MISSILES AND GUIDANCE TECHNOLOGY

Ten-position Systematic Calibration Method for FOG Strap-down Inertial Navigation System

  • ZHAO Guiling ,
  • YANG Qihang ,
  • LI Song
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  • School of Mapping and Geographical Science, Liaoning Technical University, Liaoning Fuxin 123000, China

Received date: 2014-01-09

  Online published: 2025-05-30

Abstract

In view of the characteristics of traditional systematic calibration method's high state variable dimension and poor observability, a ten-position systematic calibration method was proposed in this paper. The calibration method takes discrete calibration results as initial values, and speed error and attitude error as observables. By merging accelerometer calibration errors and fiber optic gyro (FOG) calibration errors, it reduces the dimension of Kalman filter. The calibration method uses ten positions to estimate the calibration error of strap-down inertial navigation system (SINS), then decouples the estimation and calculates the calibration parameters. The simulation and turn-table experiment results show that ten-position systematic calibration method can calibrate twenty-four parameters including scale factor, installation error and zero.

Cite this article

ZHAO Guiling , YANG Qihang , LI Song . Ten-position Systematic Calibration Method for FOG Strap-down Inertial Navigation System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(6) : 8 -12 . DOI: 10.15892/j.cnki.djzdxb.2014.06.003

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