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Acta Armamentarii ›› 2012, Vol. 33 ›› Issue (7): 826-830.doi: 10.3969/j.issn.1000-1093.2012.07.011

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Coning Error Compensation Algorithm of SINS Self-Alignment on Swaying Base

WANG Li-dong, LIU Jun, LU Jun   

  1. (Ordnance Engineering College, Shijiazhuang 050003, Hebei, China)
  • Received:2011-05-10 Revised:2011-05-10 Online:2017-02-28
  • Contact: WANG Li-dong E-mail:wlddoctor@163.com

Abstract: Coning error compensation algorithm in the process of self-alignment is put forward in light of the strapdown intertial navigation system (SINS) self-alignment error on swaying base. It reduces coning error and increases the self-alignment accuracy. The quaternion fourth-order Runge-Kutta algorithm and two-sample and three-sample and other error compensation algorithm of equivalent rotation vector and their theoretical compensation effect are analyzed and compared in theory; through simulation and experiments, it is obtained that the self-alignment error decreases along with increasing of the number of sample. When the number of sample increases 1, the self-alignment error of north-angle is reduced nearly 1 time and the dispersibility of attitude angle is reduced; with the increasing of the swaying amplitude and frequency, the self-alignment accuracy of three-sample compensation algorithm is close to stability . Considering the sampling frequency and the number of sample and calculation and alignment accuracy, the three-sample coning error compensation algorithm should be selected and it can satisfy the self-alignment requirements of SINS on swaying base.

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