SINS/GPS Integrated Navigation Algorithm for Supersonic Aerial Targets in the LCEF Frame

Kai Chen, Jun Zhou, Xing Liu, Ya Ling Zhao, Zi Xiang Zhao

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

Abstract

Regarding the application requirements of supersonic aerial targets (SATs), this paper studies the SINS/GPS integrated algorithm in the launch centered earth-fixed (LCEF) frame. Firstly, the SINS mechanization in the LCEF frame is given, and the update algorithms of SINS attitude, velocity, and position are presented. Then, the state and measurement equations of the SINS/GPS algorithm in the LCEF frame are derived. Finally, the SINS/GPS integrated algorithm is introduced to SATs, and for which a semi-physical simulation test is performed. The results indicate that the position error is less than 10 m, the velocity error is less than 0.3 m/s, the pitching and roll angle errors are <0.2°, and the yaw angle error is <0.3°.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020
EditorsLiang Yan, Haibin Duan, Xiang Yu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages315-328
Number of pages14
ISBN (Print)9789811581540
DOIs
StatePublished - 2022
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2020 - Tianjin, China
Duration: 23 Oct 202025 Oct 2020

Publication series

NameLecture Notes in Electrical Engineering
Volume644 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2020
Country/TerritoryChina
CityTianjin
Period23/10/2025/10/20

Keywords

  • Launch-centered earth-fixed frame
  • SINS/GPS integrated navigation
  • Strapdown inertial navigation algorithm
  • Supersonic aerial targets

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