huygens bridge is established, and the optimal circuit matching parameters under the model are given. On this basis, a harmonic oscillator assembly gap adjustment device is built. The gap asymmetry control precision is better than 0.1 μm, the gap uniformity is better than 0.9%, and the gap uniformity is improved by 80.4% compared with the traditional capacitance measuring instrument gap adjustment method. The experimental results of full-angle calibration tests on the gyro prototype before and after the assembly scheme improvement show that the lateral fluctuation error of the gyro output angular velocity has been suppressed after the improvement. The stability of the zero-stable gyro output for 1 s smoothing and 100 s smoothing has been improved by 71.7% and 58.7%, respectively, which proves that the precise assembly method based on the principle of Huygens's bridge resonator (HRG) can effectively improve assembly accuracy and gyro accuracy. © 2025 Editorial Department of Journal of Chinese Inertial Technology. All rights reserved.
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页码:89 / 95and106
相关论文
共 14 条
[1]  
Gou B, Cheng Y., INS/CNS integrated navigation based on corrected infrared earth measurement, IEEE Transactions on Instrumentation and Measurement, 68, 9, pp. 3358-3366, (2019)
[2]  
Benzerrouk H, Nebylov V, Nebylov A, Et al., SpacecraftINS/CNS/pulsar integrated positioning navigation and timing, International Federation of Automatic Control, 53, 2, pp. 14912-14917, (2020)
[3]  
Qu T., Review on the current advances, key technology and future, Optics & Optoelectronic technology, 20, 2, pp. 1-15, (2022)
[4]  
Jin X, Liu X, Li S, Et al., Development status and trend of hemispherical resonator gyroscope assembly technology, Flight Control & Detection, 4, 1, pp. 1-9, (2021)
[5]  
Ning Y, Yi G, Xi B, Et al., The influence of assembly inclination error in hemispherical resonator on frequency splitting, Journal of Chinese Inertial Technology, 29, 4, pp. 510-515, (2021)
[6]  
Yan K, Wang X, Zou K., Self-excitation enabled decoupling, calibration, and compensation of errors for whole-angle hemispherical resonator gyroscope, IEEE TransactIONS on INSTRUMENTATION and MEASUREMENT, 73, (2024)
[7]  
Delhaye Fabrice, SpaceNaute® the HRG based inertial reference system of ariane 6 European space launcher, Gyroscopy and Navigation, 10, 1, pp. 1-6, (2019)
[8]  
Vatanparvar D., Shkel A. M., Rate-integrating gyroscope operation in the non-linear regime[J], DGON Inertial Sensors Syst, pp. 1-18, (2022)
[9]  
Ning Y, Yi G, Xi B., The influence of assembly inclination error in hemispherical resonator on frequency splitting, Journal of Chinese Inertial Technology, 29, 4, pp. 510-515, (2021)
[10]  
Vatanparvar D., Shkel A. M., Identification of gain mismatches in control electronics of rate integrating CVGs[J], 2021 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL), (2021)