MISSILES AND GUIDANCE TECHNOLOGY

The Research on New Coning Error Compensation Algorithm for Strapdown Inertial Navigation System

  • CHENG Cheng ,
  • PAN Quan ,
  • LI Hanzhou
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  • 1 School of Automation, Northwestern Polytechnical University, Xi'an 710072, China
    2 No. 16 Research Institute of China Aerospace Times Electronics Corporation, Xi'an 710100, China

Received date: 2013-03-09

  Online published: 2025-05-29

Abstract

Considering that classic coning error compensation algorithm ignores amplitude characteristic of coning motion and exists truncation error of Taylor series high order items, in the paper minimum least-square estimation was applied to deduce weighting coefficients of error compensation algorithm by considering amplitude characteristic of coning motion which can be determined by different performance requirements of carrier. The simulation experiment result shows that the new algorithm is better than classic algorithm for effect of coning error compensation.

Cite this article

CHENG Cheng , PAN Quan , LI Hanzhou . The Research on New Coning Error Compensation Algorithm for Strapdown Inertial Navigation System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(1) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2014.01.015

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