MISSILES AND GUIDANCE TECHNOLOGY

Influence of IMU Angle Variable Motion on Positioning Accuracy of Rotary SINS

  • LIU Shi ,
  • WANG Shian ,
  • LIU Xingzhang ,
  • ZHANG Yi ,
  • YANG Xianglong
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  • 1 College of Automation, Harbin Engineering University, Harbin 150001, China
    2 Military Representative Bureau of Navy in Shenyang Area, Shenyang 110000, China
    3 Military Representative Bureau of Navy in Dalian Area, Liaoning Dalian 116000, China
    4 Beijing Aerospace Automatic Control Institute, Beijing 100854, China
    5 National Aerospace Intelligence Control Technology Laboratory, Beijing 100854, China

Received date: 2013-12-23

  Online published: 2025-05-30

Abstract

The influence of inertial measurement unit (IMU) rotary angular velocity variation on positioning accuracy of strapdown inertial navigation system (SINS) was studied. Angle variable motion model was established in geographic coordinate system. Then, the basic principles that equivalent gyro drift errors were compensated by rotary motion were derived. Combined with the widespread single-axis 4-position and 8-order rotation-stop scheme, the effect of acceleration and deceleration of IMU on positioning accuracy of SINS was analyzed in detail. Simulations based on theoretical analysis were carried out. Finally, the positioning errors of rotation schemes with different acceleration and deceleration were compared by simulation tests, the results verified that the accuracy of the rotary SINS was apparently impacted by angle variable motion.

Cite this article

LIU Shi , WANG Shian , LIU Xingzhang , ZHANG Yi , YANG Xianglong . Influence of IMU Angle Variable Motion on Positioning Accuracy of Rotary SINS[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(4) : 19 -24 . DOI: 10.15892/j.cnki.djzdxb.2014.04.043

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