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MISSILES AND GUIDANCE TECHNOLOGY

A Simulation Platform Design for Strap-down Inertial Navigation System Design and Validation

  • ZHOU Wenjun ,
  • LIU Jin ,
  • LEI Hongjie
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  • 1 National Key Laboratory of Flight Vehicle Intergrated Technology, Xi'an 710065, China
    2 Flight Automatic Control Research Institute, Xi'an 710065, China

Received date: 2011-01-25

  Online published: 2025-05-30

Abstract

According to practical application requirement of strap-down inertial navigation system (SINS), a simulation platform for design and validation of strap-down inertial navigation system based on Matlab/Simulink was designed and realized. The platform includes flight trajectory generator, inertial measurement unit (IMU), SINS unit, Kalman filter unit and navigation performance e-valuation unit. It has functions of SINS algorithm validation, error analysis, error distribution and flight data off-line analysis and so on. The research results prove the simulation platform is effective and practical.

Cite this article

ZHOU Wenjun , LIU Jin , LEI Hongjie . A Simulation Platform Design for Strap-down Inertial Navigation System Design and Validation[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(6) : 11 -14 . DOI: 10.15892/j.cnki.djzdxb.2011.06.017

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Outlines

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