中国航空学报(英文版)2024,Vol.37Issue(3) :219-236.DOI:10.1016/j.cja.2023.10.012

Integral precession calibration method of PIGA on linear vibration table

Chuang SUN Shun-qing REN Jun-wei CAO Ru HUO
中国航空学报(英文版)2024,Vol.37Issue(3) :219-236.DOI:10.1016/j.cja.2023.10.012

Integral precession calibration method of PIGA on linear vibration table

Chuang SUN 1Shun-qing REN 2Jun-wei CAO 3Ru HUO4
扫码查看

作者信息

  • 1. Department of Automation,Tsinghua University,Beijing 100084,China
  • 2. School of Astronautics,Harbin Institute of Technology,Harbin 150001,China
  • 3. Beijing National Research Center for Information Science and Technology,Tsinghua University,Beijing 100084,China
  • 4. Faculty of Information technology,Beijing University of Technology,Beijing 100124,China
  • 折叠

Abstract

Linear vibration table can provide harmonic accelerations to excite the nonlinear error terms of Pendulous Integrating Gyro Accelerometer(PIGA).Integral precession calibration method is proposed to calibrate PIGA on a linear vibration table in this paper.Based on the precise expressions of PIGA's inputs,the error calibration model of PIGA is established.Precession angu-lar velocity errors of PIGA are suppressed by integer periodic precession and the errors caused by non-integer periods vibrating are compensated.The complete calibration process,including plan-ning,preparation,PIGA testing,and coefficient identification,is designed to optimize the test oper-ations and evaluate the calibration results.The effect of the main errors on calibration uncertainty is analyzed and the relative sensitivity function is proposed to further optimize the test positions.Experimental and simulation results verify that the proposed 10-position calibration method can improve calibration uncertainties after compensating for the related errors.The order of calibration uncertainties of the second-and third-order coefficients are decreased to 10-8(rad·s-1)/g2 and 10-8(rad·s-1)/g3,respectively.Compared with the other two classical calibration methods,the calibra-tion uncertainties of PIGA's nonlinear error coefficients can be effectively reduced and the propor-tional residual errors are decreased less than 3 ×10-6(rad·s-1)/g by using the proposed calibration method.

Key words

PIGA/Linear vibration table/Vibration measurement/Calibration/Error analysis/Uncertainty analysis

引用本文复制引用

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDCSCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量24
段落导航相关论文