Research on guidance algorithm based on strap-down devices

Yongshan Liu, Xin Lu

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

This paper proposes a guidance algorithm based on strap-down devices to obtain more accurate guidance information for small missile system. This paper establishes a mathematic model of inertial devices to get the navigation information of the SINS. Then the calculation results of the navigation system are used to establish the mathematical model of the inertial line-of-sight angular velocity of the strap-down seeker. So, the extraction of guidance information can be realized. In order to reduce the influence of system noise, this paper designs extended Kalman filter and unscented Kalman filter to filter the guidance information separately and compares these two filter results with the data from the track generator. The simulation results show that the guidance algorithm is effective and can obtain the guidance information to meet the requirements.

Original languageEnglish
Title of host publicationProceedings of the 30th Chinese Control and Decision Conference, CCDC 2018
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1709-1714
Number of pages6
ISBN (Electronic)9781538612439
DOIs
Publication statusPublished - 6 Jul 2018
Event30th Chinese Control and Decision Conference, CCDC 2018 - Shenyang, China
Duration: 9 Jun 201811 Jun 2018

Publication series

NameProceedings of the 30th Chinese Control and Decision Conference, CCDC 2018

Conference

Conference30th Chinese Control and Decision Conference, CCDC 2018
Country/TerritoryChina
CityShenyang
Period9/06/1811/06/18

Keywords

  • Extended Kalman filter
  • Guidance information
  • Strap-down
  • Unscented Kalman filter

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